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DEFSTAN 00-970(PT1)SEC2/7(2011) : 2011

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

Hardcopy , PDF

Superseded date

20-07-2012

Language(s)

English

Published date

01-01-2011

€23.37
Excluding VAT

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)
DocumentType
Standard
Pages
528
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

ISO 1151-8:1992 Flight dynamics — Concepts, quantities and symbols — Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft
MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
DEFSTAN 00-35(PT5)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
ISO 1151-9:1993 Flight dynamics — Concepts, quantities and symbols — Part 9: Models of atmospheric motions along the trajectory of the aircraft
ISO 1151-1:1988 Flight dynamics — Concepts, quantities and symbols — Part 1: Aircraft motion relative to the air
ISO 1151-5:1987 Flight dynamics — Concepts, quantities and symbols — Part 5: Quantities used in measurements
ISO 1151-7:1985 Flight dynamics — Concepts, quantities and symbols — Part 7: Flight points and flight envelopes
DEFSTAN 00-35(PT3)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS
ISO 1151-4:1994 Flight dynamics — Concepts, quantities, and symbols — Part 4: Concepts and quantities used in the study of aircraft stability and control

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