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SAE ARP1107C

Current

Current

The latest, up-to-date edition.

Tail Bumpers for Piloted Aircraft

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

14-07-2017

€79.68
Excluding VAT

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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