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of the aircraft, aircraft suspension equipment and the store's electronic systems or subsystems (including all electro- explosive devices) and the test data and reports generated during development and qualification testing in accordance with MIL-STD-461 and MIL-STD-462, and the systems level requirements of MIL-E-6051, MIL-STD-1818, or MIL-STD-464, MIL-STD-1512, MIL-HDBK- 1763, Test 154, MIL-HDBK-1763, Test 224 and ADV PUB 20/30 in the environment of MIL- STD-1385 or MIL-STD-464. Note that the “aircraft” EMC/EMI and HERO classification is to Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:54Z Check the source to verify that this is the current version before use. MIL-HDBK-1763 APPENDIX C 202 include results for the aircraft and all store suspension pylon/rack combinations. MI

raft/stores compatibility disciplines. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:54Z Check the source to verify that this is the current version before use. MIL-HDBK-1763 APPENDIX C 204 PART IV - AEROELASTICITY C.IV.1 Aeroelastic data. The aeroelastic data should cover the entire range of aircraft/store configurations, including authorized and failure mode store partial downloads, wing sweeps, required mixed weapon loads, fuel expenditure, and applicable limit speeds. It should identify margins of safety for all configurations and authorized downloads in accordance with MIL-HDBK-1763 wing damping and flutter limit speeds criteria. C.IV.2 Aeroelastic ground vibration tests. This section should identify satisfactory compliance with MIL-HDBK-1763, Test 120 aeroelastic GVT to

identify satisfactory compliance with MIL-HDBK-1763, Test 120 aeroelastic GVT to help substantiate the flutter/aeroelastic analysis of all aircraft/stores configurations, their authorized downloads and failure downloads for all identified aircraft/stores configurations to the limits identified in Part I. C.IV.3 Aeroelastic wind tunnel testing. This section should identify satisfactory compliance with MIL-HDBK-1763, Test 143 for all identified aircraft/stores configurations to the limits identified in Part I. C.IV.4 Flight tests. This section should specify satisfactory compliance with MIL-HDBK-1763, Test 210 for those configurations requiring flutter flight testing to address all identified aircraft/stores configurations to the limits identified in Part I. C.IV.5 Part IV compliance. Compli

ired munitions and projectiles have clearance from the air vehicle or other stores IAW MIL-STD-1289, Clearances section and Installation Test Methods section and MIL HDBK-1763, Test 160. Prior to entering operational test/operations, verify the standard by the above and following method(s): Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:47Z Check the source to verify that this is the current version before use. MIL-HDBK-516D 740 Test. (3) Flight test: Verify stores do not contact the air vehicle or adjacent stores throughout the operational envelope. (4) Flight test: Verify that fired munitions and projectiles do not contact the air vehicle or other stores IAW MIL HDBK-1763, Test 273 and Test 274. 17.1.1.2 Mechanical function. Standard: Air vehicle and store mechanical interfa

553 DOD-STD-1686 MIL-STD-1760 MIL-STD-1763 MIL-STD-2088 HANDBOOKS MILITARY MIL-HDBK-235-1 DOD-HDBK-263 ElectroexplosiveSubsystems, Electrically Initi- ated, Design Requirements and Test Methods Digital Time Division Command/Response Multiplex Data Bus Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices)(Metric) Aircraft/Store Electrical Interconnection System Aircraft/Stores Certification Procedures Bomb Rack Unit (BRU), Aircraft,--GeneralDesign Criteria for Electromagnetic (Radiated) EnvironmentConsider- ations for Design and Procurement of Electrical and Electronic Equipment, Subsystems and Systems Electrostatic Discharae Control Handbook for Protection of Electri~al and El

EEK EAGLE support for USAF programs in production and to provide a baseline capacity of technical expertise, modeling, and simulation tools, known flight and wind tunnel testing, and SEEK EAGLE resources available for USAF programs. It is the responsibility of the aircraft or store manager to fund all other activities such as TO publication and operational flight program updates. See AFPAM 63-129 for additional information. 5.4.22.1.4. The aircraft PM applies the DoD standardized procedures in MIL-HDBK- 1763, Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures, for the certification of stores on aircraft; waivable by the MDA. MIL- HDBK-244A, Guide to Aircraft/Stores Compatibility, provides guidance on evaluating the safety and acceptability of store-air

s, known flight and wind tunnel testing, and SEEK EAGLE resources available for USAF programs. It is the responsibility of the aircraft or store manager to fund all other activities such as TO publication and operational flight program updates. See AFPAM 63-129 for additional information. 5.4.22.1.4. The aircraft PM applies the DoD standardized procedures in MIL-HDBK- 1763, Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures, for the certification of stores on aircraft; waivable by the MDA. MIL- HDBK-244A, Guide to Aircraft/Stores Compatibility, provides guidance on evaluating the safety and acceptability of store-aircraft combinations. 5.4.22.2. Store PMs produce a SEEK EAGLE store certification data package for each store that they manage and provide