DEFSTAN 00-970(PT1)SEC2/3(2003) : 2003
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - FLIGHT
Hardcopy , PDF
27-01-2006
English
01-01-2003
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Superseded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 |
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