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Landing Gear Fatigue Spectrum Development For Part 25 Aircraft
- Aerospace Standard
- AIR5914
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Information Report (AIR) provides guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear. Many of the recommendations herein are generalizations based on data obtained from a wide range of landing gears. The aircraft manufacturer or the landing gear supplier is encouraged to use data more specific to their particular undercarriage whenever possible.
Rationale
This document provides a means for deriving a spectrum of loads for assessing the life of a main and nose landing gear for Part 25 tricycle landing gear structural components. Many of the recommendations herein are generalizations based on data obtained from a wide range of landing gears.
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 | DISTRIBUTION OF DESCENT RATE PER 1000 LANDINGS | |
TABLE 2 | TAXING LOADS AND OCCURRENCES | |
TABLE 3 | TURNING SIDE LOAD LOADS AND OCCURRENCES | |
TABLE 4 | MLG BRAKING LOADS AND OCCURRENCES | |
TABLE 5 | NLG REACTIVE LOADS AND OCCURRENCES DUE TO MLG BRAKING | |
TABLE 6 | ENGINE RUN-UP | |
TABLE 7 | NLG STEERING APPLICATIONS | |
TABLE 8 | TOWBARLESS TOWING FATIGUE SPECTRUM | |
TABLE 9 | FREE EXTENSION | |
TABLE 10 | GUST AND MANEUVER āGā LOADS |
Issuing Committee
Reference
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