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Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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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Publisher
Withdrawn date
22-07-2023
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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 AFGS-87221A that has superseded this document is a controlled document only available when giving reason for request.
| DocumentType |
Standard
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| ProductNote |
New child NOT 1 1990 is added
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| Supersedes |
| 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 |
| MIL-STD-1535 Revision B:1992 | SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS (NO S/S DOCUMENT) |
| 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 (NO S/S DOCUMENT) |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| MIL-STD-499 Revision A:1974 | Engineering Management (S/S by IEEE15288.1) |
| MIL-S-52779 Revision A:1979 | Software Quality Assurance Program Requirements (S/S by DOD-STD-2168) |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MIL-STD-45662 Revision A:1988 | Calibration Systems Requirements (Refer to ISO-10012-1 and ANSI-Z540-1 or Comparable Standards as Alternatives to MIL-STD-45662) |
| MIL-S-83490 Base Document:1968 | SPECIFICATION, TYPES AND FORMS (S/S BY MIL-STD-961) |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL-P-9400 Revision C:1991 | Plastic Laminate and Sandwich Construction Parts and Assembly, Aircraft Structural, Process Specification Requirements |
| MIL-STD-414 Base Document:1957 | SAMPLING PROCEDURE AND TABLE FOR INSPECTION BY VARIABLES FOR PERCENT DEFECTIVE (S/S BY ASQC-Z1.9) |
| MIL-I-45208 Revision A:1963 | Inspection System Requirements (No S/S Document) |
| MIL-STD-965 Revision B:1993 | PARTS CONTROL PROGRAM (S/S BY MIL-HDBK-965) |
| 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 Applications (S/S by NASM1515) |
| 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 (NO S/S DOCUMENT) |
| MIL-STD-1587 Revision D:2017 | Material and Process Requirements for Aerospace Weapons Systems |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-M-38795 Revision B:1982 | Manual, Technical: System Peculiar Corrosion Control Preparation of (S/S by MIL-M-87929) |
| MIL-STD-471 Revision A:1973 | MAINTAINABILITY VERIFICATION/ DEMONSTRATION/EVALUATION (S/S BY MIL-HDBK-471) |
| MS33522 Revision C:1984 | RIVETS, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY AND MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS FOR (S/S BY NASM33522) |
| MIL-A-21180 Revision D:1984 | Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180) |
| 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 (S/S BY MIL-HDBK-1599) |
| MIL-STD-490 Revision A:1985 | SpecificationPractices (S/S by MIL-STD-961) |
| MIL-Q-9858 Revision A:1963 | Quality Program Requirements (No S/S Document) |
| MIL-M-25047 Revision C:1968 | Markings and Exterior Finish Colors for Airplanes, Airplane Parts, and Missiles (Ballistic Missiles Excluded) (No S/S Document) |
| MIL-R-9300 Revision B:1968 | Resin, Epoxy, Low-Pressure Laminating |
| MIL-STD-1519 Base Document:1971 | Test Requirements Document, Preparation of (No S/S Document) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| 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 (See Notice 5 for Replacement Information) |
| MIL A 83444 : 0 | AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
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