SAE ARP1107C
Current
The latest, up-to-date edition.
Tail Bumpers for Piloted Aircraft
Hardcopy , PDF
English
14-07-2017
FOREWORD
1. SCOPE
2. PURPOSE
3. DESIGN REQUIREMENTS
4. TAIL BUMPER LOADS
5. TESTS
6. QUALIFICATION OF COMPONENTS AND SYSTEMS
7. DATA REQUIREMENTS
8. REFERENCES
Specifies the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.
DocumentType |
Standard
|
Pages |
7
|
ProductNote |
This version is now stabilized.
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.
MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
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