Federal Aviation Administration, DOT

Section 33.5

Subpart D - Block Tests; Reciprocating
Aircraft Engines
33.41
33.42
33.43
33.45
33.47
33.49
33.51
33.53
33.55
33.57

APPENDIX B TO PART 33 - CERTIFICATION
STANDARD ATMOSPHERIC CONCENTRATIONS
OF RAIN AND HAIL
APPENDIX C TO PART 33 [RESERVED]
APPENDIX D TO PART 33 - MIXED PHASE AND
ICE CRYSTAL ICING ENVELOPE (DEEP CONVECTIVE CLOUDS)

Applicability.
General.
Vibration test.
Calibration tests.
Detonation test.
Endurance test.
Operation test.
Engine system and component tests.
Teardown inspection.
General conduct of block tests.

AUTHORITY: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
SOURCE: Docket No. 3025, 29 FR 7453, June
10, 1964, unless otherwise noted.
NOTE: For miscellaneous amendments to
cross references in this Part 33, see Amdt. 33-
2, 31 FR 9211, July 6, 1966.

Subpart E - Design and Construction;
Turbine Aircraft Engines
33.61
33.62
33.63
33.64
33.65
33.66
33.67
33.68
33.69
33.70
33.71
33.72
33.73
33.74
33.75
33.76
33.77
33.78
33.79

Subpart A - General

Applicability.
Stress analysis.
Vibration.
Pressurized engine static parts.
Surge and stall characteristics.
Bleed air system.
Fuel system.
Induction system icing.
Ignitions system.
Engine life-limited parts.
Lubrication system.
Hydraulic actuating systems.
Power or thrust response.
Continued rotation.
Safety analysis.
Bird ingestion.
Foreign object ingestion - ice.
Rain and hail ingestion.
Fuel burning thrust augmentor.

Section 33.1

[Amdt. 33-7, 41 FR 55474, Dec. 20, 1976, as
amended by Amdt. 33-14, 55 FR 32861, Aug. 10,
1990]

Section 33.3

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 unbalance 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
spaschal on DSK3GDR082PROD with CFR

Applicability.

(a) This part prescribes airworthiness
standards for the issue of type certificates 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 applicable requirements of this part and the
applicable requirements of part 34 of
this chapter.

General.

Each applicant must show that the
aircraft engine concerned meets the
applicable requirements of this part.
Section 33.4 Instructions for Continued Airworthiness.
The applicant must prepare Instructions for Continued Airworthiness in
accordance with appendix A to this
part that are acceptable to the Administrator. The instructions may be incomplete at type certification if a program 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]

33.201 Design and test requirements for
Early ETOPS eligibility.
APPENDIX A TO PART 33 - INSTRUCTIONS FOR
CONTINUED AIRWORTHINESS

Section 33.5 Instruction manual for installing
and operating the engine.
Each applicant must prepare and
make available to the Administrator

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