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]
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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.
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17:15 Jun 07, 2007
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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
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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
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://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,
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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 https://
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 https://
dms.dot.gov.
Examining the Docket
You can examine the AD docket on
the Internet at https://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
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17:15 Jun 07, 2007
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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
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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.
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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
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Ramp/Slide, off-wing, RH side .....
Slide, forward door .......................
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–300 series air–300 series air–300 series air–300 series air–300 series air–300 series air–300 series airairplanes.
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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–
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Slide, forward door .......................
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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.
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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 ......
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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.
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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 ........
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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.
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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.
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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.
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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
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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:
• https://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 https://
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
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]]>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 https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
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 https://
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 https://dms.dot.gov.
Examining the Docket
You can examine the AD docket on the Internet at https://
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
