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MRC | Criteria | Characteristic |
---|---|---|
FTLD | III FUNCTIONAL DESCRIPTION | USED IN ADJUSTMENT OF FLIGHT CONTROL SYSTEM; NOSE WHEEL STEERING SYS; BRAKE SYS; AERIAL REFUELING SYS; CARGO DOOR UPLATCH RELEASE SYS; (LOCKING FOR ADJUSTMENT IS ACCOMPLISHED BY THE INSERTION OF VARIOUS SIZE PINS INTO DEDICATED HOLES DESIGNED INTO SPECIFIC COMPONENTS OF EACH SYS) |
FEAT | SPECIAL FEATURES | THE FOLLOWING PIN SIZES ARE UTILIZED; AILERON 0.3125 X 3.250; 0.3125 X 8.000 2 EA; ELEVATOR SYS 0.3125 X 3.250 3 EA AND 0.3125 X 8.000 2 EA; RUDDER SYS 0.3125 X 3.250 1 EA AND 0.3125 X 9.500 2 EA; HORIZONTAL STABILIZER 0.3125 X 2.000 2 EA,0.3125 X 8.000 1 EA; NOSE WHEEL STEERING 0.3125 X 3.250 1 EA; BRAKE SYS 0.3125 X 8.000 1 EA; AERIAL REFUELING SYS 0.3125 X 3.250 1 EA; CARGO DOOR UPLATCH RELEASE SYS 0.3125 X 2.000 AND 0.3125 X 3.250 1 EA |
SR-5 | THE MANUFACTURERS DATA | |
AGAV | END ITEM IDENTIFICATION | C-17 ACFT |
SR-5 | DESIGN CONTROL REFERENCE | 17G140015-1 |
SR-5 | MANUFACTURERS CODE | 88277 |
RDAL | III REFERENCE DATA AND LITERATURE | TO 1C-17A-4-4; SERD 140015 |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | RIGGING EQUIPMENT, CABLE, MECHANICAL CONTROLS |
Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |