MIL A 87221 : 0
Withdrawn
Withdrawn
AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
Amended by
Publisher
Withdrawn date
07-22-2023
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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 AFGS-87221A that has superseded this document is a controlled document only available when giving reason for request.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
|
| ProductNote |
New child NOT 1 1990 is added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| 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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