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MRC | Criteria | Characteristic |
---|---|---|
FEAT | Special Features | J SHAPED STRINGER HAVING 89 DEGREE ANGLE ON LARGER SIDE CONNECTION AND 91 DEGREE ANGLE ON SHORTER SIDE CONNECTION; HAVING TWO THRU HOLES LOCATED AT 5.000 AND 15.970 INCHES FROM LEFT END; ALSO HAVING TWO ADDITIONAL THRU HOLES LOCATED BETWEEN LEFT END AND THE 5.000 INCH HOLE; LARGER SIDE PORTION HAS 21 THRU HOLES EVENLY SPACED BETWEEN THE BENDS IN THE STRINGER |
AGAV | End Item Identification | MH60 |
CZEJ | Aircraft Station Number | WL261.20 AND WL256.70 |
MDCL | Material Document And Classification | AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
CXCY | Part Name Assigned By Controlling Agency | (INAVY)STRINGER INSTALLATIOON, SIDE FUSELAGE |
CZEK | Aircraft Mission Design Series | MH60 |
MRC | Decoded Requirement | Clear Text Reply |
MATT | Material | ALUMINUM ALLOY 7075 |
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