Accepted Means of Compliance; Airworthiness Standards: Normal Category Airplanes, 13911-13923 [2022-04845]
Download as PDF
<![CDATA[
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
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
Federal Aviation
Administration, Department of
Transportation (DOT).
ACTION: Issuance of accepted means of
compliance.
AGENCY:
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 sideby-side view, linking applicable
regulations to the associated ASTM
sections.
SUMMARY:
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:
hieu.nguyen@faa.gov.
SUPPLEMENTARY INFORMATION:
DATES:
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.
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.
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.
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.
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.
13911
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 § 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.’’
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
ASTM designation No.
lotter on DSK11XQN23PROD with RULES1
F2490–20 ....................
Standard Guide for
Aircraft Electrical
Load and Power
Source Capacity
Analysis.
1 Ref Public Law 104–113 as amended by Public
Law 107–107.
2 Ref Public Law 113–53.
3 See https://www.federalregister.gov/documents/
2016/12/30/2016-30246/revision-of-airworthiness-
VerDate Sep<11>2014
Changes required for FAA acceptance 5
ASTM document title
17:21 Mar 10, 2022
Jkt 256001
Additional information 6
None.
standards-for-normal-utility-acrobatic-andcommuter-category-airplanes.
4 See https://drs.faa.gov/browse.
5 The means of compliance are inteded for
traditional part 23 airplanes, not for novel designs.
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
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: https://
www.faa.gov/aircraft/air_cert/design_approvals/
small_airplanes/small_airplanes_regs/.
E:\FR\FM\11MRR1.SGM
11MRR1
13912
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
TABLE 1—PART 23 ACCEPTED MEANS OF COMPLIANCE BASED ON ASTM CONSENSUS STANDARDS—Continued
ASTM designation No.
ASTM document title
Changes required for FAA acceptance 5
Additional information 6
F3061/F3061M–20 ......
Standard Specification
for Systems and
Equipment in Small
Aircraft.
Aircraft Type Code compliance matrix tables
found in F3061/F3061M–20 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
F3061/F3061M–20 does not contain means
for showing compliance to § 23.2310 Buoyancy for seaplanes and amphibians. If applying for certification of a seaplane or amphibian, applicants may use the provisions
of §§ 23.751, 23.755, and 23.757 at
amendment 23–63 as a means of complying with § 23.2310, or may obtain FAA
acceptance of a different method of compliance in accordance with § 23.2010.
F3062/F3062M–20 ......
Standard Specification
for Aircraft Powerplant Installation.
Standard Specification
for Aircraft Fuel and
Energy Storage and
Delivery.
Standard Specification
for Aircraft Powerplant Control, Operation, and Indication.
Standard Specification
for Aircraft Propeller
System Installation.
Standard Specification
for Aircraft Powerplant Installation
Hazard Mitigation.
Standard Specification
for Weights and
Centers of Gravity
of Aircraft.
Standard Specification
for Emergency Conditions, Occupant
Safety and Accommodations.
Standard Specification
for Aeroelasticity
Requirements.
Standard Specification
for Structures.
Standard Specification
for Structural Durability for Small
Aeroplanes.
Remove: Tables 1, 3, 4, 5, 13 and 14 ...........
Replace 17.3.1 with the following:
(a) Each electrical or electronic system that
performs a function, the failure of which
would prevent the continued safe flight and
landing of the airplane, must be designed
and installed such that—
(1) The function at the airplane level is not
adversely affected during and after the time
the airplane is exposed to lightning; and
(2) The system recovers normal operation of
that function in a timely manner after the
airplane is exposed to lightning unless the
system’s recovery conflicts with other operational or 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.
None.
F3063/F3063M–20 ......
F3064/F3064M–21 ......
F3065/F3065M–21a ....
F3066/F3066M–18 ......
F3082/F3082M–17 ......
F3083/F3083M–20a ....
F3093/F3093M–21 ......
F3114–21 ....................
lotter on DSK11XQN23PROD with RULES1
F3115/F3115M–20 ......
VerDate Sep<11>2014
16:57 Mar 10, 2022
Jkt 256001
None.
None.
None.
None.
None.
None.
None.
None.
None ................................................................
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
If applicant proposes to use F3115/F3115M–
20 section 4.3 or 6.3.3, Policy & Innovation
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).
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
13913
TABLE 1—PART 23 ACCEPTED MEANS OF COMPLIANCE BASED ON ASTM CONSENSUS STANDARDS—Continued
ASTM designation No.
ASTM document title
Changes required for FAA acceptance 5
F3116/F3116M–18e2 ..
Standard Specification
for Design Loads
and Conditions.
F3117/F3117M–20 ......
Standard Specification
for Crew Interface in
Aircraft.
F3120/F3120M–20 ......
Standard Specification
for Ice Protection for
General Aviation.
Standard Specification
for Aircraft Handling
Characteristics.
Standard Specification
for Establishing Operating Limitations
and Information for
Aeroplanes.
Standard Specification
for Performance of
Aircraft.
Standard Specification
for Low-Speed
Flight Characteristics of Aircraft.
Replace: Section 4.1.4.
With: FAA Section 4.1.4 ‘‘Appendix X1
through 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.’’.
Add:
4.3 Windshields and Windows.
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.
None.
F3173/F3173M–21 ......
F3174/F3174M–19 ......
lotter on DSK11XQN23PROD with RULES1
F3179/F3179M–20 ......
F3180/F3180M–19 ......
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
Additional information 6
None.
None.
None.
FAA does not universally accept F3180/
F3180M–19 due to inexperience with Alternative 2 within the standard. FAA previously and continues to accept F3180/
F3180M–16.
PO 00000
Frm 00013
Fmt 4700
Sfmt 4700
Applicants are encouraged to consider proposing F3180/F3180M–19, particularly Alternative 2, for development of their method of 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
§ 23.2010.
E:\FR\FM\11MRR1.SGM
11MRR1
13914
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
TABLE 1—PART 23 ACCEPTED MEANS OF COMPLIANCE BASED ON ASTM CONSENSUS STANDARDS—Continued
ASTM designation No.
ASTM document title
Changes required for FAA acceptance 5
Additional information 6
F3227/F3227M–21 ......
Standard Specification
for Environmental
Systems in Small
Aircraft.
Standard Specification
for Flight Data and
Voice Recording in
Small Aircraft.
Standard Practice for
Static Pressure System Tests in Small
Aircraft.
Standard Practice for
Safety Assessments
of Systems and
Equipment in Small
Aircraft.
Standard Specification
for Electrical Systems for Aircraft with
Combustion Engine
Electrical Power
Generation.
Standard Specification
for Flight Controls in
Small Aircraft.
Remove: Tables 1, 2, and 3 ..........................
Aircraft Type Code compliance matrix tables
found in F3227/F3227M–21, are not accepted. Applicability will be determined by
the Small Airplane Strategic Policy Section.
Aircraft Type Code compliance matrix table
found in F3228–17 are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section.
Aircraft Type Code compliance matrix table
found in F3229/F3229M–17 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
Aircraft Type Code compliance matrix table
found in F3230–20a are not accepted. Applicability will be determined by the Small
Airplane Strategic Policy Section.
F3233/F3233M–21 ......
Standard Specification
for Instrumentation
in Small Aircraft.
Remove: Table 1 ............................................
F3234/F3234M–17 ......
Standard Specification
for Exterior Lighting
in Small Aircraft.
Remove: Table 1 ............................................
F3235–17a ..................
Standard Specification
for Aircraft Storage
Batteries.
Remove: Section 4.2
Remove: Table 1.
F3236–17 ....................
Standard Specification
for High Intensity
Radiated Field
(HIRF) Protection in
Small Aircraft.
F3239–19 ....................
Standard Specification
for Aircraft Electric
Propulsion Systems.
Remove: Table 1 ............................................
Revise: Table 2 400 to 700 Mhz frequency
range field strength average value:
Replace: ‘‘100 volts/meter.’’
With: ‘‘50 volts/meter.’’
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.’’.
FAA does not universally accept F3239–19
due to inexperience with the standard.
F3254–19 ....................
Standard Specification
for Aircraft Interaction of Systems
and Structures.
F3228–17 ....................
F3229/F3229M–17 ......
F3230–20a ..................
F3231/F3231M–21 ......
lotter on DSK11XQN23PROD with RULES1
F3232/F3232M–20 ......
Remove: Table 1 ............................................
Remove: Table 1 ............................................
Remove: Table 1 ............................................
Remove: Table 1 ............................................
Aircraft Type Code compliance matrix table
found in F3231/F3231M–21 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
Remove: Tables 1 and 2 ...............................
Aircraft Type Code compliance matrix tables
found in F3232/F3232M–20 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
Aircraft Type Code compliance matrix table
found in F3233/F3233M–21 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
Aircraft Type Code compliance matrix table
found in F3234/F3234M–17 are not accepted. Applicability will be determined by the
Small Airplane Strategic Policy Section.
If applying for certification of an airplane with
installed 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 § 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.
Aircraft Type Code compliance matrix table
found in F3236–17 are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section.
Figures 2, 3 and 4 Replace: ‘‘Remote’’ .........
With: ‘‘10¥5.’’
Replace: ‘‘Extremely Improbable.’’ .................
Applicants are encouraged to consider proposing F3239–19 for development 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 § 23.2010.
Other proposed probabilities will be considered by the FAA on a case by case basis.
With: ‘‘10¥8’’ for Level 1, 2 and 3 airplanes
and with ‘‘10¥9’’ for Level 4 airplanes’’.
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00014
Fmt 4700
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
13915
TABLE 1—PART 23 ACCEPTED MEANS OF COMPLIANCE BASED ON ASTM CONSENSUS STANDARDS—Continued
ASTM designation No.
ASTM document title
F3309/F3309M–21 ......
Standard Practice for
Simplified Safety
Assessment of Systems and Equipment
in Small Aircraft.
Standard Specification
for Electrical Systems for Aircraft with
Electric or HybridElectric Propulsion.
F3316/F3316M–19 ......
F3331–18 ....................
F3367–21 ....................
F3380–19 ....................
F3396/F3396M–20 ......
F3408/F3408M–21 ......
lotter on DSK11XQN23PROD with RULES1
F3432–20a ..................
VerDate Sep<11>2014
Changes required for FAA acceptance 5
Additional information 6
None.
FAA does not universally accept F3316/
F3316M–19 due to inexperience with the
standard.
Remove: Table 1.
Applicants are encouraged to consider proposing F3316/F3316M–19 for development
of their method of compliance for 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
§ 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.
Standard Practice for
None.
Aircraft Water Loads.
Standard Practice for
Replace: paragraph 5.1.1.
Simplified Methods
With: Systems that are part of the Type Cerfor Addressing Hightificated Engine must be installed in acIntensity Radiated
cordance with the engine manufacturer’s
Fields (HIRF) and
requirements. The minimum HIRF and
Indirect Effects of
lightning qualification in accordance with
Lightning on Aircraft.
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;
• HIRF: DO–160, Section 20—R for both radiated and conducted susceptibility.
• 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.
Standard Practice for
None.
Structural Compliance of Very Light
Aeroplanes.
Standard Practice for
None.
Aircraft Simplified
Loads.
Standard Specification None.
for Aircraft Emergency Parachute
Recovery Systems.
Standard Practice for
None.
Powerplant Instruments.
16:57 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00015
Fmt 4700
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
13916
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
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 Recorders .............
23.1459 .........................
9.13 Installation of Flight Data Recorders .......
23.1529 .........................
10.6 Instructions for Continued Airworthiness
9.12.1 F3061/F3061M—20 Standard 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.
9.13.1 F3061/F3061M—20 Standard 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.
10.6.1 F3120/F3120M—20 Standard 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 Gravity ..........
23.2105 ..................
5.2 Performance Data ......................................
23.2110 ..................
5.3 Stall Speed ................................................
23.2115 ..................
5.4 Takeoff Performance .................................
23.2120 ..................
5.5 Climb Requirements ..................................
23.2125 ..................
5.6 Climb Information .......................................
23.2130 ..................
5.7 Landing ......................................................
23.2135 ..................
5.8 Controllability .............................................
23.2140 ..................
5.9 Trim ............................................................
23.2145 ..................
5.10 Stability ....................................................
23.2150 ..................
5.11 Stall Characteristics, Stall Warning, and
Spins.
5.12 Ground and Water Handling Characteristics.
5.13 Vibration, Buffeting, and High-Speed
Characteristics.
5.14 Performance and Flight Characteristics
Requirements for Flight in Icing Conditions.
23.2155 ..................
23.2160 ..................
lotter on DSK11XQN23PROD with RULES1
23.2165 ..................
Subpart C—Structures:
23.2200 ..................
6.1 Structural Design Envelope .......................
23.2205 ..................
6.2 Interaction of Systems and Structure ........
23.2210 ..................
6.3 Structural Design Loads ............................
23.2215 ..................
6.4 Flight Load Conditions ...............................
23.2220 ..................
6.5 Ground and Water Load Conditions ..........
23.2225 ..................
6.6 Component Loading Conditions ................
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00016
Fmt 4700
5.1.1 F3082/F3082M—17 Standard Specification for Weights and
Centers of Gravity of Aircraft.
5.1.2 F3114—21 Standard Specification for Structures.
5.2.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.3.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.4.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.5.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.6.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.7.1 F3179/F3179M—20 Standard Specification for Performance of
Aircraft.
5.8.1 F3173/F3173M—21 Standard Specification for Aircraft Handling
Characteristics.
5.9.1 F3173/F3173M—21 Standard Specification for Aircraft Handling
Characteristics.
5.10.1 F3173/F3173M—21 Standard Specification for Aircraft Handling Characteristics.
5.11.1 F3180/F3180M—19 Standard Specification for Low-Speed
Flight Characteristics of Aircraft.
5.12.1 F3173/F3173M—21 Standard Specification for Aircraft Handling Characteristics.
5.13.1 F3173/F3173M—21 Standard Specification for Aircraft Handling Characteristics.
5.14.1 F3120/F3120M—20 Standard Specification for Ice Protection
for General Aviation Aircraft.
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.
6.2.1 F3254—19 Standard Specification for Aircraft Interaction of
Systems and Structures.
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.
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.
6.5.1 F3116/F3116M—18e2 Standard Specification for Design Loads
and Conditions.
6.5.1.1 F3331—18 Standard Practice for Aircraft Water Loads.
6.6.1 F3061/F3061M—20 Standard 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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
13917
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
lotter on DSK11XQN23PROD with RULES1
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
23.2230 ..................
6.7 Limit and Ultimate Loads ...........................
23.2235 ..................
6.8 Structural Strength .....................................
23.2240 ..................
6.9 Structural Durability ...................................
23.2245 ..................
6.10 Aeroelasticity ............................................
23.2250 ..................
6.11 Design and Construction Principles ........
23.2255 ..................
6.12 Protection of Structure .............................
23.2260 ..................
6.13 Materials and Processes .........................
23.2265 ..................
6.14 Special Factors of Safety ........................
23.2270 ..................
6.15 Emergency Conditions .............................
Subpart D—Design and
Construction
23.2300 ..................
7.1 Flight Control Systems ..............................
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00017
Fmt 4700
ASTM F3264–21 subsection(s) 8
6.6.2.1 F3396/F3396M—20 Standard Practice for Aircraft Simplified Loads.
6.7.1 F3114—21 Standard Specification for Structures.
6.7.2 F3408/F3408M—21 Standard Specification for Aircraft Emergency Parachute Recovery Systems.
6.8.1 F3114—21 Standard Specification for Structures.
6.8.2 F3408/F3408M—21 Standard Specification for Aircraft Emergency Parachute Recovery Systems.
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.
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.
6.11.1 F3061/F3061M—20 Standard 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.
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.
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.
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.
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.
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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
13918
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
lotter on DSK11XQN23PROD with RULES1
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
ASTM F3264–21 subsection(s) 8
23.2305 ..................
7.2 Landing Gear Systems ..............................
23.2310 ..................
7.3 Buoyancy for Seaplanes and Amphibians
23.2315 ..................
7.4 Means of Egress and Emergency Exits ....
23.2320 ..................
7.5 Occupant Physical Environment ................
23.2325 ..................
7.6 Fire Protection ...........................................
23.2330 ..................
7.7 Fire Protection in Designated Fire Zones
and Adjacent Areas.
23.2335 ..................
7.8 Lightning Protection ...................................
7.2.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
7.3.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
7.4.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
7.4.2 F3083/F3083M—20a Standard Specification for Emergency
Conditions, Occupant Safety and Accommodations.
7.5.1 F3061/F3061M—20 Standard 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.
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.
7.7.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment 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.
7.8.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
Subpart E—Powerplant:
23.2400 ..................
8.1 Powerplant Installation ...............................
23.2405 ..................
8.2 Power or Thrust Control Systems .............
23.2410 ..................
8.3 Powerplant Installation Hazard Assessment.
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00018
Fmt 4700
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.
8.2.1 F3062/F3062M—20 Standard 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.
8.3.1 F3061/F3061M—20 Standard 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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
13919
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
lotter on DSK11XQN23PROD with RULES1
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
23.2415 ..................
8.4 Powerplant Installation Ice Protection .......
23.2420 ..................
8.5 Reversing Systems ....................................
23.2425 ..................
8.6 Powerplant Operational Characteristics ....
23.2430 ..................
8.7 Fuel and Energy Storage and Distribution
Systems.
23.2435 ..................
8.8 Powerplant Induction, Exhaust, and Support Systems.
23.2440 ..................
8.9 Powerplant Installation Fire Protection ......
Subpart F—Equipment:
23.2500 ..................
VerDate Sep<11>2014
9.1 Systems and Equipment Function—Requirements.
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00019
Fmt 4700
ASTM F3264–21 subsection(s) 8
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.
8.4.1 F3062/F3062M—20 Standard 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.
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.
8.6.1 F3062/F3062M—20 Standard 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.
8.7.1 F3062/F3062M—20 Standard 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.
8.8.1 F3062/F3062M—20 Standard Specification for Aircraft Powerplant Installation.
8.8.2 F3239—19 Standard Specification for Aircraft Electric Propulsion Systems.
8.9.1 F3061/F3061M—20 Standard 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.
9.1.1 F3061/F3061M—20 Standard 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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
13920
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
lotter on DSK11XQN23PROD with RULES1
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
23.2505 ..................
9.2 Equipment Function and Installation Requirements.
23.2510 ..................
9.3 Equipment, Systems, and Installation .......
23.2515 ..................
9.4 Electrical and Electronic System Lightning
Protection.
23.2520 ..................
9.5 High Intensity Radiated Fields (HIRF) Protection.
23.2525 ..................
9.6 System Power Generation, Storage, and
Distribution.
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00020
Fmt 4700
ASTM F3264–21 subsection(s) 8
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.
9.2.1 F3061/F3061M—20 Standard 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.
9.3.1 F3061/F3061M—20 Standard 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.
9.4.1 F3061/F3061M—20 Standard 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.
9.5.1 F3061/F3061M—20 Standard 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.
9.6.1 F3061/F3061M—20 Standard 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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
13921
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
lotter on DSK11XQN23PROD with RULES1
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
23.2530 ..................
9.7 External and Cockpit Lighting ....................
23.2535 ..................
9.8 Safety Equipment ......................................
23.2540 ..................
9.9 Flight in Icing Conditions ...........................
23.2545 ..................
9.10 Pressurized System Elements .................
23.2550 ..................
9.11 Equipment Containing High-Energy Rotors.
Subpart G—Flight crew
Interface and Other
Information:
23.2600 ..................
10.1 Flight crew Compartment Interface .........
23.2605 ..................
10.2 Installation and Operation Information ....
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
PO 00000
Frm 00021
Fmt 4700
ASTM F3264–21 subsection(s) 8
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.
9.7.1 F3061/F3061M—20 Standard 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.
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.
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.
9.10.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
9.10.2 F3229/F3229M—17 Standard Practice for Static Pressure
System Tests in Small Aircraft.
9.11.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment in Small Aircraft.
10.1.1 F3061/F3061M—20 Standard 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.
10.2.1 F3061/F3061M—20 Standard 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.
Sfmt 4700
E:\FR\FM\11MRR1.SGM
11MRR1
13922
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
TABLE 2—SIDE-BY-SIDE VIEW OF 14 CFR PART 23 REGULATIONS AND ASTM F3264–21 SECTIONS—Continued
Part 23
amendment 23–64
regulation(s)
ASTM F3264–21 section(s) 7
23.2610 ..................
10.3 Instrument Markings, Control Markings,
and Placards:.
23.2615 ..................
10.4 Flight, Navigation, and Powerplant Instruments.
23.2620 ..................
5.15 Operating Limitations ...............................
10.5 Airplane Flight Manual .............................
Editorial, Reapproval, Revision or
Withdrawal
lotter on DSK11XQN23PROD with RULES1
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
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.
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
ASTM F3264–21 subsection(s) 8
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.
10.3.1 F3061/F3061M—20 Standard Specification for Systems and
Equipment 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.
10.4.1 F3061/F3061M—20 Standard 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.
5.15.1 F3174/F3174M—19 Standard 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.
superscript epsilon in the standard
designation (e.g., F3235–17e1). 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 https://
www.astm.org/READINGLIBRARY/.
PO 00000
Frm 00022
Fmt 4700
Sfmt 4700
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 www.astm.org or
contacting ASTM at (610) 832–9585
(phone), (610) 832–9555 (fax), or
through service@astm.org (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, jkoury@astm.org.
The FAA maintains a list of accepted
means of compliance on the FAA
website at https://www.faa.gov/aircraft/
air_cert/design_approvals/small_
airplanes/small_airplanes_regs/.
Issued in Kansas City, Missouri, on March
2, 2022.
E:\FR\FM\11MRR1.SGM
11MRR1
Federal Register / Vol. 87, No. 48 / Friday, March 11, 2022 / Rules and Regulations
Patrick Mullen,
Manager, Technical Innovation Policy
Branch, Policy and Innovation Division,
Aircraft Certification Service.
Federal Aviation Administration
connect.prattwhitney.com. You may
view this service information at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (817) 222–
5110. It is also available at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0959.
14 CFR Part 39
Examining the AD Docket
[Docket No. FAA–2021–0959; Project
Identifier AD–2021–00830–E; Amendment
39–21975; AD 2022–06–09]
You may examine the AD docket at
https://www.regulations.govby
searching for and locating Docket No.
FAA–2021–0959; 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:
Carol Nguyen, Aviation Safety Engineer,
ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone:
(781) 238–7655; fax: (781) 238–7199;
email: carol.nguyen@faa.gov.
SUPPLEMENTARY INFORMATION:
[FR Doc. 2022–04845 Filed 3–10–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
RIN 2120–AA64
Airworthiness Directives; Pratt &
Whitney Division Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2019–03–
01 and AD 2021–05–51 for certain Pratt
& Whitney Division (PW) PW4074,
PW4074D, PW4077, PW4077D,
PW4084D, PW4090, and PW4090–3
model turbofan engines. AD 2019–03–
01 required performing initial and
repetitive thermal acoustic image (TAI)
inspections for cracks in certain 1ststage low-pressure compressor (LPC)
blades and removal of those blades that
fail inspection. AD 2021–05–51 required
performing a one-time TAI inspection
for cracks in certain 1st-stage LPC
blades and removal of those blades that
fail inspection. This AD was prompted
by three in-flight failures of a 1st-stage
LPC blade, with one failure resulting in
an engine fire during flight, and
subsequent manufacturer publication of
service information specifying improved
inspections for three critical locations
on the 1st-stage LPC blade. This AD
requires initial and repetitive ultrasonic
(UT) inspections and TAI inspections
for cracks in certain 1st-stage LPC
blades and removal of those blades that
fail inspection. The FAA is issuing this
AD to address the unsafe condition on
these products.
DATES: This AD is effective April 15,
2022.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of April 15, 2022.
ADDRESSES: For service information
identified in this final rule, contact Pratt
& Whitney Division, 400 Main Street,
East Hartford, CT 06118; phone: (860)
565–0140; email: help24@
prattwhitney.com; website: https://
lotter on DSK11XQN23PROD with RULES1
SUMMARY:
VerDate Sep<11>2014
16:15 Mar 10, 2022
Jkt 256001
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2019–03–01,
Amendment 39–19553 (84 FR 4320,
February 15, 2019) (AD 2019–03–01),
and AD 2021–05–51, Amendment 39–
21470 (86 FR 13445, March 9, 2021) (AD
2021–05–51). AD 2019–03–01 and AD
2021–05–51 applied to certain PW
PW4074, PW4074D, PW4077,
PW4077D, PW4084D, PW4090, and
PW4090–3 model turbofan engines. The
NPRM published in the Federal
Register on December 28, 2021 (86 FR
73699). The NPRM was prompted by the
manufacturer developing an improved
UT inspection for the three critical
locations on the 1st-stage LPC blade,
two at the mid span region of the blade
and one at the flow path region of the
blade, following three in-flight failures
of a 1st-stage LPC blade, with one
failure resulting in an engine fire during
flight. The manufacturer published Pratt
& Whitney Alert Service Bulletin (ASB)
PW4G–112–A72–361, dated October 15,
2021, which provides instructions for
performing both the improved UT
inspection and the TAI inspection. The
manufacturer also determined that it
was necessary to adjust the initial TAI
inspection threshold and lower the
Frm 00023
Fmt 4700
Sfmt 4700
repetitive TAI inspection interval on the
1st-stage LPC blades to address the
unsafe condition. In the NPRM, the FAA
proposed to require initial and
repetitive UT inspections and TAI
inspections for cracks in certain 1ststage LPC blades and removal of those
blades that fail inspection.
Discussion of Final Airworthiness
Directive
Comments
Background
PO 00000
13923
The FAA received comments from
five commenters. The commenters were
Air Line Pilots Association,
International (ALPA), All Nippon
Airways (ANA), The Boeing Company
(Boeing), Japan Airlines (JAL), and
United Airlines (UAL). The following
presents the comments received on the
NPRM and the FAA’s response to each
comment.
Request To Revise Note and Add
Additional Note in Required Actions
UAL requested that the FAA revise
Note 2 to paragraph (g)(1)(ii) of the
NPRM [Note 1 to paragraph (g)(1)(ii) of
this AD] to ‘‘The FAA-approved TAI
inspection method and the vendors that
can perform the FAA-approved TAI
inspection are specified in the
Accomplishment Instructions section
and Vendor Services section of PW4G–
112–A72–361, respectively.’’ UAL also
requested that the FAA add the same
note to paragraph (g)(2)(iii) of this AD.
The FAA agrees and revised Note 1 to
paragraph (g)(1)(ii) of this AD and added
Note 2 to paragraph (g)(2)(iii) to this AD,
as requested by UAL.
Request To Change the Initial
Compliance Time to Before Revenue
Flight
ANA requested that the FAA change
the Required Actions, paragraph (g)(1)
Initial 1st-stage LPC Blade Inspections,
from ‘‘before further flight after the
effective of this AD’’ to ‘‘before the next
revenue flight’’ to clarify the ferry flight
requirement.
Similarly, JAL requested the FAA
change the Required Actions, paragraph
(g)(1) Initial 1st-stage LPC Blade
Inspections, from ‘‘before further flight
after the effective of this AD’’ to ‘‘before
the next revenue flight’’ or ‘‘before
further flight except the ferry flight
without passenger and cargos.’’
The FAA disagrees with changing the
initial compliance in paragraph (g) of
this AD as requested by ANA and JAL.
The FAA has determined it is necessary
to require certain actions prior to any
flight, except as permitted in paragraph
(i), Special Flight Permit, of this AD.
E:\FR\FM\11MRR1.SGM
11MRR1
]]>Agencies
[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 [www.gpo.gov]
[FR Doc No: 2022-04845]
[[Page 13911]]
=======================================================================
-----------------------------------------------------------------------
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.
-----------------------------------------------------------------------
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: [email protected].
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.
---------------------------------------------------------------------------
\1\ Ref Public Law 104-113 as amended by Public Law 107-107.
---------------------------------------------------------------------------
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.
---------------------------------------------------------------------------
\2\ Ref Public Law 113-53.
---------------------------------------------------------------------------
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.
---------------------------------------------------------------------------
\3\ See https://www.federalregister.gov/documents/2016/12/30/2016-30246/revision-of-airworthiness-standards-for-normal-utility-acrobatic-and-commuter-category-airplanes.
---------------------------------------------------------------------------
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.
---------------------------------------------------------------------------
\4\ See https://drs.faa.gov/browse.
---------------------------------------------------------------------------
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.''
---------------------------------------------------------------------------
\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: https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/.
---------------------------------------------------------------------------
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;.
HIRF: DO-160,
Section 20--R for both
radiated and conducted
susceptibility.
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 https://www.astm.org/READINGLIBRARY/.
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 www.astm.org or contacting ASTM at
(610) 832-9585 (phone), (610) 832-9555 (fax), or through
[email protected] (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, [email protected].
The FAA maintains a list of accepted means of compliance on the FAA
website at https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/.
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
