Published 2006-09-06 · Federal Register document E6-14636
Airworthiness Directives; Goodyear Aviation Tires, Part Number 217K22-1, Installed on Various Transport Category Airplanes, Including But Not Limited to Bombardier Model BD-700-1A10 and BD-700-1A11 Airplanes; and Gulfstream Model G-1159, G-1159A, G-1159B, G-IV, GIV-X, GV, and GV-SP Series Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain aviation tires installed on various transport category airplanes. This AD requires a one-time inspection of the nosewheel tires to determine if they are within a designated serial number range, and replacement if necessary. This AD results from reports of tread separations and tread-area bulges on the nosewheel tires. We are issuing this AD to prevent tread separation from a nosewheel tire during takeoff or landing, which could result in compromised nosewheel steering or ingestion of separated tread by an engine, and consequent reduced controllability of the airplane on the runway or in the air.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2006-8d787f8b35bc8016
- Source row
- results[320]
- Raw source SHA-256
- 8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2006-18-08
- Effective date printed in this edition
- 2006-10-11
Read 11 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective October 11, 2006.
Exact source excerpt. Text positions 11363–11432, end exclusive, in the original decoded publication. SHA-256: 8b5a05e4dcae079cb4dfab60a8afb1631445596a26f6134f4db04c6f6b3800c4
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 11432–11461, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to Goodyear aviation tires, part number
217K22-1, identified in Goodyear Aviation Service Bulletin SB-2005-
32-004, Revision 5, dated December 22, 2005; installed on various
transport category airplanes, certificated in any category,
including but not limited to Bombardier Model BD-700-1A10 and BD-
700-1A11 airplanes, and Gulfstream Model G-1159, G-1159A, G-1159B,
G-IV, G-IV-X, G-V, and G-V-SP series airplanes.
Exact source excerpt. Text positions 11461–11920, end exclusive, in the original decoded publication. SHA-256: c5029064c5cb22ed45a0d4805268a6336fbf7262e4eeb56711ddf65e48618442
Unsafe Condition
Unsafe Condition
(d) This AD results from reports of tread separations and tread-
area bulges on the nosewheel tires. We are issuing this AD to
prevent tread separation from a nosewheel tire during takeoff or
landing, which could result in compromised nosewheel steering or
ingestion of separated tread by an engine, and consequent reduced
controllability of the airplane on the runway or in the air.
Exact source excerpt. Text positions 11920–12331, end exclusive, in the original decoded publication. SHA-256: 8d720ecbdf0f052dc0f769ade075064c12f1d7fbb95172cf58c145e71a9b227c
Compliance
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Exact source excerpt. Text positions 12331–12509, end exclusive, in the original decoded publication. SHA-256: 64a7a1579f37f56eafecd0aeb3c528e7c89f6292ed0cb53091423917642d5847
Inspection To Determine Serial Number (S/N), and Replacement
Inspection To Determine Serial Number (S/N), and Replacement
(f) Within 60 days after the effective date of this AD: Inspect
the nosewheel tires to determine whether an affected S/N is
installed, in accordance with the Accomplishment Instructions of
Goodyear Aviation Service Bulletin SB-2005-32-004, Revision 5, dated
December 22, 2005; and, except as provided by paragraph (g) of this
AD, replace any tire with an affected S/N before further flight in
accordance with the Accomplishment Instructions of the service
bulletin.
Note 1: Bombardier Alert Service Bulletins A700-32-019 and A700-
1A11-32-007, both dated November 2, 2005; and the Gulfstream alert
customer bulletins listed in Table 1 of this AD are additional
sources of service information for identifying the affected serial
numbers and replacing the tires as applicable.
Table 1.--Gulfstream Alert Customer Bulletins
------------------------------------------------------------------------
Alert
Gulfstream model customer Date
bulletin
------------------------------------------------------------------------
G-1159 (GII) and G-1159B (G- 30 October 12, 2005.
IIB) series airplanes.
G-1159A (GIII) series 16 October 12, 2005.
airplanes.
G-IV airplanes................ 34 October 12, 2005.
G300 airplanes................ 34 October 12, 2005.
G400 airplanes................ 34 October 12, 2005.
GIV-X (G350) series airplanes. 3 October 12, 2005.
GIV-X (G450) series airplanes. 3 October 12, 2005.
GV series airplanes........... 24 October 12, 2005.
GV-SP (G500) series airplanes. 5 October 12, 2005.
GV-SP (G550) series airplanes. 5 October 12, 2005.
------------------------------------------------------------------------
Exact source excerpt. Text positions 12509–14459, end exclusive, in the original decoded publication. SHA-256: 2f802a01a581f29fbe9c1b0946a871eb15ffbe2a3dddefc149f91d72ea86aa10
Special Flight Permit
Special Flight Permit
(g) A special flight permit may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) for one flight to operate the airplane to a
location where the requirements of this AD can be accomplished,
provided no bulge is present on the tire with the affected S/N.
Exact source excerpt. Text positions 14459–14814, end exclusive, in the original decoded publication. SHA-256: 1528d308bba20c761c172ff4f5a9fab7799aa3ab4a7327ba3e5a44d23700fe40
Parts Installation
Parts Installation
(h) After the effective date of this AD, no person may install
on any airplane a nosewheel tire that has an S/N in the affected
range identified in the Accomplishment Instructions of Goodyear
Aviation Service Bulletin SB-2005-32-004, Revision 5, dated December
22, 2005.
Exact source excerpt. Text positions 14814–15114, end exclusive, in the original decoded publication. SHA-256: e6de09f5d12bd60a4f19b5074d746c2b46e5cf96d6d90a4ef095ecfc42925496
No Parts Return Required
No Parts Return Required
(i) Although Goodyear Aviation Service Bulletin SB-2005-32-004,
Revision 5, dated December 22, 2005, specifies to return tires to
the manufacturer, this AD does not require that action.
Exact source excerpt. Text positions 15114–15333, end exclusive, in the original decoded publication. SHA-256: c3a8d31c00c802228945a6ad9a8c67d08d57e28f4c577907587e9e9ecfe651e8
Actions Accomplished in Accordance With Original Issue of Service Bulletin
Actions Accomplished in Accordance With Original Issue of Service
Bulletin
(j) Actions done before the effective date of this AD in
accordance with Goodyear Aviation Service Bulletin SB-2005-32-004,
dated October 11, 2005, are acceptable for compliance with the
requirements of this AD.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Chicago Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Exact source excerpt. Text positions 15333–16086, end exclusive, in the original decoded publication. SHA-256: 9a5ee09190ec3d8b5d0acd52916043529d4599cfcfc3185ab1a235ce44a102bb
Material Incorporated by Reference
Material Incorporated by Reference
(l) You must use Goodyear Aviation Service Bulletin SB-2005-32-
004, Revision 5, dated December 22, 2005, to perform the actions
that are required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference of this document in accordance with 5 U.S.C. 552(a) and 1
CFR part 51. Contact Goodyear Tire and Rubber Company, 1144 E.
Market Street, Akron, OH 44316-0001, for a copy of this service
information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street,
SW., Room PL-401, Nassif Building, Washington, DC; on the Internet
at http://dms.dot.gov; or at the National Archives and Records
Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
[[Page 52426]]
Exact source excerpt. Text positions 16086–17073, end exclusive, in the original decoded publication. SHA-256: 6497e8aac8bef2d5510108ba4f70fce4b4e09c6508d7c1c7e4d5c62b895fd8c1
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2006-18-08 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: a98c57875a577bc27c72e7b8da2e30748a5ceed08a7a957a64fb6756bcf04a18. Source manifest: 0d7255b44c28e287ce6660e94b3e15034be26577154085b541a5e5a7065fd3ba.
Official source · 2006-09-06
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 71, Number 172 (Wednesday, September 6, 2006)]
[Rules and Regulations]
[Pages 52423-52426]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E6-14636]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24667; Directorate Identifier 2006-NM-009-AD;
Amendment 39-14746; AD 2006-18-08]
RIN 2120-AA64
Airworthiness Directives; Goodyear Aviation Tires, Part Number
217K22-1, Installed on Various Transport Category Airplanes, Including
But Not Limited to Bombardier Model BD-700-1A10 and BD-700-1A11
Airplanes; and Gulfstream Model G-1159, G-1159A, G-1159B, G-IV, GIV-X,
GV, and GV-SP Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain aviation tires installed on various transport category
airplanes. This AD requires a one-time inspection of the nosewheel
tires to determine if they are within a designated serial number range,
and replacement if necessary. This AD results from reports of tread
separations and tread-area bulges on the nosewheel tires. We are
issuing this AD to prevent tread separation from a nosewheel tire
during takeoff or landing, which could result in compromised nosewheel
steering or ingestion of separated tread by an engine, and consequent
reduced controllability of the airplane on the runway or in the air.
DATES: This AD becomes effective October 11, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of October 11,
2006.
ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Goodyear Tire and Rubber Company, 1144 E. Market Street,
Akron, OH 44316-0001, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Nick Miller, Aerospace Engineer,
Systems and Flight Test Branch, ACE-117C, Chicago Aircraft
Certification Office, FAA, 2300 East Devon Avenue, Room 107, Des
Plaines, IL 60018; telephone (847) 294-7518; fax (847) 294-7834.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (AD) docket on the
Internet at http://dms.dot.gov or in person at the Docket Management
Facility office between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Management Facility office
(telephone (800) 647-5227) is located on the plaza level of the Nassif
Building at the street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to certain aviation tires
installed on various transport category airplanes. That NPRM was
published in the Federal Register on May 3, 2006 (71 FR 25987). That
NPRM proposed to require a one-time inspection of the nosewheel
[[Page 52424]]
tires to determine if they are within a designated serial number range,
and replacement if necessary.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comments received.
Support for the NPRM
Two commenters, both private citizens, state that they support the
NPRM.
Requests To Revise Cost Estimate
The same commenters request that we revise the cost estimate in the
NPRM. Both commenters state that in their experience the inspection to
determine the serial number of the tire would take much less time than
the one hour given for that action in the NPRM. The commenters state
that the inspection should take only 10 to 15 minutes. One commenter
points out that the removal and replacement of the affected tires would
take 1 to 2 hours, depending on the current status of the airplane and
other variables.
We partially agree. We agree that the inspection may take less than
1 hour. We disagree that it is necessary to change the cost estimate
for the inspection to 10 to 15 minutes rather than 1 hour. We provide
these estimates in order to give airplane operators notice of the costs
they are likely to incur to do the actions specifically required by the
AD. To account for the worst-case cost for each operator, we generally
round dollar and hour figures to the next-highest value.
We also disagree with the request to change the cost estimate to
include the replacement cost. The replacement is an ``on condition''
action, and may or may not be required for a given airplane. The cost
figures discussed in NPRMs represent only the time necessary to perform
the specific actions actually required by the AD; in this case, the
inspection. These figures also do not typically include incidental
costs, such as the time required to gain access and close up, planning
time, or time necessitated by other administrative actions.
We have not changed the final rule in this regard.
Requests To Revise Compliance Time
The same commenters both request that we revise the compliance time
for doing the inspection from 60 days to 30 days. The commenters point
out that Goodyear Aviation Service Bulletin SB-2005-32-004, Revision 5,
dated December 22, 2005 (referred to in the NPRM as the appropriate
source of service information for accomplishing the actions),
recommends a compliance time of 14 days, which leads one commenter to
believe that this is a serious problem and should be a safety concern
for Gulfstream and Bombardier owners. One commenter says that even
though the NPRM states that most operators have already complied with
the service bulletin, that does not mean it is time to ease up on the
others' safety. The other commenter points out that it doesn't take
long to inspect the tire and determine the serial number. The
commenters both cite serious aviation accidents related to blown tires,
and state that the potential serious consequences also justify a
shorter compliance time.
We acknowledge the commenters' concerns. However, we do not agree
with the request to revise the compliance time. In developing an
appropriate compliance time, we considered the safety implications,
parts availability, and normal maintenance schedules. Further, the
manufacturer agreed with the proposed compliance time, and now reports
that of the 142 affected tires, 25 have been returned in accordance
with the instructions in Goodyear Aviation Service Bulletin SB-2005-32-
004, Revision 5. We also note that Gulfstream reports 90 percent
compliance and Bombardier reports 82 percent compliance as of the
closing date for comments on the NPRM. In addition, if we were to
shorten the compliance time, it would be necessary for us to issue a
supplemental NPRM to solicit additional public comment on the new,
shorter compliance time. The additional time for comment would add at
least 45 days to the total time it will take for the NPRM to become a
final rule and thereby add 45 days more before the tires would be
required to be inspected. Therefore, we have not changed the final rule
in this regard.
Explanation of Additional Service Information
Bombardier has informed us that it has issued two service bulletins
that give additional service information for identifying the affected
serial numbers and replacing the tires as applicable. We have reviewed
and added the following service bulletins to Note 1 of the final rule:
Bombardier Alert Service Bulletins A700-32-019 and A700-1A11-32-007,
both dated November 2, 2005.
Conclusion
We have carefully reviewed the available data, including the
comments received, and determined that air safety and the public
interest require adopting the AD with the change described previously.
We have determined that this change will neither increase the economic
burden on any operator nor increase the scope of the AD.
Costs of Compliance
There are about 1,282 Gulfstream airplanes and about 104 Bombardier
airplanes that use the affected tires in the worldwide fleet. This AD
will affect about 1,035 Gulfstream airplanes, and about 104 Bombardier
airplanes of U.S. registry. The inspection for the affected serial
numbers takes about 1 work hour per airplane, at an average labor rate
of $80 per work hour. Based on these figures, the estimated cost of the
AD for U.S. operators is $91,120, or $80 per airplane.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this 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.
[[Page 52425]]
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-18-08 Transport Category Airplanes: Amendment 39-14746. Docket
No. FAA-2006-24667; Directorate Identifier 2006-NM-009-AD.
Effective Date
(a) This AD becomes effective October 11, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Goodyear aviation tires, part number
217K22-1, identified in Goodyear Aviation Service Bulletin SB-2005-
32-004, Revision 5, dated December 22, 2005; installed on various
transport category airplanes, certificated in any category,
including but not limited to Bombardier Model BD-700-1A10 and BD-
700-1A11 airplanes, and Gulfstream Model G-1159, G-1159A, G-1159B,
G-IV, G-IV-X, G-V, and G-V-SP series airplanes.
Unsafe Condition
(d) This AD results from reports of tread separations and tread-
area bulges on the nosewheel tires. We are issuing this AD to
prevent tread separation from a nosewheel tire during takeoff or
landing, which could result in compromised nosewheel steering or
ingestion of separated tread by an engine, and consequent reduced
controllability of the airplane on the runway or in the air.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Inspection To Determine Serial Number (S/N), and Replacement
(f) Within 60 days after the effective date of this AD: Inspect
the nosewheel tires to determine whether an affected S/N is
installed, in accordance with the Accomplishment Instructions of
Goodyear Aviation Service Bulletin SB-2005-32-004, Revision 5, dated
December 22, 2005; and, except as provided by paragraph (g) of this
AD, replace any tire with an affected S/N before further flight in
accordance with the Accomplishment Instructions of the service
bulletin.
Note 1: Bombardier Alert Service Bulletins A700-32-019 and A700-
1A11-32-007, both dated November 2, 2005; and the Gulfstream alert
customer bulletins listed in Table 1 of this AD are additional
sources of service information for identifying the affected serial
numbers and replacing the tires as applicable.
Table 1.--Gulfstream Alert Customer Bulletins
------------------------------------------------------------------------
Alert
Gulfstream model customer Date
bulletin
------------------------------------------------------------------------
G-1159 (GII) and G-1159B (G- 30 October 12, 2005.
IIB) series airplanes.
G-1159A (GIII) series 16 October 12, 2005.
airplanes.
G-IV airplanes................ 34 October 12, 2005.
G300 airplanes................ 34 October 12, 2005.
G400 airplanes................ 34 October 12, 2005.
GIV-X (G350) series airplanes. 3 October 12, 2005.
GIV-X (G450) series airplanes. 3 October 12, 2005.
GV series airplanes........... 24 October 12, 2005.
GV-SP (G500) series airplanes. 5 October 12, 2005.
GV-SP (G550) series airplanes. 5 October 12, 2005.
------------------------------------------------------------------------
Special Flight Permit
(g) A special flight permit may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) for one flight to operate the airplane to a
location where the requirements of this AD can be accomplished,
provided no bulge is present on the tire with the affected S/N.
Parts Installation
(h) After the effective date of this AD, no person may install
on any airplane a nosewheel tire that has an S/N in the affected
range identified in the Accomplishment Instructions of Goodyear
Aviation Service Bulletin SB-2005-32-004, Revision 5, dated December
22, 2005.
No Parts Return Required
(i) Although Goodyear Aviation Service Bulletin SB-2005-32-004,
Revision 5, dated December 22, 2005, specifies to return tires to
the manufacturer, this AD does not require that action.
Actions Accomplished in Accordance With Original Issue of Service
Bulletin
(j) Actions done before the effective date of this AD in
accordance with Goodyear Aviation Service Bulletin SB-2005-32-004,
dated October 11, 2005, are acceptable for compliance with the
requirements of this AD.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Chicago Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Material Incorporated by Reference
(l) You must use Goodyear Aviation Service Bulletin SB-2005-32-
004, Revision 5, dated December 22, 2005, to perform the actions
that are required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference of this document in accordance with 5 U.S.C. 552(a) and 1
CFR part 51. Contact Goodyear Tire and Rubber Company, 1144 E.
Market Street, Akron, OH 44316-0001, for a copy of this service
information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street,
SW., Room PL-401, Nassif Building, Washington, DC; on the Internet
at http://dms.dot.gov; or at the National Archives and Records
Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
[[Page 52426]]
Issued in Renton, Washington, on August 23, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-14636 Filed 9-5-06; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:44:01.259309+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 0648841ec722a9b697cb0927cb094ab88dd2f894cf8fce6b51ce1dd1d7875069
- Text SHA-256
- a98c57875a577bc27c72e7b8da2e30748a5ceed08a7a957a64fb6756bcf04a18
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.