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DEFSTAN 00-970(PT1)SEC2/10(2013) : 2013

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 - PART 1: FIXED WING - SECTION 2: FLIGHT

Available format(s)

PDF

Language(s)

English

Published date

01-01-2013

Superseded date

10-01-2014

€15.80
Excluding VAT
Summarise this standard

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 for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military operation.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT1)SEC2/9(2013). (08/2013)
DocumentType
Standard
Pages
542
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

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€15.80
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