Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO), TSO-C69, TSO-C69a, TSO-C69b, and TSO-69c, Installed on Various Boeing, McDonnell Douglas, and Airbus Transport Category Airplanes, 31761-31771 [E7-10992]

Download as PDF Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules pwalker on PROD1PC71 with PROPOSALS Type of Request: New collection. Abstract: The information collection requirement in this request is essential to carry out the intent of the Act, to provide the respondents the type of service they request, and to administer the California almond marketing order program, which has been operating since 1950. The Board met on March 28, 2007, and unanimously recommended revising the requirements for interhandler transfers of almonds whereby handlers who transfer almonds to other handlers would have to report to the Board whether or not the almonds were treated to achieve a 4-log reduction in Salmonella. A mandatory treatment program to reduce the potential for Salmonella in almonds will take effect in September 2007. This action would enable the Board to track treated and untreated almonds and help facilitate administration of its mandatory treatment program. This document concerns the reporting requirements regarding this change. This information collection is only used by authorized representatives of USDA, including AMS, Fruit and Vegetable Programs regional and headquarters’ staff, and authorized employees and agents of the Board. Authorized Board employees, agents, and the industry are the primary users of the information and AMS is the secondary user. ABC Form No. 7 Interhandler Transfer of Almonds Estimate of Burden: Public reporting burden for this collection of information is estimated to be 0.5 hour per response. Respondents: Almond handlers. Estimated Number of Respondents: 50. Estimated Number of Responses per Respondent: 5. Estimated Total Annual Burden on Respondents: 125 per year. Comments: Comments are invited on: (1) Whether the proposed collection of information is necessary for the proper performance of the functions of the agency, including whether the information will have practical utility; (2) the accuracy of the agency’s estimate of the burden of the proposed collection of information, including the validity of the methodology and assumptions used; (3) ways to enhance the quality, utility, and clarity of the information to be collected; and (4) ways to minimize the burden of the collection of information on those who are to respond, including the use of appropriate automated, electronic, mechanical, or other technological collection techniques or other forms of information technology. VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 Comments should reference OMB No. 0581–NEW and the California almond marketing order, and be sent to the USDA in care of the Docket Clerk at the address above. All comments received will be available for public inspection during regular business hours at the same address. All responses to this notice will be summarized and included in the request for OMB approval. All comments will also become a matter of public record. The AMS is committed to complying with the E-Government Act, to promote the use of the Internet and other information technologies to provide increased opportunities for citizen access to Government information and services, and for other purposes. A 60-day comment period is provided to allow interested persons to comment on this proposed information collection. List of Subjects in 7 CFR Part 981 Almonds, Marketing agreements, Nuts, Reporting and recordkeeping requirements. For the reasons set forth in the preamble, 7 CFR part 981 is proposed to be amended as follows: PART 981—ALMONDS GROWN IN CALIFORNIA 1. The authority citation for 7 CFR part 981 continues to read as follows: Authority: 7 U.S.C. 601–674. 2. Section 981.455 is amended by revising paragraph (a) to read as follows: § 981.455 Interhandler transfers. (a) Transfers of almonds. Interhandler transfers of almonds pursuant to § 981.55 shall be reported to the Board on ABC Form 7. The report shall contain the following information: (1) Date of transfer; (2) The names, and plant locations of both the transferring and receiving handlers; (3) The variety of almonds transferred; (4) Whether the almonds are shelled or unshelled; (5) The name of the handler assuming reserve and assessment obligations on the almonds transferred; (6) Whether the almonds had been treated to achieve a 4-log reduction in Salmonella bacteria, pursuant to § 981.442(b); and (7) A unique handler identification number for each lot. * * * * * Dated: June 4, 2007. Lloyd C. Day, Administrator, Agricultural Marketing Service. [FR Doc. 07–2837 Filed 6–5–07; 9:48 am] BILLING CODE 3410–02–P PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 31761 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–28370; Directorate Identifier 2003–NM–239–AD] RIN 2120–AA64 Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO), TSO– C69, TSO–C69a, TSO–C69b, and TSO– 69c, Installed on Various Boeing, McDonnell Douglas, and Airbus Transport Category Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). AGENCY: SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for certain Goodrich evacuation systems approved under TSO-C69, TSO-C69a, TSO-C69b, and TSO-69c, installed on certain Boeing, McDonnell Douglas, and Airbus transport category airplanes. For certain systems, this proposed AD would require replacing the evacuation systems shear-pin restraints with new ones. For certain other systems, this proposed AD would require an inspection for manufacturing lot numbers; and a general visual inspection of the shear-pin restraint for discrepancies, and corrective actions if necessary. This proposed AD is prompted by several reports of corroded shear-pin restraints that prevented Goodrich evacuation systems from deploying properly. We are proposing this AD to prevent failure of the evacuation system, which could impede an emergency evacuation and increase the chance of injury to passengers and flightcrew during the evacuation. DATES: We must receive comments on this proposed AD by July 23, 2007. ADDRESSES: Use one of the following addresses to submit comments on this proposed AD. • DOT Docket Web site: Go to http://dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your comments electronically. • Mail: Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL–401, Washington, DC 20590. • By fax: (202) 493–2251. • Hand Delivery: Room PL–401 on the plaza level of the Nassif Building, E:\FR\FM\08JNP1.SGM 08JNP1 31762 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules 400 Seventh Street SW., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Contact Goodrich, Aircraft Interior Products, ATTN: Technical Publications, 3414 South Fifth Street, Phoenix, AZ 85040, for service information identified in this proposed AD. FOR FURTHER INFORMATION CONTACT: Tracy Ton, Aerospace Engineer, Cabin Safety/Mechanical and Environmental Systems Branch, ANM–150L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712–4137; telephone (562) 627–5352; fax (562) 627–5210. SUPPLEMENTARY INFORMATION: pwalker on PROD1PC71 with PROPOSALS Comments Invited We invite you to submit any written relevant data, views, or arguments regarding this proposed AD. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA– 2007–28370; Directorate Identifier 2003–NM–239–AD’’ in the subject line of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the proposed AD. We will consider all comments submitted by the closing date and may amend the proposed AD in light of those comments. We will post all comments we receive, without change, to http:// dms.dot.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact with FAA personnel concerning this proposed AD. Using the search function of that website, anyone can find and read the comments in any of our dockets, including the name of the individual who sent the comment (or signed the comment on behalf of an association, business, labor union, etc.). You can review DOT’s complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477–78), or you can visit http:// dms.dot.gov. Examining the Docket You can examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647–5227) is located on the plaza level of the Nassif Building at the DOT street address stated in the ADDRESSES VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 section. Comments will be available in the AD docket shortly after the DMS receives them. Discussion We have received several reports indicating that Goodrich evacuation systems installed on certain Boeing Model 747 airplanes and Model 767 airplanes have not deployed properly due to corroded shear-pin restraints. The corrosion problem arose concurrently with a 1998 change in the anodize specification for restraint bodies. Corrosion of the shear-pin restraints, if not corrected, can lead to higher than designed release values, and in severe cases, can cause the two halves of the restraints to freeze up, which can lead to improper deployment and/or loss of use of the evacuation system. That loss could impede emergency evacuation and increase the chance of injury to passengers and flightcrew during the evacuation. Other Relevant Rulemaking The reports involved certain Boeing Model 747 airplanes and Model 767 airplanes that are equipped with the affected Goodrich evacuation system as part of a type certificate (TC); however, certain Goodrich evacuation systems installed as a technical standard order (TSO) appliance on certain Airbus, Boeing and McDonnell Douglas transport category airplanes use the same restraints as those used by the affected type certificated Goodrich units. Therefore evacuation systems approved by either TSO or TC are subject to the identified unsafe condition. We are planning to issue similar rulemaking (Directorate Identifier 2005–NM–139–AD) for certain Boeing Model 747 airplanes and Model 767 airplanes that are equipped with certain type certificated Goodrich evacuation systems. Relevant Service Information We have reviewed Goodrich Service Bulletins 25–343, Revision 3, dated January 12, 2007; and 25–344, Revision 2, dated October 11, 2006. Goodrich Service Bulletin 25–343 affects evacuation systems installed on certain Boeing and McDonnell Douglas transport category airplanes. Goodrich Service Bulletin 25–344 affects evacuation systems installed on certain Airbus transport category airplanes. For certain systems, the service bulletins describe procedures for replacing the shear-pin restraints with new, improved restraints. For certain other systems, the PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 service bulletins describe procedures for an inspection to verify the manufacturing lot number of the restraints; and a general visual inspection of the restraints for discrepancies (i.e., corrosion, security of pin retainer/label, overall condition, and lack of play), and corrective action if necessary. The corrective action is replacing the shear-pin restraints with new shear-pin restraints. Accomplishing the actions specified in the service information is intended to adequately address the unsafe condition. FAA’s Determination and Requirements of the Proposed AD We have evaluated all pertinent information and identified an unsafe condition that is likely to exist or develop on other products of this same type design. Therefore, we are proposing this AD, which would require you to use the service information described previously to perform these actions, except as discussed under ‘‘Difference Between this Proposed AD and the Service Bulletins.’’ Difference Between This Proposed AD and the Service Bulletins Although the service bulletins recommend accomplishing the replacement or inspection ‘‘at the next shop visit,’’ we have determined that this imprecise compliance time would not address the identified unsafe condition soon enough to ensure an adequate level of safety for the affected fleet. In developing an appropriate compliance time for this AD, we considered the manufacturer’s recommendation, the degree of urgency associated with the subject unsafe condition, and the average utilization of the affected fleet. In light of all of these factors, we find that a compliance time of 18 months for Goodrich evacuation systems installed on Boeing Model 767 off-wing ramp/slide units and 36 months for all other evacuation systems represents an appropriate interval of time for affected airplanes to continue to operate without compromising safety. We have coordinated this difference with the manufacturer. Costs of Compliance This proposed AD would affect certain Goodrich evacuation systems installed on about 2,844 airplanes worldwide. This proposed AD would affect about 1,240 airplanes of U.S. registry. The following table provides the estimated costs for U.S. operators to comply with this proposed AD. E:\FR\FM\08JNP1.SGM 08JNP1 31763 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules ESTIMATED COSTS Action Work hours Average labor rate per hour Replacement ........... Between 2 and 9 .. $80 Inspection ............... Between 2 and 9 .. $80 Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency’s authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, ‘‘General Requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We have determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and Parts Cost per slide unit Number of slide units per airplane Fleet cost Between $58 and $638, depending on number of restraints. None ..................... Between $218 and $1,358. Between 2 and 12. Between $540,640 and $20,207,040. Between $160 and $720. Between 2 and 12. Between $396,800 and $10,713,600. responsibilities among the various levels of government. For the reasons discussed above, I certify that the proposed regulation: 1. Is not a ‘‘significant regulatory action’’ under Executive Order 12866; 2. Is not a ‘‘significant rule’’ under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and 3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. We prepared a regulatory evaluation of the estimated costs to comply with this proposed AD. See the ADDRESSES section for a location to examine the regulatory evaluation. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends 39.13 by adding the following new airworthiness directive (AD): Goodrich (Formerly BFGoodrich): Docket No. FAA–2007–28370; Directorate Identifier 2003–NM–239–AD. Comments Due Date (a) The Federal Aviation Administration (FAA) must receive comments on this AD action by July 23, 2007. Affected ADs (b) None. Applicability (c) This AD applies to: (1) Goodrich evacuation systems approved under Technical Standard Order (TSO) TSO– C69, TSO–C69a, and TSO–C69b, installed on certain Boeing airplanes, certificated in any category, as listed in Table 1 of this AD; (2) Goodrich evacuation systems approved under TSO–C69, TSO–C69a, and TSO–C69b, installed on certain McDonnell Douglas airplanes, certificated in any category, as listed in Table 2 of this AD; and (3) Goodrich evacuation systems approved under TSO–C69a, TSO–C69b, and TSO– C69c, installed on Airbus airplanes, certificated in any category, as listed in Table 3 of this AD. TABLE 1.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN BOEING MODEL AIRPLANES Goodrich evacuation systems having part number (P/N)— Having any serial number (S/N)— Component/part is named— Installed on Boeing Model— (i) 101623–303 ............................... PB0400 through PB0453 inclusive Slide, forward/aft door .................. (ii) 101630–305 .............................. (iv) 101655–305 ............................. PG0276 through PG0309 inclusive. PC0264 through PC0368 inclusive. PK0161 through PK0212 inclusive Ramp/Slide, off-wing, left-hand (LH) side. Ramp/Slide, off-wing, right-hand (RH) side. Ramp/Slide, off-wing, LH side ...... (v) 101655–306 .............................. PF0164 through PF0220 inclusive Ramp/Slide, off-wing, RH side ..... (vi) 101656–305 ............................. PH0300 through PH0390 inclusive. PD0294 through PD0378 inclusive. PAK137 through PAK150 inclusive. Ramp/Slide, off-wing, LH side ...... 767–200 and planes. 767–200 and planes. 767–200 and planes. 767–200 and planes. 767–200 and planes. 767–200 and planes. 767–200 and planes. 737–200 series pwalker on PROD1PC71 with PROPOSALS (iii) 101630–306 ............................. (vii) 101656–306 ............................ (viii) 101658–101 and 101658–103 VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00005 Fmt 4702 Ramp/Slide, off-wing, RH side ..... Slide, forward door ....................... Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 –300 series air–300 series air–300 series air–300 series air–300 series air–300 series air–300 series airairplanes. 31764 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules TABLE 1.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN BOEING MODEL AIRPLANES—Continued Goodrich evacuation systems having part number (P/N)— Having any serial number (S/N)— Component/part is named— Installed on Boeing Model— (ix) 101659–101 through 101659– 205 inclusive. (x) 101660-101 through 101660107 inclusive. (xi) 5A3086–3 and 5A3086–301 .... PAL671 through PAL738 inclusive Slide, aft door ............................... PAB611 through PAB649 inclusive. B3F315 through B3F611 inclusive Slide, forward door ....................... (xii) 5A3088–3 and 5A3088–301 ... B3A338 through B3A685 inclusive Slide, aft door ............................... (xiii) 5A3109–1 ............................... Ramp/Slide, off-wing, LH side ...... (xv) 5A3294–1 and 5A3294–2 ....... Odd S/Ns ST0015 through ST0131. Even S/Ns ST0014 through ST0128. SS0001 through SS0210 inclusive (xvi) 5A3295–1 and 5A3295–3 ...... SF0001 through SF0501 inclusive Slide/Raft, doors 1 and 4 ............. (xvii) 5A3307–1 through 5A3307–5 inclusive and 5A3307–301. (xviii) 7A1323–111 through 7A1323–114 inclusive. (xix) 7A1394–4 and 7A1394–6 ...... BNG0213 through BNG4911 inclusive. GS1340 through GS1879 inclusive. GV0214 through GV0249 inclusive. Odd S/Ns GT1591 through GT1857. Slide, forward/aft door .................. 737–200, –300, –400, and –500 series airplanes. 737–300, –400, and –500 series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 777–300 and –300ER series airplanes. 777–300 and –300ER series airplanes. 767–300 and –400ER series airplanes. 767–200, –300, and –400ER series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 747–100B SUD, –300, –400, and –400D series airplanes. 767–200 and –300 series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, –400, –400D, and 747SR series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, –400, –400D, and 747SR series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, and 747SR series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, and 747SR series airplanes. 747–400 and –400D series airplanes. 747–400 and –400D series airplanes. 747–400 and –400D series airplanes. 747–400 and –400D series airplanes. 747–300, –400, and –400D series airplanes. 747–300, –400, and –400D series airplanes. 767–300 series airplanes. 767–300 series airplanes. 767–200 and –300 series airplanes. (xiv) 5A3109–2 ............................... (xx) 7A1418–21 and 7A1418–23 ... Ramp/Slide, off-wing, RH side ..... Slide/Raft, door 2 .......................... Slide, stretched upper deck .......... Slide/Raft, forward/aft doors ......... Ramp/Slide, off-wing door 3, LH side. (xxi) 7A1418–22 and 7A1418–24 .. Even S/Ns GT1830. through Ramp/Slide, off-wing door 3, RH side. (xxii) 7A1447–39 through 7A1447– 54 inclusive. GW2682 through GW2923 inclusive. Slide/Raft, doors 1, 2, and 4 ........ (xxiii) 7A1448–5 through 7A1448– 12 inclusive. GX1538 through GX1593 inclusive. Slide/Raft, door 5 .......................... (xxiv) 7A1467–21 and 7A1467–23 Odd S/Ns GH1969 through GH2443. Even S/Ns GH1954 through GH2420. Odd S/Ns GJ909 through GJ1163 Slide/Raft, doors 1 and 4, LH side Even S/Ns GJ912 through GJ1150. Odd S/Ns GI1019 through GI1265 Slide/Raft, door 5, RH side .......... Even S/Ns GI1036 through GI1298. Odd S/Ns GK355 through GK403 Even S/Ns GK356 through GK406 PB0001 through PB0399 inclusive, and all S/Ns with a B23 prefix. PG0001 through PG0275 inclusive, and all S/Ns with a B101 prefix. PC0001 through PC0263 inclusive, and all S/Ns with a B102 prefix. PK0001 through PK0160 inclusive, and all S/Ns with a L55 prefix. PF0001 through PF0163 inclusive, and all S/Ns with a R55 prefix. PH0001 through PH0299 inclusive, and all S/Ns with a L56 prefix. PD0001 through PD0293 inclusive, and all S/Ns with a R56 prefix. Slide/Raft, door 2, RH side .......... (xxv) 7A1467–22 and 7A1467–24 (xxvi) 7A1469–13 ........................... (xxvii) 7A1469–14 .......................... (xxviii) 7A1479–13 ......................... (xxix) 7A1479–14 ........................... pwalker on PROD1PC71 with PROPOSALS (xxx) 7A1489–3 .............................. (xxxi) 7A1489–4 ............................. (xxxii) 101623–107 through 101623–303 inclusive. (xxxiii) Odd 101630–105 305. (xxxiv) Even 101630–106 306. (xxxv) Odd 101655–101 305. (xxxvi) Even 101655–102 306. (xxxvii) Odd 101656–103 305. (xxxviii) Even 101656–104 306. VerDate Aug<31>2005 dash numbers through 101630– dash numbers through 101630– dash numbers through 101655– dash numbers through 101655– dash numbers through 101656– dash numbers through 101656– 17:15 Jun 07, 2007 Jkt 211001 PO 00000 GT1576 Slide, forward door ....................... Frm 00006 Fmt 4702 Slide/Raft, doors 1 and 4, RH side Slide/Raft, door 5, LH side ........... Slide/Raft, door 2, LH side ........... Slide/Raft, mid door, LH side ....... Slide/Raft, mid door, RH side ....... Slide, forward/aft door .................. Ramp/Slide, off-wing, LH side ...... 767–200 and –300 series airplanes. Ramp/Slide, off-wing, RH side ..... 767–200 and –300 series airplanes. Ramp/Slide, off-wing, LH side ...... 767–200 and –300 series airplanes. Ramp/Slide, off-wing, RH side ..... 767–200 and –300 series airplanes. Ramp/Slide, off-wing, LH side ...... 767–200 and –300 series airplanes. Ramp/Slide, off-wing, RH side ..... 767–200 and –300 series airplanes. Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules 31765 TABLE 1.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN BOEING MODEL AIRPLANES—Continued Goodrich evacuation systems having part number (P/N)— Having any serial number (S/N)— Component/part is named— Installed on Boeing Model— (xxxix) 101658–101 and 101658– 103. (xl) 101659–101 through 101659– 205 inclusive. (xli) 101660–101 through 101660– 107 inclusive. (xlii) 5A3086–3 and 5A3086–301 .. PAK001 through PAK136 inclusive. PAL001 through PAL670 inclusive Slide, forward door ....................... 737–200 series airplanes. Slide, aft door ............................... PAB001 through PAB610 inclusive. B3F001 through B3F314 inclusive Slide, forward door ....................... (xliii) 5A3088–3 and 5A3088–301 B3A001 through B3A337 inclusive Slide, aft door ............................... (xliv) 5A3109–1 .............................. Odd S/Ns, ST0001 through ST0013. Even S/Ns, ST0002 through ST0012. BNG0001 through BNG0212 inclusive. GS0001 through GS1339 inclusive, and all S/Ns with a single G prefix. GV001 through GV213 inclusive, and all S/Ns with a single G prefix. Odd S/Ns GT0001 through GT1589, and all odd S/Ns with a single letter G prefix. Ramp/Slide, off-wing, LH side ...... 737–200, –300, –400, and –500 series airplanes. 737–300, –400, and –500 series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 777–300 and –300ER series airplanes. 777–300 and –300ER series airplanes. 737–600, –700, –700C, –800, and –900 series airplanes. 747–100B SUD, –300, –400, and –400D series airplanes. (xlv) 5A3109–2 ............................... (xlvi) 5A3307–1 through 5A3307–5 inclusive, and 5A3307–301. (xlvii) 7A1323–1 through 7A1323– 114 inclusive. (xlviii) 7A1394–3 through 7A1394– 6 inclusive. (xlix) Odd dash numbers 7A1418– 1 through 7A1418–23. Slide, forward door ....................... Ramp/Slide, off-wing, RH side ..... Slide, forward/aft door .................. Slide, Stretched upper deck ......... Slide/Raft, forward/aft doors ......... 767–200 and –300 series airplanes. Ramp/Slide, off-wing door 3, LH side. 747–100, –100B, –100B SUD, –200B, –200C, –300, –400, –400D, and 747SR series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, –400, –400D, and 747SR series airplanes. 747–100B, –200C, –300, and 747SR series airplanes. (l) Even dash numbers 7A1418–2 through 7A1418–24. Even S/Ns GT0002 through GT1574, and all even S/Ns with a single letter G prefix. Ramp/Slide, off-wing door 3, RH side. (li) 7A1437–1 through 7A1437–8 inclusive. GW0001 through GW2923 inclusive, and all S/Ns with a single letter G prefix. GX0001 through GX1593 inclusive, and all S/Ns with a single letter G prefix. GW0001 through GW2681 inclusive, and all S/Ns with a single letter G prefix. GX0001 through GX1537, and all S/Ns with a single letter G prefix. Odd S/Ns GH0001 through GH1967, and all odd S/Ns with a single letter G prefix. Even S/Ns GH0002 through GH1952, and all even S/Ns with a single letter G prefix. Odd S/Ns GJ001 through GJ907, and all odd S/Ns with a single letter G prefix. Even S/Ns GJ002 through GJ910, and all even S/Ns with a single letter G prefix. Odd S/Ns GI0001 through GI1017, and all odd S/Ns with a single letter G prefix. Even S/Ns GI0002 through GI1034, and all even S/Ns with a single letter G prefix. Odd S/Ns GK001 through GK353, and all odd S/Ns with a single letter G prefix. Even S/Ns GK002 through GK354, and all even S/Ns with a single letter G prefix. Slide/Raft, doors 1, 2, and 4 ........ (lii) 7A1439–1 through 7A1439–8 inclusive. (liii) 7A1447–1 through 7A1447–54 inclusive. (liv) 7A1448–1 through 7A1448–12 inclusive. (lv) Odd dash numbers 7A1467–1 through 7A1467–23. (lvi) Even dash numbers 7A1467– 2 through 7A1467–24. (lvii) Odd dash numbers 7A1469–1 through 7A1469–13. (lviii) Even dash numbers 7A14692 through 7A1469-14. (lix) Odd dash numbers 7A1479–1 through 7A1479–13. (lx) Even dash numbers 7A1479–2 through 7A1479–14. pwalker on PROD1PC71 with PROPOSALS (lxi) 7A1489–1 and 7A1489–3 ....... (lxii) 7A1489–2 and 7A1489–4 ...... VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00007 Fmt 4702 Slide/Raft, door 5 .......................... 747–100B, –200C, –300, 747SR series airplanes. Slide/Raft, doors 1, 2, and 4 ........ 747–100, –100B, –100B SUD, –200B, –200C, –300, and 747SR series airplanes. 747–100, –100B, –100B SUD, –200B, –200C, –300, and 747SR series airplanes. 747–400 and –400D series airplanes. Slide/Raft, door 5 .......................... Slide/Raft, doors 1 and 4, LH side and Slide/Raft, doors 1 and 4, RH side 747–400 and –400D series airplanes. Slide/Raft, door 5, LH side ........... 747–400 and –400D series airplanes. Slide/Raft, door 5, RH side .......... 747–400 and –400D series airplanes. Slide/Raft, door 2, LH side ........... 747–300, –400, and –400D series airplanes. Slide/Raft, door 2, RH side .......... 747–300, –400, and –400D series airplanes. Slide/Raft, mid door, LH side ....... 767–300 series airplanes. Slide/Raft, mid door, RH side ....... 767–300 series airplanes. Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 31766 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules TABLE 2.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN MCDONNELL DOUGLAS MODEL AIRPLANES Goodrich evacuation systems having P/N— Having any S/N— Component/part is named—≤ Installed on McDonnell Douglas Model— (i) 100504–101 through 100504– 205 inclusive. D9F161 through D9F256 inclusive, and PU0325 through PU0331 inclusive. Slide, forward door ....................... (ii) 100505–101 through 100505– 201 inclusive. D9A078 through D9A122 inclusive, and PS0151 through PS0157 inclusive. Slide, aft door ............................... (iii) 100506–103 through 100506– 203 inclusive. D9T085 through D9T127 inclusive, and PT0175 through PT0178 inclusive. Slide, tailcone ............................... (iv) 100504–101 through 100504– 205 inclusive. D9F001 through D9F160 inclusive, and PU0001 through PU0324 inclusive. Slide, forward door ....................... (v) 100505–101 through 100505– 201 inclusive. D9A001 through D9A077 inclusive, and PS0001 through PS0150 inclusive. Slide, aft door ............................... (vi) 100506–103 through 100506– 203 inclusive. D9T001 through D9T084 inclusive, and PT0001 through PT0174 inclusive. Slide, tailcone ............................... (vii) 7A1274–3 through 7A1274–12 inclusive. (viii) 7A1275–3 through 7A1275– 20 inclusive. (ix) 7A1276–3 through 7A1276–12 inclusive. All .................................................. Slide, forward/service door ........... All .................................................. Slide, aft door ............................... All .................................................. Slide, tailcone ............................... DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81), DC–9–82 (MD–82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes; Model MD–88 airplanes; and Model MD–90–30 airplanes. DC–9–81 (MD–81) and DC–9–82 (MD–82) airplanes. DC–9–81 (MD–81) and DC–9–82 (MD–82) airplanes. DC–9–11, DC–9–12, DC–9–13, DC–9–14, DC–9–15, and DC– 9–15F airplanes; Model DC–9– 21 airplanes; Model DC–9–31, DC–9–32, DC–9–32 (VC–9C), DC–9–32F, DC–9–33F, DC–9– 34, DC–9–34F, and DC–9–32F (C–9A, C–9B) airplanes; Model DC–9–41 airplanes; Model DC– 9–51 airplanes; and Model DC– 9–81 (MD–81), DC–9–82 (MD– 82), DC–9–83 (MD–83), and DC–9–87 (MD–87) airplanes. TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES pwalker on PROD1PC71 with PROPOSALS Goodrich evacuation system having P/N— Having any S/N— Component/part is named— Installed on Airbus Model— (i) 4A3928–1 .................................. (ii) 4A3928–2 ................................. (iii) 4A3931–1 and 4A3931–3 ........ AY0001 through AY0007 inclusive AZ0001 through AZ0007 inclusive AQ0001 through AQ0028 inclusive. AT0001 through AT0028 inclusive AK0001 through AK0028 inclusive AM0001 through AM0028 inclusive. Slide, door 3 type 1, LH side ....... Slide, door 3 type 1, RH side ....... Ramp/Slide, off–wing, LH side ..... A340–541 airplanes. A340–541 airplanes. A340–642 airplanes. Ramp/Slide, off–wing, RH side .... Slide/Raft, door 3, LH side ........... Slide/Raft, door 3, RH side .......... A340–642 airplanes. A340–642 airplanes. A340–642 airplanes. (iv) 4A3931–2 and 4A3931–4 ........ (v) 4A3934–1 and 4A3934–3 ........ (vi) 4A3934–2 and 4A3934–4 ........ VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules 31767 TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued Having any S/N— Component/part is named— Installed on Airbus Model— (vii) 7A1296–004 and 7A1296–005 WB0030 through WB0033 inclusive. Slide, mid door ............................. (viii) 7A1297–103 and 7A1297– 203. WF0257 through WF0273 inclusive. Ramp/Slide, off–wing door ........... (ix) 7A1298–004 and 7A1298–005 WA0327 through WA0374 inclusive. Slide, forward/aft door .................. (x) 7A1299–006 ............................. WE0149 through WE0172 inclusive. Slide, emergency door ................. (xi) 7A1300–007 ............................ WC0423 through WC0507 inclusive. Slide/Raft, forward/aft door ........... (xii) 7A1359–005 ............................ WD0134 through WD0159 inclusive. Slide/Raft, mid door ...................... (xiii) 7A1508–109 7A1508–117 inclusive. pwalker on PROD1PC71 with PROPOSALS Goodrich evacuation system having P/N— AA1041 through AA2419 inclusive Slide/Raft, doors 1 and 4 ............. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A310–203, –204, –221, and –222 airplanes; and Model A310– 304, –322, –324, and –325 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; Model A300 F4–605R and F4– 622R airplanes; and Model A310–203, –204, –221, and –222 airplanes; and Model A310–304, –322, –324, and –325 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; Model A300 F4–605R and F4– 622R airplanes; and Model A310–203, –204, –221, and –222 airplanes; and Model A310–304, –322, –324, and –325 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. VerDate Aug<31>2005 through 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 31768 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued Goodrich evacuation system having P/N— Having any S/N— Component/part is named— Installed on Airbus Model— (xiv) 7A1509–111, and 7A1509–117. 7A1509–115 AD0487 through AD1007 inclusive. Slide, door 3 type 1 ...................... (xv) 7A1510–109 through 7A1510– 117 inclusive. AB0077 through AB0150 inclusive Slide/Raft, door 3 type A, LH side (xvi) 7A1510–110 7A1510–118 inclusive. through AC0077 through AC0148 inclusive. Slide/Raft, door 3 type A, RH side (xvii) 7A1539–109 7A1539–117 inclusive. through AU0302 through AU0677 inclusive. Slide/Raft, door 2, LH side ........... (xviii) 7A1539–110 7A1539–118 inclusive. through AX0302 through AX0673 inclusive Slide/Raft, door 2, RH side .......... (xix) 7A1296–001 7A1296–004 inclusive. through WB0001 through WB0029 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. Slide, mid door ............................. (xx) 7A1297–101 through 7A1297– 203 inclusive. WF0001 through WF0256 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. WA0001 through WA0326 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. Ramp/Slide, off–wing door ........... A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A310–203, –204, –221, and –222 airplanes; and Model A310– 304, –322, –324, and –325 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; Model A300 F4–605R and F4– 622R airplanes; and Model A310–203, –204, –221, and –222 airplanes; and Model A310–304, –322, –324, and –325 airplanes. pwalker on PROD1PC71 with PROPOSALS (xxi) 7A1298–001 7A1298–004 inclusive. VerDate Aug<31>2005 through 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00010 Fmt 4702 Slide, forward/aft door .................. Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules 31769 TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued Having any S/N— Component/part is named— Installed on Airbus Model— (xxii) 7A1299–001 7A1299–006 inclusive. through WE0001 through WE0148 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. Slide, emergency door ................. (xxiii) 7A1300–001 7A1300–007 inclusive. through WC0001 through WC0422 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. Slide/Raft, forward/aft door ........... (xxiv) 7A1359–001 7A1359–005 inclusive. through WD0001 through WD0133 inclusive, all S/Ns with a single letter R prefix, and all S/Ns with a single letter G prefix. Slide/Raft, mid door ...................... (xxv) 7A1508–001 through 7A1508–017 inclusive, and 7A1508–101 through 7A1508– 117 inclusive. AA0001 through AA1040 inclusive Slide/Raft, doors 1 and 4 ............. (xxvi) 7A1509–001 through 7A1509–005 inclusive, and 7A1509–101 through 7A1509– 117 inclusive. AD0001 through AD0486 inclusive. Slide, door 3 type 1 ...................... (xxvii) 7A1510–001 through 7A1510–017 inclusive, and 7A1510–101 through 7A1510– 117 inclusive. AB0001 through AB0076 inclusive Slide/Raft, door 3 type A, LH side (xxviii) 7A1510–002 through 7A1510–018 inclusive, and 7A1510–102 through 7A1510– 118 inclusive. pwalker on PROD1PC71 with PROPOSALS Goodrich evacuation system having P/N— AC0001 through AC0076 inclusive. Slide/Raft, door 3 type A, RH side A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; Model A300 F4–605R and F4– 622R airplanes; and Model A310–203, –204, –221, and –222 airplanes; and Model A310–304, –322, –324, and –325 airplanes. A300 B2–1A, B2–1C, B2K–3C, and B2–203 airplanes; Model A300 B4–2C, B4–103, and B4– 203 airplanes; Model A300 B4– 601, B4–603, B4–620, and B4– 622 airplanes; Model A300 B4– 605R and B4–622R airplanes; and Model A300 F4–605R and F4–622R airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; and Model A340–311, –312, and –313 airplanes. VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00011 Fmt 4702 Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 31770 Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued Goodrich evacuation system having P/N— Having any S/N— Component/part is named— Installed on Airbus Model— (xxix) 7A1539–001 through 7A1539–017 inclusive, and 7A1539–101 through 7A1539– 117 inclusive. AU0001 thru AU0301 inclusive .... Slide/Raft, door 2, LH side ........... (xxx) 7A1539–002 through 7A1539–018 inclusive, and 7A1539–102 through 7A1539– 118 inclusive. AX0001 thru AX0301 inclusive ..... Slide/Raft, door 2, RH side .......... A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. A330–201, –202, –203, –223, and –243 airplanes; Model A330– 301, –321, –322, –323, –341, –342, and –343 airplanes; Model A340–211, –212, and –213 airplanes; Model A340– 311, –312, and –313 airplanes; Model A340–541 airplanes; and Model A340–642 airplanes. Unsafe Condition (d) This AD is prompted by several reports of corroded shear-pin restraints that prevented Goodrich evacuation systems from deploying properly. We are issuing this AD to prevent failure of the evacuation system, which could impede an emergency evacuation and increase the chance of injury to passengers and flightcrew during the evacuation. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Service Bulletin Reference (f) The term ‘‘service bulletin,’’ as used in this AD, means the following service bulletins, as applicable: (1) For Goodrich evacuation systems identified in Table 3 of this AD: Goodrich Service Bulletin 25–344, Revision 2, dated October 11, 2006; and (2) For Goodrich evacuation systems identified in Tables 1 and 2 of this AD: Goodrich Service Bulletin 25–343, Revision 3, dated January 12, 2007. pwalker on PROD1PC71 with PROPOSALS Compliance Times (g) Perform the actions specified in paragraph (h) of this AD at the applicable compliance time specified in paragraph (g)(1) or (g)(2) of this AD. (1) For Goodrich evacuation systems installed on Boeing Model 767 airplanes as off-wing ramp/slide units and identified in Table 1 of this AD: Do the actions within 18 months after the effective date of this AD. (2) For Goodrich evacuation systems other than those identified in paragraph (g)(1) of this AD: Do the actions within 36 months after the effective date of this AD. Replacement, or Inspections and Corrective Action (h) Do the actions specified in paragraph (h)(1) or (h)(2) of this AD in accordance with the Accomplishment Instructions of the applicable service bulletin. (1) For Goodrich evacuation systems identified in paragraphs (c)(1)(i) through (c)(1)(xxxi) inclusive in Table 1 of this AD, (c)(2)(i) through (c)(2)(iii) inclusive in Table 2 of this AD, and (c)(3)(i) through (c)(3)(xviii) inclusive in Table 3 of this AD: Replace the shear-pin restraints with new restraints. (2) For Goodrich evacuation systems identified in paragraphs (c)(1)(xxxii) through (c)(1)(lxii) inclusive in Table 1 of this AD, (c)(2)(iv) through (c)(2)(ix) inclusive in Table 2 of this AD, and (c)(3)(xix) through (c)(3)(xxx) inclusive in Table 3 of this AD: Do an inspection to verify the manufacturing lot number of the shear-pin restraint. A review of airplane maintenance records is acceptable in lieu of this inspection if the manufacturing lot number of the shear-pin restraint can be conclusively determined from that review. (i) If a manufacturing lot number from 3375 through 5551 inclusive is found, before further flight, replace the shear-pin restraint with a new restraint. (ii) If a manufacturing lot number from 3375 through 5551 inclusive is not found, do a general visual inspection of the shear-pin restraints for discrepancies (i.e., corrosion, security of pin retainer/label, overall condition, and lack of play). If any discrepancy is found, before further flight, replace the shear-pin restraint with a new restraint. Note 1: For the purposes of this AD, a general visual inspection is: ‘‘A visual examination of an interior or exterior area, installation, or assembly to detect obvious damage, failure, or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to ensure visual access to all surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked.’’ Parts Installation (i) As of the effective date of this AD, no Goodrich evacuation system identified in paragraph (h)(1) of this AD may be installed on any airplane, unless the shear-pin restraints have been replaced with new restraints in accordance with paragraph (h)(1) of this AD. (j) As of the effective date of this AD, no Goodrich evacuation system identified in paragraph (h)(2) of this AD may be installed on any airplane, unless the shear-pin restraints have been inspected and found acceptable in accordance with paragraph (h)(2) of this AD. Credit for Actions Done Using Previous Service Information (k) Replacements and inspections done before the effective date of this AD in accordance with the applicable service bulletins identified in Table 4 of this AD, are acceptable for compliance with the requirements of paragraph (h) of this AD. TABLE 4.—ACCEPTABLE GOODRICH SERVICE BULLETINS Goodrich Service Bulletin Revision level 25–343 ................................................................................................................................................. 25–343 ................................................................................................................................................. 25–343 ................................................................................................................................................. Original .................... 1 ............................... 2 ............................... VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 PO 00000 Frm 00012 Fmt 4702 Sfmt 4702 E:\FR\FM\08JNP1.SGM 08JNP1 Date October 15, 2003. January 31, 2005. October 11, 2006. Federal Register / Vol. 72, No. 110 / Friday, June 8, 2007 / Proposed Rules 31771 TABLE 4.—ACCEPTABLE GOODRICH SERVICE BULLETINS—Continued Goodrich Service Bulletin Revision level 25–344 ................................................................................................................................................. 25–344 ................................................................................................................................................. Original .................... 1 ............................... Alternative Methods of Compliance (AMOCs) (l)(1) The Manager, Los Angeles Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Issued in Renton, Washington, on May 30, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7–10992 Filed 6–7–07; 8:45 am] BILLING CODE 4910–13–P ENVIRONMENTAL PROTECTION AGENCY 40 CFR Parts 51, 78, and 97 [EPA–HQ–OAR–2004–0439, FRL–8323–4] RIN 2060–AN12 Petition for Reconsideration and Proposal for Withdrawal of Findings of Significant Contribution and Rulemaking for Georgia for Purposes of Reducing Ozone Interstate Transport Environmental Protection Agency (EPA). ACTION: Proposed rule. pwalker on PROD1PC71 with PROPOSALS AGENCY: SUMMARY: In this action, we are requesting comments on EPA’s response to a Petition for Reconsideration regarding a final rule we issued under Section 110 of the Clean Air Act (CAA) related to the interstate transport of nitrogen oxides (NOX). On April 21, 2004, we issued a final rule (Phase II NOX SIP Call Rule) that required the State of Georgia to submit revisions to its State Implementation Plan (SIP) that prohibit specified amounts of NOX emissions—one of the precursors to ozone (smog) pollution— for the purposes of reducing NOX and ozone transport across State boundaries in the eastern half of the United States. This rule became effective on June 21, 2004. Subsequently, the Georgia Coalition for Sound Environmental Policy (GCSEP VerDate Aug<31>2005 17:15 Jun 07, 2007 Jkt 211001 or Petitioners) filed a Petition for Reconsideration requesting that EPA reconsider the applicability of the NOX SIP Call Rule to the State of Georgia. In response to this Petition, and based upon review of additional available information, EPA is proposing to remove Georgia from the NOX SIP call region. Specifically, EPA proposes to rescind the applicability of the requirements of the Phase II NOX SIP Call Rule to the State of Georgia, only. DATES: Comments. Comments must be received on or before July 23, 2007. Public Hearing. If anyone contacts us requesting to speak at a public hearing by June 25, 2007, we will hold a public hearing and hold the record open for purposes of rebuttal comments. Additional information about the hearing and rebuttal comments would be published in a subsequent Federal Register notice. ADDRESSES: Submit your comments, identified by Docket ID No. EPA–HQ– OAR–2005–0439, by one of the following methods: • http://www.regulations.gov. Follow the on-line instructions for submitting comments. • E-mail: a-and-r-Docket@epa.gov. • Fax: (202) 566–9744. • Mail: Attention Docket ID No. EPA– HQ–OAR–2004–0439, U.S. Environmental Protection Agency, EPA West (Air Docket), Room 3334, 1301 Constitution Avenue, Northwest, Washington, DC. Please include a total of two copies. • Hand Delivery: U.S. Environmental Protection Agency, EPA West (Air Docket), 1301 Constitution Avenue, Northwest, Room 3334, Washington, DC 20004. Such deliveries are only accepted during the Docket’s normal hours of operation, and special arrangements should be made for deliveries of boxed information. Instructions: Direct your comments to Docket ID No. EPA–HQ–OAR–2004– 0439. EPA’s policy is that all comments received will be included in the public docket without change and may be made available online at www.regulations.gov, including any personal information provided, unless the comment includes information claimed to be Confidential Business Information (CBI) or other information whose disclosure is restricted by statute. PO 00000 Frm 00013 Fmt 4702 Sfmt 4702 Date October 15, 2003. January 31, 2005. Do not submit information that you consider to be CBI or otherwise protected through www.regulations.gov or e-mail. The www.regulations.gov Web site is an ‘‘anonymous access’’ system, which means EPA will not know your identity or contact information unless you provide it in the body of your comment. If you send an e-mail comment directly to EPA without going through www.regulations.gov your email address will be automatically captured and included as part of the comment that is placed in the public docket and made available on the Internet. If you submit an electronic comment, EPA recommends that you include your name and other contact information in the body of your comment and with any disk or CD–ROM you submit. If EPA cannot read your comment due to technical difficulties and cannot contact you for clarification, EPA may not be able to consider your comment. Electronic files should avoid the use of special characters, any form of encryption, and be free of any defects or viruses. For additional information about EPA’s public docket visit the EPA Docket Center homepage at http:// www.epa.gov/epahome/dockets.htm. Docket: All documents in the docket are listed in the www.regulations.gov index. Although listed in the index, some information is not publicly available, e.g., CBI or other information whose disclosure is restricted by statute. Certain other material, such as copyrighted material, will be publicly available only in hard copy. Publicly available docket materials are available either electronically in www.regulations.gov or in hard copy at the Air Docket, EPA/DC, EPA West, Room 3334, 1301 Constitution Ave., NW., Washington, DC. This Docket Facility is open from 8:30 a.m. to 4:30 p.m., Monday through Friday, excluding legal holidays. The telephone number for the Public Reading Room is (202) 566–1744, and the telephone number for the Air Docket is (202) 566–1742. FOR FURTHER INFORMATION CONTACT: Tim Smith, Air Quality Policy Division, Geographic Strategies Group (C539–04), Environmental Protection Agency, Research Triangle Park, NC 27711, telephone (919) 541–4718, e-mail smith.tim@epa.gov. For legal questions, please contact Winifred Okoye, U.S. E:\FR\FM\08JNP1.SGM 08JNP1

Agencies

[Federal Register Volume 72, Number 110 (Friday, June 8, 2007)]
[Proposed Rules]
[Pages 31761-31771]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-10992]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28370; Directorate Identifier 2003-NM-239-AD]
RIN 2120-AA64


Airworthiness Directives; Goodrich Evacuation Systems Approved 
Under Technical Standard Order (TSO), TSO-C69, TSO-C69a, TSO-C69b, and 
TSO-69c, Installed on Various Boeing, McDonnell Douglas, and Airbus 
Transport Category Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Goodrich evacuation systems approved under TSO-C69, TSO-
C69a, TSO-C69b, and TSO-69c, installed on certain Boeing, McDonnell 
Douglas, and Airbus transport category airplanes. For certain systems, 
this proposed AD would require replacing the evacuation systems shear-
pin restraints with new ones. For certain other systems, this proposed 
AD would require an inspection for manufacturing lot numbers; and a 
general visual inspection of the shear-pin restraint for discrepancies, 
and corrective actions if necessary. This proposed AD is prompted by 
several reports of corroded shear-pin restraints that prevented 
Goodrich evacuation systems from deploying properly. We are proposing 
this AD to prevent failure of the evacuation system, which could impede 
an emergency evacuation and increase the chance of injury to passengers 
and flightcrew during the evacuation.

DATES: We must receive comments on this proposed AD by July 23, 2007.

ADDRESSES: Use one of the following addresses to submit comments on 
this proposed AD.
     DOT Docket Web site: Go to http://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to http://
www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401, 
Washington, DC 20590.
     By fax: (202) 493-2251.
     Hand Delivery: Room PL-401 on the plaza level of the 
Nassif Building,

[[Page 31762]]

400 Seventh Street SW., Washington, DC, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
    Contact Goodrich, Aircraft Interior Products, ATTN: Technical 
Publications, 3414 South Fifth Street, Phoenix, AZ 85040, for service 
information identified in this proposed AD.

FOR FURTHER INFORMATION CONTACT: Tracy Ton, Aerospace Engineer, Cabin 
Safety/Mechanical and Environmental Systems Branch, ANM-150L, FAA, Los 
Angeles Aircraft Certification Office, 3960 Paramount Boulevard, 
Lakewood, California 90712-4137; telephone (562) 627-5352; fax (562) 
627-5210.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to submit any written relevant data, views, or 
arguments regarding this proposed AD. Send your comments to an address 
listed under ADDRESSES. Include ``Docket No. FAA-2007-28370; 
Directorate Identifier 2003-NM-239-AD'' in the subject line of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the proposed AD. We will 
consider all comments submitted by the closing date and may amend the 
proposed AD in light of those comments.
    We will post all comments we receive, without change, to http://
dms.dot.gov, including any personal information you provide. We will 
also post a report summarizing each substantive verbal contact with FAA 
personnel concerning this proposed AD. Using the search function of 
that website, anyone can find and read the comments in any of our 
dockets, including the name of the individual who sent the comment (or 
signed the comment on behalf of an association, business, labor union, 
etc.). You can review DOT's complete Privacy Act Statement in the 
Federal Register published on April 11, 2000 (65 FR 19477-78), or you 
can visit http://dms.dot.gov.

Examining the Docket

    You can examine the AD docket on the Internet at http://
dms.dot.gov, or in person at the Docket Management Facility office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT 
street address stated in the ADDRESSES section. Comments will be 
available in the AD docket shortly after the DMS receives them.

Discussion

    We have received several reports indicating that Goodrich 
evacuation systems installed on certain Boeing Model 747 airplanes and 
Model 767 airplanes have not deployed properly due to corroded shear-
pin restraints. The corrosion problem arose concurrently with a 1998 
change in the anodize specification for restraint bodies. Corrosion of 
the shear-pin restraints, if not corrected, can lead to higher than 
designed release values, and in severe cases, can cause the two halves 
of the restraints to freeze up, which can lead to improper deployment 
and/or loss of use of the evacuation system. That loss could impede 
emergency evacuation and increase the chance of injury to passengers 
and flightcrew during the evacuation.

Other Relevant Rulemaking

    The reports involved certain Boeing Model 747 airplanes and Model 
767 airplanes that are equipped with the affected Goodrich evacuation 
system as part of a type certificate (TC); however, certain Goodrich 
evacuation systems installed as a technical standard order (TSO) 
appliance on certain Airbus, Boeing and McDonnell Douglas transport 
category airplanes use the same restraints as those used by the 
affected type certificated Goodrich units. Therefore evacuation systems 
approved by either TSO or TC are subject to the identified unsafe 
condition. We are planning to issue similar rulemaking (Directorate 
Identifier 2005-NM-139-AD) for certain Boeing Model 747 airplanes and 
Model 767 airplanes that are equipped with certain type certificated 
Goodrich evacuation systems.

Relevant Service Information

    We have reviewed Goodrich Service Bulletins 25-343, Revision 3, 
dated January 12, 2007; and 25-344, Revision 2, dated October 11, 2006. 
Goodrich Service Bulletin 25-343 affects evacuation systems installed 
on certain Boeing and McDonnell Douglas transport category airplanes. 
Goodrich Service Bulletin 25-344 affects evacuation systems installed 
on certain Airbus transport category airplanes. For certain systems, 
the service bulletins describe procedures for replacing the shear-pin 
restraints with new, improved restraints. For certain other systems, 
the service bulletins describe procedures for an inspection to verify 
the manufacturing lot number of the restraints; and a general visual 
inspection of the restraints for discrepancies (i.e., corrosion, 
security of pin retainer/label, overall condition, and lack of play), 
and corrective action if necessary. The corrective action is replacing 
the shear-pin restraints with new shear-pin restraints. Accomplishing 
the actions specified in the service information is intended to 
adequately address the unsafe condition.

FAA's Determination and Requirements of the Proposed AD

    We have evaluated all pertinent information and identified an 
unsafe condition that is likely to exist or develop on other products 
of this same type design. Therefore, we are proposing this AD, which 
would require you to use the service information described previously 
to perform these actions, except as discussed under ``Difference 
Between this Proposed AD and the Service Bulletins.''

Difference Between This Proposed AD and the Service Bulletins

    Although the service bulletins recommend accomplishing the 
replacement or inspection ``at the next shop visit,'' we have 
determined that this imprecise compliance time would not address the 
identified unsafe condition soon enough to ensure an adequate level of 
safety for the affected fleet. In developing an appropriate compliance 
time for this AD, we considered the manufacturer's recommendation, the 
degree of urgency associated with the subject unsafe condition, and the 
average utilization of the affected fleet. In light of all of these 
factors, we find that a compliance time of 18 months for Goodrich 
evacuation systems installed on Boeing Model 767 off-wing ramp/slide 
units and 36 months for all other evacuation systems represents an 
appropriate interval of time for affected airplanes to continue to 
operate without compromising safety. We have coordinated this 
difference with the manufacturer.

Costs of Compliance

    This proposed AD would affect certain Goodrich evacuation systems 
installed on about 2,844 airplanes worldwide. This proposed AD would 
affect about 1,240 airplanes of U.S. registry. The following table 
provides the estimated costs for U.S. operators to comply with this 
proposed AD.

[[Page 31763]]



                                                                     Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
                                                           Average
              Action                    Work hours       labor rate          Parts         Cost per slide unit    Number of slide         Fleet cost
                                                          per hour                                               units per airplane
--------------------------------------------------------------------------------------------------------------------------------------------------------
Replacement......................  Between 2 and 9....          $80   Between $58 and      Between $218 and     Between 2 and 12...  Between $540,640
                                                                       $638, depending on   $1,358.                                   and $20,207,040.
                                                                       number of
                                                                       restraints.
Inspection.......................  Between 2 and 9....          $80   None...............  Between $160 and     Between 2 and 12...  Between $396,800
                                                                                            $720.                                     and $10,713,600.
--------------------------------------------------------------------------------------------------------------------------------------------------------

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, Section 106, describes the 
authority of the FAA Administrator. Subtitle VII, Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in 
Subtitle VII, Part A, Subpart III, Section 44701, ``General 
Requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We have determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that the proposed 
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this proposed AD. See the ADDRESSES section for a location 
to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

    1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

    2. The FAA amends 39.13 by adding the following new airworthiness 
directive (AD):

Goodrich (Formerly BFGoodrich): Docket No. FAA-2007-28370; 
Directorate Identifier 2003-NM-239-AD.

Comments Due Date

    (a) The Federal Aviation Administration (FAA) must receive 
comments on this AD action by July 23, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to:
    (1) Goodrich evacuation systems approved under Technical 
Standard Order (TSO) TSO-C69, TSO-C69a, and TSO-C69b, installed on 
certain Boeing airplanes, certificated in any category, as listed in 
Table 1 of this AD;
    (2) Goodrich evacuation systems approved under TSO-C69, TSO-
C69a, and TSO-C69b, installed on certain McDonnell Douglas 
airplanes, certificated in any category, as listed in Table 2 of 
this AD; and
    (3) Goodrich evacuation systems approved under TSO-C69a, TSO-
C69b, and TSO-C69c, installed on Airbus airplanes, certificated in 
any category, as listed in Table 3 of this AD.

                Table 1.--Goodrich Evacuation Systems Installed on Certain Boeing Model Airplanes
----------------------------------------------------------------------------------------------------------------
  Goodrich evacuation systems having      Having any serial        Component/part is       Installed on Boeing
         part number (P/N)--                number (S/N)--              named--                  Model--
----------------------------------------------------------------------------------------------------------------
(i) 101623-303.......................  PB0400 through PB0453    Slide, forward/aft door  767-200 and -300 series
                                        inclusive.                                        airplanes.
(ii) 101630-305......................  PG0276 through PG0309    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               left-hand (LH) side.     airplanes.
(iii) 101630-306.....................  PC0264 through PC0368    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               right-hand (RH) side.    airplanes.
(iv) 101655-305......................  PK0161 through PK0212    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               LH side.                 airplanes.
(v) 101655-306.......................  PF0164 through PF0220    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               RH side.                 airplanes.
(vi) 101656-305......................  PH0300 through PH0390    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               LH side.                 airplanes.
(vii) 101656-306.....................  PD0294 through PD0378    Ramp/Slide, off-wing,    767-200 and -300 series
                                        inclusive.               RH side.                 airplanes.
(viii) 101658-101 and 101658-103.....  PAK137 through PAK150    Slide, forward door....  737-200 series
                                        inclusive.                                        airplanes.

[[Page 31764]]

 
(ix) 101659-101 through 101659-205     PAL671 through PAL738    Slide, aft door........  737-200, -300, -400,
 inclusive.                             inclusive.                                        and -500 series
                                                                                          airplanes.
(x) 101660-101 through 101660-107      PAB611 through PAB649    Slide, forward door....  737-300, -400, and -500
 inclusive.                             inclusive.                                        series airplanes.
(xi) 5A3086-3 and 5A3086-301.........  B3F315 through B3F611    Slide, forward door....  737-600, -700, -700C, -
                                        inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xii) 5A3088-3 and 5A3088-301........  B3A338 through B3A685    Slide, aft door........  737-600, -700, -700C, -
                                        inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xiii) 5A3109-1......................  Odd S/Ns ST0015 through  Ramp/Slide, off-wing,    777-300 and -300ER
                                        ST0131.                  LH side.                 series airplanes.
(xiv) 5A3109-2.......................  Even S/Ns ST0014         Ramp/Slide, off-wing,    777-300 and -300ER
                                        through ST0128.          RH side.                 series airplanes.
(xv) 5A3294-1 and 5A3294-2...........  SS0001 through SS0210    Slide/Raft, door 2.....  767-300 and -400ER
                                        inclusive.                                        series airplanes.
(xvi) 5A3295-1 and 5A3295-3..........  SF0001 through SF0501    Slide/Raft, doors 1 and  767-200, -300, and -
                                        inclusive.               4.                       400ER series
                                                                                          airplanes.
(xvii) 5A3307-1 through 5A3307-5       BNG0213 through BNG4911  Slide, forward/aft door  737-600, -700, -700C, -
 inclusive and 5A3307-301.              inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xviii) 7A1323-111 through 7A1323-114  GS1340 through GS1879    Slide, stretched upper   747-100B SUD, -300, -
 inclusive.                             inclusive.               deck.                    400, and -400D series
                                                                                          airplanes.
(xix) 7A1394-4 and 7A1394-6..........  GV0214 through GV0249    Slide/Raft, forward/aft  767-200 and -300 series
                                        inclusive.               doors.                   airplanes.
(xx) 7A1418-21 and 7A1418-23.........  Odd S/Ns GT1591 through  Ramp/Slide, off-wing     747-100, -100B, -100B
                                        GT1857.                  door 3, LH side.         SUD, -200B, -200C, -
                                                                                          300, -400, -400D, and
                                                                                          747SR series
                                                                                          airplanes.
(xxi) 7A1418-22 and 7A1418-24........  Even S/Ns GT1576         Ramp/Slide, off-wing     747-100, -100B, -100B
                                        through GT1830.          door 3, RH side.         SUD, -200B, -200C, -
                                                                                          300, -400, -400D, and
                                                                                          747SR series
                                                                                          airplanes.
(xxii) 7A1447-39 through 7A1447-54     GW2682 through GW2923    Slide/Raft, doors 1, 2,  747-100, -100B, -100B
 inclusive.                             inclusive.               and 4.                   SUD, -200B, -200C, -
                                                                                          300, and 747SR series
                                                                                          airplanes.
(xxiii) 7A1448-5 through 7A1448-12     GX1538 through GX1593    Slide/Raft, door 5.....  747-100, -100B, -100B
 inclusive.                             inclusive.                                        SUD, -200B, -200C, -
                                                                                          300, and 747SR series
                                                                                          airplanes.
(xxiv) 7A1467-21 and 7A1467-23.......  Odd S/Ns GH1969 through  Slide/Raft, doors 1 and  747-400 and -400D
                                        GH2443.                  4, LH side.              series airplanes.
(xxv) 7A1467-22 and 7A1467-24........  Even S/Ns GH1954         Slide/Raft, doors 1 and  747-400 and -400D
                                        through GH2420.          4, RH side.              series airplanes.
(xxvi) 7A1469-13.....................  Odd S/Ns GJ909 through   Slide/Raft, door 5, LH   747-400 and -400D
                                        GJ1163.                  side.                    series airplanes.
(xxvii) 7A1469-14....................  Even S/Ns GJ912 through  Slide/Raft, door 5, RH   747-400 and -400D
                                        GJ1150.                  side.                    series airplanes.
(xxviii) 7A1479-13...................  Odd S/Ns GI1019 through  Slide/Raft, door 2, LH   747-300, -400, and -
                                        GI1265.                  side.                    400D series airplanes.
(xxix) 7A1479-14.....................  Even S/Ns GI1036         Slide/Raft, door 2, RH   747-300, -400, and -
                                        through GI1298.          side.                    400D series airplanes.
(xxx) 7A1489-3.......................  Odd S/Ns GK355 through   Slide/Raft, mid door,    767-300 series
                                        GK403.                   LH side.                 airplanes.
(xxxi) 7A1489-4......................  Even S/Ns GK356 through  Slide/Raft, mid door,    767-300 series
                                        GK406.                   RH side.                 airplanes.
(xxxii) 101623-107 through 101623-303  PB0001 through PB0399    Slide, forward/aft door  767-200 and -300 series
 inclusive.                             inclusive, and all S/                             airplanes.
                                        Ns with a B23 prefix.
(xxxiii) Odd dash numbers 101630-105   PG0001 through PG0275    Ramp/Slide, off-wing,    767-200 and -300 series
 through 101630-305.                    inclusive, and all S/    LH side.                 airplanes.
                                        Ns with a B101 prefix.
(xxxiv) Even dash numbers 101630-106   PC0001 through PC0263    Ramp/Slide, off-wing,    767-200 and -300 series
 through 101630-306.                    inclusive, and all S/    RH side.                 airplanes.
                                        Ns with a B102 prefix.
(xxxv) Odd dash numbers 101655-101     PK0001 through PK0160    Ramp/Slide, off-wing,    767-200 and -300 series
 through 101655-305.                    inclusive, and all S/    LH side.                 airplanes.
                                        Ns with a L55 prefix.
(xxxvi) Even dash numbers 101655-102   PF0001 through PF0163    Ramp/Slide, off-wing,    767-200 and -300 series
 through 101655-306.                    inclusive, and all S/    RH side.                 airplanes.
                                        Ns with a R55 prefix.
(xxxvii) Odd dash numbers 101656-103   PH0001 through PH0299    Ramp/Slide, off-wing,    767-200 and -300 series
 through 101656-305.                    inclusive, and all S/    LH side.                 airplanes.
                                        Ns with a L56 prefix.
(xxxviii) Even dash numbers 101656-    PD0001 through PD0293    Ramp/Slide, off-wing,    767-200 and -300 series
 104 through 101656-306.                inclusive, and all S/    RH side.                 airplanes.
                                        Ns with a R56 prefix.

[[Page 31765]]

 
(xxxix) 101658-101 and 101658-103....  PAK001 through PAK136    Slide, forward door....  737-200 series
                                        inclusive.                                        airplanes.
(xl) 101659-101 through 101659-205     PAL001 through PAL670    Slide, aft door........  737-200, -300, -400,
 inclusive.                             inclusive.                                        and -500 series
                                                                                          airplanes.
(xli) 101660-101 through 101660-107    PAB001 through PAB610    Slide, forward door....  737-300, -400, and -500
 inclusive.                             inclusive.                                        series airplanes.
(xlii) 5A3086-3 and 5A3086-301.......  B3F001 through B3F314    Slide, forward door....  737-600, -700, -700C, -
                                        inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xliii) 5A3088-3 and 5A3088-301......  B3A001 through B3A337    Slide, aft door........  737-600, -700, -700C, -
                                        inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xliv) 5A3109-1......................  Odd S/Ns, ST0001         Ramp/Slide, off-wing,    777-300 and -300ER
                                        through ST0013.          LH side.                 series airplanes.
(xlv) 5A3109-2.......................  Even S/Ns, ST0002        Ramp/Slide, off-wing,    777-300 and -300ER
                                        through ST0012.          RH side.                 series airplanes.
(xlvi) 5A3307-1 through 5A3307-5       BNG0001 through BNG0212  Slide, forward/aft door  737-600, -700, -700C, -
 inclusive, and 5A3307-301.             inclusive.                                        800, and -900 series
                                                                                          airplanes.
(xlvii) 7A1323-1 through 7A1323-114    GS0001 through GS1339    Slide, Stretched upper   747-100B SUD, -300, -
 inclusive.                             inclusive, and all S/    deck.                    400, and -400D series
                                        Ns with a single G                                airplanes.
                                        prefix.
(xlviii) 7A1394-3 through 7A1394-6     GV001 through GV213      Slide/Raft, forward/aft  767-200 and -300 series
 inclusive.                             inclusive, and all S/    doors.                   airplanes.
                                        Ns with a single G
                                        prefix.
(xlix) Odd dash numbers 7A1418-1       Odd S/Ns GT0001 through  Ramp/Slide, off-wing     747-100, -100B, -100B
 through 7A1418-23.                     GT1589, and all odd S/   door 3, LH side.         SUD, -200B, -200C, -
                                        Ns with a single                                  300, -400, -400D, and
                                        letter G prefix.                                  747SR series
                                                                                          airplanes.
(l) Even dash numbers 7A1418-2         Even S/Ns GT0002         Ramp/Slide, off-wing     747-100, -100B, -100B
 through 7A1418-24.                     through GT1574, and      door 3, RH side.         SUD, -200B, -200C, -
                                        all even S/Ns with a                              300, -400, -400D, and
                                        single letter G prefix.                           747SR series
                                                                                          airplanes.
(li) 7A1437-1 through 7A1437-8         GW0001 through GW2923    Slide/Raft, doors 1, 2,  747-100B, -200C, -300,
 inclusive.                             inclusive, and all S/    and 4.                   and 747SR series
                                        Ns with a single                                  airplanes.
                                        letter G prefix.
(lii) 7A1439-1 through 7A1439-8        GX0001 through GX1593    Slide/Raft, door 5.....  747-100B, -200C, -300,
 inclusive.                             inclusive, and all S/                             and 747SR series
                                        Ns with a single                                  airplanes.
                                        letter G prefix.
(liii) 7A1447-1 through 7A1447-54      GW0001 through GW2681    Slide/Raft, doors 1, 2,  747-100, -100B, -100B
 inclusive.                             inclusive, and all S/    and 4.                   SUD, -200B, -200C, -
                                        Ns with a single                                  300, and 747SR series
                                        letter G prefix.                                  airplanes.
(liv) 7A1448-1 through 7A1448-12       GX0001 through GX1537,   Slide/Raft, door 5.....  747-100, -100B, -100B
 inclusive.                             and all S/Ns with a                               SUD, -200B, -200C, -
                                        single letter G prefix.                           300, and 747SR series
                                                                                          airplanes.
(lv) Odd dash numbers 7A1467-1         Odd S/Ns GH0001 through  Slide/Raft, doors 1 and  747-400 and -400D
 through 7A1467-23.                     GH1967, and all odd S/   4, LH side.              series airplanes.
                                        Ns with a single
                                        letter G prefix.
(lvi) Even dash numbers 7A1467-2       Even S/Ns GH0002         Slide/Raft, doors 1 and  747-400 and -400D
 through 7A1467-24.                     through GH1952, and      4, RH side.              series airplanes.
                                        all even S/Ns with a
                                        single letter G prefix.
(lvii) Odd dash numbers 7A1469-1       Odd S/Ns GJ001 through   Slide/Raft, door 5, LH   747-400 and -400D
 through 7A1469-13.                     GJ907, and all odd S/    side.                    series airplanes.
                                        Ns with a single
                                        letter G prefix.
(lviii) Even dash numbers 7A1469-2     Even S/Ns GJ002 through  Slide/Raft, door 5, RH   747-400 and -400D
 through 7A1469-14.                     GJ910, and all even S/   side.                    series airplanes.
                                        Ns with a single
                                        letter G prefix.
(lix) Odd dash numbers 7A1479-1        Odd S/Ns GI0001 through  Slide/Raft, door 2, LH   747-300, -400, and -
 through 7A1479-13.                     GI1017, and all odd S/   side.                    400D series airplanes.
                                        Ns with a single
                                        letter G prefix.
(lx) Even dash numbers 7A1479-2        Even S/Ns GI0002         Slide/Raft, door 2, RH   747-300, -400, and -
 through 7A1479-14.                     through GI1034, and      side.                    400D series airplanes.
                                        all even S/Ns with a
                                        single letter G prefix.
(lxi) 7A1489-1 and 7A1489-3..........  Odd S/Ns GK001 through   Slide/Raft, mid door,    767-300 series
                                        GK353, and all odd S/    LH side.                 airplanes.
                                        Ns with a single
                                        letter G prefix.
(lxii) 7A1489-2 and 7A1489-4.........  Even S/Ns GK002 through  Slide/Raft, mid door,    767-300 series
                                        GK354, and all even S/   RH side.                 airplanes.
                                        Ns with a single
                                        letter G prefix.
----------------------------------------------------------------------------------------------------------------


[[Page 31766]]


          Table 2.--Goodrich Evacuation Systems Installed on Certain McDonnell Douglas Model Airplanes
----------------------------------------------------------------------------------------------------------------
Goodrich evacuation systems having P/                              Component/part is      Installed on McDonnell
                 N--                       Having any S/N--             named-->             Douglas Model--
----------------------------------------------------------------------------------------------------------------
(i) 100504-101 through 100504-205      D9F161 through D9F256    Slide, forward door....  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PU0325                             82 (MD-82), DC-9-83
                                        through PU0331                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(ii) 100505-101 through 100505-201     D9A078 through D9A122    Slide, aft door........  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PS0151                             82 (MD-82), DC-9-83
                                        through PS0157                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(iii) 100506-103 through 100506-203    D9T085 through D9T127    Slide, tailcone........  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PT0175                             82 (MD-82), DC-9-83
                                        through PT0178                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(iv) 100504-101 through 100504-205     D9F001 through D9F160    Slide, forward door....  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PU0001                             82 (MD-82), DC-9-83
                                        through PU0324                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(v) 100505-101 through 100505-201      D9A001 through D9A077    Slide, aft door........  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PS0001                             82 (MD-82), DC-9-83
                                        through PS0150                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(vi) 100506-103 through 100506-203     D9T001 through D9T084    Slide, tailcone........  DC-9-81 (MD-81), DC-9-
 inclusive.                             inclusive, and PT0001                             82 (MD-82), DC-9-83
                                        through PT0174                                    (MD-83), and DC-9-87
                                        inclusive.                                        (MD-87) airplanes;
                                                                                          Model MD-88 airplanes;
                                                                                          and Model MD-90-30
                                                                                          airplanes.
(vii) 7A1274-3 through 7A1274-12       All....................  Slide, forward/service   DC-9-81 (MD-81) and DC-
 inclusive.                                                      door.                    9-82 (MD-82)
                                                                                          airplanes.
(viii) 7A1275-3 through 7A1275-20      All....................  Slide, aft door........  DC-9-81 (MD-81) and DC-
 inclusive.                                                                               9-82 (MD-82)
                                                                                          airplanes.
(ix) 7A1276-3 through 7A1276-12        All....................  Slide, tailcone........  DC-9-11, DC-9-12, DC-9-
 inclusive.                                                                               13, DC-9-14, DC-9-15,
                                                                                          and DC-9-15F
                                                                                          airplanes; Model DC-9-
                                                                                          21 airplanes; Model DC-
                                                                                          9-31, DC-9-32, DC-9-32
                                                                                          (VC-9C), DC-9-32F, DC-
                                                                                          9-33F, DC-9-34, DC-9-
                                                                                          34F, and DC-9-32F (C-
                                                                                          9A, C-9B) airplanes;
                                                                                          Model DC-9-41
                                                                                          airplanes; Model DC-9-
                                                                                          51 airplanes; and
                                                                                          Model DC-9-81 (MD-81),
                                                                                          DC-9-82 (MD-82), DC-9-
                                                                                          83 (MD-83), and DC-9-
                                                                                          87 (MD-87) airplanes.
----------------------------------------------------------------------------------------------------------------


                Table 3.--Goodrich Evacuation Systems Installed on Certain Airbus Model Airplanes
----------------------------------------------------------------------------------------------------------------
 Goodrich evacuation system having P/                              Component/part is       Installed on Airbus
                 N--                       Having any S/N--             named--                  Model--
----------------------------------------------------------------------------------------------------------------
(i) 4A3928-1.........................  AY0001 through AY0007    Slide, door 3 type 1,    A340-541 airplanes.
                                        inclusive.               LH side.
(ii) 4A3928-2........................  AZ0001 through AZ0007    Slide, door 3 type 1,    A340-541 airplanes.
                                        inclusive.               RH side.
(iii) 4A3931-1 and 4A3931-3..........  AQ0001 through AQ0028    Ramp/Slide, off-wing,    A340-642 airplanes.
                                        inclusive.               LH side.
(iv) 4A3931-2 and 4A3931-4...........  AT0001 through AT0028    Ramp/Slide, off-wing,    A340-642 airplanes.
                                        inclusive.               RH side.
(v) 4A3934-1 and 4A3934-3............  AK0001 through AK0028    Slide/Raft, door 3, LH   A340-642 airplanes.
                                        inclusive.               side.
(vi) 4A3934-2 and 4A3934-4...........  AM0001 through AM0028    Slide/Raft, door 3, RH   A340-642 airplanes.
                                        inclusive.               side.

[[Page 31767]]

 
(vii) 7A1296-004 and 7A1296-005......  WB0030 through WB0033    Slide, mid door........  A300 B2-1A, B2-1C, B2K-
                                        inclusive.                                        3C, and B2-203
                                                                                          airplanes; Model A300
                                                                                          B4-2C, B4-103, and B4-
                                                                                          203 airplanes; Model
                                                                                          A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; and Model
                                                                                          A300 F4-605R and F4-
                                                                                          622R airplanes.
(viii) 7A1297-103 and 7A1297-203.....  WF0257 through WF0273    Ramp/Slide, off-wing     A310-203, -204, -221,
                                        inclusive.               door.                    and -222 airplanes;
                                                                                          and Model A310-304, -
                                                                                          322, -324, and -325
                                                                                          airplanes.
(ix) 7A1298-004 and 7A1298-005.......  WA0327 through WA0374    Slide, forward/aft door  A300 B2-1A, B2-1C, B2K-
                                        inclusive.                                        3C, and B2-203
                                                                                          airplanes; Model A300
                                                                                          B4-2C, B4-103, and B4-
                                                                                          203 airplanes; Model
                                                                                          A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; Model A300
                                                                                          F4-605R and F4-622R
                                                                                          airplanes; and Model
                                                                                          A310-203, -204, -221,
                                                                                          and -222 airplanes;
                                                                                          and Model A310-304, -
                                                                                          322, -324, and -325
                                                                                          airplanes.
(x) 7A1299-006.......................  WE0149 through WE0172    Slide, emergency door..  A300 B2-1A, B2-1C, B2K-
                                        inclusive.                                        3C, and B2-203
                                                                                          airplanes; Model A300
                                                                                          B4-2C, B4-103, and B4-
                                                                                          203 airplanes; Model
                                                                                          A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; and Model
                                                                                          A300 F4-605R and F4-
                                                                                          622R airplanes.
(xi) 7A1300-007......................  WC0423 through WC0507    Slide/Raft, forward/aft  A300 B2-1A, B2-1C, B2K-
                                        inclusive.               door.                    3C, and B2-203
                                                                                          airplanes; Model A300
                                                                                          B4-2C, B4-103, and B4-
                                                                                          203 airplanes; Model
                                                                                          A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; Model A300
                                                                                          F4-605R and F4-622R
                                                                                          airplanes; and Model
                                                                                          A310-203, -204, -221,
                                                                                          and -222 airplanes;
                                                                                          and Model A310-304, -
                                                                                          322, -324, and -325
                                                                                          airplanes.
(xii) 7A1359-005.....................  WD0134 through WD0159    Slide/Raft, mid door...  A300 B2-1A, B2-1C, B2K-
                                        inclusive.                                        3C, and B2-203
                                                                                          airplanes; Model A300
                                                                                          B4-2C, B4-103, and B4-
                                                                                          203 airplanes; Model
                                                                                          A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; and Model
                                                                                          A300 F4-605R and F4-
                                                                                          622R airplanes.
(xiii) 7A1508-109 through 7A1508-117   AA1041 through AA2419    Slide/Raft, doors 1 and  A330-201, -202, -203, -
 inclusive.                             inclusive.               4.                       223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; Model A340-
                                                                                          311, -312, and -313
                                                                                          airplanes; Model A340-
                                                                                          541 airplanes; and
                                                                                          Model A340-642
                                                                                          airplanes.

[[Page 31768]]

 
(xiv) 7A1509-111, 7A1509-115 and       AD0487 through AD1007    Slide, door 3 type 1...  A330-201, -202, -203, -
 7A1509-117.                            inclusive.                                        223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; and Model
                                                                                          A340-311, -312, and -
                                                                                          313 airplanes.
(xv) 7A1510-109 through 7A1510-117     AB0077 through AB0150    Slide/Raft, door 3 type  A330-201, -202, -203, -
 inclusive.                             inclusive.               A, LH side.              223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; and Model
                                                                                          A340-311, -312, and -
                                                                                          313 airplanes.
(xvi) 7A1510-110 through 7A1510-118    AC0077 through AC0148    Slide/Raft, door 3 type  A330-201, -202, -203, -
 inclusive.                             inclusive.               A, RH side.              223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; and Model
                                                                                          A340-311, -312, and -
                                                                                          313 airplanes.
(xvii) 7A1539-109 through 7A1539-117   AU0302 through AU0677    Slide/Raft, door 2, LH   A330-201, -202, -203, -
 inclusive.                             inclusive.               side.                    223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; Model A340-
                                                                                          311, -312, and -313
                                                                                          airplanes; Model A340-
                                                                                          541 airplanes; and
                                                                                          Model A340-642
                                                                                          airplanes.
(xviii) 7A1539-110 through 7A1539-118  AX0302 through AX0673    Slide/Raft, door 2, RH   A330-201, -202, -203, -
 inclusive.                             inclusive.               side.                    223, and -243
                                                                                          airplanes; Model A330-
                                                                                          301, -321, -322, -323,
                                                                                          -341, -342, and -343
                                                                                          airplanes; Model A340-
                                                                                          211, -212, and -213
                                                                                          airplanes; Model A340-
                                                                                          311, -312, and -313
                                                                                          airplanes; Model A340-
                                                                                          541 airplanes; and
                                                                                          Model A340-642
                                                                                          airplanes.
(xix) 7A1296-001 through 7A1296-004    WB0001 through WB0029    Slide, mid door........  A300 B2-1A, B2-1C, B2K-
 inclusive.                             inclusive, all S/Ns                               3C, and B2-203
                                        with a single letter R                            airplanes; Model A300
                                        prefix, and all S/Ns                              B4-2C, B4-103, and B4-
                                        with a single letter G                            203 airplanes; Model
                                        prefix.                                           A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; and Model
                                                                                          A300 F4-605R and F4-
                                                                                          622R airplanes.
(xx) 7A1297-101 through 7A1297-203     WF0001 through WF0256    Ramp/Slide, off-wing     A310-203, -204, -221,
 inclusive.                             inclusive, all S/Ns      door.                    and -222 airplanes;
                                        with a single letter R                            and Model A310-304, -
                                        prefix, and all S/Ns                              322, -324, and -325
                                        with a single letter G                            airplanes.
                                        prefix.
(xxi) 7A1298-001 through 7A1298-004    WA0001 through WA0326    Slide, forward/aft door  A300 B2-1A, B2-1C, B2K-
 inclusive.                             inclusive, all S/Ns                               3C, and B2-203
                                        with a single letter R                            airplanes; Model A300
                                        prefix, and all S/Ns                              B4-2C, B4-103, and B4-
                                        with a single letter G                            203 airplanes; Model
                                        prefix.                                           A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; Model A300
                                                                                          F4-605R and F4-622R
                                                                                          airplanes; and Model
                                                                                          A310-203, -204, -221,
                                                                                          and -222 airplanes;
                                                                                          and Model A310-304, -
                                                                                          322, -324, and -325
                                                                                          airplanes.

[[Page 31769]]

 
(xxii) 7A1299-001 through 7A1299-006   WE0001 through WE0148    Slide, emergency door..  A300 B2-1A, B2-1C, B2K-
 inclusive.                             inclusive, all S/Ns                               3C, and B2-203
                                        with a single letter R                            airplanes; Model A300
                                        prefix, and all S/Ns                              B4-2C, B4-103, and B4-
                                        with a single letter G                            203 airplanes; Model
                                        prefix.                                           A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; and Model
                                                                                          A300 F4-605R and F4-
                                                                                          622R airplanes.
(xxiii) 7A1300-001 through 7A1300-007  WC0001 through WC0422    Slide/Raft, forward/aft  A300 B2-1A, B2-1C, B2K-
 inclusive.                             inclusive, all S/Ns      door.                    3C, and B2-203
                                        with a single letter R                            airplanes; Model A300
                                        prefix, and all S/Ns                              B4-2C, B4-103, and B4-
                                        with a single letter G                            203 airplanes; Model
                                        prefix.                                           A300 B4-601, B4-603,
                                                                                          B4-620, and B4-622
                                                                                          airplanes; Model A300
                                                                                          B4-605R and B4-622R
                                                                                          airplanes; Model A300