Used on fixed wing aircraft, boeing model757. 0.376" hole diameter subassembly is fairing instl-wingte mlg trun; refer to boeing i.p.c. BOE2431 32-12-10-01 no. 250 anodize surface treated
Used on fixed wing aircraft, boeing model757. 0.4380" hole diameter subassembly is flap assy-te inbd; refer to boeing i.p.c. BOE2427 27-51-02-10a no. 712 cadmium surface treated
Used on fixed wing aircraft, boeing model757. 0.498" hole diameter subassembly isfairing instl-wing te mlg trun; refer to boeing i.p.c. BOE2413, 32-12-10-01 no. 190 passivate surface treated
Used on b757 aircraft. 0.250" hole diameter washer, plain heat treat to tensile strength per ams-h-6875; service temperature 450.0 degrees f; used on transmission installation-inboard t.e. flap drive outboard (inboard t.e. flap transmissions only) cadmium surface treated
