TAIL BUMPERS FOR PILOTED AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

14-07-2017

Publisher

SAE International

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.

Committee	A-5B
DocumentType	Standard
Pages	7
ProductNote	This version is now stabilized.
PublisherName	SAE International
Status	Current
Supersedes	SAE ARP 1107 : 2012

MIL-A-8863 Revision C:1993

AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES

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SAE ARP 1107 : 2017

TAIL BUMPERS FOR PILOTED AIRCRAFT

Table of Contents

Abstract

General Product Information

Standards Referencing This Book

Category

Subcategory