MIL A 87221 : 0

Withdrawn

Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503

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Withdrawn date: 22-07-2023

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Publisher: US Military Specs/Standards/Handbooks

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Abstract - (Show below) - (Hide below)

Outlines structural performance and verification prerequisites for an airframe. Provides a reference document outlining rationale, lessons learned, guidance, and instructions necessary to tailor sections 3 and 4 of the basic specification (MIL-A-87221) for a specific usage. AFGS-87221A that has superseded this document is a controlled document only available when giving reason for request.

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Document Type	Standard
ISBN
Pages
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Withdrawn
Supersedes	MIL A 8892 : 0 MIL A 8893 : 0 MIL A 008867 : B MIL A 008866 : B NOTICE 1 MIL A 008870 : A MIL-A-8871 Revision A:1971 MIL A 008865 : A NOTICE 1

Standards Referenced By This Book - (Show below) - (Hide below)

MIL-HDBK-244 Revision A:1990	GUIDE TO AIRCRAFT - STORES COMPATIBILITY
MIL STD 1763 : A	AIRCRAFT STORES CERTIFICATION PROCEDURES
MIL M 87158 : A	MANUALS, TECHNICAL, AIRCRAFT BATTLE DAMAGE ASSESSMENT AND REPAIR
DEFSTAN 00-970(PT7)SEC2/3(2010) : 2010	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT
DEFSTAN 00-970(PT7)SEC2/2(2007) : 2007	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT
DEFSTAN 00-970(PT7)SEC2/1(2006) : 2006	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT
MIL M 87222 : 0	MECHANICAL SYSTEMS FOR AIRCRAFT DOORS AND CANOPIES

Standards Referencing This Book - (Show below) - (Hide below)

MIL-STD-1535 Revision B:1992	SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS
MIL W 87161 : 0	WIRE STRAND, NONFLEXIBLE, FOR AIRCRAFT CONTROL
MIL HDBK 5 : G_VOL2	METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
MIL-STD-1530 Revision D:2016	AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
MIL-M-46062 Revision C:1985	MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH
MIL B 83054 : B	BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK
MIL-STD-499 Revision A:1974	ENGINEERING MANAGEMENT
MIL-S-52779 Revision A:1979	SOFTWARE QUALITY ASSURANCE PROGRAM REQUIREMENTS
MIL-A-22771 Revision D:1984	ALUMINUM ALLOY FORGINGS, HEAT TREATED
DOD STD 100 : C NOTICE 6	ENGINEERING DRAWING PRACTICES
MIL-STD-45662 Revision A:1988	CALIBRATION SYSTEMS REQUIREMENTS
MIL-S-83490 Base Document:1968	SPECIFICATION, TYPES AND FORMS
MIL STD 470 : B	MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
MIL-P-9400 Revision C:1991	PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS
MIL-STD-414 Base Document:1957	SAMPLING PROCEDURE AND TABLE FOR INSPECTION BY VARIABLES FOR PERCENT DEFECTIVE
MIL-I-45208 Revision A:1963	INSPECTION SYSTEM REQUIREMENTS
MIL-STD-965 Revision B:1993	PARTS CONTROL PROGRAM
MIL F 9490 : D	FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-STD-1515 Revision A:1978	FASTENER SYSTEMS FOR AEROSPACE APPLICATION
MIL-STD-1568 Revision D:2015	MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS
MIL-STD-1520 Revision C:1986	CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL
MIL-STD-1587 Revision D:2017	MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
MIL-STD-882 Revision E:2012	STANDARD PRACTICE FOR SYSTEM SAFETY
MIL-M-38795 Revision B:1982	MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF.
MIL-STD-471 Revision A:1973	MAINTAINABILITY DEMONSTRATION
MS33522 Revision C:1984	RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS
MIL-A-21180 Revision D:1984	ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
MIL-STD-1472 Revision G:2012	HUMAN ENGINEERING
MIL-STD-1599 Base Document:1980	BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
MIL-STD-490 Revision A:1985	SPECIFICATION PRACTICES
MIL-Q-9858 Revision A:1963	QUALITY PROGRAM REQUIREMENTS
MIL-M-25047 Revision C:1968	MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED)
MIL-R-9300 Revision B:1968	RESIN, EPOXY, LOW-PRESSURE LAMINATING
MIL-STD-1519 Base Document:1971	TEST REQUIREMENTS DOCUMENT, PREPARATION OF
MIL-STD-105 Revision E:1989	SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES
MIL-STD-785 Revision B:1980	RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
MIL-F-83142 Revision A:1969	FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
MIL A 83444 : 0	AIRPLANE DAMAGE TOLERANCE REQUIREMENTS

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