[Federal Register: March 14, 2008 (Volume 73, Number 51)] [Proposed Rules] [Page 13806-13809] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr14mr08-17] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0313; Directorate Identifier 2007-CE-095-AD] RIN 2120-AA64 Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain M7 Aerospace LP SA226 and SA227 series airplanes. This proposed AD would require you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson. If chafing/arcing is found, this proposed AD would require you to reposition, repair, and/or replace all chafed electrical wires, components, and hydraulic and bleed air tube assemblies, as required. This proposed AD would also require you to reposition the battery lead cables, cover four-gauge wires leaving the battery box with firesleeving and secure with clamps, and protect the battery power cable. This proposed AD results from five reports of chafing between the bleed air tube and the electrical starter cables with one incident resulting in a fire. We are proposing this AD to detect and correct chafing/arcing of electrical wires, components, and bleed air lines. This condition could result in arcing of the exposed wires and burn a hole in the bleed air line or the nearby hydraulic line, and lead to a possible hydraulic fluid leak and fire in the engine nacelle compartment. DATES: We must receive comments on this proposed AD by May 13, 2008. ADDRESSES: Use one of the following addresses to comment on this proposed AD: Federal eRulemaking Portal: Go to http:// www.regulations.gov. Follow the instructions for submitting comments. Fax: (202) 493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact M7 Aerospace Repair Station, P.O. Box 790490, San Antonio, Texas 78279- 0490; telephone: (210) 824-9421; fax: (210) 804-7789. FOR FURTHER INFORMATION CONTACT: Werner Koch, Aerospace Engineer, FAA, Airplane Certification Office, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone: (817) 222-5133; fax: (817) 222-5960. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments regarding this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number, ``FAA- 2008-0313; Directorate Identifier 2007-CE-095-AD'' at the beginning 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 received 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:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive concerning this proposed AD. Discussion We have received five reports of chafing between the bleed air tube and the electrical starter cables on SA226 and SA227 series airplanes. One report also noted the chafing damage resulted in a fire on a Model SA226TC airplane. Subsequent review by the FAA of the service experience of SA226 and SA227 series airplanes indicates that inadequate clearance for electrical wires/components, hydraulic and bleed air tube assemblies at LH/RH inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed- through locations into the LH/RH inboard keelson caused the chafing/ arcing. This condition, if not corrected, could result in arcing of the exposed wires and burn a hole in the bleed air line or the nearby hydraulic line, and lead to a possible hydraulic fluid leak and fire in the engine nacelle compartment. Relevant Service Information We have reviewed the following service bulletins and procedures: ------------------------------------------------------------------------ Applicable model(s) Service Bulletin of airplane(s) Procedures described ------------------------------------------------------------------------ M7 Aerospace SA226 Series SA226-AT, SA226-T, Inspecting Service Bulletin No. 226-24- and SA226-TC. electrical wires/ 036, issued: September 19, components, 2007. hydraulic and bleed air tube assemblies at LH/RH inboard wing leading edge/ battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed- through locations into the LH/RH inboard keelson. [[Page 13807]] M7 Aerospace SA227 Series SA227-AC and SA227- Service Bulletin No. 227-24- AT. 019, issued: September 19, 2007. M7 Aerospace SA227 Series SA227-CC and SA227- Commuter Category Service DC. Bulletin No. CC7-24-010, issued: September 19, 2007. Swearingen Aviation SA226-AT, SA226-T, Repositioning Corporation SA226 Series and SA226-TC. battery lead Service Bulletin No. SB 24- cables. 001, revised: September 16, 1975. Fairchild Aircraft SA226-AT, SA226-T, Covering four-gauge Corporation SA226 Series and SA226-TC. wires leaving Service Bulletin No. SB24- battery box with 019, revised: May 17, 1983. firesleeving and securing with clamp. Fairchild Aircraft SA227-AC and SA227- Corporation SA227 Series AT. Service Bulletin No. SB24- 001, revised: May 17, 1983. Fairchild Aircraft SA226-AT, and SA226- Protect battery Corporation SA226 Series TC. power cable. Service Bulletin No. SB24- 020, revised: February 15, 1984. Fairchild Aircraft SA227-AC and SA227- Corporation SA227 Series AT. Service Bulletin No. SB24- 002, revised: February 15, 1984. ------------------------------------------------------------------------ FAA's Determination and Requirements of the Proposed AD We are proposing this AD because we evaluated all information and determined the unsafe condition described previously is likely to exist or develop on other products of the same type design. This proposed AD would require you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at LH and RH inboard wing leading edge/ battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson. If chafing/ arcing is found, this proposed AD would require you to reposition, repair, and/or replace all chafed electrical wires, components, and hydraulic and bleed air tube assemblies, as required. This proposed AD would also require you to reposition the battery lead cables, cover four-gauge wires leaving battery box with firesleeving and secure with clamps, and protect the battery power cable. Costs of Compliance We estimate that this proposed AD would affect 330 airplanes in the U.S. registry. We estimate the following costs for all Models SA226, SA227, SA227- CC, and SA227-DC airplanes to do the proposed inspection required by SA226 Series Service Bulletin No. 226-24-036, SA227 Series Service Bulletin No. 227-24-019, or SA227 Series Commuter Category Service Bulletin No. CC7-24-010: ---------------------------------------------------------------------------------------------------------------- Total cost per Total cost on Labor cost Parts cost airplane U.S. operators ---------------------------------------------------------------------------------------------------------------- 4 work-hours x $80 per hour = $320........ Not Applicable.............. $320 $105,600 ---------------------------------------------------------------------------------------------------------------- We estimate the following costs for certain Models SA226-AT, SA226- T, and SA226-TC airplanes for the proposed repositioning of battery lead cables following SA226 Series Service Bulletin No. SB 24-001: ---------------------------------------------------------------------------------------------------------------- Number of Labor cost Parts cost Total cost per airplanes Total cost on airplane affected U.S. operators ---------------------------------------------------------------------------------------------------------------- 4 work-hours x $80 per hour = $320.......... $6.80 $326.80 2 $653.60 ---------------------------------------------------------------------------------------------------------------- We estimate the following costs for certain Models SA226-AT, SA226- T, SA226-TC, SA227-AC, and SA227-AT airplanes following SA226 Series Service Bulletin No. SB24-019 or SA227 Series Service Bulletin No. SB24-001, for the proposed covering of four-gauge wires leaving battery box with firesleeving and securing with clamp: ---------------------------------------------------------------------------------------------------------------- Number of Labor cost Parts cost Total cost per airplanes Total cost on airplane affected U.S. operators ---------------------------------------------------------------------------------------------------------------- 13 work-hours x $80 per hour = $1,040....... $6.80 $1,046.80 70 $73,276 ---------------------------------------------------------------------------------------------------------------- We estimate the following costs for certain Models SA226-AT, SA226- TC, SA227-AC, and SA227-AT airplanes following SA226 Series Service Bulletin No. SB24-020 or SA227 Series Service Bulletin No. SB24-002, for the proposed protection of the battery power cable: [[Page 13808]] ---------------------------------------------------------------------------------------------------------------- Number of Labor cost Parts cost Total cost per airplanes Total cost on airplane affected U.S. operators ---------------------------------------------------------------------------------------------------------------- 50 work-hours x $80 per hour = $4,000....... $3,000 $7,000 60 $420,000 ---------------------------------------------------------------------------------------------------------------- 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 and placed it in the AD docket. Examining the AD Docket You may examine the AD docket that contains the proposed AD, the regulatory evaluation, any comments received, and other information on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone (800) 647-5527) is located at the street address stated in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. 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 Sec. 39.13 by adding the following new AD: M7 Aerospace LP: Docket No. FAA-2008-0313; Directorate Identifier 2007-CE-095-AD. Comments Due Date (a) We must receive comments on this airworthiness directive (AD) action by May 13, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers (S/N) that are certificated in any category: (1) Group 1: Model SA226-AT Airplanes, All S/N. (2) Group 2: Model SA226-T Airplanes, All S/N. (3) Group 3: Model SA226-TC Airplanes, All S/N. (4) Group 4: Model SA227-AC Airplanes, All S/N. (5) Group 5: Model SA227-AT Airplanes, All S/N. (6) Group 6: Model SA227-CC Airplanes, All S/N. (7) Group 7: Model SA227-DC Airplanes, All S/N. Unsafe Condition (d) This AD results from five reports of chafing between the bleed air tube and the electrical starter cables with one incident resulting in a fire. We are proposing this AD to detect and correct chafing/arcing of electrical wires, components, and bleed air lines. This condition could result in arcing of the exposed wires and burn a hole in the bleed air line or the nearby hydraulic line, and lead to a possible hydraulic fluid leak and fire in the engine nacelle compartment. Compliance (e) To address this problem, you must do the following, unless already done: ------------------------------------------------------------------------ Actions Compliance Procedures ------------------------------------------------------------------------ (1) For Group 1, Group 2, Within 250 hours Follow M7 Aerospace and Group 3 Airplanes: time-in-service SA226 Series (i) Inspect electrical wires/ (TIS) after the Service Bulletin components, hydraulic and effective date of No. 226-24-036, bleed air tube assemblies this AD. issued: September at left-hand (LH)/right- Repetitively 19, 2007; hand (RH) inboard wing thereafter inspect Swearingen Aviation leading edge/battery box (paragraph Corporation SA226 areas, LH/RH wing stations (e)(1)(i) of this Series Service 51.167 to 81.174, and at AD) at intervals Bulletin No. SB 24- all feed-through locations not to exceed 12 001, issued: May into the LH/RH inboard months. 18, 1971; revised: keelson for any evidence of September 16, 1975; chafing/arcing. Clear, Fairchild Aircraft repair, and/or replace all Corporation SA226 chafed electrical wires and Series Service components, hydraulic, and Bulletin No. SB 24- bleed air tube assemblies, 019, issued: June and all feed-through 2, 1982; revised: locations, as required. May 17, 1983; and Fairchild Aircraft Corporation SA226 Series Service Bulletin No. SB 24- 020, issued: January 18, 1983; revised: February 15, 1984. [[Page 13809]] (ii) Reposition battery lead cables, protect the battery power cable, and cover four- gauge wires leaving battery box with firesleeving and secure with clamp. (2) For Group 4 and Group 5 Within 250 hours TIS Follow M7 Aerospace Airplanes: after the effective SA227 Series (i) Inspect electrical wires/ date of this AD. Service Bulletin components, hydraulic and Repetitively No. 227-24-019, bleed air tube assemblies thereafter inspect issued: September at LH/RH inboard wing (paragraph 19, 2007; Fairchild leading edge/battery box (e)(2)(i) of this Aircraft areas, LH/RH wing stations AD) at intervals Corporation SA227 51.167 to 81.174, and at not to exceed 12 Series Service all feed-through locations months. Bulletin No. SB24- into the LH/RH inboard 001, issued: June keelson for any evidence of 2, 1982; revised: chafing/arcing. Clear, May 17, 1983; and repair, and/or replace all Fairchild Aircraft chafed electrical wires and Corporation SA227 components, hydraulic, and Series Service bleed air tube assemblies, Bulletin No. SB24- and all feed-through 002, issued: locations, as required. January 18, 1983; revised: February 15, 1984. (ii) Protect the battery power cable and cover four-gauge wires leaving battery box with firesleeving and secure with clamp. (3) For Group 6 and Group 7 Within 250 hours TIS Follow M7 Aerospace Airplanes: Inspect after the effective SA227 Series electrical wires/ date of this AD. Commuter Category components, hydraulic and Repetitively Service Bulletin bleed air tube assemblies thereafter inspect No. CC7-24-010, at LH/RH inboard wing at intervals not to issued: September leading edge/battery box exceed 12 months. 19, 2007. areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson for any evidence of chafing/arcing. Clear, repair, and/or replace all chafed electrical wires and components, hydraulic, and bleed air tube assemblies, and all feed-through locations, as required. ------------------------------------------------------------------------ Note: Although not a requirement of this AD, you may incorporate Swearingen Aviation Corporation SA226 Series Service Bulletin No. 57-010, Revised: December 5, 1975, on those airplanes that have not installed the access panel. Installation of the access panel will simplify the incorporation of the service bulletins referenced in this AD and future inspections of the areas of concern. Alternative Methods of Compliance (AMOCs) (f) The Manager, Fort Worth Airplane Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Werner Koch, Aerospace Engineer, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone: (817) 222-5133; fax: (817) 222-5960. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. Related Information (g) To get copies of the service information referenced in this AD, contact M7 Aerospace Repair Station, P.O. Box 790490, San Antonio, Texas 78279-0490; telephone: (210) 824-9421; fax: (210) 804-7789. To view the AD docket, go to U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at http://www.regulations.gov. The docket number is Docket No. FAA-2008-0313; Directorate Identifier 2007-CE-095-AD. Issued in Kansas City, Missouri, on March 7, 2008. David R. Showers, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-5193 Filed 3-13-08; 8:45 am] BILLING CODE 4910-13-P
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