Published 2023-01-24 · Federal Register document 2023-01164
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all Gulfstream Aerospace Corporation (Gulfstream) Model GV and GV-SP airplanes. This AD was prompted by the omission of a life limit in the airworthiness limitations section (ALS) of the maintenance manual for a certain main landing gear (MLG) trunnion pin. This AD requires revising the ALS of the existing instructions for continued airworthiness (ICA) or inspection program for the airplane to establish a life limit for the affected MLG trunnion pin. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[8]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-02-02
- Effective date printed in this edition
- 2023-02-28
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective February 28,
2023.
Exact source excerpt. Text positions 7074–7166, end exclusive, in the original decoded publication. SHA-256: 674a44185b93c6d4fab586b9a3ffafed025f56467a10864c78aba2c9bf501612
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 7166–7195, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Gulfstream Aerospace Corporation Model GV and
GV-SP airplanes, all serial numbers, certificated in any category.
Note 1 to paragraph (c): Model GV-SP airplanes are also referred
to by the marketing designations G500, G550, and G500-5000.
Exact source excerpt. Text positions 7195–7482, end exclusive, in the original decoded publication. SHA-256: 2931596f46875a699b739ea3ec1a479d12163e477b806f28156010484cbb2a67
Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 3200, Landing Gear
System.
Exact source excerpt. Text positions 7482–7572, end exclusive, in the original decoded publication. SHA-256: c2d56876108948795f70b5157a13d62b8315c416b4d8f2431982c13f1eefc9fd
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by the omission of a life limit in the
airworthiness limitations section (ALS) for a certain main landing
gear (MLG) trunnion pin. The FAA is issuing this AD to prevent a MLG
trunnion pin from remaining in service beyond its life limit. This
unsafe condition, if not addressed, could result in MLG failure and
could lead to a runway excursion.
Exact source excerpt. Text positions 7572–7969, end exclusive, in the original decoded publication. SHA-256: afbfc0aaef9f153dd6efdda4e9d883c0edde9a51b591bf0aecd8b4ecc15b73eb
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 7969–8071, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Incorporation of ALS Revisions
(g) Incorporation of ALS Revisions
Within 12 months after the effective date of this AD, revise the
existing ALS of the instructions for continued airworthiness or
aircraft inspection program for your airplane by establishing a life
limit of 20,000 flight cycles for each MLG trunnion pin part number
(P/N) 1159SCL566-17.
Note 2 to paragraph (g): The life limit in paragraph (g) of this
AD is contained in table 5 in Section 05-10-10 of the Gulfstream V
Aircraft Maintenance Manual, Revision 55, dated March 15, 2022;
table 4 in Section 05-10-10 of the Gulfstream G500-5000 Aircraft
Maintenance Manual, Revision 36, dated March 15, 2022; and table 4
in Section 05-10-10 of the Gulfstream G550 Aircraft Maintenance
Manual, Revision 36, dated March 15, 2022.
Exact source excerpt. Text positions 8071–8848, end exclusive, in the original decoded publication. SHA-256: 2a413b7e15be50803ecec9f96b2161fce5bb21ff67e4d2ab2344b9f3943a680a
Alternative Methods of Compliance (AMOCs)
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Atlanta ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or responsible Flight Standards Office,
as appropriate. If sending information directly to the manager of
the certification office, send it to the attention of the person
identified in paragraph (i)(1) of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
Exact source excerpt. Text positions 8848–9523, end exclusive, in the original decoded publication. SHA-256: 57f1eded72562008b617a93100220b62f9d83d077659b5b3e25f72991cc6264b
Related Information
(i) Related Information
(1) For more information about this AD, contact Miral Patel,
Aerospace Engineer, Systems and Equipment Section, FAA, Atlanta ACO
Branch, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-
474-5590; email: [email protected].
(2) For service information identified in this AD that is not
incorporated by reference, contact Gulfstream Aerospace Corporation,
Technical Publications Dept., P.O. Box 2206, Savannah, GA 31402-
2206; phone: (800) 810-4853; email: [email protected]; website:
gulfstream.com/en/customer-support/. You may view this service
information at the FAA, Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des Moines, WA. For information
on the availability of this material at the FAA, call 206-231-3195.
Exact source excerpt. Text positions 9523–10324, end exclusive, in the original decoded publication. SHA-256: 163a6f52d83338d69e63d5254df9bffcced007c21ecb5f0578885b17c8b8bf60
Material Incorporated by Reference
(j) Material Incorporated by Reference
None.
Exact source excerpt. Text positions 10324–10375, end exclusive, in the original decoded publication. SHA-256: 9d583edbcf085b1fae94c8be8274ba3ce59b91db7bf15c5f5fd81fff2816eec7
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 2023-02-02 · 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: 9dd22a58efb90488f067b9052b4296d84c2e8a81da8ffc8ad1780e65bedb74a1. Source manifest: 3c8eeb692919b1ba58caebe7c02c1332b848ff78e9facedc4c1fa99632ed4810.
Official source · 2023-01-24
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 88, Number 15 (Tuesday, January 24, 2023)]
[Rules and Regulations]
[Pages 4080-4081]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-01164]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1305; Project Identifier AD-2022-00913-T;
Amendment 39-22309; AD 2023-02-02]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace Corporation
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Gulfstream Aerospace Corporation (Gulfstream) Model GV and GV-SP
airplanes. This AD was prompted by the omission of a life limit in the
airworthiness limitations section (ALS) of the maintenance manual for a
certain main landing gear (MLG) trunnion pin. This AD requires revising
the ALS of the existing instructions for continued airworthiness (ICA)
or inspection program for the airplane to establish a life limit for
the affected MLG trunnion pin. The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective February 28, 2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1305; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, any comments received, and other
information. The address for Docket Operations is 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: Miral Patel, Aerospace Engineer,
Systems and Equipment Section, FAA, Atlanta ACO Branch, 1701 Columbia
Avenue, College Park, GA 30337; phone: 404-474-5590; email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all Gulfstream Model GV
and GV-SP airplanes. The NPRM published in the Federal Register on
October 27, 2022 (87 FR 65018). The NPRM was prompted by a report
indicating a life limit for replacing MLG trunnion pin part number (P/
N) 1159SCL566-17 had been omitted from the ALS of the maintenance
manual for Model GV and GV-SP airplanes. Gulfstream revised the ALS for
the applicable airplanes to establish a life limit of 20,000 flight
cycles for the affected MLG trunnion pin. A trunnion pin remaining in
service beyond its life limit could lead to fracture and failure of the
trunnion pin. This condition, if not addressed, could result in MLG
failure and could lead to a runway excursion.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adopting this AD as proposed. Accordingly, the FAA is issuing
this AD to address the unsafe condition on these products. Except for
minor editorial changes, this AD is adopted as proposed in the NPRM.
None of the changes will increase the economic burden on any operator.
Other Related Service Information
The FAA reviewed Gulfstream GV Aircraft Maintenance Manual,
Revision 55, dated March 15, 2022; Gulfstream G550 Aircraft Maintenance
Manual, Revision 36, dated March 15, 2022; and Gulfstream G500-5000
Aircraft Maintenance Manual, Revision 36, dated March 15, 2022. The
service information adds a life limit for MLG trunnion pin P/N
1159SCL566-17.
Costs of Compliance
The FAA estimates that this AD affects 582 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost/airplane operators
----------------------------------------------------------------------------------------------------------------
Revise ALS............................ 1 work-hour x $85 = $85. N/A $85 $49,470
----------------------------------------------------------------------------------------------------------------
[[Page 4081]]
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.
The FAA is 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) Will not affect intrastate aviation in Alaska, 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
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 airworthiness
directive:
2023-02-02 Gulfstream Aerospace Corporation: Amendment 39-22309;
Docket No. FAA-2022-1305; Project Identifier AD-2022-00913-T.
(a) Effective Date
This airworthiness directive (AD) is effective February 28,
2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Gulfstream Aerospace Corporation Model GV and
GV-SP airplanes, all serial numbers, certificated in any category.
Note 1 to paragraph (c): Model GV-SP airplanes are also referred
to by the marketing designations G500, G550, and G500-5000.
(d) Subject
Joint Aircraft System Component (JASC) Code 3200, Landing Gear
System.
(e) Unsafe Condition
This AD was prompted by the omission of a life limit in the
airworthiness limitations section (ALS) for a certain main landing
gear (MLG) trunnion pin. The FAA is issuing this AD to prevent a MLG
trunnion pin from remaining in service beyond its life limit. This
unsafe condition, if not addressed, could result in MLG failure and
could lead to a runway excursion.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Incorporation of ALS Revisions
Within 12 months after the effective date of this AD, revise the
existing ALS of the instructions for continued airworthiness or
aircraft inspection program for your airplane by establishing a life
limit of 20,000 flight cycles for each MLG trunnion pin part number
(P/N) 1159SCL566-17.
Note 2 to paragraph (g): The life limit in paragraph (g) of this
AD is contained in table 5 in Section 05-10-10 of the Gulfstream V
Aircraft Maintenance Manual, Revision 55, dated March 15, 2022;
table 4 in Section 05-10-10 of the Gulfstream G500-5000 Aircraft
Maintenance Manual, Revision 36, dated March 15, 2022; and table 4
in Section 05-10-10 of the Gulfstream G550 Aircraft Maintenance
Manual, Revision 36, dated March 15, 2022.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Atlanta ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or responsible Flight Standards Office,
as appropriate. If sending information directly to the manager of
the certification office, send it to the attention of the person
identified in paragraph (i)(1) of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(i) Related Information
(1) For more information about this AD, contact Miral Patel,
Aerospace Engineer, Systems and Equipment Section, FAA, Atlanta ACO
Branch, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-
474-5590; email: [email protected].
(2) For service information identified in this AD that is not
incorporated by reference, contact Gulfstream Aerospace Corporation,
Technical Publications Dept., P.O. Box 2206, Savannah, GA 31402-
2206; phone: (800) 810-4853; email: [email protected]; website:
gulfstream.com/en/customer-support/. You may view this service
information at the FAA, Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des Moines, WA. For information
on the availability of this material at the FAA, call 206-231-3195.
(j) Material Incorporated by Reference
None.
Issued on January 18, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-01164 Filed 1-23-23; 8:45 am]
BILLING CODE 4910-13-P
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- 9dd22a58efb90488f067b9052b4296d84c2e8a81da8ffc8ad1780e65bedb74a1
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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.
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