Used on fixed wing aircraft, boeing model757. 0.4000" overall length subassembly is valve chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.4300" overall length subassembly is support instl-winginbd te pnl; refer to boeing i.p.c. BOE2438 57-51-01-07 no. 162 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.4400" overall length subassembly is mechanism instl-passenger door handle; refer to boeing i.p.c. BOE2439 52-11-13-01 no. 420 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.4500" overall length subassembly is compartment instl-ovhd stowage; refer to boeing i.p.c. BOE2440 25-28-00-72m no. 225 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.5000" overall length subassembly is door assy-no. 2 passenger; refer to boeing i.p.c. BOE2442 52-11-01-28 no. 380 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.5300" overall length subassembly is compartment instl-aft sect. ovhd stowage; refer to boeing i.p.c. BOE2443 25-28-00-72p no. 225 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.5800" overall length subassembly is door instl-no. 4 passenger; refer to boeing i.p.c. BOE2444 52-11-01-01 no. 542 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.7200" overall length subassembly is control unit instl-rud pwr chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.8100" overall length subassembly is door assy-no. 2 passenger; refer to boeing i.p.c. BOE2447 52-11-01-28 no. 190 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.8400" overall length subassembly is mechanism instl-passenger door no. 4 emer operation; refer to boeing i.p.c. BOE2436 52-11-20-30 no. 230 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.9000" overall length subassembly is door assy no. 2 passenger; refer to boeing i.p.c. BOE2449 52-11-01-28 no. 200 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 1.1800" overall length subassembly is mechanical instl passenger door no. 2 emer operation; refer to boeing i.p.c. BOE2451 52-11-20-01 no. 150 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.2400" overall length subassembly is fairing instl-strut aft; refer to boeing i.p.c. BOE2425 54-52-01-03 no. 70 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.2500" overall length subassembly is actuator instl-nlg; refer to boeing i.p.c. BOE2423 32-3 5-21-01 no. 45 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.9900" overall length subassembly is track instl-wing le aux; refer to boeing i.p.c. BOE2446 27-81-11-05 no. 175 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.5000" overall length subassembly is flap instl-te inbd; refer to boeing i.p.c. BOE2415 27-51-02-02 no. 40 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.1000" overall length subassembly is pump instl-ram airturb hydr; refer to boeing i.p.c. BOE2416 29-21-01-01 no. 95 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.5600" overall length subassembly is rib instl-main track outbd fxd le sprt; refer to boeing i.p.c. BOE2417 57-22-51-15 no. 45 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.6100" overall length subassembly is rib instl-rud sta 156.074 vert. stab. fxd te; refer to boeing i.p.c. BOE2331 55-36-52-03 no. 95 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.6200" overall length subassembly is carriage assy-inbd; refer to boeing i.p.c. BOE2418 27-51-05-01no. 4.5 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 1.0000" overall length subassembly is rudder instl; refer to boeing i.p.c. BOE2419 55-40-51-01no. 140 chromate surface treated 17c solid, plain, no outside flanges
Used on fixed wing aircraft, boeing model757. 0.1400" overall length sub assembly is aileron instl; refer to boeing i.p, c. BOE2420 27-11-21-01 no. 640 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. subassembly is rib instl-rud sta 156.074 vert. stab. fxd te; refer to boeing i.p.c. BOE2320 55-36-52-03 no. 155
0.1600" overall length subassembly is track instl-wing le aux; refer to boeing i.p.c. BOE2329 27-81-11-05 no. 85 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing 757. 0.1100" overall length subassembly is valve instl-nlg door operated seq; refer to boeing i.p.c. BOE2345 32-34-05-01 no. 445 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing 757. 0.1300" overall length subassembly is spar instl-vert. stab. rear aft torque box; refer to boeing i.p.c. BOE2344 55-33-00-01 no. 16 5 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.2000" overall length subassembly is door instl-no. 1 passenger lh; refer to boeing i.p.c. BOE2343 52-11-01-03 no. 411 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.2500" overall length subassembly is valve instl-nlg door operated seq; refer to boeing i.p.c. BOE2342 32-34-05-01 no. 365 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.1800" overall length subassembly is door instl-no. 4 passenger; refer to boeing i.p.c. BOE2341 52-11-01-01 no. 308 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.1800" overall length subassembly is door instl-no.4 passenger; refer to boeing i.p.c. BOE2340 52-11-01-01 no. 312 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.1900" overall length subassembly is support instl-winginbd te pnl; refer to boeing i.p.c. b OE2330 57-51-01-07 no. 111 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing 757. 0.4800" overall length subassembly is door instl-no. 1 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. subassembly is mechanism instl-emer operation pass. door no. 1l; refer to boeing i.p.c. BOE2328 52-11-20-05 no. 185 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. subassembly is support inst-no. 1cargo door hinge; refer to boeing i.p.c. BOE2421 53-33-58-01 no. 100 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. 0.1000" overall length subassembly is gear instl-sect. 62 nlg var; refer to boeing i.p.c. BOE2422 32-21-00-01b no. 175 cadmium surface treated 22c solid, external flange one end
Used on fixed wing aircraft, boeing model757. subassembly is release instl-nlg door; refer to boeing i.p.c. BOE2435 32-35-22-01 no. 145 cadmium surface treated 22c solid, external flange one end
