• Shopping Cart
    There are no items in your cart

MIL-F-8785 Revision C:1980

Current

Current

The latest, up-to-date edition.

Flying Qualities of Piloted Airplanes

Available format(s)

PDF

Published date

11-05-1980

US$20.00
Excluding Tax where applicable

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

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

This specification contains the requirements for the flying and handling qualities, in flight and on the ground, of U.S. Military, manned, piloted airplanes except for flight at airspeeds below Vcon (MIL-F-83300).

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 (S/S BY MIL-HDBK-2069)
MIL-HDBK-2069 Base Document:1997 Aircraft Survivability
MIL-C-005011 Revision B:1977 Charts, Standard Aircraft Characteristics and Performance,Piloted Aircraft (Fixed Wing) (No S/S Document)
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
MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
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 III 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, Design and Installation Requirements for (S/S by SAE-AS5440)
MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
MIL-T-5522 Revision D:1975 Test Requirementsand Methodsfor Aircraft Hydraulicand Emergency Pneumatic Systems (S/S By MIL-STD-5522)
MIL-STD-884 Revision C:1975 ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (NO S/S DOCUMENT)
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 Human Engineering Design Guidelines (No S/S Document)
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 (No S/S Document)
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 ARP5770 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 (NO S/S DOCUMENT)
SAE AIR4094A Aircraft Flight Control Systems Descriptions
MIL-D-8708 Revision C:1991 Demonstration: Aircraft Weapon Systems, General Specification for
MIL-STD-1793 Base Document:1985 FLIGHT PERFORMANCE, A1R VEHICLE (S/S BY MIL-HDBK-1793)
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 & PREDICTION (NO S/S DOCUMENT)
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: Aircraft Weapon Systems, General Specification for
MIL F 18372 : 0 FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR)

Access your standards online with a subscription

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

US$20.00
Excluding Tax where applicable