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DEFSTAN 00-970(PT1)SEC2/3(2003) : 2003

Superseded

Superseded

View Superseded by

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - FLIGHT

Available format(s)

PDF

Language(s)

English

Published date

01-01-2003

Superseded date

01-27-2006

US$20.00
Excluding Tax where applicable

Preface
Main Text
SECTION 2 - FLIGHT
  2.0 Introduction and Abbreviations
  2.1 General requirements and definitions
  2.2 General handling flight test requirements
  2.3 Ground handling
  2.4 Take off and initial climb
  2.5 Circuit, approach, landing and overshoot
  2.6 Longitudinal trim, stability and control
  2.7 Demonstration of limits of flight and manoeuvre
       envelopes
  2.8 Lateral and directional trim, stability and control
  2.9 Rapid rolling/roll coupling
  2.10 Behaviour at or near the stall
  2.11 Lift boundaries
  2.12 Spinning
  2.13 Aerobatic manoeuvres
  2.14 Effect of engine failures
  2.15 Effect of system failures
  2.16 Automatic flight control systems and flight directors
  2.17 General handling
  2.18 Air to air refueling
  2.19 Handling tests specific to VSTOL aeroplanes
  2.20 Handling performance in icing conditions
  2.21 Longitudinal flying qualities
  2.22 Lateral and directional flying qualities
  2.23 Requirements for structural and equipment exposure to
       noise and vibration
  2.24 Stalling, post-stall gyrations and spins and
       miscellaneous flying qualities
  2.25 Handling requirements for VSTOL aeroplanes
Section 2 - Tables
SUPPLEMENTS
Section 2 - Leaflet 0 to 66

Provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT1)SEC2/2(1999) (04/2005)
DocumentType
Standard
Pages
290
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

US$20.00
Excluding Tax where applicable