Document ID: FAA-2020-0199-0001
Agency: faa
Document Type: Rule
Title: Airworthiness Directives: Gulfstream Aerospace Corporation Airplanes
Posted Date: 2020-03-13T04:00Z

[Federal Register Volume 85, Number 50 (Friday, March 13, 2020)]
[Rules and Regulations]
[Pages 14562-14565]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-05242]

[[Page 14562]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0199; Product Identifier 2020-NM-035-AD; Amendment 
39-19860; AD 2020-05-12]
RIN 2120-AA64

Airworthiness Directives; Gulfstream Aerospace Corporation 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Gulfstream Aerospace Corporation Model GVII-G500 and GVII-G600 
airplanes. This AD requires revising the airplane flight manual (AFM) 
for your airplane to incorporate revised limitations and procedures. 
This AD was prompted by a report of a landing incident where the alpha 
limiter engaged in the landing flare in unstable air while on the 
approach, resulting in a high rate of descent landing and damage to the 
airplane. The FAA is issuing this AD to address the unsafe condition on 
these products.

DATES: This AD is effective March 13, 2020.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of March 13, 
2020.
    The FAA must receive comments on this AD by April 27, 2020.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this final rule, contact 
Gulfstream Aerospace Corporation, Technical Publications Dept., P.O. 
Box 2206, Savannah, GA 31402-2206; telephone 800-810-4853; fax 912-965-
3520; email pubs@gulfstream.com; internet https://www.gulfstream.com/customer-support. You may view this service information at the FAA, 
Policy and Innovation Division, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the FAA, 
call 816-329-4148. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0199.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0199; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The street address for Docket Operations is listed 
above. Comments will be available in the AD docket shortly after 
receipt.

FOR FURTHER INFORMATION CONTACT: Myles Jalalian, Aerospace Engineer, 
Systems and Equipment Section, FAA, Atlanta ACO Branch, 1701 Columbia 
Avenue, College Park, GA 30337; phone: 404-474-5572; fax: 404-474-5606; 
email: Myles.Jalalian@faa.gov.

SUPPLEMENTARY INFORMATION: 

Discussion

    The FAA has received a report of a Gulfstream Model GVII-G500 
airplane that was involved in a landing incident where the alpha (angle 
of attack) limiter engaged during the landing flare in unstable air. 
The engagement of the alpha limiter resulted in insufficient nose-up 
authority to control the descent rate at touchdown even though the 
sidestick was in the full aft position. The airplane landed in a 900-
feet-per-minute descent, with resulting damage to the airplane. The 
flight control system alpha limiter can engage even when the airplane 
is not near a critical angle of attack and limit the pilot's pitch 
authority in the flare, resulting in a landing at a high rate of 
descent. Unstable air, combined with rapid, large, and alternating 
pitch commands, contributes to the alpha limiter engaging at an 
inappropriate time, possibly resulting in a high rate of descent 
contact with the runway and loss of control of the airplane as a result 
of a hard landing. To address this issue, the FAA is requiring 
revisions to be made to the AFM for your airplane. The revised AFM 
limits the maximum crosswind component for landing, and also increases 
the normal approach speeds, based on steady-state winds and wind gusts. 
These new and revised operating limitations and revised landing 
procedures minimize the possibility of unintended alpha limiter 
engagement thereby minimizing the possibility of reduced pilot flight 
control authority during the landing flare.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed following service information, which has been 
revised to provide new and revised operating limitations and flight 
control and landing procedures in strong winds and gusty conditions.
    Gulfstream GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-
0001, Revision 5, dated March 3, 2020.
     Step 3., ``Wind Conditions,'' of Section 01-02-10, 
``Runway, Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS.''
     Step 15., ``Approach Speed,'' of Section 01-03-40, 
``Airspeed Limitations,'' of Chapter 01, ``LIMITATIONS.''
     Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS.''
     Step 5., Section 01-34-40, ``Takeoff and Landing Data 
(TOLD),'' of Chapter 01, ``LIMITATIONS.''
     ``WARNING,'' preceding Step 4. of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS.''
     Step 11., ``Landing,'' of Section 03-12-10, ``Zero Flaps 
or Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES.''
     Step 8., ``Final Approach Fix,'' of Section 04-08-40, 
``One Engine Inoperative Landing Procedure,'' of Chapter 04, 
``EMERGENCY PROCEDURES.''
     Step 1, ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE FAA BASELINE.''
     Step 1, ``Introduction,'' of Section 5A-11-10, ``Threshold 
Speeds,'' of Chapter 5A, ``PERFORMANCE (ASC 022).''
    Gulfstream GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-
0001, Revision 3, dated March 3, 2020.
     Step 3., ``Wind Conditions,'' of Section 01-02-10, 
``Runway, Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS.''
     Step 15., ``Approach Speed,'' of Section 01-03-40, 
``Airspeed Limitations,'' of Chapter 01, ``LIMITATIONS.''
     Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS.''
     Steps 3. and 4., Section 01-34-40, ``Takeoff and Landing 
Data (TOLD),'' of Chapter 01, ``LIMITATIONS.''

[[Page 14563]]

     ``WARNING,'' preceding Step 4., of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS.''
     Step 11., ``Landing,'' of Section 03-12-10, ``Zero Flaps 
or Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES.''
     Step 8.,'' ``Final Approach Fix,'' of Section 04-08-40, 
``One Engine Inoperative Landing Procedure,'' of Chapter 04, 
``EMERGENCY PROCEDURES.''
     Step 1, ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE.''
     Step 1, ``Introduction,'' of Section 05-11-20, ``Tire 
Speed and BKE Limited Maximum Landing Weight,'' of Chapter 05, 
``PERFORMANCE.''
    These documents are distinct because they apply to different 
airplane models. This service information is reasonably available 
because the interested parties have access to it through their normal 
course of business or by the means identified in the ADDRESSES section.

FAA's Determination

    The FAA is issuing this AD because the agency evaluated all the 
relevant information and determined the unsafe condition described 
previously is likely to exist or develop in other products of the same 
type design.

AD Requirements

    This AD requires revising the AFM for your airplane to incorporate 
revised limitations and procedures. Specific revisions must be made to 
the sections of the applicable AFM described previously.
    This AD specifies that the owner/operator (pilot) may revise the 
AFM. Revising an AFM is not considered a maintenance action that must 
be performed by a certified person as specified in 14 CFR 43.3 and may 
be done by a pilot holding at least a private pilot certificate. This 
action must be recorded in the aircraft maintenance records to show 
compliance with this AD.

Interim Action

    The FAA considers this AD interim action. The manufacturer is 
currently developing a modification that will address the unsafe 
condition identified in this AD. Once this modification is developed, 
approved, and available, the FAA might consider additional rulemaking.

Justification for Immediate Adoption and Determination of the Effective 
Date

    Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 
U.S.C.) authorizes agencies to dispense with notice and comment 
procedures for rules when the agency, for ``good cause,'' finds that 
those procedures are ``impracticable, unnecessary, or contrary to the 
public interest.'' Under this section, an agency, upon finding good 
cause, may issue a final rule without seeking comment prior to the 
rulemaking. Similarly, Section 553(d) of the APA authorizes agencies to 
make rules effective in less than thirty days, upon a finding of good 
cause.
    An unsafe condition exists that requires the immediate adoption of 
this AD without providing an opportunity for public comments prior to 
adoption. The FAA has found that the risk to the flying public 
justifies foregoing notice and comment prior to adoption of this rule 
because, as described in the Discussion section of this AD, 
inappropriate alpha limiter engagement during the landing flare limits 
the pilot's pitch authority during a critical phase of flight near the 
ground, and could result in a landing at a high rate of descent and the 
possible consequent loss of control of the airplane. Given the 
significance of the risk presented by this unsafe condition, it must be 
immediately addressed.
    Accordingly, notice and opportunity for prior public comment are 
impracticable pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the 
reasons stated above, the FAA finds that good cause exists pursuant to 
5 U.S.C. 553(d) for making this amendment effective in less than 30 
days.

Regulatory Flexibility Act (RFA)

    The requirements of the RFA do not apply when an agency finds good 
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and 
comment. Because the FAA has determined that it has good cause to adopt 
this rule without notice and comment, RFA analysis is not required.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety and was not preceded by notice and an opportunity for public 
comment. However, the FAA invites you to send any written data, views, 
or arguments about this final rule. Send your comments to an address 
listed under the ADDRESSES section. Include the docket number FAA-2020-
0199 and Product Identifier 2020-NM-035-AD at the beginning of your 
comments. The FAA specifically invites comments on the overall 
regulatory, economic, environmental, and energy aspects of this final 
rule. The FAA will consider all comments received by the closing date 
and may amend this final rule because of those comments.
    The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide. 
The FAA will also post a report summarizing each substantive verbal 
contact received about this final rule.

Costs of Compliance

    The FAA estimates that this AD affects 62 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
AFM revision..........................  1 work-hour x $85 per                 $0             $85          $5,270
                                         hour = $85.
----------------------------------------------------------------------------------------------------------------

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.
    The FAA is 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.

[[Page 14564]]

Regulatory Findings

    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, and
    (2) Will not affect intrastate aviation in Alaska.

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 airworthiness 
directive (AD):

2020-05-12 Gulfstream Aerospace Corporation: Amendment 39-19860; 
Docket No. FAA-2020-0199; Product Identifier 2020-NM-035-AD.

(a) Effective Date

    This AD is effective March 13, 2020.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Gulfstream Aerospace Corporation Model GVII-
G500 and GVII-G600 airplanes, certificated in any category, all 
serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 27, Flight 
controls.

(e) Unsafe Condition

    This AD was prompted by report of a landing incident in which 
the alpha limiter engaged in the landing flare in unstable air while 
on the approach, resulting in a high rate of descent landing and 
damage to the airplane. The FAA is issuing this AD to address 
inappropriate alpha limiter engagement during the landing flare, 
which can limit pilot pitch authority during a critical phase of 
flight near the ground, and result in a high rate of descent landing 
and the possible consequent loss of control of the airplane on 
landing.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) AFM Revision for GVII-G500

    For Model GVII-G500 airplanes: Within 5 days after the effective 
date of this AD, revise the airplane flight manual (AFM) for your 
airplane to incorporate the information specified in paragraphs 
(g)(1) through (9) of this AD.
    (1) Step 3. ``Wind Conditions'' of Section 01-02-10, ``Runway, 
Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS,'' of the 
Gulfstream GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-
0001, Revision 5, dated March 3, 2020.
    (2) Step 15. ``Approach Speed'' of Section 01-03-40, ``Airspeed 
Limitations,'' of Chapter 01, ``LIMITATIONS,'' of the Gulfstream 
GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-0001, 
Revision 5, dated March 3, 2020.
    (3) Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS,'' of the Gulfstream GVII-G500 Airplane Flight Manual, 
GAC-AC-GVII-G500-OPS-0001, Revision 5, dated March 3, 2020.
    (4) Step 5. of Section 01-34-40, ``Takeoff and Landing Data 
(TOLD),'' of Chapter 01, ``LIMITATIONS,'' of the Gulfstream GVII-
G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-0001, Revision 5, 
dated March 3, 2020.
    (5) ``WARNING,'' preceding Step 4., of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS,'' of the Gulfstream 
GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-0001, 
Revision 5, dated March 3, 2020.
    (6) Step 11. ``Landing,'' of Section 03-12-10, ``Zero Flaps or 
Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES,'' of 
the Gulfstream GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-
OPS-0001, Revision 5, dated March 3, 2020.
    (7) Step 8. ``Final Approach Fix,'' of Section 04-08-40, ``One 
Engine Inoperative Landing Procedure,'' of Chapter 04, ``EMERGENCY 
PROCEDURES,'' of the Gulfstream GVII-G500 Airplane Flight Manual, 
GAC-AC-GVII-G500-OPS-0001, Revision 5, dated March 3, 2020.
    (8) Step 1., ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE FAA BASELINE,'' of the 
Gulfstream GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-
0001, Revision 5, dated March 3, 2020.
    (9) Step 1., ``Introduction,'' of Section 5A-11-10, ``Threshold 
Speeds,'' of Chapter 5A, ``PERFORMANCE (ASC 022),'' of the 
Gulfstream GVII-G500 Airplane Flight Manual, GAC-AC-GVII-G500-OPS-
0001, Revision 5, dated March 3, 2020.

(h) AFM Revision for GVII-G600

    For Model GVII-G600 airplanes: Within 5 days after the effective 
date of this AD, revise the AFM for your airplane to incorporate the 
information specified in paragraphs (h)(1) through (9) of this AD.
    (1) Step 3., ``Wind Conditions'' of Section 01-02-10, ``Runway, 
Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS,'' of the 
Gulfstream GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-
0001, Revision 3, dated March 3, 2020.
    (2) Step 15., ``Approach Speed'' of Section 01-03-40, ``Airspeed 
Limitations,'' of Chapter 01, ``LIMITATIONS,'' of the Gulfstream 
GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-0001, 
Revision 3, dated March 3, 2020.
    (3) Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS,'' of the Gulfstream GVII-G600 Airplane Flight Manual, 
GAC-AC-GVII-G600-OPS-0001, Revision 3, dated March 3, 2020.
    (4) Steps 3. and 4. of Section 01-34-40, ``Takeoff and Landing 
Data (TOLD),'' of Chapter 01, ``LIMITATIONS,'' of the Gulfstream 
GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-0001, 
Revision 3, dated March 3, 2020.
    (5) ``WARNING,'' preceding Step 4., of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS,'' of the Gulfstream 
GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-0001, 
Revision 3, dated March 3, 2020.
    (6) Step 11., ``Landing,'' of Section 03-12-10, ``Zero Flaps or 
Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES,'' of 
the Gulfstream GVII-G600 Airplane Flight Manual, GAC-AC-GVII-G600-
OPS-0001, Revision 3, dated March 3, 2020.
    (7) Step 8., ``Final Approach Fix,'' of Section 04-08-40, ``One 
Engine Inoperative Landing Procedure,'' of Chapter 04, ``EMERGENCY 
PROCEDURES,'' of the Gulfstream GVII-G600 Airplane Flight Manual, 
GAC-AC-GVII-G600-OPS-0001, Revision 3, dated March 3, 2020.
    (8) Step 1, ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE,'' of the Gulfstream GVII-
G600 Airplane Flight Manual, GAC-AC-GVII-G600-OPS-0001, Revision 3, 
dated March 3, 2020.
    (9) Step 1, ``Introduction,'' of Section 05-11-20, ``Tire Speed 
and BKE Limited Maximum Landing Weight,'' of Chapter 05, 
``PERFORMANCE,'' of the Gulfstream GVII-G600 Airplane Flight Manual, 
GAC-AC-GVII-G600-OPS-0001, Revision 3, dated March 3, 2020.

(i) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Atlanta ACO Branch, 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 
manager of the certification office, send it to the attention of the 
person identified in paragraph (j) of this AD.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager

[[Page 14565]]

of the local flight standards district office/certificate holding 
district office.

(j) Related Information

    For more information about this AD, contact Myles Jalalian, 
Aerospace Engineer, Systems and Equipment Section, FAA, Atlanta ACO 
Branch, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-
474-5572; fax: 404-474-5606; email: Myles.Jalalian@faa.gov.

(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 GVII-G500 Airplane Flight Manual, GAC-AC-GVII-
G500-OPS-0001, Revision 5, dated March 3, 2020.
    (A) Step 3., ``Wind Conditions,'' of Section 01-02-10, ``Runway, 
Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS.''
    (B) Step 15., ``Approach Speed,'' of Section 01-03-40, 
``Airspeed Limitations,'' of Chapter 01, ``LIMITATIONS.''
    (C) Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS.''
    (D) Step 5., Section 01-34-40, ``Takeoff and Landing Data 
(TOLD),'' of Chapter 01, ``LIMITATIONS.''
    (E) ``WARNING,'' preceding Step 4. of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS.''
    (F) Step 11., ``Landing,'' of Section 03-12-10, ``Zero Flaps or 
Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES.''
    (G) Step 8., ``Final Approach Fix,'' of Section 04-08-40, ``One 
Engine Inoperative Landing Procedure,'' of Chapter 04, ``EMERGENCY 
PROCEDURES.''
    (H) Step 1, ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE FAA BASELINE.''
    (I) Step 1, ``Introduction,'' of Section 5A-11-10, ``Threshold 
Speeds,'' of Chapter 5A, ``PERFORMANCE (ASC 022).''
    (ii) Gulfstream GVII-G600 Airplane Flight Manual, GAC-AC-GVII-
G600-OPS-0001, Revision 3, dated March 3, 2020.
    (A) Step 3., ``Wind Conditions,'' of Section 01-02-10, ``Runway, 
Slope and Wind Conditions,'' of Chapter 01, ``LIMITATIONS.''
    (B) Step 15., ``Approach Speed,'' of Section 01-03-40, 
``Airspeed Limitations,'' of Chapter 01, ``LIMITATIONS.''
    (C) Section 01-27-10, ``Normal Control Laws,'' of Chapter 01, 
``LIMITATIONS.''
    (D) Steps 3. and 4., Section 01-34-40, ``Takeoff and Landing 
Data (TOLD),'' of Chapter 01, ``LIMITATIONS.''
    (E) ``WARNING,'' preceding Step 4. of Section 02-05-50, 
``Landing,'' of Chapter 02, ``NORMAL OPERATIONS.''
    (F) Step 11., ``Landing,'' of Section 03-12-10, ``Zero Flaps or 
Partial Flaps Landings,'' of Chapter 03, ``ABNORMAL PROCEDURES.''
    (G) Step 8., ``Final Approach Fix,'' of Section 04-08-40, ``One 
Engine Inoperative Landing Procedure,'' of Chapter 04, ``EMERGENCY 
PROCEDURES.''
    (H) Step 1, ``Introduction,'' of Section 05-11-10, ``Threshold 
Speeds,'' of Chapter 05, ``PERFORMANCE.''
    (I) Step 1, ``Introduction,'' of Section 05-11-20, ``Tire Speed 
and BKE Limited Maximum Landing Weight,'' of Chapter 05, 
``PERFORMANCE.''
    (3) For service information identified in this AD, contact 
Gulfstream Aerospace Corporation, Technical Publications Dept., P.O. 
Box 2206, Savannah, GA 31402-2206; telephone 800-810-4853; fax 912-
965-3520; email pubs@gulfstream.com; internet https://www.gulfstream.com/customer-support.
    (4) You may view this service information at the FAA, Policy and 
Innovation Division, 901 Locust, Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
816-329-4148.
    (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, email fedreg.legal@nara.gov, or go to https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on March 6, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2020-05242 Filed 3-11-20; 11:15 am]
 BILLING CODE 4910-13-P