757
Federal Aviation Administration, DOT
§ 35.3
§§ 34.61–34.71
[Reserved]
PART 35—AIRWORTHINESS
STANDARDS: PROPELLERS
Subpart A—General
Sec.
35.1
Applicability.
35.2
Propeller configuration.
35.3
Instructions for propeller installation
and operation.
35.4
Instructions for Continued Airworthi-
ness.
35.5
Propeller ratings and operating limita-
tions.
35.7
Features and characteristics.
Subpart B—Design and Construction
35.11
[Reserved]
35.13
[Reserved]
35.15
Safety analysis.
35.16
Propeller critical parts.
35.17
Materials and manufacturing methods.
35.19
Durability.
35.21
Variable and reversible pitch propel-
lers.
35.22
Feathering propellers.
35.23
Propeller control system.
35.24
Strength.
Subpart C—Tests and Inspections
35.31
[Reserved]
35.33
General.
35.34
Inspections, adjustments and repairs.
35.35
Centrifugal load tests.
35.36
Bird impact.
35.37
Fatigue limits and evaluation.
35.38
Lightning strike.
35.39
Endurance test.
35.40
Functional test.
35.41
Overspeed and overtorque.
35.42
Components of the propeller control
system.
35.43
Propeller hydraulic components.
35.45–35.47
[Reserved]
A
PPENDIX
A
TO
P
ART
35—I
NSTRUCTIONS FOR
C
ONTINUED
A
IRWORTHINESS
A
UTHORITY
: 49 U.S.C. 106(f), 106(g), 40113,
44701–44702, 44704.
S
OURCE
: Docket No. 2095, 29 FR 7458, June
10, 1964, unless otherwise noted.
Subpart A—General
§ 35.1
Applicability.
(a) This part prescribes airworthiness
standards for the issue of type certifi-
cates and changes to those certificates,
for propellers.
(b) Each person who applies under
part 21 for such a certificate or change
must show compliance with the appli-
cable requirements of this part.
(c) An applicant is eligible for a pro-
peller type certificate and changes to
those certificates after demonstrating
compliance with subparts A, B, and C
of this part. However, the propeller
may not be installed on an airplane un-
less the applicant has shown compli-
ance with either § 23.2400(c) or § 25.907 of
this chapter, as applicable, or compli-
ance is not required for installation on
that airplane.
(d) For the purposes of this part, the
propeller consists of those components
listed in the propeller type design, and
the propeller system consists of the
propeller and all the components nec-
essary for its functioning, but not nec-
essarily included in the propeller type
design.
[Amdt. 35–3, 41 FR 55475, Dec. 20, 1976, as
amended by Amdt. 35–8, 73 FR 63346, Oct. 24,
2008; Doc. FAA–2015–1621, Amdt. 35–10, 81 FR
96700, Dec. 30, 2016]
§ 35.2
Propeller configuration.
The applicant must provide a list of
all the components, including ref-
erences to the relevant drawings and
software design data, that define the
type design of the propeller to be ap-
proved under § 21.31 of this chapter.
[Amdt. 35–8, 73 FR 63346, Oct. 24, 2008]
§ 35.3
Instructions for propeller instal-
lation and operation.
The applicant must provide instruc-
tions that are approved by the Admin-
istrator. Those approved instructions
must contain:
(a) Instructions for installing the
propeller, which:
(1) Include a description of the oper-
ational modes of the propeller control
system and functional interface of the
control system with the airplane and
engine systems;
(2) Specify the physical and func-
tional interfaces with the airplane, air-
plane equipment and engine;
(3) Define the limiting conditions on
the interfaces from paragraph (a)(2) of
this section;
(4) List the limitations established
under § 35.5;
(5) Define the hydraulic fluids ap-
proved for use with the propeller, in-
cluding grade and specification, related
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