DEFSTAN 00-970(PT1)SEC2/10(2013) : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
Hardcopy , PDF
01-10-2014
English
01-01-2013
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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Superseded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 |
| 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 00-970(PT1)SEC7/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 7: OPERATING LIMITATIONS AND INFORMATION |
| DEFSTAN 00-35(PT5)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS |
| DEFSTAN 00-970(PT1)SEC1/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 1: GENERAL |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| 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 00-970(PT1)SEC3/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-35(PT3)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS |
| DEFSTAN 00-970(PT13)/6(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| ISO 1151-4:1994 | Flight dynamics — Concepts, quantities, and symbols — Part 4: Concepts and quantities used in the study of aircraft stability and control |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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