Published 2013-02-19 · Federal Register document 2013-03403
Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for all Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Model Gulfstream G150 airplanes. This AD was prompted by a review that determined that the runway slope and anti-ice corrections to V<INF>1</INF> and take-off distances in the Gulfstream G150 Airplane Flight Manual (AFM) were presented in a non-conservative manner. This AD requires revising the performance section of the AFM to include procedures to advise the flightcrew of certain runway slope and anti-ice corrections and take-off distance values. We are issuing this AD to prevent the use of published non-conservative data, which could result in the inability to meet the required take-off performance, with consequent hazard to safe operation during performance-limited take-off operations.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
- Source row
- results[59]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2013-03-23
- Effective date printed in this edition
- 2013-03-26
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective March 26,
2013.
Exact source excerpt. Text positions 7473–7567, end exclusive, in the original decoded publication. SHA-256: 3fb6c2a11909e9fdefa7d8ef3b83f0c301bb48b525c923fdc069c10ce6751920
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 7567–7596, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Gulfstream Aerospace LP (Type Certificate
previously held by Israel Aircraft Industries, Ltd.) Model
Gulfstream G150 airplanes; certificated in any category; all serial
numbers.
Exact source excerpt. Text positions 7596–7820, end exclusive, in the original decoded publication. SHA-256: 236159dfa1dafeda4ac2ac7e422ed7a9921c0898a1f1fd08350c01ab21716ba1
Subject
(d) Subject
Air Transport Association (ATA) of America Code 01, Operations
information.
Exact source excerpt. Text positions 7820–7915, end exclusive, in the original decoded publication. SHA-256: e5b58637387b38c3cd167121cf79e8d09961fba179040f69089055b0f0b46ab4
Reason
(e) Reason
This AD was prompted by a review that determined that the runway
slope and anti-ice corrections to V<INF>1</INF> and take-off
distances in the G150 Airplane Flight Manual (AFM) were presented in
a non-conservative manner. We are issuing this AD to prevent the use
of published non-conservative data, which could result in the
inability to meet the required take-off performance, with consequent
hazard to safe operation during performance-limited take-off
operations.
Exact source excerpt. Text positions 7915–8407, end exclusive, in the original decoded publication. SHA-256: be32e8246cf9f641cd11ad1212f2e3b28e1b842a8fadfa19ff79f19db407543e
Compliance
(f) Compliance
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 8407–8585, end exclusive, in the original decoded publication. SHA-256: af3956da952ca797ed39bc4b318e4356f7014ac5b4c12bda0147d37f1ffa6cb8
AFM Revision
(g) AFM Revision
Within 60 days after the effective date of this AD, revise
Section V, Performance, of the Gulfstream G150 AFM to include the
information in Gulfstream G150 Temporary Revision (TR) 3, dated
December 14, 2011. This TR introduces corrections for runway slope.
Operate the airplane according to the procedures in this TR.
Note 1 to paragraph (g) of this AD: The AFM revision required
by paragraph (g) of this AD may be done by inserting copies of
Gulfstream G150 TR 3, dated December 14, 2011, in the AFM. When this
TR has been included in general revisions of the AFM, the general
revisions may be inserted in the AFM, provided the relevant
information in the general revision is identical to that in
Gulfstream G150 TR 3, dated December 14, 2011, and the TR may be
removed.
Exact source excerpt. Text positions 8585–9397, end exclusive, in the original decoded publication. SHA-256: ae40d3df94d7a1a163951da98025bdf8de0820112a8c0a8baa1a5e7cd1b5686e
Other FAA AD Provisions
(h) Other FAA AD Provisions
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. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to ATTN: Tom Groves,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-
3356; telephone 425-227-1503; fax 425-227-1149. Information may be
emailed to: [email protected]. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the local flight
standards district office/certificate holding district office. The
AMOC approval letter must specifically reference this AD.
(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.
Exact source excerpt. Text positions 9397–10839, end exclusive, in the original decoded publication. SHA-256: 7779411a696ecbaacce9ff0faf1ef131ad0fde3a357c96857c2b716b5ab94dfd
Special Flight Permits
(i) Special Flight Permits
Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
Exact source excerpt. Text positions 10839–11029, end exclusive, in the original decoded publication. SHA-256: fcf4614d7210cd903b18985adfea6dee1a88f4a3dba31b999e58f95459295c8b
Related Information
(j) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Israeli Airworthiness Directive 01-12-02-02, dated March 2, 2012;
and Gulfstream G150 TR 3, dated December 14, 2011, to Section V,
Performance, of the Gulfstream G150 AFM; for related information.
Exact source excerpt. Text positions 11029–11322, end exclusive, in the original decoded publication. SHA-256: 84913114808d5848fe127e17f881547e775b2352296ad6cc1533c5054005f771
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Gulfstream G150 Temporary Revision 3, dated December 14,
2011, to Section V, Performance, of the Gulfstream G150 Airplane
Flight Manual.
(ii) Reserved.
(3) For service information identified in this AD, contact
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25,
Savannah, GA 31402-2206; telephone 800-810-4853; fax 912-965-3520;
email [email protected]; Internet http://www.gulfstream.com/product_support/technical_pubs/pubs/index.htm.
(4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA.
For information on the availability of this material at the FAA,
call 425-227-1221.
(5) You may view this service information that is incorporated
by reference 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 11322–12679, end exclusive, in the original decoded publication. SHA-256: 441920b7c101376dff9e1a10078917bba6af1221bf1450196b8358bef6e82050
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 2013-03-23 · 1 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: c0778e38b160af676ff966c82b6d2583787b2acf0f7ab195f9aa29a7ea5d6611. Source manifest: 47f4d5060d0a47e669e9e03362241f257989668f99fa2751dff7092a1a6ef7ed.
Official source · 2013-02-19
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 78, Number 33 (Tuesday, February 19, 2013)]
[Rules and Regulations]
[Pages 11567-11568]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-03403]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0986; Directorate Identifier 2012-NM-077-AD;
Amendment 39-17357; AD 2013-03-23]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP (Type
Certificate Previously Held by Israel Aircraft Industries, Ltd.)
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Gulfstream Aerospace LP (Type Certificate Previously Held by Israel
Aircraft Industries, Ltd.) Model Gulfstream G150 airplanes. This AD was
prompted by a review that determined that the runway slope and anti-ice
corrections to V<INF>1</INF> and take-off distances in the Gulfstream
G150 Airplane Flight Manual (AFM) were presented in a non-conservative
manner. This AD requires revising the performance section of the AFM to
include procedures to advise the flightcrew of certain runway slope and
anti-ice corrections and take-off distance values. We are issuing this
AD to prevent the use of published non-conservative data, which could
result in the inability to meet the required take-off performance, with
consequent hazard to safe operation during performance-limited take-off
operations.
DATES: This AD becomes effective March 26, 2013.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 26,
2013.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.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: Tom Groves, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1503;
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 September 20, 2012
(77 FR 58323). That NPRM proposed to correct an unsafe condition for
the specified products. The Mandatory Continuing Airworthiness
Information (MCAI) states:
This [Israeli] AD mandates revised limitations in the G150 AFM,
pertaining to the Performance Section. Each operator must
incorporate Temporary Rev. 3 to the G150 AFM.
The unsafe condition is the use of published non-conservative data,
which could result in the inability to meet the required take-off
performance, with consequent hazard to safe operation during
performance-limited take-off operations. 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 (77 FR 58323, September
20, 2012) 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 except for
minor editorial changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 58323, September 20, 2012) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 58323, September 20, 2012).
Costs of Compliance
We estimate that this AD will affect 56 products of U.S. registry.
We also estimate that it will take about 1 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Based on these figures, we estimate the cost of
this AD to the U.S. operators to be $4,760, or $85 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
[[Page 11568]]
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 the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. 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://www.regulations.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 (77 FR 58323, September 20,
2012), 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
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:
2013-03-23 Gulfstream Aerospace LP (Type Certificate Previously Held
by Israel Aircraft Industries, Ltd.): Amendment 39-17357. Docket No.
FAA-2012-0986; Directorate Identifier 2012-NM-077-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective March 26,
2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Gulfstream Aerospace LP (Type Certificate
previously held by Israel Aircraft Industries, Ltd.) Model
Gulfstream G150 airplanes; certificated in any category; all serial
numbers.
(d) Subject
Air Transport Association (ATA) of America Code 01, Operations
information.
(e) Reason
This AD was prompted by a review that determined that the runway
slope and anti-ice corrections to V<INF>1</INF> and take-off
distances in the G150 Airplane Flight Manual (AFM) were presented in
a non-conservative manner. We are issuing this AD to prevent the use
of published non-conservative data, which could result in the
inability to meet the required take-off performance, with consequent
hazard to safe operation during performance-limited take-off
operations.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) AFM Revision
Within 60 days after the effective date of this AD, revise
Section V, Performance, of the Gulfstream G150 AFM to include the
information in Gulfstream G150 Temporary Revision (TR) 3, dated
December 14, 2011. This TR introduces corrections for runway slope.
Operate the airplane according to the procedures in this TR.
Note 1 to paragraph (g) of this AD: The AFM revision required
by paragraph (g) of this AD may be done by inserting copies of
Gulfstream G150 TR 3, dated December 14, 2011, in the AFM. When this
TR has been included in general revisions of the AFM, the general
revisions may be inserted in the AFM, provided the relevant
information in the general revision is identical to that in
Gulfstream G150 TR 3, dated December 14, 2011, and the TR may be
removed.
(h) Other FAA AD Provisions
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. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to ATTN: Tom Groves,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-
3356; telephone 425-227-1503; fax 425-227-1149. Information may be
emailed to: [email protected]. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the local flight
standards district office/certificate holding district office. The
AMOC approval letter must specifically reference this AD.
(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.
(i) Special Flight Permits
Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
(j) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Israeli Airworthiness Directive 01-12-02-02, dated March 2, 2012;
and Gulfstream G150 TR 3, dated December 14, 2011, to Section V,
Performance, of the Gulfstream G150 AFM; for related information.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Gulfstream G150 Temporary Revision 3, dated December 14,
2011, to Section V, Performance, of the Gulfstream G150 Airplane
Flight Manual.
(ii) Reserved.
(3) For service information identified in this AD, contact
Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D-25,
Savannah, GA 31402-2206; telephone 800-810-4853; fax 912-965-3520;
email [email protected]; Internet http://www.gulfstream.com/product_support/technical_pubs/pubs/index.htm.
(4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA.
For information on the availability of this material at the FAA,
call 425-227-1221.
(5) You may view this service information that is incorporated
by reference 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 February 7, 2013.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-03403 Filed 2-15-13; 8:45 am]
BILLING CODE 4910-13-P
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- Text SHA-256
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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.