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
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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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