699
Federal Aviation Administration, DOT
§ 33.5
Subpart D—Block Tests; Reciprocating
Aircraft Engines
33.41
Applicability.
33.42
General.
33.43
Vibration test.
33.45
Calibration tests.
33.47
Detonation test.
33.49
Endurance test.
33.51
Operation test.
33.53
Engine system and component tests.
33.55
Teardown inspection.
33.57
General conduct of block tests.
Subpart E—Design and Construction;
Turbine Aircraft Engines
33.61
Applicability.
33.62
Stress analysis.
33.63
Vibration.
33.64
Pressurized engine static parts.
33.65
Surge and stall characteristics.
33.66
Bleed air system.
33.67
Fuel system.
33.68
Induction system icing.
33.69
Ignitions system.
33.70
Engine life-limited parts.
33.71
Lubrication system.
33.72
Hydraulic actuating systems.
33.73
Power or thrust response.
33.74
Continued rotation.
33.75
Safety analysis.
33.76
Bird ingestion.
33.77
Foreign object ingestion—ice.
33.78
Rain and hail ingestion.
33.79
Fuel burning thrust augmentor.
Subpart F—Block Tests; Turbine Aircraft
Engines
33.81
Applicability.
33.82
General.
33.83
Vibration test.
33.84
Engine overtorque test.
33.85
Calibration tests.
33.87
Endurance test.
33.88
Engine overtemperature test.
33.89
Operation test.
33.90
Initial maintenance inspection test.
33.91
Engine system and component tests.
33.92
Rotor locking tests.
33.93
Teardown inspection.
33.94
Blade containment and rotor unbal-
ance tests.
33.95
Engine-propeller systems tests.
33.96
Engine tests in auxiliary power unit
(APU) mode.
33.97
Thrust reversers.
33.99
General conduct of block tests.
Subpart G—Special Requirements: Turbine
Aircraft Engines
33.201
Design and test requirements for
Early ETOPS eligibility.
A
PPENDIX
A
TO
P
ART
33—I
NSTRUCTIONS FOR
C
ONTINUED
A
IRWORTHINESS
A
PPENDIX
B
TO
P
ART
33—C
ERTIFICATION
S
TANDARD
A
TMOSPHERIC
C
ONCENTRATIONS
OF
R
AIN AND
H
AIL
A
PPENDIX
C
TO
P
ART
33 [R
ESERVED
]
A
PPENDIX
D
TO
P
ART
33—M
IXED
P
HASE AND
I
CE
C
RYSTAL
I
CING
E
NVELOPE
(D
EEP
C
ON
-
VECTIVE
C
LOUDS
)
A
UTHORITY
: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
S
OURCE
: Docket No. 3025, 29 FR 7453, June
10, 1964, unless otherwise noted.
N
OTE
: For miscellaneous amendments to
cross references in this Part 33, see Amdt. 33–
2, 31 FR 9211, July 6, 1966.
Subpart A—General
§ 33.1
Applicability.
(a) This part prescribes airworthiness
standards for the issue of type certifi-
cates and changes to those certificates,
for aircraft engines.
(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 and the
applicable requirements of part 34 of
this chapter.
[Amdt. 33–7, 41 FR 55474, Dec. 20, 1976, as
amended by Amdt. 33–14, 55 FR 32861, Aug. 10,
1990]
§ 33.3
General.
Each applicant must show that the
aircraft engine concerned meets the
applicable requirements of this part.
§ 33.4
Instructions for Continued Air-
worthiness.
The applicant must prepare Instruc-
tions for Continued Airworthiness in
accordance with appendix A to this
part that are acceptable to the Admin-
istrator. The instructions may be in-
complete at type certification if a pro-
gram exists to ensure their completion
prior to delivery of the first aircraft
with the engine installed, or upon
issuance of a standard certificate of
airworthiness for the aircraft with the
engine installed, whichever occurs
later.
[Amdt. 33–9, 45 FR 60181, Sept. 11, 1980]
§ 33.5
Instruction manual for installing
and operating the engine.
Each applicant must prepare and
make available to the Administrator
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