MIL=STD-810D Downloaded from https://www.everyspec.com 19 JUIY 1983 NOTE: The speeds will be utilized as specified unless the speed poses an unsafe driving condition, in which case the maximum safe operating speed will be utilized. (a) Coarae waahboard (6-inch waves spaced 72 inches apart) - 5 I t@H I (b) Belgian block - 20 MPH (c) Radial waahboard (2-inoh to I 4-inch wavea) - 15 MPH . . . (d) 2-inch waahboard - 10 MPH 5 (e) 3-inoh spaced bump - 20 MPH Step 9. Inapeot,the shelter/test item and oompare t.opr.e-teatcriteria and physical condition. ,. Step 10~ Verify the teat items’.functionality. Step 11. Document the test in accordance with paragraph II-4,.
II-3.4 Procedure IV - Qu~lon (extfamaldy carried . . . let aircraft stOr&. Step 1. Check teat item for performance in accordance with requirements. Step 2, Expose test item to functional test levels. Function the teat item aa if it were in operational usage. Duration of.step 3 shall be one-half of the required duration of functional test. o See I-3.2.7b for durationa. Step 3 . Expose test item to endurance teat levels. The test item need not be functioning during endurance testing. See 1-3.1.7b for durationa. Step 4. Expose teat item to second half of functional teat. Follow step 3 procedure. , Step 5. If test item doea not have a free-flight phase, go to step 9 . Step 6 .
If free-flight teat ia required, expose test ite,mto test levels and duration as defined in paragraph I-3.2.7 (Free Flight). Step 7. Function stores thru free-flight performance requirements during - step 7. Step 8 . If life analysia shows that atore shall not be exposed to buffet vibration, go to step 12. M3THOD 514.3 19 JUIY 1983 514.3-74