Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Orders (TSOs) TSO-C69, TSO-C69a, TSO-C69b, and TSO-C69c, Installed on Various Boeing, McDonnell Douglas, and Airbus Transport Category Airplanes, 15399-15409 [E8-5375]
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
Applicability
(c) This AD applies to all Boeing Model
737–300, –400, and –500 series airplanes,
certificated in any category.
Unsafe Condition
(d) This AD results from reports of fuel
leaking from a puncture in the slat track
housing (referred to as ‘‘slat can’’). We are
issuing this AD to detect and correct loose or
missing parts from the main slat track
downstop assemblies, which could puncture
the slat can and result in a fuel leak and
consequent fire.
Compliance
(e) Comply with this AD within the
compliance times specified, unless already
done.
pwalker on PROD1PC71 with RULES
Repetitive Inspections and Corrective
Actions
(f) At the applicable time specified in Table
1 of paragraph 1.E. of Boeing Alert Service
Bulletin 737–57A1301, dated February 5,
2008, except as provided by paragraph (f)(1)
of this AD: Do a detailed inspection or
borescope inspection of the downstop
assemblies on the main tracks of the No. 2,
3, 4, and 5 slats and the inboard track of the
No. 1 and 6 slats to verify if any parts are
missing, damaged, or in the wrong order; and
do all the other specified, related
investigative, and corrective actions as
applicable; by accomplishing all of the
applicable actions specified in the
Accomplishment Instructions of the service
bulletin, except as provided by paragraphs
(f)(2) and (f)(3) of this AD. Repeat the
inspection thereafter at the applicable
interval specified in Table 1 of paragraph 1.E.
of the service bulletin. Do all applicable
related investigative and corrective actions
before further flight.
(1) Where the service bulletin specifies
counting the compliance time from ‘‘* * *
the date on the service bulletin,’’ this AD
requires counting the compliance time from
the effective date of this AD.
(2) For airplanes on which any downstop
assembly part is missing or damaged, a
borescope inspection of the inside of the slat
can for loose parts and damage to the wall
of the slat can may be accomplished in lieu
of the detailed inspection of the inside of the
slat can that is specified in the service
bulletin.
(3) If any damaged slat can is found during
any inspection required by this AD: Before
further flight, either replace the slat can with
a new slat can having the same part number
or repair the slat can using a method
approved in accordance with the procedures
specified in paragraph (g) of this AD.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. 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.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD, if it is approved by an
Authorized Representative for the Boeing
Commercial Airplanes Delegation Option
Authorization Organization who has been
authorized by the Manager, Seattle ACO, to
make those findings. For a repair method to
be approved, the repair must meet the
certification basis of the airplane, and the
approval must specifically refer to this AD.
Material Incorporated by Reference
(h) You must use Boeing Alert Service
Bulletin 737–57A1301, dated February 5,
2008, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact Boeing Commercial
Airplanes, P.O. Box 3707, Seattle,
Washington 98124–2207.
(3) You may review copies of the service
information incorporated by reference at the
FAA, Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, Washington; or at
the National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on March
11, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E8–5702 Filed 3–21–08; 8:45 am]
BILLING CODE 4910–13–P
Alternative Methods of Compliance
(AMOCs)
(g)(1) The Manager, Seattle Aircraft
Certification Office (ACO), FAA, Attn: Nancy
Marsh, Aerospace Engineer, Airframe
Branch, ANM–120S, 1601 Lind Avenue, SW.,
Renton, Washington 98057–3356; telephone
(425) 917–6440; fax (425) 917–6590; has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19.
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15399
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–28370; Directorate
Identifier 2003–NM–239–AD; Amendment
39–15439; AD 2008–06–27]
RIN 2120–AA64
Airworthiness Directives; Goodrich
Evacuation Systems Approved Under
Technical Standard Orders (TSOs)
TSO–C69, TSO–C69a, TSO–C69b, and
TSO–C69c, Installed on Various
Boeing, McDonnell Douglas, and
Airbus Transport Category Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Goodrich evacuation systems approved
under Technical Standard Orders
(TSOs) TSO–C69, TSO–C69a, TSO–
C69b, and TSO–C69c, installed on
certain Boeing, McDonnell Douglas, and
Airbus transport category airplanes. For
certain systems, this AD requires
replacing the evacuation system’s shearpin restraints with new ones. For certain
other systems, this AD requires an
inspection for manufacturing lot
numbers; and a general visual
inspection of the shear-pin restraint for
discrepancies, and corrective actions if
necessary. This AD results from several
reports of corroded shear-pin restraints
that prevented Goodrich evacuation
systems from deploying properly. We
are issuing this AD to prevent failure of
an evacuation system, which could
impede an emergency evacuation and
increase the chance of injury to
passengers and flightcrew during the
evacuation.
This AD is effective April 28,
2008.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of April 28, 2008.
The Director of the Federal Register
approved the incorporation by reference
of a certain other publication listed in
this AD as of March 11, 2008 (73 FR
6586, February 5, 2008).
ADDRESSES: For service information
identified in this AD, contact Goodrich,
Aircraft Interior Products, ATTN:
Technical Publications, 3414 South
Fifth Street, Phoenix, AZ 85040–1169.
DATES:
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
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 AD
docket contains this AD, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (telephone 800–647–5527)
is the Document Management Facility,
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC 20590.
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:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness
directive (AD) that would apply to
certain Goodrich evacuation systems
approved under Technical Standard
Orders (TSOs) TSO–C69, TSO–C69a,
TSO–C69b, and TSO–C69c, installed on
certain Boeing, McDonnell Douglas, and
Airbus transport category airplanes.
That NPRM was published in the
Federal Register on June 8, 2007 (72 FR
31761). For certain systems, that NPRM
proposed to require replacing the
evacuation systems shear-pin restraints
with new ones. For certain other
systems, that NPRM proposed to require
an inspection for manufacturing lot
numbers; and a general visual
inspection of the shear-pin restraint for
discrepancies, and corrective actions if
necessary.
pwalker on PROD1PC71 with RULES
Comments
We gave the public the opportunity to
participate in developing this AD. We
considered the comments received from
the 5 commenters.
Supportive Comments
Air Line Pilots Association,
International (ALPA), and Air Transport
Association (ATA), on behalf of its
member Continental Airlines, support
the intent of the rule. Continental states
that it has captured Goodrich Service
Bulletin 25–343 on a total of 969 slide
assemblies since the service bulletin’s
October 2003 release.
Request To Combine Two AD Actions
Into One AD Action
ATA, on behalf of its member United
Airlines, notes that this NPRM is similar
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16:13 Mar 21, 2008
Jkt 214001
to NPRM 2005–NM–139–AD (AD 2008–
03–05, amendment 39–15354 (73 FR
6586, February 5, 2008)). United
requests that this AD action be
incorporated into NPRM 2005–NM–
139–AD.
We do not agree with the commenter’s
request. While the evacuation slides
affected by this AD and AD 2008–03–05
are identified in the same service
bulletin and have the same unsafe
condition, the individual evacuation
slides were approved under different
certification processes. This AD affects
certain evacuation slides that were
approved under a TSO that specified
certain requirements for evacuation
slides. AD 2008–03–05 affects airplanes
that had certain other evacuation slides
approved as part of a type certificate.
The TSO approval process specifies the
airplane model(s) on which a specific
evacuation slide can be installed. These
two approval processes affect how we
issue ADs. We have not changed this
AD or AD 2008–03–05 in this regard.
Request To Accept Certain Service
Bulletins for Accomplishment
ATA, on behalf of its member United
Airlines, requests that the FAA accept
accomplishment of either Goodrich
Service Bulletin 25–343, Revision 1,
dated January 31, 2005; or Revision 2,
dated October 11, 2006; after the
effective date of the AD. The
commenters explain that there are no
technical or procedural changes
between these revisions and the most
recent revision, Revision 3, dated
January 12, 2007.
We disagree with the request to accept
accomplishment of earlier service
bulletin revisions after the effective date
of the AD. It is our policy to require
compliance with the most recent
revision of service information.
However, in paragraph (k) of this AD,
we provide credit for accomplishment
of the earlier service bulletin revisions
if done before the effective date of the
AD. We have not changed the AD in this
regard.
Request To Extend Compliance Times
Request To Refer to Current Service
Bulletins as Acceptable for Credit
ATA, on behalf of its member United
Airlines, requests that the compliance
times be extended from 18 months after
the effective date of the AD for Model
767 airplane off-wing evacuation
systems and 36 months after the
effective date of the AD for the other
evacuation systems to 36 and 48 months
respectively. The commenters state that
extended compliance times would
match routine overhaul cycles, account
for parts lead-time, take into
consideration the large quantity of
affected evacuation systems, and relieve
a burden on resources and capacity.
We disagree with the request to
extend the compliance times. A
significant number of affected
evacuation systems have already been
modified. We have received
confirmation from Goodrich that parts
are available to support the 18- and 36month compliance times. 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 not changed the AD in this
regard.
Goodrich, the evacuation slide
manufacturer, requests that we give
credit for accomplishing paragraph (h)
of this AD to airlines/overhaul shops
that might have accomplished Revision
3 of Goodrich Service Bulletin 25–343,
dated January 12, 2007; and Revision 2
of Goodrich Service Bulletin 25–344,
dated October 11, 2006; before the
effective date of this AD. Goodrich
states that ‘‘The wording of paragraph
(k) does not clearly provide credit for
actions done in compliance with 25–
343, revision 3, and 25–344, revision 2,
unless it occurs ‘after the effective date
of this AD’.’’
We infer that Goodrich interprets the
text of paragraph (k) of the AD to mean
that operators that have accomplished
Revision 3 of Goodrich Service Bulletin
25–343 or Revision 2 of Goodrich
Service Bulletin 25–344 before the
effective date would be required to
accomplish those actions again after the
effective date to comply with this AD.
We find that clarification is necessary.
Paragraph (e) of this AD states that the
actions must be done as specified in the
AD ‘‘unless the actions have already
been done,’’ so it is not necessary to
repeat this information in paragraph (k)
of the AD. We refer to Goodrich Service
Bulletin 25–343, Revision 3, dated
January 12, 2007; and Goodrich Service
Bulletin 25–344, Revision 2, dated
October 11, 2006; as the sources of
service information for accomplishing
the requirements of paragraph (h) of this
AD. Accomplishing the requirements of
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
this AD in accordance with these
service bulletins before the effective
date of the AD is acceptable for
compliance with this AD. We have not
changed the AD in this regard.
Request To Allow Other Methods of
Recording Compliance
ATA, on behalf of its member United
Airlines, states that the
Accomplishment Instructions of
Goodrich Service Bulletin 25–343
instruct the operator to record service
bulletin compliance on the system
information card. United requests that
the method of recording compliance on
the card be made optional, as operators
have alternative means to record
compliance and the system information
card might not be available.
We infer that the commenters want us
to revise the AD to allow different
methods of recording compliance with
the service bulletin. We agree with the
request to revise the AD. We have
revised paragraph (h) of this AD to
specify that recording compliance with
the service bulletin in accordance with
the service bulletin instructions is not
required by this AD. Operators may
record service bulletin compliance
whichever way their applicable recordkeeping system specifies. However,
recording compliance with the AD is
still required. Recording AD compliance
is accomplished in a maintenance log,
on job/task cards, or some other method
approved by the operator’s principal
inspector or local flight standards
district office. We have not changed the
AD in this regard.
Request To Reverse Order of SubParagraphs
Goodrich requests that we reverse the
sequence of paragraphs (f)(1) and (f)(2)
of the NPRM so that the references to
Tables 1 and 2 of the AD are called out
first before Table 3.
We agree with the commenter’s
request. Revising the sequence of the
paragraphs to match the sequence of the
tables will reduce confusion. We have
changed paragraphs (f)(1) and (f)(2) of
this AD as requested.
Clarification of Alternative Method of
Compliance (AMOC) Paragraph
We have revised this action to clarify
the appropriate procedure for notifying
the principal inspector before using any
approved AMOC on any airplane to
which the AMOC applies.
Conclusion
We reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting the AD
with the changes described previously.
We also determined that this change
will not increase the economic burden
on any operator or increase the scope of
the AD.
Costs of Compliance
This AD affects certain Goodrich
evacuation systems installed on about
2,844 airplanes worldwide. This AD
affects about 1,240 airplanes of U.S.
registry. The following table provides
the estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Action
Work hours
Average labor
rate per hour
Replacement ....
Between 2 and
9.
$80
Inspection .........
Between 2 and
9.
80
Parts
Number of slide
units per airplane
Fleet cost
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.
Cost per slide unit
Between $58 and
$638, depending
on number of restraints.
None .......................
pwalker on PROD1PC71 with RULES
Authority for This Rulemaking
Regulatory Findings
List of Subjects in 14 CFR Part 39
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.
This AD will not have federalism
implications under Executive Order
13132. This AD will 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 this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under
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.
You can find our regulatory
evaluation and the estimated costs of
compliance in the AD Docket.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
VerDate Aug<31>2005
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Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
I
2008–06–27 Goodrich (Formerly
BFGoodrich): Amendment 39–15439.
Docket No. FAA–2007–28370;
Directorate Identifier 2003–NM–239–AD.
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
Effective Date
(a) This airworthiness directive (AD) is
effective April 28, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to:
(1) Goodrich evacuation systems approved
under Technical Standard Orders (TSOs)
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 TSOs 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 TSOs TSO–C69a, TSO–C69b, and
TSO–C69c, installed on certain 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.
PG0276 through PG0309 inclusive.
PC0264 through PC0368 inclusive.
PK0161 through PK0212 inclusive.
PF0164 through PF0220 inclusive
Slide, forward/aft door ..................
PH0300 through PH0390 inclusive.
PD0294 through PD0378 inclusive.
PAK137 through PAK150 inclusive.
PAL671 through PAL738 inclusive.
PAB611 through PAB649 inclusive.
B3F315 through B3F611 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
B3A338 through B3A685 inclusive.
Odd S/Ns ST0015 through
ST0131.
Even S/Ns ST0014 through
ST0128.
SS0001 through SS0210 inclusive.
SF0001 through SF0501 inclusive
Slide, aft door ...............................
BNG0213 through BNG4911 inclusive.
GS1340 through GS1879 inclusive.
GV0214 through GV0249 inclusive.
Odd S/Ns GT1591 through
GT1857.
Slide, forward/aft door ..................
(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, doors1, 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
GJ1150.
Slide/Raft, door 5, RH side ..........
(ii) 101630–305 ...............................
(iii) 101630–306 ..............................
(iv) 101655–305 ..............................
(v) 101655–306 ...............................
(vi) 101656–305 ..............................
(vii) 101656–306 .............................
(viii) 101658–101 and 101658–103
(ix) 101659–101 through 101659–
205 inclusive.
(x) 101660–101 through 101660–
107 inclusive.
(xi) 5A3086–3 and 5A3086–301 .....
(xii) 5A3088–3 and 5A3088–301 ....
(xiii) 5A3109–1 ................................
(xiv) 5A3109–2 ................................
(xv) 5A3294–1 and 5A3294–2 ........
(xvi) 5A3295–1 and 5A3295–3 .......
(xvii) 5A3307–1 through 5A3307–5
inclusive and 5A3307–301.
(xviii)
7A1323–111
through
7A1323–114 inclusive.
(xix) 7A1394–4 and 7A1394–6 .......
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(xx) 7A1418–21 and 7A1418–23 ....
(xxv) 7A1467–22 and 7A1467–24 ..
(xxvi) 7A1469–13 ............................
(xxvii) 7A1469–14 ...........................
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Ramp/Slide, off-wing, left-hand
(LH) side.
Ramp/Slide, off-wing, right-hand
(RH) side.
Ramp/Slide, off-wing, LH side .....
Ramp/Slide, off-wing, RH side .....
Ramp/Slide, off-wing, RH side .....
Slide, forward door .......................
Slide, aft door ...............................
Slide, forward door .......................
Slide, forward door .......................
Ramp/Slide, off-wing, LH side .....
Ramp/Slide, off-wing, RH side .....
Slide/Raft, door 2 .........................
Slide/Raft, doors 1 and 4 .............
Slide, stretched upper deck .........
Slide/Raft, forward/aft doors ........
Ramp/Slide, off-wing door 3, LH
side.
Slide/Raft, doors 1 and 4, RH
side.
Slide/Raft, door 5, LH side ...........
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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.
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.
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15403
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—
(xxviii) 7A1479–13 ...........................
Odd
S/Ns
GI1019
through
GI1265.
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 an L55
prefix.
PF0001 through PF0163 inclusive, and all S/Ns with an R55
prefix.
PH0001 through PH0299 inclusive, and all S/Ns with an L56
prefix.
PD0001 through PD0293 inclusive, and all S/Ns with an R56
prefix.
PAK001 through PAK136 inclusive.
PAL001 through PAL670 inclusive.
PAB001 through PAB610 inclusive.
B3F001 through B3F314 inclusive
Slide/Raft, door 2, LH side ...........
747–300, –400, and –400D series
airplanes.
747–300, –400, and –400D series
airplanes.
767–300 series airplanes.
767–300 series airplanes.
B3A001 through B3A337 inclusive.
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.
Slide, aft door ...............................
(xxix) 7A1479–14 ............................
(xxx) 7A1489–3 ...............................
(xxxi) 7A1489–4 ..............................
(xxxii)
101623–107
101623–303 inclusive.
through
(xxxiii) Odd dash numbers 101630–
105 through 101630–305.
(xxxiv)
Even
dash
numbers
101630–106 through 101630–
306.
(xxxv) Odd dash numbers 101655–
101 through 101655–305.
(xxxvi)
Even
dash
numbers
101655–102 through 101655–
306.
(xxxvii)
Odd
dash
numbers
101656–103 through 101656–
305.
(xxxviii) Even dash numbers
101656–104 through 101656–
306.
(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 ...
(xliii) 5A3088–3 and 5A3088–301 ...
(xliv) 5A3109–1 ...............................
(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/Raft, door 2, RH side ..........
Slide/Raft, mid door, LH side .......
Slide/Raft, mid door, RH side ......
Slide, forward/aft door ..................
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.
Ramp/Slide, off-wing, LH side .....
767–200 and –300 series airplanes.
Ramp/Slide, off-wing, RH side .....
767–200 and –300 series airplanes.
Slide, forward door .......................
737–200 series airplanes.
Slide, 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.
737–600, –700, –700C, –800,
and –900 series airplanes.
747–100B SUD, –300, –400, and
–400D series airplanes.
Slide, forward door .......................
Slide, forward door .......................
Ramp/Slide, off-wing, LH side .....
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.
Slide/Raft, doors 1, 2, and 4 ........
pwalker on PROD1PC71 with RULES
(lii) 7A1439–1 through 7A1439–8
inclusive.
(liii) 7A1447–1 through 7A1447–54
inclusive.
(liv) 7A1448–1 through 7A1448–12
inclusive.
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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.
Slide/Raft, door 5 .........................
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15404
Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
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—
(lv) Odd dash numbers 7A1467–1
through 7A1467–23.
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 and 4, LH side
747–400 and –400D series airplanes.
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.
(lvi) Even dash numbers 7A1467–2
through 7A1467–24.
(lvii) Odd dash numbers 7A1469–1
through 7A1469–13.
(lviii) Even dash numbers 7A1469–
2 through 7A1469–14.
(lix) Odd dash numbers 7A1479–1
through 7A1479–13.
(lx) Even dash numbers 7A1479–2
through 7A1479–14.
(lxi) 7A1489–1 and 7A1489–3 ........
(lxii) 7A1489–2 and 7A1489–4 .......
TABLE 2.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN MCDONNELL DOUGLAS MODEL AIRPLANES
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.
pwalker on PROD1PC71 with RULES
Goodrich evacuation systems having P/N—
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.
All .................................................
Slide, forward/ service door .........
All .................................................
Slide, aft door ...............................
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.
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
15405
TABLE 2.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN MCDONNELL DOUGLAS MODEL AIRPLANES—
Continued
Goodrich evacuation systems having P/N—
Having any S/N—
Component/part is named—
Installed on McDonnell Douglas
Model—
(ix) 7A1276–3 through 7A1276–12
inclusive.
All .................................................
Slide, tailcone ...............................
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
Goodrich evacuation system having
P/N—
Having any S/N—
Component/part is named—
Installed on Airbus Model—
(i) 4A3928–1 ....................................
AY0001 through AY0007 inclusive.
AZ0001 through AZ0007 inclusive
AQ0001 through AQ0028 inclusive.
AT0001 through AT0028 inclusive
AK0001 through AK0028 inclusive.
AM0001 through AM0028 inclusive.
WB0030 through WB0033 inclusive.
Slide, door 3 type 1, LH side .......
A340–541 airplanes.
Slide, door 3 type 1, RH side ......
Ramp/Slide, off-wing, LH side .....
A340–541 airplanes.
A340–642 airplanes.
Ramp/Slide, off-wing, RH side .....
Slide/Raft, door 3, LH side ...........
A340–642 airplanes.
A340–642 airplanes.
Slide/Raft, door 3, RH side ..........
A340–642 airplanes.
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 .................
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.
(ii) 4A3928–2 ...................................
(iii) 4A3931–1 and 4A3931–3 .........
(iv) 4A3931–2 and 4A3931–4 .........
(v) 4A3934–1 and 4A3934–3 ..........
(vi) 4A3934–2 and 4A3934–4 .........
pwalker on PROD1PC71 with RULES
(vii) 7A1296–004 and 7A1296–005
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15406
Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued
Having any S/N—
Component/part is named—
Installed on Airbus Model—
(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 through 7A1508–
117 inclusive.
AA1041 through AA2419 inclusive.
Slide/Raft, doors 1 and 4 .............
(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 through 7A1510–
118 inclusive.
AC0077 through AC0148 inclusive.
Slide/Raft, door 3 type A, RH side
(xvii)
7A1539–109
7A1539–117 inclusive.
pwalker on PROD1PC71 with RULES
Goodrich evacuation system having
P/N—
AU0302 through AU0677 inclusive.
Slide/Raft, door 2, LH 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;
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.
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. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
15407
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—
(xviii)
7A1539–110
7A1539–118 inclusive.
through
AX0302 through AX0673 inclusive.
Slide/Raft, door 2, RH side ..........
(xix) 7A1296–001 through 7A1296–
004 inclusive.
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; 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.
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.
(xxi) 7A1298–001 through 7A1298–
004 inclusive.
Slide, forward/aft door ..................
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.
pwalker on PROD1PC71 with RULES
(xxii)
7A1299–001
7A1299–006 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 .....................
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
TABLE 3.—GOODRICH EVACUATION SYSTEMS INSTALLED ON CERTAIN AIRBUS MODEL AIRPLANES—Continued
Having any S/N—
Component/part is named—
Installed on Airbus Model—
(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.
AC0001 through AC0076 inclusive.
Slide/Raft, door 3 type A, RH side
(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.
pwalker on PROD1PC71 with RULES
Goodrich evacuation system having
P/N—
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; 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.
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 an 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
VerDate Aug<31>2005
16:13 Mar 21, 2008
Jkt 214001
the compliance times specified, unless the
actions have already been done.
Service Bulletin 25–344, Revision 2, dated
October 11, 2006.
Service Bulletin Reference
Compliance Times
(f) The term ‘‘service bulletin,’’ as used in
this AD, means the following service
bulletins, as applicable:
(1) For Goodrich evacuation systems
identified in Tables 1 and 2 of this AD:
Goodrich Service Bulletin 25–343, Revision
3, dated January 12, 2007; and
(2) For Goodrich evacuation systems
identified in Table 3 of this AD: Goodrich
(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.
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Federal Register / Vol. 73, No. 57 / Monday, March 24, 2008 / Rules and Regulations
(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, except where the
service bulletin specifies to record service
bulletin compliance on a system information
card, this AD requires recording
accomplishment in accordance with an FAAapproved record-keeping system.
(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
25–343
25–343
25–343
25–344
25–344
...........................................................................................................
...........................................................................................................
...........................................................................................................
...........................................................................................................
...........................................................................................................
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) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. 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.
Material Incorporated by Reference
pwalker on PROD1PC71 with RULES
Revision level
(m) You must use Goodrich Service
Bulletin 25–343, Revision 3, dated January
12, 2007; or Goodrich Service Bulletin 25–
344, Revision 2, dated October 11, 2006; as
applicable; to do the actions required by this
AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
Goodrich Service Bulletin 25–344, Revision
2, dated October 11, 2006, under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) The Director of the Federal Register
previously approved the incorporation by
reference of Goodrich Service Bulletin 25–
343, Revision 3, dated January 12, 2007, on
VerDate Aug<31>2005
16:13 Mar 21, 2008
Jkt 214001
Original ..........................................................
1 ....................................................................
2 ....................................................................
Original ..........................................................
1 ....................................................................
March 11, 2008 (73 FR 6586, February 5,
2008).
(3) For service information identified in
this AD, contact Goodrich, Aircraft Interior
Products, ATTN: Technical Publications,
3414 South Fifth Street, Phoenix, AZ 85040–
1169.
(4) You may review copies of the service
information that is incorporated by reference
at the FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton,
Washington; or at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/ibr
_locations.html.
Issued in Renton, Washington, on March 9,
2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E8–5375 Filed 3–21–08; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Date
October
January
October
October
January
15,
31,
11,
15,
31,
2003.
2005.
2006.
2003.
2005.
DEPARTMENT OF STATE
22 CFR Part 126
[Public Notice: 6145]
Amendment to the International Traffic
in Arms Regulations: Sri Lanka
Department of State.
Final Rule.
AGENCY:
ACTION:
SUMMARY: In accordance with the
Department of State, Foreign
Operations, and Related Programs
Appropriations Act, 2008 (Div. J, Pub. L.
110–161), the Department of State is
amending the International Traffic in
Arms Regulations (ITAR) regarding Sri
Lanka, to make it United States policy
to deny licenses and other approvals to
export or otherwise transfer defense
articles and defense services to Sri
Lanka except, on a case-by-case basis,
for technical data or equipment made
available for the limited purposes of
maritime and air surveillance and
communications.
Effective Date: This rule is
effective March 24, 2008.
DATES:
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]]>Agencies
[Federal Register Volume 73, Number 57 (Monday, March 24, 2008)]
[Rules and Regulations]
[Pages 15399-15409]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-5375]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-28370; Directorate Identifier 2003-NM-239-AD;
Amendment 39-15439; AD 2008-06-27]
RIN 2120-AA64
Airworthiness Directives; Goodrich Evacuation Systems Approved
Under Technical Standard Orders (TSOs) TSO-C69, TSO-C69a, TSO-C69b, and
TSO-C69c, Installed on Various Boeing, McDonnell Douglas, and Airbus
Transport Category Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Goodrich evacuation systems approved under Technical Standard Orders
(TSOs) TSO-C69, TSO-C69a, TSO-C69b, and TSO-C69c, installed on certain
Boeing, McDonnell Douglas, and Airbus transport category airplanes. For
certain systems, this AD requires replacing the evacuation system's
shear-pin restraints with new ones. For certain other systems, this AD
requires an inspection for manufacturing lot numbers; and a general
visual inspection of the shear-pin restraint for discrepancies, and
corrective actions if necessary. This AD results from several reports
of corroded shear-pin restraints that prevented Goodrich evacuation
systems from deploying properly. We are issuing this AD to prevent
failure of an evacuation system, which could impede an emergency
evacuation and increase the chance of injury to passengers and
flightcrew during the evacuation.
DATES: This AD is effective April 28, 2008.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 28,
2008.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of March
11, 2008 (73 FR 6586, February 5, 2008).
ADDRESSES: For service information identified in this AD, contact
Goodrich, Aircraft Interior Products, ATTN: Technical Publications,
3414 South Fifth Street, Phoenix, AZ 85040-1169.
Examining the AD Docket
You may examine the AD docket on the Internet at https://
[[Page 15400]]
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 AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (telephone 800-647-5527) is the Document Management
Facility, U.S. Department of Transportation, Docket Operations, M-30,
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
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:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness directive (AD) that would apply to
certain Goodrich evacuation systems approved under Technical Standard
Orders (TSOs) TSO-C69, TSO-C69a, TSO-C69b, and TSO-C69c, installed on
certain Boeing, McDonnell Douglas, and Airbus transport category
airplanes. That NPRM was published in the Federal Register on June 8,
2007 (72 FR 31761). For certain systems, that NPRM proposed to require
replacing the evacuation systems shear-pin restraints with new ones.
For certain other systems, that NPRM proposed to require an inspection
for manufacturing lot numbers; and a general visual inspection of the
shear-pin restraint for discrepancies, and corrective actions if
necessary.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comments received from the 5 commenters.
Supportive Comments
Air Line Pilots Association, International (ALPA), and Air
Transport Association (ATA), on behalf of its member Continental
Airlines, support the intent of the rule. Continental states that it
has captured Goodrich Service Bulletin 25-343 on a total of 969 slide
assemblies since the service bulletin's October 2003 release.
Request To Combine Two AD Actions Into One AD Action
ATA, on behalf of its member United Airlines, notes that this NPRM
is similar to NPRM 2005-NM-139-AD (AD 2008-03-05, amendment 39-15354
(73 FR 6586, February 5, 2008)). United requests that this AD action be
incorporated into NPRM 2005-NM-139-AD.
We do not agree with the commenter's request. While the evacuation
slides affected by this AD and AD 2008-03-05 are identified in the same
service bulletin and have the same unsafe condition, the individual
evacuation slides were approved under different certification
processes. This AD affects certain evacuation slides that were approved
under a TSO that specified certain requirements for evacuation slides.
AD 2008-03-05 affects airplanes that had certain other evacuation
slides approved as part of a type certificate. The TSO approval process
specifies the airplane model(s) on which a specific evacuation slide
can be installed. These two approval processes affect how we issue ADs.
We have not changed this AD or AD 2008-03-05 in this regard.
Request To Extend Compliance Times
ATA, on behalf of its member United Airlines, requests that the
compliance times be extended from 18 months after the effective date of
the AD for Model 767 airplane off-wing evacuation systems and 36 months
after the effective date of the AD for the other evacuation systems to
36 and 48 months respectively. The commenters state that extended
compliance times would match routine overhaul cycles, account for parts
lead-time, take into consideration the large quantity of affected
evacuation systems, and relieve a burden on resources and capacity.
We disagree with the request to extend the compliance times. A
significant number of affected evacuation systems have already been
modified. We have received confirmation from Goodrich that parts are
available to support the 18- and 36-month compliance times. 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 not changed the AD in this regard.
Request To Accept Certain Service Bulletins for Accomplishment
ATA, on behalf of its member United Airlines, requests that the FAA
accept accomplishment of either Goodrich Service Bulletin 25-343,
Revision 1, dated January 31, 2005; or Revision 2, dated October 11,
2006; after the effective date of the AD. The commenters explain that
there are no technical or procedural changes between these revisions
and the most recent revision, Revision 3, dated January 12, 2007.
We disagree with the request to accept accomplishment of earlier
service bulletin revisions after the effective date of the AD. It is
our policy to require compliance with the most recent revision of
service information. However, in paragraph (k) of this AD, we provide
credit for accomplishment of the earlier service bulletin revisions if
done before the effective date of the AD. We have not changed the AD in
this regard.
Request To Refer to Current Service Bulletins as Acceptable for Credit
Goodrich, the evacuation slide manufacturer, requests that we give
credit for accomplishing paragraph (h) of this AD to airlines/overhaul
shops that might have accomplished Revision 3 of Goodrich Service
Bulletin 25-343, dated January 12, 2007; and Revision 2 of Goodrich
Service Bulletin 25-344, dated October 11, 2006; before the effective
date of this AD. Goodrich states that ``The wording of paragraph (k)
does not clearly provide credit for actions done in compliance with 25-
343, revision 3, and 25-344, revision 2, unless it occurs `after the
effective date of this AD'.''
We infer that Goodrich interprets the text of paragraph (k) of the
AD to mean that operators that have accomplished Revision 3 of Goodrich
Service Bulletin 25-343 or Revision 2 of Goodrich Service Bulletin 25-
344 before the effective date would be required to accomplish those
actions again after the effective date to comply with this AD. We find
that clarification is necessary. Paragraph (e) of this AD states that
the actions must be done as specified in the AD ``unless the actions
have already been done,'' so it is not necessary to repeat this
information in paragraph (k) of the AD. We refer to Goodrich Service
Bulletin 25-343, Revision 3, dated January 12, 2007; and Goodrich
Service Bulletin 25-344, Revision 2, dated October 11, 2006; as the
sources of service information for accomplishing the requirements of
paragraph (h) of this AD. Accomplishing the requirements of
[[Page 15401]]
this AD in accordance with these service bulletins before the effective
date of the AD is acceptable for compliance with this AD. We have not
changed the AD in this regard.
Request To Allow Other Methods of Recording Compliance
ATA, on behalf of its member United Airlines, states that the
Accomplishment Instructions of Goodrich Service Bulletin 25-343
instruct the operator to record service bulletin compliance on the
system information card. United requests that the method of recording
compliance on the card be made optional, as operators have alternative
means to record compliance and the system information card might not be
available.
We infer that the commenters want us to revise the AD to allow
different methods of recording compliance with the service bulletin. We
agree with the request to revise the AD. We have revised paragraph (h)
of this AD to specify that recording compliance with the service
bulletin in accordance with the service bulletin instructions is not
required by this AD. Operators may record service bulletin compliance
whichever way their applicable record-keeping system specifies.
However, recording compliance with the AD is still required. Recording
AD compliance is accomplished in a maintenance log, on job/task cards,
or some other method approved by the operator's principal inspector or
local flight standards district office. We have not changed the AD in
this regard.
Request To Reverse Order of Sub-Paragraphs
Goodrich requests that we reverse the sequence of paragraphs (f)(1)
and (f)(2) of the NPRM so that the references to Tables 1 and 2 of the
AD are called out first before Table 3.
We agree with the commenter's request. Revising the sequence of the
paragraphs to match the sequence of the tables will reduce confusion.
We have changed paragraphs (f)(1) and (f)(2) of this AD as requested.
Clarification of Alternative Method of Compliance (AMOC) Paragraph
We have revised this action to clarify the appropriate procedure
for notifying the principal inspector before using any approved AMOC on
any airplane to which the AMOC applies.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously. We also determined that
this change will not increase the economic burden on any operator or
increase the scope of the AD.
Costs of Compliance
This AD affects certain Goodrich evacuation systems installed on
about 2,844 airplanes worldwide. This AD affects about 1,240 airplanes
of U.S. registry. The following table provides the estimated costs for
U.S. operators to comply with this AD.
Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
Average labor Number of slide
Action Work hours rate per hour Parts Cost per slide unit units per airplane Fleet cost
--------------------------------------------------------------------------------------------------------------------------------------------------------
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
This AD will not have federalism implications under Executive Order
13132. This AD will 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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under 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.
You can find our regulatory evaluation and the estimated costs of
compliance in the AD Docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new AD:
2008-06-27 Goodrich (Formerly BFGoodrich): Amendment 39-15439.
Docket No. FAA-2007-28370; Directorate Identifier 2003-NM-239-AD.
[[Page 15402]]
Effective Date
(a) This airworthiness directive (AD) is effective April 28,
2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to:
(1) Goodrich evacuation systems approved under Technical
Standard Orders (TSOs) 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 TSOs 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 TSOs TSO-C69a,
TSO-C69b, and TSO-C69c, installed on certain 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 any serial number Component/part is named-- Installed on Boeing
having part number (P/N)-- (S/N)-- 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, LH 767-200 and -300 series
inclusive. side. airplanes.
(v) 101655-306................... PF0164 through PF0220 Ramp/Slide, off-wing, RH 767-200 and -300 series
inclusive. side. airplanes.
(vi) 101656-305.................. PH0300 through PH0390 Ramp/Slide, off-wing, LH 767-200 and -300 series
inclusive. side. airplanes.
(vii) 101656-306................. PD0294 through PD0378 Ramp/Slide, off-wing, RH 767-200 and -300 series
inclusive. side. airplanes.
(viii) 101658-101 and 101658-103. PAK137 through PAK150 Slide, forward door..... 737-200 series
inclusive. airplanes.
(ix) 101659-101 through 101659- PAL671 through PAL738 Slide, aft door......... 737-200, -300, -400, and
205 inclusive. inclusive. -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, LH 777-300 and -300ER
ST0131. side. series airplanes.
(xiv) 5A3109-2................... Even S/Ns ST0014 through Ramp/Slide, off-wing, RH 777-300 and -300ER
ST0128. 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- GS1340 through GS1879 Slide, stretched upper 747-100B SUD, -300, -
114 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 through Ramp/Slide, off-wing 747-100, -100B, -100B
GT1830. door 3, RH side. SUD, -200B, -200C, -
300, -400, -400D, and
747SR series airplanes.
(xxii) 7A1447-39 through 7A1447- GW2682 through GW2923 Slide/Raft, doors1, 2, 747-100, -100B, -100B
54 inclusive. inclusive. and 4. SUD, -200B, -200C, -
300, and 747SR series
airplanes.
(xxiii) 7A1448-5 through 7A1448- GX1538 through GX1593 Slide/Raft, door 5...... 747-100, -100B, -100B
12 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 series
GH2443. 4, LH side. airplanes.
(xxv) 7A1467-22 and 7A1467-24.... Even S/Ns GH1954 through Slide/Raft, doors 1 and 747-400 and -400D series
GH2420. 4, RH side. airplanes.
(xxvi) 7A1469-13................. Odd S/Ns GJ909 through Slide/Raft, door 5, LH 747-400 and -400D series
GJ1163. side. airplanes.
(xxvii) 7A1469-14................ Even S/Ns GJ912 through Slide/Raft, door 5, RH 747-400 and -400D series
GJ1150. side. airplanes.
[[Page 15403]]
(xxviii) 7A1479-13............... Odd S/Ns GI1019 through Slide/Raft, door 2, LH 747-300, -400, and -400D
GI1265. side. series airplanes.
(xxix) 7A1479-14................. Even S/Ns GI1036 through Slide/Raft, door 2, RH 747-300, -400, and -400D
GI1298. side. series airplanes.
(xxx) 7A1489-3................... Odd S/Ns GK355 through Slide/Raft, mid door, LH 767-300 series
GK403. side. airplanes.
(xxxi) 7A1489-4.................. Even S/Ns GK356 through Slide/Raft, mid door, RH 767-300 series
GK406. side. airplanes.
(xxxii) 101623-107 through 101623- PB0001 through PB0399 Slide, forward/aft door. 767-200 and -300 series
303 inclusive. inclusive, and all S/Ns airplanes.
with a B23 prefix.
(xxxiii) Odd dash numbers 101630- PG0001 through PG0275 Ramp/Slide, off-wing, LH 767-200 and -300 series
105 through 101630-305. inclusive, and all S/Ns side. airplanes.
with a B101 prefix.
(xxxiv) Even dash numbers 101630- PC0001 through PC0263 Ramp/Slide, off-wing, RH 767-200 and -300 series
106 through 101630-306. inclusive, and all S/Ns side. airplanes.
with a B102 prefix.
(xxxv) Odd dash numbers 101655- PK0001 through PK0160 Ramp/Slide, off-wing, LH 767-200 and -300 series
101 through 101655-305. inclusive, and all S/Ns side. airplanes.
with an L55 prefix.
(xxxvi) Even dash numbers 101655- PF0001 through PF0163 Ramp/Slide, off-wing, RH 767-200 and -300 series
102 through 101655-306. inclusive, and all S/Ns side. airplanes.
with an R55 prefix.
(xxxvii) Odd dash numbers 101656- PH0001 through PH0299 Ramp/Slide, off-wing, LH 767-200 and -300 series
103 through 101656-305. inclusive, and all S/Ns side. airplanes.
with an L56 prefix.
(xxxviii) Even dash numbers PD0001 through PD0293 Ramp/Slide, off-wing, RH 767-200 and -300 series
101656-104 through 101656-306. inclusive, and all S/Ns side. airplanes.
with an R56 prefix.
(xxxix) 101658-101 and 101658-103 PAK001 through PAK136 Slide, forward door..... 737-200 series
inclusive. airplanes.
(xl) 101659-101 through 101659- PAL001 through PAL670 Slide, aft door......... 737-200, -300, -400, and
205 inclusive. inclusive. -500 series airplanes.
(xli) 101660-101 through 101660- PAB001 through PAB610 Slide, forward door..... 737-300, -400, and -500
107 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 through Ramp/Slide, off-wing, LH 777-300 and -300ER
ST0013. side. series airplanes.
(xlv) 5A3109-2................... Even S/Ns, ST0002 through Ramp/Slide, off-wing, RH 777-300 and -300ER
ST0012. 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- GS0001 through GS1339 Slide, stretched upper 747-100B SUD, -300, -
114 inclusive. inclusive, and all S/Ns deck. 400, and -400D series
with a single G prefix. airplanes.
(xlviii) 7A1394-3 through 7A1394- GV001 through GV213 Slide/Raft, forward/aft 767-200 and -300 series
6 inclusive. inclusive, and all S/Ns doors. airplanes.
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/Ns door 3, LH side. SUD, -200B, -200C, -
with a single letter G 300, -400, -400D, and
prefix. 747SR series airplanes.
(l) Even dash numbers 7A1418-2 Even S/Ns GT0002 through Ramp/Slide, off-wing 747-100, -100B, -100B
through 7A1418-24. GT1574, and all even S/ door 3, RH side. SUD, -200B, -200C, -
Ns with a single letter 300, -400, -400D, and
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/Ns and 4. and 747SR series
with a single letter G airplanes.
prefix.
(lii) 7A1439-1 through 7A1439-8 GX0001 through GX1593 Slide/Raft, door 5...... 747-100B, -200C, -300,
inclusive. inclusive, and all S/Ns and 747SR series
with a single letter G airplanes.
prefix.
(liii) 7A1447-1 through 7A1447-54 GW0001 through GW2681 Slide/Raft, doors 1, 2, 747-100, -100B, -100B
inclusive. inclusive, and all S/Ns and 4. SUD, -200B, -200C, -
with a single letter G 300, and 747SR series
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.
[[Page 15404]]
(lv) Odd dash numbers 7A1467-1 Odd S/Ns GH0001 through Slide/Raft, doors 1 and 747-400 and -400D series
through 7A1467-23. GH1967, and all odd S/Ns 4, LH side. airplanes.
with a single letter G
prefix.
(lvi) Even dash numbers 7A1467-2 Even S/Ns GH0002 through Slide/Raft, doors 1 and 747-400 and -400D series
through 7A1467-24. GH1952, and all even S/ 4, RH side. airplanes.
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 series
through 7A1469-13. GJ907, and all odd S/Ns side. airplanes.
with a single letter G
prefix.
(lviii) Even dash numbers 7A1469- Even S/Ns GJ002 through Slide/Raft, door 5, RH 747-400 and -400D series
2 through 7A1469-14. GJ910, and all even S/Ns side. airplanes.
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 -400D
through 7A1479-13. GI1017, and all odd S/Ns side. series airplanes.
with a single letter G
prefix.
(lx) Even dash numbers 7A1479-2 Even S/Ns GI0002 through Slide/Raft, door 2, RH 747-300, -400, and -400D
through 7A1479-14. GI1034, and all even S/ side. series airplanes.
Ns with a single letter
G prefix.
(lxi) 7A1489-1 and 7A1489-3...... Odd S/Ns GK001 through Slide/Raft, mid door, LH 767-300 series
GK353, and all odd S/Ns side. airplanes.
with a single letter G
prefix.
(lxii) 7A1489-2 and 7A1489-4..... Even S/Ns GK002 through Slide/Raft, mid door, RH 767-300 series
GK354, and all even S/Ns side. airplanes.
with a single letter G
prefix.
----------------------------------------------------------------------------------------------------------------
Table 2.--Goodrich Evacuation Systems Installed on Certain McDonnell Douglas Model Airplanes
----------------------------------------------------------------------------------------------------------------
Goodrich evacuation systems Component/part is named-- Installed on McDonnell
having P/N-- Having any S/N-- Douglas Model--
----------------------------------------------------------------------------------------------------------------
(i) 100504-101 through 100504-205 D9F161 through D9F256 Slide, forward door..... DC-9-81 (MD-81), DC-9-82
inclusive. inclusive, and PU0325 (MD-82), DC-9-83 (MD-
through PU0331 inclusive. 83), and DC-9-87 (MD-
87) airplanes; Model MD-
88 airplanes; and Model
MD-90-30 airplanes.
(ii) 100505-101 through 100505- D9A078 through D9A122 Slide, aft door......... DC-9-81 (MD-81), DC-9-82
201 inclusive. inclusive, and PS0151 (MD-82), DC-9-83 (MD-
through PS0157 inclusive. 83), and DC-9-87 (MD-
87) airplanes; Model MD-
88 airplanes; and Model
MD-90-30 airplanes.
(iii) 100506-103 through 100506- D9T085 through D9T127 Slide, tailcone......... DC-9-81 (MD-81), DC-9-82
203 inclusive. inclusive, and PT0175 (MD-82), DC-9-83 (MD-
through PT0178 inclusive. 83), and DC-9-87 (MD-
87) airplanes; Model MD-
88 airplanes; and Model
MD-90-30 airplanes.
(iv) 100504-101 through 100504- D9F001 through D9F160 Slide, forward door..... DC-9-81 (MD-81), DC-9-82
205 inclusive. inclusive, and PU0001 (MD-82), DC-9-83 (MD-
through PU0324 inclusive. 83), and DC-9-87 (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-9-82
inclusive. inclusive, and PS0001 (MD-82), DC-9-83 (MD-
through PS0150 inclusive. 83), and DC-9-87 (MD-
87) airplanes; Model MD-
88 airplanes; and Model
MD-90-30 airplanes.
(vi) 100506-103 through 100506- D9T001 through D9T084 Slide, tailcone......... DC-9-81 (MD-81), DC-9-82
203 inclusive. inclusive, and PT0001 (MD-82), DC-9-83 (MD-
through PT0174 inclusive. 83), and DC-9-87 (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-9-
inclusive. door. 82 (MD-82) airplanes.
(viii) 7A1275-3 through 7A1275-20 All...................... Slide, aft door......... DC-9-81 (MD-81) and DC-9-
inclusive. 82 (MD-82) airplanes.
[[Page 15405]]
(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 Component/part is named-- Installed on Airbus
P/N-- Having any S/N-- Model--
----------------------------------------------------------------------------------------------------------------
(i) 4A3928-1..................... AY0001 through AY0007 Slide, door 3 type 1, LH A340-541 airplanes.
inclusive. side.
(ii) 4A3928-2.................... AZ0001 through AZ0007 Slide, door 3 type 1, RH A340-541 airplanes.
inclusive. side.
(iii) 4A3931-1 and 4A3931-3...... AQ0001 through AQ0028 Ramp/Slide, off-wing, LH A340-642 airplanes.
inclusive. side.
(iv) 4A3931-2 and 4A3931-4....... AT0001 through AT0028 Ramp/Slide, off-wing, RH A340-642 airplanes.
inclusive. 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.
(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.
[[Page 15406]]
(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- AA1041 through AA2419 Slide/Raft, doors 1 and A330-201, -202, -203, -
117 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.
(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- AB0077 through AB0150 Slide/Raft, door 3 type A330-201, -202, -203, -
117 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- AC0077 through AC0148 Slide/Raft, door 3 type A330-201, -202, -203, -
118 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- AU0302 through AU0677 Slide/Raft, door 2, LH A330-201, -202, -203, -
117 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.
[[Page 15407]]
(xviii) 7A1539-110 through 7A1539- AX0302 through AX0673 Slide/Raft, door 2, RH A330-201, -202, -203, -
118 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- WB0001 through WB0029 Slide, mid door......... A300 B2-1A, B2-1C, B2K-
004 inclusive. inclusive, all S/Ns with 3C, and B2-203
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- WF0001 through WF0256 Ramp/Slide, off-wing A310-203, -204, -221,
203 inclusive. inclusive, all S/Ns with door. and -222 airplanes; and
a single letter R Model A310-304, -322, -
prefix, and all S/Ns 324, and -325
with a single letter G airplanes.
prefix.
(xxi) 7A1298-001 through 7A1298- WA0001 through WA0326 Slide, forward/aft door. A300 B2-1A, B2-1C, B2K-
004 inclusive. inclusive, all S/Ns with 3C, and B2-203
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.
(xxii) 7A1299-001 through 7A1299- WE0001 through WE0148 Slide, emergency door... A300 B2-1A, B2-1C, B2K-
006 inclusive. inclusive, all S/Ns with 3C, and B2-203
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- WC0001 through WC0422 Slide/Raft, forward/aft A300 B2-1A, B2-1C, B2K-
007 inclusive. inclusive, all S/Ns with door. 3C, and B2-203
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 B
