MIL-STD-1289D APPENDIX A
TOPIC (paragraph reference) (MIL-STD-1289D requirement) |
COMPLIES |
PHOTO TAKEN |
DEVIATIONS/ COMMENTS |
Loading Clearance (see 4.3.1). Sufficient to conduct loading/unloading. |
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Sufficient at aircraft maximum AUW. |
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External Store Clearances (see 4.3.2) Store to aircraft (see 4.3.2.1) (Minimum is 25.4 mm-wing sweep limits [if applicable].) |
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Store to store (see 4.3.2.2 and also 4.3.4 for fuzes) (Minimum is 25.4 mm for adjacent and tandem.) |
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Store to pylon (see 4.3.2.3) (Minimum is 12.7 mm-noting that exceptions allowed.) |
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Rail launched (see 4.3.2.4) (Minimum is 25.4 mm.) |
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Ejection launched (see 4.3.2.5) (Minimum is 25.4 mm.) |
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Intake duct (see 4.3.2.6) (Assessment of aircraft stall/flameout/FOD?) |
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Arming control system (ACS) (see 4.3.2.7) (Adequate to enable operation of ACS.) |
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Propeller/rotor disk clearance (see 4.3.2.8) (Minimum is 152.4 mm + 5o half angle.) |
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Damage from spent ammunition precluded (see 4.3.2.8) |
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Internal Store Clearances (see 4.3.3) Store to aircraft (see 4.3.3.1) (Minimum is 25.4 mm.) |
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Store to store (same as 4.3.2.2) (Minimum store to store is 25.4 mm; Navy 63.5 mm.) |
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