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906
14 CFR Ch. I (1–1–14 Edition)
§ 35.45
§ 35.45
[Reserved]
§ 35.47
[Reserved]
A
PPENDIX
A
TO
P
ART
35—I
NSTRUCTIONS
FOR
C
ONTINUED
A
IRWORTHINESS
A
35.1
GENERAL
(a) This appendix specifies requirements
for the preparation of Instructions for Con-
tinued Airworthiness as required by § 35.4.
(b) The Instructions for Continued Air-
worthiness for each propeller must include
the Instructions for Continued Airworthiness
for all propeller parts. If Instructions for
Continued Airworthiness are not supplied by
the propeller part manufacturer for a pro-
peller part, the Instructions for Continued
Airworthiness for the propeller must include
the information essential to the continued
airworthiness of the propeller.
(c) The applicant must submit to the FAA
a program to show how changes to the In-
structions for Continued Airworthiness made
by the applicant or by the manufacturers of
propeller parts will be distributed.
A
35.2
FORMAT
(a) The Instructions for Continued Air-
worthiness must be in the form of a manual
or manuals as appropriate for the quantity
of data to be provided.
(b) The format of the manual or manuals
must provide for a practical arrangement.
A
35.3
CONTENT
The contents of the manual must be pre-
pared in the English language. The Instruc-
tions for Continued Airworthiness must con-
tain the following sections and information:
(a)
Propeller Maintenance Section. (1) Intro-
duction information that includes an expla-
nation of the propeller’s features and data to
the extent necessary for maintenance or pre-
ventive maintenance.
(2) A detailed description of the propeller
and its systems and installations.
(3) Basic control and operation information
describing how the propeller components and
systems are controlled and how they oper-
ate, including any special procedures that
apply.
(4) Instructions for uncrating, acceptance
checking, lifting, and installing the pro-
peller.
(5) Instructions for propeller operational
checks.
(6) Scheduling information for each part of
the propeller that provides the recommended
periods at which it should be cleaned, ad-
justed, and tested, the applicable wear toler-
ances, and the degree of work recommended
at these periods. However, the applicant may
refer to an accessory, instrument, or equip-
ment manufacturer as the source of this in-
formation if it shows that the item has an
exceptionally high degree of complexity re-
quiring specialized maintenance techniques,
test equipment, or expertise. The rec-
ommended overhaul periods and necessary
cross-references to the Airworthiness Limi-
tations section of the manual must also be
included. In addition, the applicant must in-
clude an inspection program that includes
the frequency and extent of the inspections
necessary to provide for the continued air-
worthiness of the propeller.
(7) Troubleshooting information describing
probable malfunctions, how to recognize
those malfunctions, and the remedial action
for those malfunctions.
(8) Information describing the order and
method of removing and replacing propeller
parts with any necessary precautions to be
taken.
(9) A list of the special tools needed for
maintenance other than for overhauls.
(b)
Propeller Overhaul Section. (1) Dis-
assembly information including the order
and method of disassembly for overhaul.
(2) Cleaning and inspection instructions
that cover the materials and apparatus to be
used and methods and precautions to be
taken during overhaul. Methods of overhaul
inspection must also be included.
(3) Details of all fits and clearances rel-
evant to overhaul.
(4) Details of repair methods for worn or
otherwise substandard parts and components
along with information necessary to deter-
mine when replacement is necessary.
(5) The order and method of assembly at
overhaul.
(6) Instructions for testing after overhaul.
(7) Instructions for storage preparation in-
cluding any storage limits.
(8) A list of tools needed for overhaul.
A
35.4
AIRWORTHINESS LIMITATIONS SECTION
The Instructions for Continued Airworthi-
ness must contain a section titled Airworthi-
ness Limitations that is segregated and
clearly distinguishable from the rest of the
document. This section must set forth each
mandatory replacement time, inspection in-
terval, and related procedure required for
type certification. This section must contain
a legible statement in a prominent location
that reads: ‘‘The Airworthiness Limitations
section is FAA approved and specifies main-
tenance required under §§ 43.16 and 91.403 of
the Federal Aviation Regulations unless an
alternative program has been FAA ap-
proved.’’
[Amdt. 35–5, 45 FR 60182, Sept. 11, 1980, as
amended by Amdt. 35–6, 54 FR 34330, Aug. 18,
1989]
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