01-105-8310
Structural Component Air Support
01-105-8311
Structural Component Air Support
Used on acft model f-111f. c/o bracket 1 ea p/n 12E3131-7, bracket assy 1 ea p/n 12E3129-3, rivet as required p/n MS20470AD5, 10.600 in.lg, 2.500 in.w, 2.350 in.h, used on weapons bay
01-105-8312
Structural Component Air Support
Used on acft model f-111f. c/o bracket 1 ea p/n 12E1046-147, washer 12 ea, screw 4 ea, nut 4 ea, rivet as required
01-105-8313
Structural Component Air Support
Used on acft model f-111f. al alloy 2024-T851 per fms-1010-T851, 3.000 in.thk, 13.000 in.w, 32.000 in.lg, used on fwd pave tack pod
01-105-8314
Structural Component Air Support
Used on acft model f-111f. al alloy 2024-T851 per fms-1010-T851, 3.000 in.thk, 11.000 in.w, 37.656 in.lg, used on aft pave tack pod
01-105-8316
Longeron
Used on acft model f-16a usaf. 106.000" overall length 10.000" overall width 2.750" material thickness
01-105-8317
Aircraft Skin
55.000" overall length 17.000" overall width superseded p/N16B1318-29, effecti vity 5c 0001 9999, ecn 2C169, nha 16B1932-3
01-105-8318
Aircraft Skin
55.000" overall length 17.000" overall width superseded p/N16B1318-27 i/c code ni, effectivity 62 0077 9999, ecn 93839, nha 16B2932-5
01-105-8319
Aircraft Skin
Used on f-16 airplane.. 16.000" overall length 7.000" overall width
01-105-8320
Vertical Stabilizer
Used on f-16a/b usaf aircraft.
01-105-8797
Bell Crank
Used on ch-47, rotary wing aircraft.
01-105-9521
Access Aircraft Door
Used on acft b52. pressure tested to withstand 8 psi pressure
01-105-9998
Aircraft Former
Used on aircraft,c-5a. 3.140" overall length 1.300" overall width 0.040" material thickness
01-106-0408
Fuselage Aircraft Fairing
Used on boeing acft model 727. u/o fin to body instl trailing edge forward;
01-106-1642
Exhaust Pipe Flange
01-106-1808
Structural Aircraft Plate
Used on acft model rf4c. al alloy 2024-T3 per qq-a-250/4, 3.900 in.w, 4.000 in.lg, 0.350 in.to 1.050 in.h
01-106-1811
Structural Component Air Support
Used on acft model f4e. al alloy A356-T61 per mil-a-21180, class 11, cond T61, right hand, 4.800 in.lg, 0.108 in.thk, located at cfs 74.470
01-106-1813
Aircraft Skin
46.000" overall length 27.000" overall width
01-106-1815
Aircraft Skin
46.000" overall length 27.000" overall width
01-106-2270
Bell Crank
Used on ch-47, rotary wing aircraft.
01-106-2280
Access Aircraft Cover
Cover
01-106-2281
Access Aircraft Door
Used on eh-60a,uh-60a aircrafts.
01-106-4130
Former
Aluminum alloy 2024-0; size 0.032 by 7.000 by 19.500; door assy engine access; F4 aircraft;
01-106-4133
Aircraft Skin
56.000" overall length 27.000" overall width inboard skin
01-106-5057
Access Aircraft Cover
01-106-6019
Structural Aircraft Panel
19.120" overall length 0.225" overall width countersink for nas 517-3 screw eight places; opposite p/n 4F34210-603a
01-106-6020
Structural Component Air Support
9.000" overall length 2.000" overall width 0.500" material thickness supercedes p/n: 16B6221-11; n/a: 16B603-3, 61 0260 9999; matl:alum aly per fms 3002
01-106-6031
Aircraft Skin
Used on acft model f-16. 54.000" overall length 41.000" overall width
01-106-6032
Aircraft Skin
Used on acft model f-16. 54.000" overall length 41.000" overall width
01-106-6828
Structural Aircraft Plate
20.310" overall length part of a/A32h-4a cargo handling system; used as: slide strip; material: LS30876-1
01-106-7079
Structural Aircraft Plate
Material cres type 303 per astm A5B2; finish passivate per qq-p-35, 2.00 in. lg, 0.38 in. w, 1.50 in. h, 2 1/4-28 in. holes 1.000 in.c to c, 0.50 in. from ends, 0.625 in. from top
01-106-7136
Aircraft Frame
01-106-7137
Aircraft Frame
01-106-7173
Aircraft Door
01-106-7656
Former
Used on f-16a/b usaf. location-fs 137.00; made from -19 forging; material-aluminum alloy per qq-a-367; finish-A100; nha-1681931-5; eff on 61 0262 9999;
01-106-7657
Access Aircraft Door
Used on F-16. rh lower strake FS190 to FS217
01-106-7660
Structural Aircraft Plate
15.000" overall length shield, internal heat
01-106-7680
Fuselage Aircraft Fairing
Used on acft model f-16.
01-106-7685
Aircraft Floor
Used on F-16. c/o stiffener 1 ea p/n 16B1705-31, stiffener 1 ea p/n 16B1705-33, stiffener 1 ea p/n 16B1705-35, web 1 ea p/n 16B1705-37, plate 1 ea p/n 16B1705-39
01-106-7686
Aircraft Skin
Used on f-16b usaf aircraft. 40.000" overall length 11.000" overall width location-aft canopy, upper, fs 231.8-242.6; c/o-16B5888-1 insulation -13 skin 0.250 x 11X40 in.; replaces -13 ni; nha 16B212-13; eff on -62 0077 9999
01-106-9092
Access Aircraft Door
01-106-9482
Access Aircraft Door
01-106-9753
Structural Component Air Support
Opp p/n 18-32103-1
01-106-9756
Structural Component Air Support
Manufacture name: arm, actuator opp p/n 18-32102-1
01-107-0118
Structural Component Air Bracket
01-107-0129
Aircraft Skin
Used on c-135 airplane.. 81.300" overall length 20.200" overall width matt clad, heat treat per T6,
01-107-1882
Aircraft Trailing Edge
