0.329" hole diameter 0.595" outside diameter 0.057" material thickness service temperature alloy steel-600 f, (900 f for intermittent operation) cadmium surface treated 15 recessed
0.344" hole diameter 0.595" outside diameter 0.057" material thickness service temperature alloy steel-680 f (900 f for intermittent operation) cadmium surface treated 15 recessed
Used on fixed wing aircraft, boeing model757. 0.376" hole diameter 0.725" outside diameter 0.057" material thickness subassembly is support instl-l anodize surface treated shouldered
Used on fixed wing aircraft, boeing model757. 0.376" hole diameter 0.725" outside diameter 0.057" material thickness subassembly is power assist instl-passenger door no. 1 r emer; refer toboeing i.p.c. BOE2430 52-11-30-01 no. 695 passivate or cadmium surface treated shouldered
Used on fixed wing aircraft, boeing model757. 0.376" hole diameter 0.830" outside diameter 0.064" material thickness subassembly is transmission instl-inbd te flap drive outbd; refer to boeing i.p.c. BOE2429 27-51-06-01no. 22 anodize surface treated shouldered
Used on fixed wing aircraft, boeing model757. 0.501" hole diameter 0.950" outside diameter 0.064" material thickness subassembly is rib instl-rud sta 131.108 vert. stab. fxd te; refer to boeing i.p.c. BOE2358 55-36-52-02 no. 40 passivate or cadmium surface treated shouldered
