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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


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:56:55.566903+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
ee3ed836170c49254db2f503bd42dc317fed2f0b31543fd8ff9ae9a9af2141e3
Text SHA-256
c0778e38b160af676ff966c82b6d2583787b2acf0f7ab195f9aa29a7ea5d6611

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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.