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Published 2021-12-21 · Federal Register document 2021-27511

Airworthiness Directives; Embraer S.A. Airplanes

Publication summary

The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. Model EMB-500 and EMB-505 airplanes. This AD was prompted by a report that the operational envelope does not contain airspeed limitations and procedures for operating the airplane at static air temperatures below -54 [deg]C. This AD requires revising the airplane flight manual (AFM) to incorporate new and revised airspeed limitations and procedures. The FAA is issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2021-9c919420683447c6
Source row
results[475]
Raw source SHA-256
9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2021-24-21
Effective date printed in this edition
2022-01-25
Read 10 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective January 25, 2022.

Exact source excerpt. Text positions 10133–10223, end exclusive, in the original decoded publication. SHA-256: 8d378fb3ed451904a2c511b974931f6d6070c7fd33739e123696bee180c57499

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 10223–10252, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to Embraer S.A. Model EMB-500 and EMB-505 
airplanes, all serial numbers, certificated in any category, with 
Model PW617F-E or PW617F1-E engines (for Model EMB-500 airplanes) or 
Model PW535E engines (for Model EMB-505 airplanes) installed.

Exact source excerpt. Text positions 10252–10534, end exclusive, in the original decoded publication. SHA-256: c95bef279a4e102567decf52169c592acc379fd3dcf95a30d6464ce81f5e604e

Subject
(d) Subject

    Joint Aircraft System Component (JASC) Code 0200, Operations.

Exact source excerpt. Text positions 10534–10614, end exclusive, in the original decoded publication. SHA-256: cca456c1580855d93ab74d4ed209b83337a1c3db88cd7dea2b93abefb527e3ec

Unsafe Condition
(e) Unsafe Condition

    This AD was prompted by a report that the operational envelope 
does not contain airspeed limitations and procedures for operating 
the airplane at static air temperatures below -54 [deg]C. The FAA is 
issuing this AD to prevent inadequate operation below the allowable 
temperature. The unsafe condition, if not addressed, could result in 
multiple systems failures and compromise safe flight of the 
airplane.

Exact source excerpt. Text positions 10614–11053, end exclusive, in the original decoded publication. SHA-256: 30271b56d16d5be13800faea71d68984f64d18721bdfb16f55fee2d8960db27e

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 11053–11155, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Revision of the Airplane Flight Manual (AFM)
(g) Revision of the Airplane Flight Manual (AFM)

    Within 30 days after the effective date of this AD:
    (1) For Model EMB-500 airplanes: Revise Section 2 Limitations 
and Section 5 Performance of the existing AFM for your airplane by 
incorporating the information in ``V--OPERATING INFORMATION,'' of 
Embraer Phenom Operational Bulletin No. 500-001/20, dated March 9, 
2020. You may use a different document provided the language is 
identical to the language in ``V--OPERATING INFORMATION,'' of 
Embraer Phenom Operational Bulletin No. 500-001/20, dated March 9, 
2020.
    (2) For Model EMB-505 airplanes: Revise Section 2 Limitations, 
Section 5 Performance, and Supplement 2 of the existing AFM for your 
airplane by incorporating the information in ``V--OPERATING 
INFORMATION,'' of Embraer Phenom Operational Bulletin No. 505-005/
13, Revision 1, dated March 9, 2020. You may use a different 
document provided the language is identical to the language in V--
OPERATING INFORMATION,'' of Embraer Phenom Operational Bulletin No. 
505-005/13, Revision 1, dated March 9, 2020.

Exact source excerpt. Text positions 11155–12243, end exclusive, in the original decoded publication. SHA-256: c2adfa567c438dc0beeac9c708c04e94fab2101c9ae124d74396f28d0a89eca8

Alternative Methods of Compliance (AMOCs)
(h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, International Validation Branch, FAA, has the 
authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19. Send your request to the person 
identified in paragraph (i)(1) of this AD and email: [email protected].
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspection, the manager 
of the local Flight Standards District Office.

Exact source excerpt. Text positions 12243–12743, end exclusive, in the original decoded publication. SHA-256: 3b91ee587cd69280144e66d2d9641e79c3941245199fcc98e483f6b416c98b97

Related Information
(i) Related Information

    (1) For more information about this AD, contact Jim Rutherford, 
Aviation Safety Engineer, FAA, General Aviation & Rotorcraft 
Section, International Validation Branch, 901 Locust, Room 301, 
Kansas City, MO 64106; phone: (816) 329-4165; fax: (816) 329-4090; 
email: [email protected].
    (2) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil AD 
2020-05-03, effective June 1, 2020, for related information. This 
MCAI may be found in the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2020-1077.

Exact source excerpt. Text positions 12743–13379, end exclusive, in the original decoded publication. SHA-256: e42e784ddd13929429f3741f79fbee6272e0b9dbfc43da0952c605a6c446635b

Material Incorporated by Reference
(j) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference 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) Embraer Phenom Operational Bulletin No. 500-001/20, dated 
March 9, 2020.
    (ii) Embraer Phenom Operational Bulletin No. 505-005/13, 
Revision 1, dated March 9, 2020.
    (3) For service information identified in this AD, contact 
Phenom Maintenance Support, Avenida Brigadeiro Faria Lima, 2170, 
P.O. Box 36/2, S[atilde]o Jos[eacute] dos Campos, 12227-901, Brazil; 
phone: +55 12 3927 1000; email: [email protected];

[[Page 72186]]

website: https://www.embraer.com.br/en-US/Pages/home.aspx.
    (4) You may view this service information at FAA, Airworthiness 
Products Section, Operational Safety Branch, 901 Locust, Kansas 
City, MO 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: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 13379–14783, end exclusive, in the original decoded publication. SHA-256: eb6156ad325e487f5157a80d13542773aa8156ca330f4326d9d749b9a44793b3

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 2021-24-21 · 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: 4239177a7ae039d294d581bd5e79838738f3aca576d34347b06718ccc249a8c4. Source manifest: 86f7eaed06d969e334500fd311d952fb8f6ea61f1cc9cc64abeb50f71d991ff7.

Official source · 2021-12-21

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 86, Number 242 (Tuesday, December 21, 2021)]
[Rules and Regulations]
[Pages 72183-72186]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-27511]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-1077; Project Identifier MCAI-2020-00819-A; 
Amendment 39-21842; AD 2021-24-21]
RIN 2120-AA64


Airworthiness Directives; Embraer S.A. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Embraer S.A. Model EMB-500 and EMB-505 airplanes. This AD was 
prompted by a report that the

[[Page 72184]]

operational envelope does not contain airspeed limitations and 
procedures for operating the airplane at static air temperatures below 
-54 [deg]C. This AD requires revising the airplane flight manual (AFM) 
to incorporate new and revised airspeed limitations and procedures. The 
FAA is issuing this AD to address the unsafe condition on these 
products.

DATES: This AD is effective January 25, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of January 25, 
2022.

ADDRESSES: For service information identified in this final rule, 
contact Phenom Maintenance Support, Avenida Brigadeiro Faria Lima, 
2170, P.O. Box 36/2, S[atilde]o Jos[eacute] dos Campos, 12227-901, 
Brazil; phone: +55 12 3927 1000; email: 
[email protected]; website: https://www.embraer.com.br/en-US/Pages/home.aspx. You may view this service information at the 
FAA, Airworthiness Products Section, Operational Safety Branch, 901 
Locust, Kansas City, MO 64106. For information on the availability of 
this material at the FAA, call (816) 329-4148. It is also available at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2020-1077.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2020-1077; 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 
mandatory continuing airworthiness information (MCAI), 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: Jim Rutherford, Aviation Safety 
Engineer, FAA, General Aviation & Rotorcraft Section, International 
Validation Branch, 901 Locust, Room 301, Kansas City, MO 64106; phone: 
(816) 329-4165; fax: (816) 329-4090; email: [email protected].

SUPPLEMENTARY INFORMATION:

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 by adding an AD that would apply to all Embraer S.A. Model 
EMB-500 and EMB-505 airplanes with certain engines installed. The NPRM 
published in the Federal Register on August 2, 2021 (86 FR 41410). The 
NPRM was prompted by MCAI originated by the Ag[ecirc]ncia Nacional de 
Avia[ccedil][atilde]o Civil (ANAC), which is the aviation authority for 
Brazil. ANAC issued AD 2020-05-03, effective June 1, 2020 (ANAC AD 
2020-05-03) (also referred to after this as ``the MCAI''), to correct 
an unsafe condition on Embraer S.A. Model EMB-500 and EMB-505 airplanes 
with certain engines installed. Although the affected airplanes were 
designed for operation at temperatures below -54 [deg]C, the 
operational envelope in the AFM does not contain the necessary 
limitations and procedures to operate safely in these colder 
temperatures. The MCAI states that operation of the affected airplanes 
at static air temperatures below -54 [deg]C without these limitations 
could cause several systems and components to operate inadequately, 
resulting in multiple systems failures.
    Accordingly, the MCAI requires updating the AFM to incorporate a 
modified operational envelope that establishes restrictions and minimum 
airspeed required for each static temperature range. In the NPRM, the 
FAA proposed to require revising the AFM to incorporate the new and 
revised airspeed limitations and procedures specified in the 
manufacturer's service information. The FAA is issuing this AD to 
prevent inadequate operation below the allowable temperature, which 
could result in multiple systems failures and compromise safe flight of 
the airplane.
    You may examine the MCAI in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
1077.

Discussion of Final Airworthiness Directive

Comments

    The FAA received a comment on the NPRM from Embraer. The following 
presents the comment received and the FAA's response to the comment.
    Embraer requested that the FAA change the final rule to allow 
operators to revise the AFM using EMB-500 AFM 2656, Revision 24, dated 
March 17, 2020, and EMB-505 AFM-2665, Revision 21, dated March 13, 
2020, as well as future FAA-approved AFM revisions. Embraer stated that 
the information in the service information proposed for incorporation 
by reference has been included in the March 2020 AFM revisions for each 
model type.
    The FAA agrees and has revised the AD to allow use of a different 
document provided the language is identical to the language in the 
service information incorporated by reference.

Conclusion

    This product has been approved by the aviation authority of another 
country and is approved for operation in the United States. Pursuant to 
the FAA's bilateral agreement with this State of Design Authority, it 
has notified the FAA of the unsafe condition described in the MCAI 
referenced above. The FAA reviewed the relevant data, considered the 
comment received, and determined that air safety requires adopting this 
AD as proposed. Accordingly, the FAA is issuing this AD to address the 
unsafe condition on these products. Except for the changes described 
previously, this AD is adopted as proposed in the NPRM. None of the 
changes will increase the economic burden on any operator.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Embraer Phenom Operational Bulletin No. 500-001/
20, dated March 9, 2020; and Operational Bulletin No. 505-005/13, 
Revision 1, dated March 9, 2020. This service information specifies 
revising the AFM to incorporate limitations and procedures for the 
minimum airspeed in the affected region of the operational envelope. 
These documents are distinct since 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.

Costs of Compliance

    The FAA estimates that this AD affects 590 airplanes of U.S. 
registry.

[[Page 72185]]



                                      Estimated Costs for Revising the AFM
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
.5 work-hour x $85 per hour = $42.50.........................              $0           $42.50          $25,075
----------------------------------------------------------------------------------------------------------------

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.

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:

2021-24-21 Embraer S.A.: Amendment 39-21842; Docket No. FAA-2020-
1077; Project Identifier MCAI-2020-00819-A.

(a) Effective Date

    This airworthiness directive (AD) is effective January 25, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Embraer S.A. Model EMB-500 and EMB-505 
airplanes, all serial numbers, certificated in any category, with 
Model PW617F-E or PW617F1-E engines (for Model EMB-500 airplanes) or 
Model PW535E engines (for Model EMB-505 airplanes) installed.

(d) Subject

    Joint Aircraft System Component (JASC) Code 0200, Operations.

(e) Unsafe Condition

    This AD was prompted by a report that the operational envelope 
does not contain airspeed limitations and procedures for operating 
the airplane at static air temperatures below -54 [deg]C. The FAA is 
issuing this AD to prevent inadequate operation below the allowable 
temperature. The unsafe condition, if not addressed, could result in 
multiple systems failures and compromise safe flight of the 
airplane.

(f) Compliance

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

(g) Revision of the Airplane Flight Manual (AFM)

    Within 30 days after the effective date of this AD:
    (1) For Model EMB-500 airplanes: Revise Section 2 Limitations 
and Section 5 Performance of the existing AFM for your airplane by 
incorporating the information in ``V--OPERATING INFORMATION,'' of 
Embraer Phenom Operational Bulletin No. 500-001/20, dated March 9, 
2020. You may use a different document provided the language is 
identical to the language in ``V--OPERATING INFORMATION,'' of 
Embraer Phenom Operational Bulletin No. 500-001/20, dated March 9, 
2020.
    (2) For Model EMB-505 airplanes: Revise Section 2 Limitations, 
Section 5 Performance, and Supplement 2 of the existing AFM for your 
airplane by incorporating the information in ``V--OPERATING 
INFORMATION,'' of Embraer Phenom Operational Bulletin No. 505-005/
13, Revision 1, dated March 9, 2020. You may use a different 
document provided the language is identical to the language in V--
OPERATING INFORMATION,'' of Embraer Phenom Operational Bulletin No. 
505-005/13, Revision 1, dated March 9, 2020.

(h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, International Validation Branch, FAA, has the 
authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19. Send your request to the person 
identified in paragraph (i)(1) of this AD and email: [email protected].
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspection, the manager 
of the local Flight Standards District Office.

(i) Related Information

    (1) For more information about this AD, contact Jim Rutherford, 
Aviation Safety Engineer, FAA, General Aviation & Rotorcraft 
Section, International Validation Branch, 901 Locust, Room 301, 
Kansas City, MO 64106; phone: (816) 329-4165; fax: (816) 329-4090; 
email: [email protected].
    (2) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil AD 
2020-05-03, effective June 1, 2020, for related information. This 
MCAI may be found in the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2020-1077.

(j) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference 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) Embraer Phenom Operational Bulletin No. 500-001/20, dated 
March 9, 2020.
    (ii) Embraer Phenom Operational Bulletin No. 505-005/13, 
Revision 1, dated March 9, 2020.
    (3) For service information identified in this AD, contact 
Phenom Maintenance Support, Avenida Brigadeiro Faria Lima, 2170, 
P.O. Box 36/2, S[atilde]o Jos[eacute] dos Campos, 12227-901, Brazil; 
phone: +55 12 3927 1000; email: [email protected];

[[Page 72186]]

website: https://www.embraer.com.br/en-US/Pages/home.aspx.
    (4) You may view this service information at FAA, Airworthiness 
Products Section, Operational Safety Branch, 901 Locust, Kansas 
City, MO 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: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on November 19, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-27511 Filed 12-20-21; 8:45 am]
BILLING CODE 4910-13-P


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c8bb27c991cdf915ca979cea43fbbceeeee1edb36baf75db30cef90f58dc5ace
Text SHA-256
4239177a7ae039d294d581bd5e79838738f3aca576d34347b06718ccc249a8c4

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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.