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DEFSTAN 00-970(PT1)SEC4/2(1999) : 1999

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - DESIGN AND CONSTRUCTION

Available format(s)

Hardcopy , PDF

Superseded date

01-10-2003

Language(s)

English

Published date

01-01-1999

€17.95
Excluding VAT

Content
Preface
Main text
SECTION 4 - DESIGN AND CONSTRUCTION
4 Introduction
4.1 General detail design
4.2 Marking of aeroplane parts
4.3 Protection of structure
4.4 Accessibility, maintenance and servicing
4.5 Material strength properties and values
4.6 Processes and working of materials
4.7 Castings
4.8 Aero-Elasticit, flutter and vibration
4.9 Birdstrike damage
4.10 Control systems
4.11 Design of undercarriages
4.12 Wheels, tyres and brakes
4.13 Operation from rough ground/ground clearance
4.14 Nose wheel steering
4.15 Crew stations - general requirements
4.16 Pilot's station - layout
4.17 View and clear vision
4.18 Optically transparent components
4.19 Cockpit controls
4.20 Doors
4.21 Seats, berths, safety belts and harnesses
4.22 Crash landing & ditching
4.23 Emergency provisions
4.24 Ventilation & heating
4.25 Pressurised air ducts
4.26 Fire precautions
4.27 Electrical bonding
Tables
Diagrams

Gives requirements for the design and construction of the aircraft, which should be implemented with the aim that no design features or details of the aircraft should be known to be hazardous or unreliable and that areas of doubt concerning design details and parts should be confirmed by test and analysis.

DevelopmentNote
Supersedes DEFSTAN 00-970/VOL1/1(1983)
DocumentType
Standard
Pages
942
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

SAE AIR 5914 : 2014 LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT

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