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Published 2007-08-28 · Federal Register document E7-16655

Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy Airplanes and Model Gulfstream 200 Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:23.906952+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2007-daaa03e810180273
Source row
results[315]
Raw source SHA-256
daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2007-17-16
Effective date printed in this edition
2007-10-02
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This airworthiness directive (AD) becomes effective October 
2, 2007.

Exact source excerpt. Text positions 8179–8274, end exclusive, in the original decoded publication. SHA-256: 306a92164e7895aa14de3b67c90829fafb1ad509b6628a5ed44ca3ed93e66878

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 8274–8303, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to Gulfstream Model Galaxy airplanes and 
Model Gulfstream 200 airplanes, serial numbers 101 through 104, 109, 
110, and 118, certificated in any category.

Exact source excerpt. Text positions 8303–8499, end exclusive, in the original decoded publication. SHA-256: bd5ce3447e04f36ec6e6643aa0cde4736486a35f303da7efd49008d75c7cb16a

Subject
Subject

    (d) Air Transport Association (ATA) of America Code 21: Air 
Conditioning.

Exact source excerpt. Text positions 8499–8588, end exclusive, in the original decoded publication. SHA-256: fd79c1b49743a5eaefec1ae6baa2f7b90b4257646b4d37c6d81958aa6918f3c5

Reason
Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:

    During the manufacturing process of the Poppet Covers of the 
Pressurization Safety Valves, burrs that could damage the Valve 
Diaphragms were not removed. The damage may eventually cause faulty 
operation of the relief valves resulting in an unsafe condition when 
combined with additional failures. The serial numbers of the 
defective valves and the affected aircraft were identified.

The unsafe condition is damage and subsequent failure of the safety 
relief valves, which could result in rapid decompression of the 
airplane. The corrective action includes replacing the 
pressurization safety valve, part number 103842-3.

Exact source excerpt. Text positions 8588–9307, end exclusive, in the original decoded publication. SHA-256: 7fd9a9bf71441e6ab2fba3981806f407146f6cc752c9d88e7cd2cdb3847d76e5

Actions and Compliance
Actions and Compliance

    (f) Unless already done, do the following actions. Within 500 
flight hours or 12 months after the effective date of this AD, 
whichever occurs first: Replace the pressurization safety valve, 
part number 103842-3, according to Gulfstream Service Bulletin 200-
21-308, dated February 23, 2007.

FAA AD Differences

    Note: This AD differs from the MCAI and/ or service information 
as follows: No differences.

Exact source excerpt. Text positions 9307–9748, end exclusive, in the original decoded publication. SHA-256: 05b8f11aeb1e81dd2cb67e6a8bf4c5e9f38e068e986b71d9ee042109220cf1bf

Other FAA AD Provisions
Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. Send information to ATTN: Mike 
Borfitz, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
Washington 98057-3356; telephone (425) 227-2677; fax (425) 227-1149. 
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.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in 
this AD, under the provisions of the Paperwork Reduction Act, the 
Office of Management and Budget (OMB) has approved the information 
collection requirements and has assigned OMB Control Number 2120-
0056.

Exact source excerpt. Text positions 9748–11174, end exclusive, in the original decoded publication. SHA-256: 2943c82eff31b90f3d19c4995a444a206b4ed913b525d08d1a556927799839e0

Related Information
Related Information

    (h) Refer to MCAI Israeli Airworthiness Directive 21-07-01-01, 
dated February 20, 2007; and Gulfstream Service Bulletin 200-21-308, 
dated February 23, 2007; and Honeywell Service Bulletin 103842-21-
4126, dated December 5, 2006; for related information.

Exact source excerpt. Text positions 11174–11456, end exclusive, in the original decoded publication. SHA-256: 9f3c7aaaec2c12efd45d698beab066b8edf4854273e448eb02371a0a864dd16e

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use Gulfstream Service Bulletin 200-21-308, dated 
February 23, 2007, 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 
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25, 
Savannah, Georgia 31402-2206.

[[Page 49172]]

    (3) You may review copies 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 11456–12331, end exclusive, in the original decoded publication. SHA-256: d071c5f5c785b6af46b7bf346bac42bd21008f695313b1d0adcec9c00b8f43f2

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 2007-17-16 · 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: 968db27e34d50b6213412948de1cfb38dd7745925da86151f0c0d196d3d25ff5. Source manifest: c892194b213215f05ee03c79cadc8905f13e1a5789b7a19bab1679ec35c8ac90.

Official source · 2007-08-28

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 72, Number 166 (Tuesday, August 28, 2007)]
[Rules and Regulations]
[Pages 49170-49172]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-16655]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28353; Directorate Identifier 2007-NM-065-AD; 
Amendment 39-15174; AD 2007-17-16]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy 
Airplanes and Model Gulfstream 200 Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) originated by an aviation authority of 
another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as:

    During the manufacturing process of the Poppet Covers of the 
Pressurization Safety Valves, burrs that could damage the Valve 
Diaphragms were not removed. The damage may eventually cause faulty 
operation of the relief valves resulting in an unsafe condition when 
combined with additional failures. The serial numbers of the 
defective valves and the affected aircraft were identified.

The unsafe condition is damage and subsequent failure of the safety 
relief valves, which could result in rapid decompression of the 
airplane. We are issuing this AD to require actions to correct the 
unsafe condition on these products.

DATES: This AD becomes effective October 2, 2007.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 2, 
2007.

ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the U.S. Department of Transportation, 
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 
New Jersey Avenue SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 
227-2677; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on June 6, 2007 (72 FR 
31204). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    During the manufacturing process of the Poppet Covers of the 
Pressurization Safety Valves, burrs that could damage the Valve 
Diaphragms were not removed. The damage may eventually cause faulty 
operation of the relief valves resulting in an unsafe condition when 
combined with additional failures. The serial numbers of the 
defective valves and the affected aircraft were identified.

The unsafe condition is damage and subsequent failure of the safety 
relief valves, which could result in rapid decompression of the 
airplane. The corrective action includes replacing the pressurization 
safety valve, part number 103842-3. You may obtain further information 
by examining the MCAI in the AD docket.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

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

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in 
general, agree with their substance. But we might have found it 
necessary to use different words from those in the MCAI to ensure the 
AD is clear for U.S. operators and is enforceable. In making these 
changes, we do not intend to differ substantively from the information 
provided in the MCAI and related service information.

    We might also have required different actions in this AD from those 
in the MCAI in order to follow our FAA policies. Any such differences 
are highlighted in a NOTE within the AD.

Costs of Compliance

    Based on the service information, we estimate that this AD affects 
about 7 products of U.S. registry. We also estimate that it takes about 
10 work-hours per product to comply with the basic requirements of this 
AD. The

[[Page 49171]]

average labor rate is $80 per work-hour. Required parts cost about $0 
per product. Where the service information lists required parts costs 
that are covered under warranty, we have assumed that there will be no 
charge for these costs. As we do not control warranty coverage for 
affected parties, some parties may incur costs higher than estimated 
here. Based on these figures, we estimate the cost of the AD on U.S. 
operators to be $5,600, or $800 per product.

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 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 this AD:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this AD and placed it in the AD docket.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://dms.dot.gov; or in person at the Docket Operations office between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD 
docket contains the NPRM, the regulatory evaluation, any comments 
received, and other information. The street address for the Docket 
Operations office (telephone (800) 647-5527) is in the ADDRESSES 
section. Comments will be available in the AD docket shortly after 
receipt.

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:

2007-17-16 Gulfstream Aerospace LP (Formerly Israel Aircraft 
Industries, Ltd.): Amendment 39-15174. Docket No. FAA-2007-28353; 
Directorate Identifier 2007-NM-065-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective October 
2, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Gulfstream Model Galaxy airplanes and 
Model Gulfstream 200 airplanes, serial numbers 101 through 104, 109, 
110, and 118, certificated in any category.

Subject

    (d) Air Transport Association (ATA) of America Code 21: Air 
Conditioning.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:

    During the manufacturing process of the Poppet Covers of the 
Pressurization Safety Valves, burrs that could damage the Valve 
Diaphragms were not removed. The damage may eventually cause faulty 
operation of the relief valves resulting in an unsafe condition when 
combined with additional failures. The serial numbers of the 
defective valves and the affected aircraft were identified.

The unsafe condition is damage and subsequent failure of the safety 
relief valves, which could result in rapid decompression of the 
airplane. The corrective action includes replacing the 
pressurization safety valve, part number 103842-3.

Actions and Compliance

    (f) Unless already done, do the following actions. Within 500 
flight hours or 12 months after the effective date of this AD, 
whichever occurs first: Replace the pressurization safety valve, 
part number 103842-3, according to Gulfstream Service Bulletin 200-
21-308, dated February 23, 2007.

FAA AD Differences

    Note: This AD differs from the MCAI and/ or service information 
as follows: No differences.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. Send information to ATTN: Mike 
Borfitz, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
Washington 98057-3356; telephone (425) 227-2677; fax (425) 227-1149. 
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.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in 
this AD, under the provisions of the Paperwork Reduction Act, the 
Office of Management and Budget (OMB) has approved the information 
collection requirements and has assigned OMB Control Number 2120-
0056.

Related Information

    (h) Refer to MCAI Israeli Airworthiness Directive 21-07-01-01, 
dated February 20, 2007; and Gulfstream Service Bulletin 200-21-308, 
dated February 23, 2007; and Honeywell Service Bulletin 103842-21-
4126, dated December 5, 2006; for related information.

Material Incorporated by Reference

    (i) You must use Gulfstream Service Bulletin 200-21-308, dated 
February 23, 2007, 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 
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25, 
Savannah, Georgia 31402-2206.

[[Page 49172]]

    (3) You may review copies 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on August 14, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E7-16655 Filed 8-27-07; 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 2026-10-09T03:36:31.546621+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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a3013e52c47b4b06657a6aa7d3aad8b213d48b3bf90c4e3ccc69f58415b82d35
Text SHA-256
968db27e34d50b6213412948de1cfb38dd7745925da86151f0c0d196d3d25ff5

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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.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.