Rule2022-04845
Accepted Means of Compliance; Airworthiness Standards: Normal Category Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
March 11, 2022
Effective
March 11, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
This document announces ASTM International (ASTM) consensus standards for use as a means of compliance to the applicable airworthiness standards for normal category airplanes. The FAA accepts ASTM Designation F3264-21 as a means of compliance for applicable airworthiness standards for normal category airplanes, with the changes identified in Table 1 of this document. For ease of use, Table 2 provides a side-by-side view, linking applicable regulations to the associated ASTM sections.
Full Text
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<title>Federal Register, Volume 87 Issue 48 (Friday, March 11, 2022)</title>
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[Federal Register Volume 87, Number 48 (Friday, March 11, 2022)]
[Rules and Regulations]
[Pages 13911-13923]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-04845]
[[Page 13911]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 23
[Docket No. FAA-2022-0217; Notice No. NOA-23-22-01]
Accepted Means of Compliance; Airworthiness Standards: Normal
Category Airplanes
AGENCY: Federal Aviation Administration, Department of Transportation
(DOT).
ACTION: Issuance of accepted means of compliance.
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SUMMARY: This document announces ASTM International (ASTM) consensus
standards for use as a means of compliance to the applicable
airworthiness standards for normal category airplanes. The FAA accepts
ASTM Designation F3264-21 as a means of compliance for applicable
airworthiness standards for normal category airplanes, with the changes
identified in Table 1 of this document. For ease of use, Table 2
provides a side-by-side view, linking applicable regulations to the
associated ASTM sections.
DATES: The FAA accepts the means of compliance effective March 11,
2022.
FOR FURTHER INFORMATION CONTACT: Hieu Nguyen, Federal Aviation
Administration, Policy and Innovation Division, Small Airplane
Strategic Policy Section, AIR-615, 901 Locust Street, Room 301, Kansas
City, Missouri 64106; telephone (316) 946-4123; facsimile: (316) 946-
4107; email: <a href="/cdn-cgi/l/email-protection#375f5e5242195950424e52597751565619505841"><span class="__cf_email__" data-cfemail="630b0a06164d0d04161a060d230502024d040c15">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
Under the provisions of the National Technology Transfer and
Advancement Act of 1995 \1\ and Office of Management and Budget (OMB)
Circular A-119, ``Federal Participation in the Development and Use of
Voluntary Consensus Standards and in Conformity Assessment
Activities,'' effective January 27, 2016, the FAA participates in the
development of consensus standards and uses consensus standards as a
means of carrying out its policy objectives where appropriate.
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\1\ Ref Public Law 104-113 as amended by Public Law 107-107.
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Consistent with the Small Airplane Revitalization Act of 2013,\2\
the FAA has been working with industry and other stakeholders through
the ASTM International (ASTM) F44 Committee on General Aviation
Aircraft to develop consensus standards as a means of compliance in
certificating small airplanes under title 14, Code of Federal
Regulations (14 CFR), part 23.
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\2\ Ref Public Law 113-53.
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In part 23, amendment 23-64 \3\ (81 FR 96572, published on December
30, 2016), the final rule described the FAA would publish those
consensus standards in the Federal Register, when the Administrator
accepts the consensus standards as an acceptable means of compliance.
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\3\ See <a href="https://www.federalregister.gov/documents/2016/12/30/2016-30246/revision-of-airworthiness-standards-for-normal-utility-acrobatic-and-commuter-category-airplanes">https://www.federalregister.gov/documents/2016/12/30/2016-30246/revision-of-airworthiness-standards-for-normal-utility-acrobatic-and-commuter-category-airplanes</a>.
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Additionally, the FAA published Advisory Circular (AC) 23.2010-
1,\4\ dated March 27, 2017, titled ``FAA Accepted Means of Compliance
Process for 14 CFR part 23''. In paragraph 5.5, the AC also describes
that a notice will be published when the Administrator accepts a
standard.
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\4\ See <a href="https://drs.faa.gov/browse">https://drs.faa.gov/browse</a>.
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The means of compliance accepted by this document is one means, but
not the only means of complying with part 23 regulatory requirements.
The FAA reviewed the published ASTM consensus standards developed
by ASTM Committee F44 as the basis for means of compliance to 65
sections of part 23, amendment 23-64.
In some cases, the Administrator found sections of the ASTM
Standard Designation F3264-21, titled ``Standard Specification for
Normal Category Aeroplanes Certification,'' without changes, accepted
as means of compliance with the airworthiness requirements of amendment
23-64, and within the scope and applicability of the consensus
standards.
In other cases, the means of compliance, while based on ASTM
consensus standards, include additional FAA provisions necessary to
comply with the airworthiness requirements of amendment 23-64.
Applicants who desire to use means of compliance reflected by other
revisions to ASTM standards not previously accepted, may seek guidance
and possible acceptance from the FAA for the use of those means of
compliance on a case-by-case basis. Applicants may also propose
alternative means of compliance for FAA review and possible acceptance.
Part 23, amendment 23-64, established airworthiness requirements
based on the safety requirements outlined in amendment 23-63, except in
areas that address loss of control and icing, where the FAA increased
the safety level. Depending on the details of a design, the applicant
may require use of a different means of compliance beyond those
accepted by this document. For example, novel airplane designs, such as
unmanned airplanes or vertical takeoff and landing airplanes, may be
outside the scope of this document, and applicants may need to propose
alternative means of compliance applicable to their designs accepted
under Sec. 23.2010.
Means of Compliance Accepted
This document accepts only the revisions of the standards
referenced in ASTM International Standard Designation (ASTM) F3264-21,
``Standard Specification for Normal Category Aeroplanes
Certification.''
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\5\ The means of compliance are inteded for traditional part 23
airplanes, not for novel designs. Novel designs require evaluation
and possible modification of the means of compliance.
\6\ You may find additional information on the FAA Small
Airplane Issues List (SAIL) here: <a href="https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/">https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/</a>.
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Table 1. The FAA accepts ASTM F3264-21 as a means of compliance for
part 23, amendment 23-64, with the changes identified.
Table 2. For ease of use, Table 2 provides a side-by-side view,
linking the applicable part 23 regulations to the ASTM F3264-21
sections. The ASTM F3264-21 sections must incorporate the changes
required for FAA acceptance from Table 1.
Table 1--Part 23 Accepted Means of Compliance Based on ASTM Consensus Standards
----------------------------------------------------------------------------------------------------------------
Changes required for FAA Additional information
ASTM designation No. ASTM document title acceptance \5\ \6\
----------------------------------------------------------------------------------------------------------------
F2490-20.......................... Standard Guide for None. .........................
Aircraft Electrical
Load and Power
Source Capacity
Analysis.
[[Page 13912]]
F3061/F3061M-20................... Standard Remove: Tables 1, 3, 4, 5, Aircraft Type Code
Specification for 13 and 14. compliance matrix tables
Systems and Replace 17.3.1 with the found in F3061/F3061M-20
Equipment in Small following:. are not accepted.
Aircraft. (a) Each electrical or Applicability will be
electronic system that determined by the Small
performs a function, the Airplane Strategic
failure of which would Policy Section.
prevent the continued F3061/F3061M-20 does not
safe flight and landing contain means for
of the airplane, must be showing compliance to
designed and installed Sec. 23.2310 Buoyancy
such that--. for seaplanes and
(1) The function at the amphibians. If applying
airplane level is not for certification of a
adversely affected during seaplane or amphibian,
and after the time the applicants may use the
airplane is exposed to provisions of Sec. Sec.
lightning; and. 23.751, 23.755, and
(2) The system recovers 23.757 at amendment 23-
normal operation of that 63 as a means of
function in a timely complying with Sec.
manner after the airplane 23.2310, or may obtain
is exposed to lightning FAA acceptance of a
unless the system's different method of
recovery conflicts with compliance in accordance
other operational or with Sec. 23.2010.
functional requirements
of the system..
Replace 17.3.2 with the .........................
following:
(b) Each electrical and .........................
electronic system that
performs a function, the
failure of which would
significantly reduce the
capability of the
airplane or the ability
of the flight crew to
respond to an adverse
operating condition, must
be designed and installed
such that the system
recovers normal operation
of that function in a
timely manner after the
airplane is exposed to
lightning
Remove 17.3.3.............
F3062/F3062M-20................... Standard None. .........................
Specification for
Aircraft Powerplant
Installation.
F3063/F3063M-20................... Standard None. .........................
Specification for
Aircraft Fuel and
Energy Storage and
Delivery.
F3064/F3064M-21................... Standard None. .........................
Specification for
Aircraft Powerplant
Control, Operation,
and Indication.
F3065/F3065M-21a.................. Standard None. .........................
Specification for
Aircraft Propeller
System Installation.
F3066/F3066M-18................... Standard None. .........................
Specification for
Aircraft Powerplant
Installation Hazard
Mitigation.
F3082/F3082M-17................... Standard None. .........................
Specification for
Weights and Centers
of Gravity of
Aircraft.
F3083/F3083M-20a.................. Standard None. .........................
Specification for
Emergency
Conditions, Occupant
Safety and
Accommodations.
F3093/F3093M-21................... Standard None. .........................
Specification for
Aeroelasticity
Requirements.
F3114-21.......................... Standard None. .........................
Specification for
Structures.
F3115/F3115M-20................... Standard None...................... If applicant proposes to
Specification for use F3115/F3115M-20
Structural section 4.3 or 6.3.3,
Durability for Small Policy & Innovation
Aeroplanes. Division will be
involved as the standard
is applied during
projects to review the
approach to determining
similarity (F3115/F3115M-
20 section 4.3) and
criteria defining
obvious damage (F3115/
F3115M-20 section
6.3.3).
[[Page 13913]]
F3116/F3116M-18e2................. Standard Replace: Section 4.1.4.
Specification for With: FAA Section 4.1.4
Design Loads and ``Appendix X1 through
Conditions. Appendix X4 provides,
within the limitations
specified within the
appendix, a simplified
means of compliance with
several of the
requirements set forth in
Sections 4.2 to 4.26 and
7.1 to 7.9 that can be
applied as one (but not
the only) means to
comply. If the simplified
methods in appendix X1
through X3 are used, they
must be used together in
their entirety..
Replace: Section X1.1.1...
With: FAA Section X1.1.1
``The methods provided in
this appendix provide one
possible means (but not
the only possible means)
of compliance and can
only be applied to level
1 and level 2 low speed
airplanes.''.
Replace: Section X2.1.1...
With: FAA Section X2.1.1
``The methods provided in
this appendix provide one
possible means (but not
the only possible means)
of compliance and can
only be applied to level
1 and level 2 low speed
airplanes.''.
Replace: Section X3.1.1...
With: FAA Section X3.1.1
``The methods provided in
this appendix provide one
possible means (but not
the only possible means)
of compliance and can
only be applied to level
1 and level 2 low speed
airplanes.''.
Replace: Section X4.1.1. .........................
With: FAA Section X4.1.1
``The methods provided in
this appendix provide one
possible means (but not
the only possible means)
of compliance and can
only be applied to level
1 low speed airplanes.''.
F3117/F3117M-20................... Standard Add:
Specification for 4.3 Windshields and
Crew Interface in Windows..
Aircraft. 4.3.1 For Level 4
airplanes, the windshield
panels in front of the
pilots must be arranged
so that, assuming the
loss of vision through
any one panel, one or
more panels remain
available for use by a
pilot seated at a pilot
station to permit
continued safe flight and
landing.
Or For Level 4 Airplanes .........................
Add F3117/F3117M--21a
Section 4.3.
F3120/F3120M-20................... Standard None. .........................
Specification for
Ice Protection for
General Aviation.
F3173/F3173M-21................... Standard None. .........................
Specification for
Aircraft Handling
Characteristics.
F3174/F3174M-19................... Standard None. .........................
Specification for
Establishing
Operating
Limitations and
Information for
Aeroplanes.
F3179/F3179M-20................... Standard None. .........................
Specification for
Performance of
Aircraft.
F3180/F3180M-19................... Standard FAA does not universally Applicants are encouraged
Specification for accept F3180/F3180M-19 to consider proposing
Low-Speed Flight due to inexperience with F3180/F3180M-19,
Characteristics of Alternative 2 within the particularly Alternative
Aircraft. standard. FAA previously 2, for development of
and continues to accept their method of
F3180/F3180M-16. compliance for low speed
handling qualities on a
project-by-project
basis, or may obtain FAA
acceptance of a
different method of
compliance in accordance
with Sec. 23.2010.
[[Page 13914]]
F3227/F3227M-21................... Standard Remove: Tables 1, 2, and 3 Aircraft Type Code
Specification for compliance matrix tables
Environmental found in F3227/F3227M-
Systems in Small 21, are not accepted.
Aircraft. Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3228-17.......................... Standard Remove: Table 1........... Aircraft Type Code
Specification for compliance matrix table
Flight Data and found in F3228-17 are
Voice Recording in not accepted.
Small Aircraft. Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3229/F3229M-17................... Standard Practice for Remove: Table 1........... Aircraft Type Code
Static Pressure compliance matrix table
System Tests in found in F3229/F3229M-17
Small Aircraft. are not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3230-20a......................... Standard Practice for Remove: Table 1........... Aircraft Type Code
Safety Assessments compliance matrix table
of Systems and found in F3230-20a are
Equipment in Small not accepted.
Aircraft. Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3231/F3231M-21................... Standard Remove: Table 1........... Aircraft Type Code
Specification for compliance matrix table
Electrical Systems found in F3231/F3231M-21
for Aircraft with are not accepted.
Combustion Engine Applicability will be
Electrical Power determined by the Small
Generation. Airplane Strategic
Policy Section.
F3232/F3232M-20................... Standard Remove: Tables 1 and 2.... Aircraft Type Code
Specification for compliance matrix tables
Flight Controls in found in F3232/F3232M-20
Small Aircraft. are not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3233/F3233M-21................... Standard Remove: Table 1........... Aircraft Type Code
Specification for compliance matrix table
Instrumentation in found in F3233/F3233M-21
Small Aircraft. are not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3234/F3234M-17................... Standard Remove: Table 1........... Aircraft Type Code
Specification for compliance matrix table
Exterior Lighting in found in F3234/F3234M-17
Small Aircraft. are not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3235-17a......................... Standard Remove: Section 4.2 If applying for
Specification for Remove: Table 1........... certification of an
Aircraft Storage airplane with installed
Batteries. lithium batteries,
applicants may use the
guidance provided by
RTCA DO-311A, or may
obtain FAA acceptance of
a different method of
compliance in accordance
with Sec. 23.2010.
Aircraft Type Code
compliance matrix table
found in F3235-17a are
not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3236-17.......................... Standard Remove: Table 1........... Aircraft Type Code
Specification for Revise: Table 2 400 to 700 compliance matrix table
High Intensity Mhz frequency range field found in F3236-17 are
Radiated Field strength average value:. not accepted.
(HIRF) Protection in Replace: ``100 volts/ Applicability will be
Small Aircraft. meter.''. determined by the Small
With: ``50 volts/meter.''. Airplane Strategic
Policy Section.
Replace: Section 4.2.3.3..
With: FAA Section 4.2.3.3
``From 40 to 400 MHz, use
conducted susceptibility
tests, starting at a
minimum of 30 mA at 40
MHz, decreasing 20 dB per
frequency decade to a
minimum of 3 mA at 400
MHz.''.
F3239-19.......................... Standard FAA does not universally Applicants are encouraged
Specification for accept F3239-19 due to to consider proposing
Aircraft Electric inexperience with the F3239-19 for development
Propulsion Systems. standard. of their method of
compliance for electric
propulsion systems on a
project-by-project
basis. Any method of
compliance proposed must
establish a level of
safety equivalent to
certified reciprocating
and turbine propulsion
systems and receive
acceptance by FAA in
accordance with Sec.
23.2010.
F3254-19.......................... Standard Figures 2, 3 and 4 Other proposed
Specification for Replace: ``Remote''. probabilities will be
Aircraft Interaction With: ``10-\5\.''......... considered by the FAA on
of Systems and Replace: ``Extremely a case by case basis.
Structures. Improbable.''.
With: ``10-\8\'' for Level
1, 2 and 3 airplanes and
with ``10-\9\'' for Level
4 airplanes''.
[[Page 13915]]
F3309/F3309M-21................... Standard Practice for None. .........................
Simplified Safety
Assessment of
Systems and
Equipment in Small
Aircraft.
F3316/F3316M-19................... Standard FAA does not universally Applicants are encouraged
Specification for accept F3316/F3316M-19 to consider proposing
Electrical Systems due to inexperience with F3316/F3316M-19 for
for Aircraft with the standard. development of their
Electric or Hybrid- Remove: Table 1........... method of compliance for
Electric Propulsion. electrical systems
installed on airplanes
with electric or hybrid-
electric propulsion
systems on a project-by-
project basis.
Applicants may obtain
FAA acceptance of a
different method of
compliance in accordance
with Sec. 23.2010.
Aircraft Type Code
compliance matrix table
found in F3316/F3316M-19
are not accepted.
Applicability will be
determined by the Small
Airplane Strategic
Policy Section.
F3331-18.......................... Standard Practice for None. .........................
Aircraft Water Loads.
F3367-21.......................... Standard Practice for Replace: paragraph 5.1.1.
Simplified Methods With: Systems that are
for Addressing High- part of the Type
Intensity Radiated Certificated Engine must
Fields (HIRF) and be installed in
Indirect Effects of accordance with the
Lightning on engine manufacturer's
Aircraft. requirements. The minimum
HIRF and lightning
qualification in
accordance with Sections
8 and 9 of this ASTM
practice should be met at
the aircraft level,
except for engine control
systems in Level 1 and 2
airplanes which should
meet the following;.
<bullet> HIRF: DO-160,
Section 20--R for both
radiated and conducted
susceptibility.
<bullet> Lightning:
Utilize Guidance in AC
33.28-3.
For metallic fuselage DO-
160G, Section 22--A3J3L3
(shielded) and A3H3L3
(unshielded).
For composite fuselage DO-
160G, Section 22--B3K3L3
(shielded) and B3H3L3
(unshielded).
Use of lower HIRF and .........................
lighting induced voltage
& current levels may be
acceptable for electronic
engine control systems if
substantiated at the
airplane level (by test
in the proposed
installation or similar)
when exposed to external
HIRF environment per AC20-
158A and Lightning per
AC20-136B; using
shielding and grounding
of the electronic engine
control system and
accessories in the given
installation.
F3380-19.......................... Standard Practice for None. .........................
Structural
Compliance of Very
Light Aeroplanes.
F3396/F3396M-20................... Standard Practice for None. .........................
Aircraft Simplified
Loads.
F3408/F3408M-21................... Standard None. .........................
Specification for
Aircraft Emergency
Parachute Recovery
Systems.
F3432-20a......................... Standard Practice for None. .........................
Powerplant
Instruments.
----------------------------------------------------------------------------------------------------------------
[[Page 13916]]
Table 2--Side-By-Side View of 14 CFR Part 23 Regulations and ASTM F3264-21 Sections
----------------------------------------------------------------------------------------------------------------
Part 23 amendment 23-64
regulation(s) ASTM F3264-21 section(s) \7\ ASTM F3264-21 subsection(s) \8\
----------------------------------------------------------------------------------------------------------------
23.1457............................... 9.12 Installation of Cockpit 9.12.1 F3061/F3061M--20 Standard
Recorders. Specification for Systems and Equipment
in Small Aircraft.
9.12.1.1 F3228--17 Standard
Specification for Flight Data and
Voice Recording in Small Aircraft.
23.1459............................... 9.13 Installation of Flight 9.13.1 F3061/F3061M--20 Standard
Data Recorders. Specification for Systems and Equipment
in Small Aircraft.
9.13.1.1 F3228--17 Standard
Specification for Flight Data and
Voice Recording in Small Aircraft.
23.1529............................... 10.6 Instructions for 10.6.1 F3120/F3120M--20 Standard
Continued Airworthiness. Specification for Ice Protection for
General Aviation.
10.6.2 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
10.6.3 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
Subpart B--Flight:
23.2100........................... 5.1 Weight/Mass and Centre of 5.1.1 F3082/F3082M--17 Standard
Gravity. Specification for Weights and Centers
of Gravity of Aircraft.
5.1.2 F3114--21 Standard Specification
for Structures.
23.2105........................... 5.2 Performance Data.......... 5.2.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2110........................... 5.3 Stall Speed............... 5.3.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2115........................... 5.4 Takeoff Performance....... 5.4.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2120........................... 5.5 Climb Requirements........ 5.5.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2125........................... 5.6 Climb Information......... 5.6.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2130........................... 5.7 Landing................... 5.7.1 F3179/F3179M--20 Standard
Specification for Performance of
Aircraft.
23.2135........................... 5.8 Controllability........... 5.8.1 F3173/F3173M--21 Standard
Specification for Aircraft Handling
Characteristics.
23.2140........................... 5.9 Trim...................... 5.9.1 F3173/F3173M--21 Standard
Specification for Aircraft Handling
Characteristics.
23.2145........................... 5.10 Stability................ 5.10.1 F3173/F3173M--21 Standard
Specification for Aircraft Handling
Characteristics.
23.2150........................... 5.11 Stall Characteristics, 5.11.1 F3180/F3180M--19 Standard
Stall Warning, and Spins. Specification for Low-Speed Flight
Characteristics of Aircraft.
23.2155........................... 5.12 Ground and Water Handling 5.12.1 F3173/F3173M--21 Standard
Characteristics. Specification for Aircraft Handling
Characteristics.
23.2160........................... 5.13 Vibration, Buffeting, and 5.13.1 F3173/F3173M--21 Standard
High-Speed Characteristics. Specification for Aircraft Handling
Characteristics.
23.2165........................... 5.14 Performance and Flight 5.14.1 F3120/F3120M--20 Standard
Characteristics Requirements Specification for Ice Protection for
for Flight in Icing General Aviation Aircraft.
Conditions.
Subpart C--Structures:
23.2200........................... 6.1 Structural Design Envelope 6.1.1 F3116/F3116M--18e2 Standard
Specification for Design Loads and
Conditions.
6.1.1.1 F3396/F3396M--20 Standard
Practice for Aircraft Simplified
Loads.
23.2205........................... 6.2 Interaction of Systems and 6.2.1 F3254--19 Standard Specification
Structure. for Aircraft Interaction of Systems and
Structures.
23.2210........................... 6.3 Structural Design Loads... 6.3.1 F3116/F3116M--18e2 Standard
Specification for Design Loads and
Conditions.
6.3.1.1 F3396/F3396M--20 Standard
Practice for Aircraft Simplified
Loads.
6.3.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2215........................... 6.4 Flight Load Conditions.... 6.4.1 F3116/F3116M--18e2 Standard
Specification for Design Loads and
Conditions.
6.4.1.1 F3396/F3396M--20 Standard
Practice for Aircraft Simplified
Loads.
23.2220........................... 6.5 Ground and Water Load 6.5.1 F3116/F3116M--18e2 Standard
Conditions. Specification for Design Loads and
Conditions.
6.5.1.1 F3331--18 Standard Practice
for Aircraft Water Loads.
23.2225........................... 6.6 Component Loading 6.6.1 F3061/F3061M--20 Standard
Conditions. Specification for Systems and Equipment
in Small Aircraft.
6.6.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
6.6.2 F3116/F3116M--18e2 Standard
Specification for Design Loads and
Conditions.
[[Page 13917]]
6.6.2.1 F3396/F3396M--20 Standard
Practice for Aircraft Simplified
Loads.
23.2230........................... 6.7 Limit and Ultimate Loads.. 6.7.1 F3114--21 Standard Specification
for Structures.
6.7.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2235........................... 6.8 Structural Strength....... 6.8.1 F3114--21 Standard Specification
for Structures.
6.8.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2240........................... 6.9 Structural Durability..... 6.9.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
6.9.2 F3066/F3066M -18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
6.9.3 F3115/F3115M--20 Standard
Specification for Structural Durability
for Small Aeroplanes.
6.9.3.1 F3380 -19 Standard Practice
for Structural Compliance of Very
Light Aeroplanes.
6.9.4 F3116/F3116M--18e2 Standard
Specification for Design Loads and
Conditions.
23.2245........................... 6.10 Aeroelasticity........... 6.10.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
6.10.2 F3093/F3093M--21 Standard
Specification for Aeroelasticity
Requirements.
23.2250........................... 6.11 Design and Construction 6.11.1 F3061/F3061M--20 Standard
Principles. Specification for Systems and Equipment
in Small Aircraft.
6.11.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
6.11.2 F3114--21 Standard Specification
for Structures.
6.11.2.1 F3380--19 Standard Practice
for Structural Compliance of Very
Light Aeroplanes.
6.11.3 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2255........................... 6.12 Protection of Structure.. 6.12.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
6.12.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
6.12.2 F3114--21 Standard Specification
for Structures.
6.12.2.1 F3380--19 Standard Practice
for Structural Compliance of Very
Light Aeroplanes.
6.12.3 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
6.12.4 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2260........................... 6.13 Materials and Processes.. 6.13.1 F3114--21 Standard Specification
for Structures.
6.13.1.1 F3380--19 Standard Practice
for Structural Compliance of Very
Light Aeroplanes.
6.13.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2265........................... 6.14 Special Factors of Safety 6.14.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
6.14.2 F3114--21 Standard Specification
for Structures.
6.14.2.1 F3380 -19 Standard Practice for
Structural Compliance of Very Light
Aeroplanes.
23.2270........................... 6.15 Emergency Conditions..... 6.15.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
6.15.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
6.15.2 F3083/F3083M--20a Standard
Specification for Emergency Conditions,
Occupant Safety and Accommodations.
6.15.3 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
Subpart D--Design and Construction
23.2300........................... 7.1 Flight Control Systems.... 7.1.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
7.1.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
7.1.2 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
7.1.3 F3117/F3117M--20 Standard
Specification for Crew Interface.
[[Page 13918]]
23.2305........................... 7.2 Landing Gear Systems...... 7.2.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
23.2310........................... 7.3 Buoyancy for Seaplanes and 7.3.1 F3061/F3061M--20 Standard
Amphibians. Specification for Systems and Equipment
in Small Aircraft.
23.2315........................... 7.4 Means of Egress and 7.4.1 F3061/F3061M--20 Standard
Emergency Exits. Specification for Systems and Equipment
in Small Aircraft.
7.4.2 F3083/F3083M--20a Standard
Specification for Emergency Conditions,
Occupant Safety and Accommodations.
23.2320........................... 7.5 Occupant Physical 7.5.1 F3061/F3061M--20 Standard
Environment. Specification for Systems and Equipment
in Small Aircraft.
7.5.1.1 F3227/F3227M--21 Standard
Specification for Environmental
Systems in Small Aircraft.
7.5.2 F3083/F3083M--20a Standard
Specification for Emergency Conditions,
Occupant Safety and Accommodations.
7.5.3 F3114--21 Standard Specification
for Structures.
7.5.4 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
23.2325........................... 7.6 Fire Protection........... 7.6.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
7.6.1.1 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
7.6.1.2 F3234/F3234M--17 Standard
Specification for Exterior Lighting
in Small Aircraft.
7.6.1.3 F3316/F3316M--19 Standard
Specification for Electrical Systems
for Aircraft with Electric or Hybrid-
Electric Propulsion.
7.6.2 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
7.6.3 F3083/F3083M--20a Standard
Specification for Emergency Conditions,
Occupant Safety and Accommodations.
7.6.4 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2330........................... 7.7 Fire Protection in 7.7.1 F3061/F3061M--20 Standard
Designated Fire Zones and Specification for Systems and Equipment
Adjacent Areas. in Small Aircraft.
7.7.1.1 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
7.7.2 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
7.7.3 F3114--21 Standard Specification
for Structures.
23.2335........................... 7.8 Lightning Protection...... 7.8.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
Subpart E--Powerplant:
23.2400........................... 8.1 Powerplant Installation... 8.1.1 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
8.1.2 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
8.1.3 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
8.1.4 F3065/F3065M--21a Standard
Specification for Aircraft Propeller
System Installation.
8.1.5 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.1.6 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2405........................... 8.2 Power or Thrust Control 8.2.1 F3062/F3062M--20 Standard
Systems. Specification for Aircraft Powerplant
Installation.
8.2.2 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
8.2.3 F3065/F3065M--21a Standard
Specification for Aircraft Propeller
System Installation.
8.2.4 F3117/F3117M--20 Standard
Specification for Crew Interface.
23.2410........................... 8.3 Powerplant Installation 8.3.1 F3061/F3061M--20 Standard
Hazard Assessment. Specification for Systems and Equipment
in Small Aircraft.
8.3.2 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
8.3.3 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
8.3.4 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
[[Page 13919]]
8.3.5 F3065/F3065M--21a Standard
Specification for Aircraft Propeller
System Installation.
8.3.6 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.3.7 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
8.3.8 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2415........................... 8.4 Powerplant Installation 8.4.1 F3062/F3062M--20 Standard
Ice Protection. Specification for Aircraft Powerplant
Installation.
8.4.2 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
8.4.3 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.4.4 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2420........................... 8.5 Reversing Systems......... 8.5.1 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
8.5.2 F3065/F3065M--21a Standard
Specification for Aircraft Propeller
System Installation.
8.5.3 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2425........................... 8.6 Powerplant Operational 8.6.1 F3062/F3062M--20 Standard
Characteristics. Specification for Aircraft Powerplant
Installation.
8.6.2 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
8.6.3 F3065/F3065M--21a Standard
Specification for Aircraft Propeller
System Installation.
8.6.4 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.6.5 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
8.6.6 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2430........................... 8.7 Fuel and Energy Storage 8.7.1 F3062/F3062M--20 Standard
and Distribution Systems. Specification for Aircraft Powerplant
Installation.
8.7.2 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
8.7.3 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
8.7.4 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.7.5 F3114--21 Standard Specification
for Structures.
8.7.6 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2435........................... 8.8 Powerplant Induction, 8.8.1 F3062/F3062M--20 Standard
Exhaust, and Support Systems. Specification for Aircraft Powerplant
Installation.
8.8.2 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
23.2440........................... 8.9 Powerplant Installation 8.9.1 F3061/F3061M--20 Standard
Fire Protection. Specification for Systems and Equipment
in Small Aircraft.
8.9.2 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
8.9.3 F3063/F3063M--20 Standard
Specification for Aircraft Fuel an
Energy Storage and Delivery.
8.9.4 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
8.9.5 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
8.9.6 F3239--19 Standard Specification
for Aircraft Electric Propulsion
Systems.
Subpart F--Equipment:
23.2500........................... 9.1 Systems and Equipment 9.1.1 F3061/F3061M--20 Standard
Function--Requirements. Specification for Systems and Equipment
in Small Aircraft.
9.1.1.1 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
9.1.1.1(a) F3235--17a Standard
Specification for Aircraft Storage
Batteries.
[[Page 13920]]
9.1.1.2 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
9.1.1.3 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.1.1.3(a) F3229/F3229M--17 Standard
Practice for Static Pressure System
Tests in Small Aircraft.
9.1.1.4 F3316/F3316M--19 Standard
Specification for Electrical Systems
for Aircraft with Electric or Hybrid-
Electric Propulsion.
9.1.2 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
9.1.3 F3066/F3066M--18 Standard
Specification for Aircraft Powerplant
Installation Hazard Mitigation.
9.1.4 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
9.1.5 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
9.1.6 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2505........................... 9.2 Equipment Function and 9.2.1 F3061/F3061M--20 Standard
Installation Requirements. Specification for Systems and Equipment
in Small Aircraft.
9.2.1.1 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
9.2.1.1(a) F3235--17a Standard
Specification for Aircraft Storage
Batteries.
9.2.1.2 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
9.2.1.3 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.2.1.4 F3316/F3316M--19 Standard
Specification for Electrical Systems
for Aircraft with Electric or Hybrid-
Electric Propulsion.
9.2.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2510........................... 9.3 Equipment, Systems, and 9.3.1 F3061/F3061M--20 Standard
Installation. Specification for Systems and Equipment
in Small Aircraft.
9.3.1.1 F3230--20a Standard Practice
for Safety Assessments of Systems
and Equipment in Small Aircraft.
9.3.1.2 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.3.1.3 F3227/F3227M--21 Standard
Specification for Environmental
Systems in Small Aircraft.
9.3.1.4 F3309/F3309M--21 Standard
Practice for Simplified Safety
Assessment of Systems and Equipment
in Small Aircraft.
9.3.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2515........................... 9.4 Electrical and Electronic 9.4.1 F3061/F3061M--20 Standard
System Lightning Protection. Specification for Systems and Equipment
in Small Aircraft.
9.4.1.1 F3367--21 Standard Practice
for Simplified Methods for
Addressing High-Intensity Radiated
Fields (HIRF) and Indirect Effects
of Lightning on Aircraft.
23.2520........................... 9.5 High Intensity Radiated 9.5.1 F3061/F3061M--20 Standard
Fields (HIRF) Protection. Specification for Systems and Equipment
in Small Aircraft.
9.5.1.1 F3236--17 Standard
Specification for High Intensity
Radiated Field (HIRF) Protection in
Small Aircraft.
9.5.1.2 F3367--21 Standard Practice
for Simplified Methods for
Addressing High-Intensity Radiated
Fields (HIRF) and Indirect Effects
of Lightning on Aircraft.
23.2525........................... 9.6 System Power Generation, 9.6.1 F3061/F3061M--20 Standard
Storage, and Distribution. Specification for Systems and Equipment
in Small Aircraft.
9.6.1.1 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
9.6.1.1(a) F2490--20 Standard Guide
for Aircraft Electrical Load and
Power Source Capacity Analysis.
9.6.1.2 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.6.1.3 F3316/F3316M--19 Standard
Specification for Electrical Systems
for Aircraft with Electric or Hybrid-
Electric Propulsion.
[[Page 13921]]
9.6.1.3(a) F2490--20 Standard Guide
for Aircraft Electrical Load and
Power Source Capacity Analysis.
9.6.2 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
9.6.3 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
23.2530........................... 9.7 External and Cockpit 9.7.1 F3061/F3061M--20 Standard
Lighting. Specification for Systems and Equipment
in Small Aircraft.
9.7.1.1 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.7.1.2 F3234/F3234M--17 Standard
Specification for Exterior Lighting
in Small Aircraft.
9.7.2 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
9.7.3 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
23.2535........................... 9.8 Safety Equipment.......... 9.8.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
9.8.2 F3083/F3083M--20a Standard
Specification for Emergency Conditions,
Occupant Safety and Accommodations.
9.8.3 F3117/F3117M--20 Standard
Specification for Crew Interface.
23.2540........................... 9.9 Flight in Icing Conditions 9.9.1 F3061/F3061M--20 Standard
Specification for Systems and Equipment
in Small Aircraft.
9.9.1.1 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
9.9.2 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
23.2545........................... 9.10 Pressurized System 9.10.1 F3061/F3061M--20 Standard
Elements. Specification for Systems and Equipment
in Small Aircraft.
9.10.2 F3229/F3229M--17 Standard
Practice for Static Pressure System
Tests in Small Aircraft.
23.2550........................... 9.11 Equipment Containing High- 9.11.1 F3061/F3061M--20 Standard
Energy Rotors. Specification for Systems and Equipment
in Small Aircraft.
Subpart G--Flight crew Interface and
Other Information:
23.2600........................... 10.1 Flight crew Compartment 10.1.1 F3061/F3061M--20 Standard
Interface. Specification for Systems and Equipment
in Small Aircraft.
10.1.1.1 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
10.1.2 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
10.1.3 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
10.1.4 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
10.1.5 F3114--21 Standard Specification
for Structures.
10.1.6 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
10.1.7 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2605........................... 10.2 Installation and 10.2.1 F3061/F3061M--20 Standard
Operation Information. Specification for Systems and Equipment
in Small Aircraft.
10.2.1.1 F3227/F3227M--21 Standard
Specification for Environmental
Systems in Small Aircraft.
10.2.1.2 F3231/F3231M--21 Standard
Specification for Electrical Systems
for Aircraft with Combustion Engine
Electrical Power Generation.
10.2.1.3 F3232/F3232M--20 Standard
Specification for Flight Controls in
Small Aircraft.
10.2.1.4 F3233/F3233M--21 Standard
Specification for Instrumentation in
Small Aircraft.
10.2.2 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
10.2.3 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
10.2.4 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
10.2.5 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
[[Page 13922]]
10.2.6 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
10.2.7 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2610........................... 10.3 Instrument Markings, 10.3.1 F3061/F3061M--20 Standard
Control Markings, and Specification for Systems and Equipment
Placards:. in Small Aircraft.
10.3.2 F3063/F3063M--20 Standard
Specification for Aircraft Fuel and
Energy Storage and Delivery.
10.3.3 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
10.3.4 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
10.3.5 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
23.2615........................... 10.4 Flight, Navigation, and 10.4.1 F3061/F3061M--20 Standard
Powerplant Instruments. Specification for Systems and Equipment
in Small Aircraft.
10.4.2 F3062/F3062M--20 Standard
Specification for Aircraft Powerplant
Installation.
10.4.3 F3064/F3064M--21 Standard
Specification for Aircraft Powerplant
Control, Operation, and Indication.
10.4.3.1 F3432--20a Standard Practice
for Powerplant Instruments.
10.4.4 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
23.2620........................... 5.15 Operating Limitations.... 5.15.1 F3174/F3174M--19 Standard
10.5 Airplane Flight Manual... Specification for Establishing
Operating Limitations and Information
for Aeroplanes.
5.15.2 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
10.5.1 F3117/F3117M--20 Standard
Specification for Crew Interface in
Aircraft.
10.5.2 F3174/F3174M--19 Standard
Specification for Establishing
Operating Limitations and Information
for Aeroplanes.
10.5.3 F3120/F3120M--20 Standard
Specification for Ice Protection for
General Aviation Aircraft.
10.5.4 F3408/F3408M--21 Standard
Specification for Aircraft Emergency
Parachute Recovery Systems.
----------------------------------------------------------------------------------------------------------------
Editorial, Reapproval, Revision or Withdrawal
---------------------------------------------------------------------------
\7\ The ASTM F3264-21 Section(s) provides a means of compliance
intended to be used on projects for traditional part 23 airplanes,
not for novel designs. Novel designs require evaluation and possible
modification of the means of compliance.
\8\ The FAA does not accept the Aircraft Type Code compliance
matrix tables included in F3061/F3061M-20, F3227/F3227M-21, F3228-
17, F3229/F3229M-17, F3230-20a, F3231/F3231M-21, F3232/F3232M-20,
F3233/F3233M-21, F3234/F3234M-17, F3235-17a, F3236-17, and F3316/
F3316M-19. Applicability will be determined by the Small Airplane
Strategic Policy Section.
---------------------------------------------------------------------------
ASTM policy is that a consensus standard should be reviewed in its
entirety by the responsible subcommittee and must be balloted for
reapproval, revision, or withdrawal, within five years of its last
approval date. When an ASTM standard is reapproved, that reapproval is
denoted by the year in parentheses (e.g., F2427-05a(2013)).
This date indicates the completion of a review cycle with no
technical changes made to the standard. ASTM issues editorial changes
denoted by a superscript epsilon in the standard designation (e.g.,
F3235-17[epsi]1). This indicates information was corrected, and it did
not change the meaning or intent of a standard. Any means of compliance
accepted by this document, that is based on a standard later reapproved
or editorially changed, is also considered accepted and without the
need for a notice in the Federal Register.
ASTM revises a standard to make changes to its technical content.
Revisions to consensus standards serving as the basis for means of
compliance accepted by this document, will not be automatically
accepted, and will require further FAA acceptance in order for the
revisions to be an accepted means of compliance.
Availability
ASTM International Standard Designation F3264-21, ``Standard
Specification for Normal Category Aeroplanes Certification,'' is
available for online reading at <a href="https://www.astm.org/READINGLIBRARY/">https://www.astm.org/READINGLIBRARY/</a>.
ASTM copyrights these consensus standards, and charges the public a fee
for service. Individual downloads or reprints of a standard (single or
multiple copies, or special compilations and other related technical
information) may be obtained through <a href="http://www.astm.org">www.astm.org</a> or contacting ASTM at
(610) 832-9585 (phone), (610) 832-9555 (fax), or through
<a href="/cdn-cgi/l/email-protection#93e0f6e1e5faf0f6d3f2e0e7febdfce1f4"><span class="__cf_email__" data-cfemail="e89b8d9a9e818b8da8899b9c85c6879a8f">[email protected]</span></a> (email). To inquire about consensus standard content
and/or membership or about ASTM Offices abroad, contact Joe Koury,
Staff Manager for Committee F44 on General Aviation Aircraft: (610)
832-9804, <a href="/cdn-cgi/l/email-protection#b0dadbdfc5c2c9f0d1c3c4dd9edfc2d7"><span class="__cf_email__" data-cfemail="2d474642585f546d4c5e594003425f4a">[email protected]</span></a>.
The FAA maintains a list of accepted means of compliance on the FAA
website at <a href="https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/">https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/</a>.
Issued in Kansas City, Missouri, on March 2, 2022.
[[Page 13923]]
Patrick Mullen,
Manager, Technical Innovation Policy Branch, Policy and Innovation
Division, Aircraft Certification Service.
[FR Doc. 2022-04845 Filed 3-10-22; 8:45 am]
BILLING CODE 4910-13-P
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</html>Indexed from Federal Register on March 11, 2022.
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