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| MRC | Criteria | Characteristic |
|---|---|---|
| ALCD | Usage Design | AFT ESCAPE HATCH,CARRIAGE EJECTION SEAT,FUEL BLOWER LINE REPLACEMENT UNIT,EJECTION SEAT,CHAFF/FLARES PKG,ACCESSORY DRIVE SUBSYSTEM,HYDRAULIC ACCUMULATOR OF AUXILIARY POWER UNIT,FORWARD ESCAPE HATCH,INTEGRATED DRIVE GENERATOR,AUXILIARY POWER UNIT,HYDRAULIC RESERVOIR,WING SWEEP POWER DRIVE UNIT,FUEL COOLER HEAT EXCHANGER,WINDSHIELD |
| FEAT | Special Features | CONSISTS OF HOISTING RING; THREE LEGS WITH SQUARE EYE SWIVEL SNAP,POLYESTER WEB STRAP,ADJUSTABLE BUCKLE,JAW AND EYE TURNBUCKLE,CONNECTING LINK,SWIVEL EYE SNAP; STORAGE CONTAINER; LIFT LOADS UP TO 500 LBS |
| AGAV | End Item Identification | B-1B AIRCRAFT |
| FCLS | Functional Classification | HH-1.5 |
| MRC | Decoded Requirement | Clear Text Reply |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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