MIL-STD-1822 Nuclear Compatibility Certification Of Nuclear Weapon Systems, Subsystems And Support EquipmentThis document describes standard practices for nuclear compatibility certification of nuclear weapon systems excluding nuclear facilities. Nuclear weapon system compatibility certification authority is derived from the 1953 Atomic Energy Commission AEC/Department of Defense DoD Memorandum of Agreement MOA and restated within numerous DoD and Air Force AF directives.

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MIL-STD-1822A(USAF) APPENDIX A

a. F-15E: 22 stations required; five aircraft over a two-year moving window if five stations remain certified on the aircraft, eight aircraft over a two-year moving window if certified stations are reduced to three per aircraft.

b. F-16C/D: 22 stations required; 11 aircraft over a two-year moving window

c. B-2A: 21 stations required; two aircraft over a two-year moving window. This is based on eight stations per RLA (Rotary Launcher Assembly), and the number of RLAs at the B-2A home station.

d. B-52H: 22 stations required for gravity bombs; three aircraft over a two-year moving window. NOTE: Surveillance testing is not currently conducted on cruise missiles since they are not governed by System 1 Specification. SNL conducts a functional check of AMAC signals between the aircraft and cruise missile with nominal electrical current loads, but does not measure the signals at the W80-1 to ALCM interface. The AMAC POG is investigating the proper test protocol to measure the physical signals at the DOD/DoE interface.

e. F-16 MLU: (Belgium and Netherlands) 21 stations required; 11 aircraft over a two- year moving window.

f. PA-200: (Germany and Italy) 21 stations required; 11 aircraft over a two-year moving window.