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AFGS-87221 - Aircraft Structures, General Specification For (S/S By Jssg-2006)

This specification establishes the structural performance and verification requirements for an airframe. These requirements are derived from operational needs and apply to the airframe structure which is required to function and sustain loads during usage. This usage includes take-off, flight, landing ground handling, maintenance, and tests. This specification also establishes certain structural design criteria which, as a minimum, are necessary to enable the airframe to meet these structural performance requirements.

AFGS-87235 - Emergency Escape, Aircraft (S/S By Jssg-2010-11)

AFGS-87237 - Navigation Equipment, Airborne

This specification establishes the development and production requirements and verifications for airborne navigation equipment procured as a critical or prime item or as part of a weapon system.

MIL-A-008862 - Airplane Strength And Rigidity, Landing And Ground Handling Loads (S/S By Mil-A-8863)

MIL-A-83444 - Airplane Damage Tolerance Requirements (For Future Procurements -(S/S By Mil-A-87221)

MIL-A-87221 - Aircraft Structures General Specification For (S/S By Afgs-87221)

MIL-A-8860 - Airplane Strength And Rigidity, General Specification For

This specification contains general requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes.

MIL-A-8861 - Airplane Strength And Rigidity Flight Loads

This specification covers the requirements for strength and rigidity for flight loading conditions applicable to airplanes.

MIL-A-8862 - Airplane Strength And Rigidity-Landplane Landing And Ground Handling Loads (Use Mil-A-8863)

MIL-A-8863 - Airplane Strength And Rigidity Ground Loads For Navy Acquired Airplanes

This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground maneuvering. d. Ground handling. e. Supplemental loads.

MIL-A-8864 - Airplane Strength And Rigidity Water And Handling Loads For Sea Planes

MIL-A-8865 - Airplane Strength And Rigidity Miscellaneous Loads

This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airplanes.

MIL-A-8866 - Airplane Strength And Rigidity Reliability Requirements, Repeated Loads, Fatigue And Damage Tolerance

This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.

MIL-A-8868 - Airplane Strength And Rigidity Data And Reports

This specification contains the requirements for data necessary to show compliance with the design and test requirements of MIL-A-8860 through MIL-A-8870 for the acquisition of naval airplanes, and to show the dependent relationship between the schedules for structural engineering analyses and testing and schedules for manufacturing.

MIL-A-8869 - Airplane Strength And Rigidity Nuclear Weapons Effects

This specification establishes the basic nuclear weapons effects requirements for airplanes which are Intended to deliver nuclear weapons or operate in a nuclear conflict environment.

MIL-A-8871 - Airplane Strength And Rigidity Flight And Ground Operations Tests (For Future Procure. (See Mil-A-87221)

This specification covers the flight test requirements for the structural integrity flight and ground evaluation and demonstration of piloted airplanes.

MIL-A-8892 - Airplane Strength And Rigidity, Vibration (For Future Procure. (See Mil-A-87221)

MIL-A-8893 - Airplane Strength And Rigidity, Sonic Fatigue (For Future Procure. (See Mil-A-87221)

MIL-D-8708 - Demonstration: Aircraft Weapon Systems, General Specification For

This specification establishes the general requirements for demonstration of Naval aircraft weapon systems during full scale engineering development.

MIL-F-25352 - Flutter, Divergence, And Reversal In Aircraft, Prevention Of (Supersedes 1817)

MIL-F-83691 - Flight Test Demonstration Requirements For Departure Resistance And Post-Departure Characteristics Of Piloted Airplanes

This specification contains the demonstration requirements of the high angle of attack (AOA) flight characteristics of piloted airplanes.

MIL-N-87237 - Navigation Equipment, Airborne (S/S By Afgs-87237)

MIL-P-11747 - Painting, Marking, And Insignia For U. S. Army Aircraft, General Specification For.

MIL-STD-1791 - Designing For Internal Aerial Delivery In Fixed Wing Aircraft

This standard provides design and performance requirements to assure the airworthiness of USAF fixed wing aircraft whose missions involve the safe and effective transport of cargo. It presents design requirements and operating limits from the basic aircraft loading manuals and technical publications and is supplemented by additional useful air transport data.

MIL-STD-1793 - Flight Performance, A1R Vehicle (S/S By Mil-Hdbk-1793)

This standard establishes definitions, performance criteria, requirements and verifications for air vehicle flight performance.

MIL-STD-203 - Aircrew Station Controls And Displays: Location, Arrangement And Actuation Of, For Fixed Wing Aircraft

This document establishes the requirements for the uniform location , arrangement, and actuation of controls and displays used in the functional crew stations of military fixed wing aircraft.

MIL-STD-2066 - Catapulting And Arresting Gear Forcing Functions For Aircraft Structural Design (S/S By Mil-Hdbk-2066)

The information contained herein presents loading characteristics, associated parameters, and methods to be used in calculating the catapulting and arresting loads of MIL-A-8863 and MIL-A-8866 for the design of U.S. Navy airplanes operating from shipboard and shorebased launching and recovery gears. A listing of such gears for which data is contained herein is given in Table 1.