DEFSTAN 00-970(PT1)SEC2/7(2011) : 2011
Superseded
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT
English
01-01-2011
20-07-2012
Preface
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 refuelling
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
Leaflet 0 to 66
Specifies requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC2/6(2011). (11/2011)
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| DocumentType |
Standard
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| Pages |
528
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| PublisherName |
UK Ministry of Defence Standards
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |