Number | Title | Status | Office | Date |
---|---|---|---|---|
33.70-1 |
Guidance Material for Aircraft Engine Life-Limited Parts Requirements
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of § 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33). |
Active | AIR-600 | 2009-07-31 |
33.70-4 |
Fatigue Life of Nickel Powder Rotating Life-Limited Parts
This advisory circular (AC) provides guidance that may be used to demonstrate compliance with Title 14, Code of Federal Regulations (14 CFR) 33.70 for rotating life-limited engine parts made of nickel powder. |
Active | AIR-625 | 2023-08-15 |
33.70-2 |
Damage Tolerance of Hole Features in High-Energy Turbine
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in § 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts. |
Active | AIR-600 | 2009-08-28 |
33.70-3 |
Damage Tolerance for Material Anomalies in Titanium Life-Limited Turbine Engine Rotors
This advisory circular (AC) describes an acceptable means for demonstrating compliance with the requirements of title 14, Code of Federal Regulations (14 CFR) 33.70, Engine Life-Limited Parts. |
Active | AIR-624 | 2023-04-17 |