FLYING QUALITIES OF PILOTED AIRPLANES

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Covers requirements for the flying and handling qualities, in flight and on the ground, of US Military, manned, piloted airplanes.

Committee	FSC 15GP
DevelopmentNote	INACTIVE FOR NEW DESIGN 28/8/96
DocumentType	Standard
Pages	96
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
MIL-STD-2069 Base Document:1961	REQUIREMENTS FOR AIRCRAFT NONNUCLEAR SURVIVABILITY PROGRAM
MIL-HDBK-2069 Base Document:1997	AIRCRAFT SURVIVABILITY
MIL-C-005011 Revision B:1977	CHARTS: STANDARD AIRCRAFT CHARACTERISTICS AND PERFORMANCE, PILOTED AIRCRAFT (FIXED WING)
DEFSTAN 00-970(PT0)/9(2012) : 2012	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/17(2016) : 2016	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/15(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/16(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
MIL-H-8891 Revision A:1978	HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
MIL-HDBK-244 Revision A:1990	GUIDE TO AIRCRAFT - STORES COMPATIBILITY
DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
MIL-H-5440 Revision H:1993	HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
MIL STD 1763 : A	AIRCRAFT STORES CERTIFICATION PROCEDURES
MIL-T-5522 Revision D:1975	TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
MIL-STD-884 Revision C:1975	ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION
DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
MIL-HDBK-759 Revision C:1995	HANDBOOK FOR HUMAN ENGINEERING DESIGN GUIDELINES
MIL-S-8812 Revision D:1975	STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
MIL-HDBK-2089 Base Document:1997	AIRCRAFT SURVIVABILITY TERMS
MIL-D-23143 Revision A:1982	DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES
MIL T 25920 : C	TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION
JSSG-2001 Revision B:2004	Air Vehicle
DEFSTAN 00-970(PT1)SEC2/10(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT
DEFSTAN 00-970(PT1)SEC2/9(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT
SAE ARP 5770 : 2012	MECHANICAL CONTROL DESIGN GUIDE
MIL-DTL-9490 Revision E:2008	FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-I-8671 Revision D:1994	INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
MIL-HDBK-1763 Base Document:1998	AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
MIL-STD-2072 Base Document:1977	SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR
SAE AIR 4094 : 2016	AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS
MIL-D-8708 Revision C:1991	DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-STD-1793 Base Document:1985	FLIGHT PERFORMANCE, AIR VEHICLE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON RFB OH 45433-6503
DEFSTAN 00-970(PT1)SEC2/7(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT
MIL-C-18244 Revision A:1962	CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

MIL-C-18244 Revision A:1962	CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-STD-756 Revision B:1981	RELIABILITY MODELING AND PREDICTION
MIL F 9490 : D	FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-A-8861 Revision B:1986	AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
MIL S 83691 : A	STALL, POST-STALL, SPIN FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-D-8708 Revision C:1991	DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL F 18372 : 0	FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR)