AD 2020-26-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream Aerospace LP | Gulfstream G280 | Airworthiness Directives; Gulfstream Aerospace LP Airplanes |
Unsafe Condition
solder cracking of the flight control electronic control units (FCECUs), which, combined with latent failure of the horizontal stabilizer trim actuator (HSTA) ``no-back'' mechanism, could result in uncontrolled HSTA operation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Comply with all required actions and compliance times specified in, and in accordance with, Civil Aviation Authority of Israel (CAAI) AD ISR-I-04-2020-06-02, dated June 28, 2020 (CAAI AD ISR-I-04-2020-06-02).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 work-hours per operator, although the agency recognizes that this number may vary from operator to operator.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Gulfstream Aerospace LP Model Gulfstream G280 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before September 15, 2019.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Gulfstream Aerospace LP Model Gulfstream G280 airplanes. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a Civil Aviation Authority of Israel (CAAI) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to all Gulfstream Aerospace LP Model Gulfstream
G280 airplanes, certificated in any category, with an original
airworthiness certificate or original export certificate of
airworthiness issued on or before September 15, 2019.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 85, Number 248 (Monday, December 28, 2020)]
[Rules and Regulations]
[Pages 84199-84201]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2020-28406]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 85, No. 248 / Monday, December 28, 2020 /
Rules and Regulations
[[Page 84199]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0796; Project Identifier MCAI-2020-00902-T;
Amendment 39-21367; AD 2020-26-12]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Gulfstream Aerospace LP Model Gulfstream G280 airplanes. This
AD was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. This AD requires revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations, as
specified in a Civil Aviation Authority of Israel (CAAI) AD, which is
incorporated by reference. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective February 1, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of February 1,
2021.
ADDRESSES: For material incorporated by reference (IBR) in this AD, The
Civil Aviation Authority of Israel (CAAI), P.O. Box 1101, Golan Street,
Airport City, 70100, Israel; phone: 972-3-9774665; fax: 972-3-9774592;
email: <a href="/cdn-cgi/l/email-protection#f7969e87b79a9883d9909881d99e9b"><span class="__cf_email__" data-cfemail="e9888099a984869dc78e869fc78085">[email protected]</span></a>. You may find this IBR material on the CAAI
website at <a href="https://www.caa.gov.il">https://www.caa.gov.il</a>. You may view this IBR material at
the FAA, Airworthiness Products Section, Operational Safety Branch,
2200 South 216th St., Des Moines, WA. For information on the
availability of this material at the FAA, call 206-231-3195. It is also
available in the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2020-
0796.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2020-
0796; 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, any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3226;
email: <a href="/cdn-cgi/l/email-protection#c3b7acaeedb1aca7b1aaa4b6a6b983a5a2a2eda4acb5"><span class="__cf_email__" data-cfemail="01756e6c2f736e6573686674647b416760602f666e77">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Discussion
The CAAI, which is the aviation authority for Israel, has issued
CAAI AD ISR-I-04-2020-06-02, dated June 28, 2020 (CAAI AD ISR-I-04-
2020-06-02) (also referred to as the Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an unsafe condition for all
Gulfstream Aerospace LP Model Gulfstream G280 airplanes. Airplanes with
an original airworthiness certificate or original export certificate of
airworthiness issued after September 15, 2019, must comply with the
airworthiness limitations specified as part of the approved type design
and referenced on the type certificate data sheet; this AD therefore
does not include those airplanes in the applicability.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Gulfstream
Aerospace LP Model Gulfstream G280 airplanes. The NPRM published in the
Federal Register on September 16, 2020 (85 FR57799). The NPRM was
prompted by a determination that new or more restrictive airworthiness
limitations are necessary. The NPRM proposed to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations, as
specified in CAAI AD ISR-I-04-2020-06-02.
The FAA is issuing this AD to address solder cracking of the flight
control electronic control units (FCECUs), which, combined with latent
failure of the horizontal stabilizer trim actuator (HSTA) ``no-back''
mechanism, could result in uncontrolled HSTA operation. See the MCAI
for additional background information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed,
except for minor editorial changes. The FAA has determined that these
minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
CAAI AD ISR-I-04-2020-06-02 describes new or more restrictive
airworthiness limitations for airplane structures and safe life limits.
This material 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.
Costs of Compliance
The FAA estimates that this AD affects 160 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. In the past, the agency has estimated that this action
[[Page 84200]]
takes 1 work-hour per airplane. Since operators incorporate maintenance
or inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the agency estimates the average total
cost per operator to be $7,650 (90 work-hours x $85 per work-hour).
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.
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,
(2) Will not affect intrastate aviation in Alaska, 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.
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:
2020-26-12 Gulfstream Aerospace LP: Amendment 39-21367; Docket No.
FAA-2020-0796; Project Identifier MCAI-2020-00902-T.
(a) Effective Date
This airworthiness directive (AD) is effective February 1, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Gulfstream Aerospace LP Model Gulfstream
G280 airplanes, certificated in any category, with an original
airworthiness certificate or original export certificate of
airworthiness issued on or before September 15, 2019.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
controls.
(e) Reason
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address solder cracking of the flight control
electronic control units (FCECUs), which, combined with latent
failure of the horizontal stabilizer trim actuator (HSTA) ``no-
back'' mechanism, could result in uncontrolled HSTA operation.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, Civil Aviation Authority of Israel (CAAI) AD ISR-I-
04-2020-06-02, dated June 28, 2020 (CAAI AD ISR-I-04-2020-06-02).
(h) Exceptions to CAAI AD ISR-I-04-2020-06-02
(1) Where CAAI AD ISR-I-04-2020-06-02 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where CAAI AD ISR-I-04-2020-06-02 refers to the date of its
issuance, this AD requires using the effective date of this AD.
(i) Provisions for Alternative Actions, Intervals, and Critical Design
Configuration Control Limitations (CDCCLs)
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections), intervals, and CDCCLs are allowed
unless they are approved as specified in the provisions of CAAI AD
ISR-I-04-2020-06-02.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, International Validation 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 responsible Flight
Standards Office, as appropriate. If sending information directly to
the Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (k) of this
AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#f7cedab6a1a4dab6bea5dac0c4c7dab6bab8b4b7919696d9909881"><span class="__cf_email__" data-cfemail="ead3c7abbcb9c7aba3b8c7ddd9dac7aba7a5a9aa8c8b8bc48d859c">[email protected]</span></a>.
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, Large Aircraft
Section, International Validation Branch, FAA; or CAAI; or CAAI's
authorized Designee. If approved by the CAAI Designee, the approval
must include the Designee's authorized signature.
(k) Related Information
For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and
fax: 206-231-3226; email: <a href="/cdn-cgi/l/email-protection#fe8a9193d08c919a8c97998b9b84be989f9fd0999188"><span class="__cf_email__" data-cfemail="8cf8e3e1a2fee3e8fee5ebf9e9f6cceaededa2ebe3fa">[email protected]</span></a>.
(l) 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 this AD specifies otherwise.
(i) The Civil Aviation Authority of Israel (CAAI) AD ISR-I-04-
2020-06-02, dated June 28, 2020.
(ii) [Reserved]
(3) For CAAI AD ISR-I-04-2020-06-02, contact the CAAI, P.O. Box
1101, Golan Street, Airport City, 70100, Israel; phone: 972-3-
9774665; fax: 972-3-9774592; email: <a href="/cdn-cgi/l/email-protection#ef8e869faf82809bc1888099c18683"><span class="__cf_email__" data-cfemail="0d6c647d4d606279236a627b236461">[email protected]</span></a>. You may find
this IBR material on the CAAI website at <a href="https://www.caa.gov.il">https://www.caa.gov.il</a>.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St.,
Des Moines, WA. For information on the availability of this material
at the FAA, call 206-231-3195. This material may be found in the AD
docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching
for and locating Docket No. FAA-2020-0796.
[[Page 84201]]
(5) You may view this material that is incorporated by reference
at the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, email
<a href="/cdn-cgi/l/email-protection#325457564057551c5e5755535e725c5340531c555d44"><span class="__cf_email__" data-cfemail="5e383b3a2c3b3970323b393f321e303f2c3f70393128">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on December 10, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-28406 Filed 12-23-20; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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