Back to publication catalog

Published 2005-01-06 · Federal Register document 05-284

Airworthiness Directives; Gulfstream Aerospace LP Model Gulfstream 100 Airplanes; and Model Astra SPX and 1125 Westwind Astra Series Airplanes

Publication summary

The FAA is adopting a new airworthiness directive (AD) for certain Gulfstream Aerospace LP Model Gulfstream 100 airplanes; and Model Astra SPX and 1125 Westwind Astra series airplanes. This AD requires adjusting the ground contact switches of the main landing gear. This AD is prompted by two occurrences of uncommanded deployments of the ground airbrakes during descent. We are issuing this AD to prevent a false "Ground" position signal, which could result in deployment of the ground airbrakes and reduced controllability of the airplane.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:17.300228+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2005-5d43d153038ee1c1
Source row
results[16]
Raw source SHA-256
5d43d153038ee1c1c214f5c3688e38e25e37b832227fe65d52f7420a65ee20f2

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2004-25-01
Effective date printed in this edition
2005-02-10
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This AD becomes effective February 10, 2005.

Exact source excerpt. Text positions 6556–6626, end exclusive, in the original decoded publication. SHA-256: a0c63a4eee0d43cde8724f313033f73515a02b113af3b4277a53e74a715eb3b7

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 6626–6655, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to Gulfstream Aerospace LP Model Gulfstream 
100 airplanes; and Model Astra SPX and 1125 Westwind Astra series 
airplanes; serial numbers 004 through 127 inclusive; certificated in 
any category.

Exact source excerpt. Text positions 6655–6891, end exclusive, in the original decoded publication. SHA-256: 1ca69d42c9a213b191ff25629ca9fd2f5241f86a1c9ef43f0c90b8cd6054852f

Unsafe Condition
Unsafe Condition

    (d) This AD was prompted by two occurrences of uncommanded 
deployments of the ground airbrakes during descent. We are issuing 
this AD to prevent a false ``Ground'' position signal, which could 
result in deployment of the ground airbrakes and reduced 
controllability of the airplane.

Exact source excerpt. Text positions 6891–7201, end exclusive, in the original decoded publication. SHA-256: 7d6a55ab1d387c7c9cd114dc8aaccf11fa160a4295e9d37dc5d48c5323ab3209

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 7201–7379, end exclusive, in the original decoded publication. SHA-256: 64a7a1579f37f56eafecd0aeb3c528e7c89f6292ed0cb53091423917642d5847

Corrective Action
Corrective Action

    (f) Within 250 flight hours after the effective date of this AD, 
adjust the ground contact switches of the left and right main 
landing gear, in accordance with the Accomplishment Instructions of 
Gulfstream Alert Service Bulletin 1125-32A-233, Revision 1, dated 
August 1, 2003. Although the service bulletin referenced in this AD 
specifies to submit certain information to the manufacturer, this AD 
does not include that requirement.

Exact source excerpt. Text positions 7379–7842, end exclusive, in the original decoded publication. SHA-256: d6b365f1e707f74ef62348e4c6433b27db7522679afca48c78ab46d5ef64000f

Alternative Methods of Compliance (AMOCs)
Alternative Methods of Compliance (AMOCs)

    (g) The Manager, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, has the authority to approve AMOCs for 
this AD, if requested in accordance with the procedures found in 14 
CFR 39.19.

Exact source excerpt. Text positions 7842–8096, end exclusive, in the original decoded publication. SHA-256: 388d94c6a00925c9400ac4e74157a44ddf33122e52ba6883359f64c0412bd168

Related Information
Related Information

    (h) Israeli airworthiness directive 32-03-08-05, dated September 
4, 2003, also addresses the subject of this AD.

Exact source excerpt. Text positions 8096–8236, end exclusive, in the original decoded publication. SHA-256: 5970e54ebfc83f67a7c4e2f8d387dca75834cc0e7a58e1482f71046367fa291e

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use Gulfstream Alert Service Bulletin 1125-32A-233, 
Revision 1, dated August 1, 2003, to perform the actions that are 
required by this AD, unless the AD specifies otherwise. The Director 
of the Federal Register approves the incorporation by reference of 
this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. 
For copies of the service information, contact Gulfstream Aerospace 
Corporation, P.O. Box 2206, Mail Station D-25, Savannah, Georgia 
31402. For information on the availability of this material at the 
National Archives and Records Administration (NARA), call (202) 741-
6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. You may view the AD docket 
at the Docket Management Facility, U.S. Department of 
Transportation, 400 Seventh Street SW., room PL-401, Nassif 
Building, Washington, DC.


[[Page 1182]]

Exact source excerpt. Text positions 8236–9178, end exclusive, in the original decoded publication. SHA-256: 4cb952b07c357937fa62cede6bf9c4e8bd7d746f95f2dd92017a955a05e32fc5

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 2004-25-01 · 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: 798d9441dba6f069beb8d0cb0f3667ae54e55ea6eb9f7f903e596453c071756c. Source manifest: b15629e52bc7cb51391308fcc34a0d202346ea57723424bc61c281fa67e2afab.

Official source · 2005-01-06

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 70, Number 4 (Thursday, January 6, 2005)]
[Rules and Regulations]
[Pages 1180-1182]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-284]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19138; Directorate Identifier 2004-NM-102-AD; 
Amendment 39-13888; AD 2004-25-01]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Aerospace LP Model 
Gulfstream 100 Airplanes; and Model Astra SPX and 1125 Westwind Astra 
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 Gulfstream Aerospace LP Model Gulfstream 100 airplanes; and 
Model Astra SPX and 1125 Westwind Astra series airplanes. This AD 
requires adjusting the ground contact switches of the main landing 
gear. This AD is prompted by two occurrences of uncommanded deployments 
of the ground airbrakes during descent. We are issuing this AD to 
prevent a false ``Ground'' position signal, which could result in 
deployment of the ground airbrakes and reduced controllability of the 
airplane.

DATES: This AD becomes effective February 10, 2005.
    The incorporation by reference of a certain publication listed in 
the AD is approved by the Director of the Federal Register as of 
February 10, 2005.

ADDRESSES: For service information identified in this AD, contact 
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25, 
Savannah, Georgia 31402. You can examine this information 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: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
    Docket: The AD docket contains the proposed AD, comments, and any 
final disposition. You can examine the 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 U.S. 
Department of Transportation, 400 Seventh Street SW., room PL-401,

[[Page 1181]]

Washington, DC. This docket number is FAA-2004-19138; the directorate 
identifier for this docket is 2004-NM-102-AD.

FOR FURTHER INFORMATION CONTACT:
    Technical information: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2125; fax (425) 227-1149.
    Plain language information: Marcia Walters, [email protected].

SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 
with an AD for certain Gulfstream Aerospace LP Model Gulfstream 100 
airplanes; and Model Astra SPX and 1125 Westwind Astra series 
airplanes. That action, published in the Federal Register on October 4, 
2004 (69 FR 59147), proposed to require adjusting the ground contact 
switches of the main landing gear.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. No comments have been submitted on the proposed 
AD or on the determination of the cost to the public.

Conclusion

    We have carefully reviewed the available data and determined that 
air safety and the public interest require adopting the AD as proposed.

Costs of Compliance

    This AD will affect about 106 airplanes of U.S. registry. The 
actions will take about 3 work hours per airplane, at an average labor 
rate of $65 per work hour. Based on these figures, the estimated cost 
of the AD for U.S. operators is $20,670, or $195 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.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this AD. See the ADDRESSES section for a location to 
examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, 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 airworthiness 
directive (AD):

2004-25-01 Gulfstream Aerospace LP (Formerly Israel Aircraft 
Industries, Ltd.): Amendment 39-13888. Docket No. FAA-2004-19138; 
Directorate Identifier 2004-NM-102-AD.

Effective Date

    (a) This AD becomes effective February 10, 2005.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Gulfstream Aerospace LP Model Gulfstream 
100 airplanes; and Model Astra SPX and 1125 Westwind Astra series 
airplanes; serial numbers 004 through 127 inclusive; certificated in 
any category.

Unsafe Condition

    (d) This AD was prompted by two occurrences of uncommanded 
deployments of the ground airbrakes during descent. We are issuing 
this AD to prevent a false ``Ground'' position signal, which could 
result in deployment of the ground airbrakes and reduced 
controllability of the airplane.

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.

Corrective Action

    (f) Within 250 flight hours after the effective date of this AD, 
adjust the ground contact switches of the left and right main 
landing gear, in accordance with the Accomplishment Instructions of 
Gulfstream Alert Service Bulletin 1125-32A-233, Revision 1, dated 
August 1, 2003. Although the service bulletin referenced in this AD 
specifies to submit certain information to the manufacturer, this AD 
does not include that requirement.

Alternative Methods of Compliance (AMOCs)

    (g) The Manager, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, has the authority to approve AMOCs for 
this AD, if requested in accordance with the procedures found in 14 
CFR 39.19.

Related Information

    (h) Israeli airworthiness directive 32-03-08-05, dated September 
4, 2003, also addresses the subject of this AD.

Material Incorporated by Reference

    (i) You must use Gulfstream Alert Service Bulletin 1125-32A-233, 
Revision 1, dated August 1, 2003, to perform the actions that are 
required by this AD, unless the AD specifies otherwise. The Director 
of the Federal Register approves the incorporation by reference of 
this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. 
For copies of the service information, contact Gulfstream Aerospace 
Corporation, P.O. Box 2206, Mail Station D-25, Savannah, Georgia 
31402. For information on the availability of this material at the 
National Archives and Records Administration (NARA), call (202) 741-
6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. You may view the AD docket 
at the Docket Management Facility, U.S. Department of 
Transportation, 400 Seventh Street SW., room PL-401, Nassif 
Building, Washington, DC.


[[Page 1182]]


    Issued in Renton, Washington, on December 29, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-284 Filed 1-5-05; 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 2026-10-09T03:59:38.640997+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
c06f13d92f7c8943985f4e9d393c34dbb445dc92ace3329ba8dc710e8c769224
Text SHA-256
798d9441dba6f069beb8d0cb0f3667ae54e55ea6eb9f7f903e596453c071756c

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.