Title 14

PART 33 SUBPART e

Subpart E - Design and Construction; Turbine Aircraft Engines

• 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.
• Docket No. 3025, 29 FR 7453, June 10, 1964, unless otherwise noted.

14:1.0.1.3.17.5.283.1	SECTION 33.61	33.61 Applicability.
14:1.0.1.3.17.5.283.2	SECTION 33.62	33.62 Stress analysis.
14:1.0.1.3.17.5.283.3	SECTION 33.63	33.63 Vibration.
14:1.0.1.3.17.5.283.4	SECTION 33.64	33.64 Pressurized engine static parts.
14:1.0.1.3.17.5.283.5	SECTION 33.65	33.65 Surge and stall characteristics.
14:1.0.1.3.17.5.283.6	SECTION 33.66	33.66 Bleed air system.
14:1.0.1.3.17.5.283.7	SECTION 33.67	33.67 Fuel system.
14:1.0.1.3.17.5.283.8	SECTION 33.68	33.68 Induction system icing.
14:1.0.1.3.17.5.283.9	SECTION 33.69	33.69 Ignitions system.
14:1.0.1.3.17.5.283.10	SECTION 33.70	33.70 Engine life-limited parts.
14:1.0.1.3.17.5.283.11	SECTION 33.71	33.71 Lubrication system.
14:1.0.1.3.17.5.283.12	SECTION 33.72	33.72 Hydraulic actuating systems.
14:1.0.1.3.17.5.283.13	SECTION 33.73	33.73 Power or thrust response.
14:1.0.1.3.17.5.283.14	SECTION 33.74	33.74 Continued rotation.
14:1.0.1.3.17.5.283.15	SECTION 33.75	33.75 Safety analysis.
14:1.0.1.3.17.5.283.16	SECTION 33.76	33.76 Bird ingestion.
14:1.0.1.3.17.5.283.17	SECTION 33.77	33.77 Foreign object ingestion - ice.
14:1.0.1.3.17.5.283.18	SECTION 33.78	33.78 Rain and hail ingestion.
14:1.0.1.3.17.5.283.19	SECTION 33.79	33.79 Fuel burning thrust augmentor.

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