01-172-8816
Access Aircraft Cover
01-172-8817
Access Aircraft Door
01-172-8823
Fuselage Aircraft Fairing
01-172-8824
Aircraft Fairing
01-172-9079
Access Aircraft Door
Used on acft model c-135. used on door assy-trailing edge fairing inbd strut; -628 c/o doubler (5) stock size-.032X2.3X2.3in, finish f-2.10, ht tr T81; zee member (4) stock size all-.032X2.4, -614 9.2in l, -642 18.5in l, -643 10.7in l, -644 18.3in l, finish f-2.10, ht tr T62; outer skin (1) stock size-.080X15.0X22.5, finish f-2.10, ht tr T81; inner skin (1) stock size-.032X12.0X20.0, finish f-2.10, ht tr T81; core (1) stock size-.25X12.0X20.0, aluminum honeycomb core per BMS4-4, 3-30n; doubler (1) stock size-.032X15.0X22.5, finish f-2.10, ht tr T81; sleeve bolt (23) ; retainer ring (23)
01-172-9081
Access Aircraft Door
01-172-9195
Aircraft Bulkhead
Used on aircraft model h-1. navy managed item
01-172-9324
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 5.000 in. lg, 1.500 in. w, 0.050 in. thk
01-172-9325
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 5.000 in. lg, 1.540 in. w, 0.050 in. thk
01-172-9326
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 5.000 in. lg, 1.540 in. w, 0.050 in. thk
01-172-9327
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 12.000 in. lg, 2.540 in. w, 0.050 in. thk
01-172-9328
Structural Aircraft Plate
Used on acft model b-52. magnesium alloy sheet per qq-m-44condition a f-3.35, 51.000 in. lg, 2.000in. w, 0.050 in. thk
01-172-9329
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 14.000 in. lg, 2.540 in. w, 0.030 in. thk
01-172-9330
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy clad sheet per qq-a-362 2024-0, 27.500 in. lg, 2.500 in. w, 0.050 in. thk
01-172-9331
Structural Component Air Support
Used on f-4 acft. matl st, mil-s-5000, 4340; 6.410 in. lg; used as lug suspension, fuel tank
01-172-9333
Structural Component Air Support
Used on acft model kc-135. stock size-.063X4.40X9.50in; material 2024-0 alclad sheet per qq-a-250/5; heat treat T4; finish srf-2.115; used on bracket support-reversing crank
01-172-9334
Structural Component Air Support
Used on acft model kc-135. stock size-.050X3.60X7.00in; material 2024-T3 alclad sheet per qq-a-250/5; heat treat T4; finish srf-2.115; used on bracket support-reversing crank
01-172-9335
Structural Component Air Support
Used on acft model kc-135. alter bac-1505-18884; material 2024-T4 extruded per qq-a-200/3; finish srf-2.30; used on bracket support-reversing crank
01-172-9337
Structural Component Air Support
01-172-9338
Structural Component Air Support
Used on acft model kc-135. material 2024al aly bar per qq-a-268, T4 temp; finish srf-2.30; height-6.80in, w/bevelled edges on both ends of top of support, center portion is .32in thick; width-1.03in; depth-1.50in
01-172-9339
Structural Component Air Support
Used on acft model kc-135. support alter BAC1518-357; material 7075-T6 per qq-a-200/11 T6 temper; finish srf-2.30; used on -1 support assy-feel mechanism rudder
01-172-9340
Aircraft Former
01-172-9341
Structural Component Air Support
Used on acft model kc-135. stock size-.050X6.90X8.50in; matl 2024-0 alum sheet per qq-a-355, 0 temper; ht tr T4; finish srf-2.30; used on -2 bracket assy-pulley, rudder trim
01-172-9342
Structural Component Air Support
Used on acft model kc-135. stock size-.05X5.00X10.40in; material 2024-0 aluminum sheet per qq-a-355 0 temper; heat treat to T4; finish f-2.22; used on bracket assy-pulley, rudder trim; part of -3
01-172-9344
Structural Component Air Support
Used on acft model kc-135. ral alloy clad sheet 2024-0 per qq-a-362, 0 temp; heat treated to cond. T4; finish f-2.115; stock size 12.000 in. square, 0.050 in. thk; contains 2 0.500 in. dia holes, 8 0.250 in. dia holes; opposite p/n -4; nha 65-19985
01-172-9345
Structural Component Air Support
Used on acft model kc-135. stock size-.071X4.7X3.10in; material-2024-0 alclad per qq-a-362, 0 temper; ht tr T4; finish f-2.115; 4 bolt holes, 1/4dia., two in each end
01-172-9346
Structural Component Air Support
Used on acft model kc-135.
01-172-9347
Structural Component Air Support
Used on acft model c-135.
01-172-9363
Aircraft Former
01-172-9641
Airframe Modification Kit
Used on f/a-18 non-hsp (hornet support plan)support.
01-172-9642
Airframe Modification Kit
Used on aircraft model f/a-18 non-hsp (hornet support plan) support.
01-173-0537
Structural Component Air Support
Used on c-5 acft. matl al alloy, qq-a-367, 7075-T6; 50, 000 psi tension
01-173-0539
Structural Component Air Bracket
01-173-0540
Structural Component Air Support
Used on acft model f-16a/b. corrosion resistant steel bar PH13-8mo per ams-5629; heat treated to H1000 condition per fps-3014; finish S457; base 2.760 in. lg, .920 in. w, .162 in. thk, contains 2 0.530 in. slots; forked projection perpendicular to base, 1.640 in. lg, 1.650 in. w, 0.410 in. thk at base, 0.110 in. thk slot centered in thk 1.150 in. deep; serial no. effectivity 61 0001 0261; nha 16W020-845; opposite p/n -9
01-173-0541
Structural Component Air Support
Used on f-4 acft. matl al alloy, A356, class 1, mil-a-21180; made from p/n 311J006-1; used as support, aft, aircraft fuel tank-casting
01-173-2506
Aircraft Wing Assembly
01-173-2507
Aircraft Wing Assembly
01-173-3143
Aircraft Fairing
Nha 16E3147-3; effect on 5c 00001-99999; alum alloy A356-T61; finish A44
01-173-3146
Structural Component Air Support
Used on c-5a acft. used as bracket assy on duct, bleed air
01-173-3147
Structural Component Air Support
Used on f-16b usaf aircraft. ec/o--1 insert, -3 clinch ring, fabric flange; material-insert-al aly 6061-T651 per qq-a-250/11 or qq-a-225/8, of ring-al aly 6061-T6 per qq-a-250/11 or qq-a-225/8; circular shape-5.980 max dia, 0.198 thk
01-173-3148
Structural Component Air Support
Used on f-16b usaf aircraft. function-fitting assy, support; c/o--1 insert, -3 clinch ring, fabric flange, 3 self-locking inserts; shape-triangle with rounded corners; dimensions-base-2.900 in., height-2.730 in.; self-locking inserts-0.190-32 unjf-3b M45932-9l; max thickness-0.750 in.; eff on 0003 9999
01-173-3149
Structural Component Air Support
Used on f-16b usaf aircraft. qfunction-fitting assy, combination; c/o--1 insert, -3 clinch ring, fabric flange; material-insert-al aly 6061-t-651 per qq-a-250/11, of ring-al aly 6061-T6 per qq-a-250/11; max w.-9.00 x max h.-12.82 in. x max thk-0.343 in.
01-173-3150
Structural Component Air Support
Used on f-16b usaf aircraft. function-fitting assy, combination; c/o--1 insert, -3 clinch ring, fabric flange, 4 M45932/1-13l inserts; material--1 insert-al aly 6061-T651 per qq-a-250/11, of ring-al aly 6061-T6 per qq-a-250/11; 4 inserts-0.250-28 unjf-3b self-locking; oval shape-max w-12.350 in x max l-8.840 in x max thk-0.750 in.; eff on-0003 9999
01-173-3151
Structural Component Air Support
Used on f-16b usaf aircraft. function-fitting assy, access; c/o--1 insert, -3 clinch ring, fabric flange, 2 MS21209-F1-15 inserts, 42 MS21209-F4-15 inserts; material-of -1 insert-al aly 6061-T651 per qq-a-250/11, of ring-al aly 6061-T6 per qq-a-250/11; rectangular shape with rounded corners; dimensions-20.530 in. w x 12.680 in h thru centers of holes x 0.875 thk; eff on-0003 9999
01-173-3152
Structural Component Air Support
Used on f-16c/d usaf aircraft. made from aluminum alloy casting per ams-4218-T6, finish A100; dimensions-2.320 in. h x 3.000 in w; nha 16H1900-1; eff on 5c 0001 9999
01-173-3153
Structural Component Air Support
Used on acft model b-1b. made from -003 forging per mil-f-83142; 28.500 in. o/a lg, 12.440 in. o/a w, 6.000 in. o/a h; nha L6312001
01-173-3154
Structural Component Air Support
Used on acft model b-1b. c/o 2 7075-T6 al sheets per qq-a-250/12, -003 5.540 in. lg, 5.010 in. w, 0.190 in. thk, -005 5.650 in. lg, 5.130 in. w, 0.190 in. thk, 1 shim, 1 stop, 8 bolts, 8 washers, 8 nuts; nha L6311583
01-173-3155
Structural Component Air Support
Used on acft model b-1b. c/o 1 fitting, 5 assorted shims; fitting al alloy plate 7075-T651 per qq-a-250/12; hard anodize per mil-a-8625; 5.600 in. lg, 5.120 in. w, 1.680 in. h; nha L6311083
01-173-3156
Structural Component Air Support
Used on acft model b-1b. machined al rolled bar 2024-T851 per qq-a-225/6; hard anodize per mil-a-8625; 3.460 in. o/a lg, 2.870 in. o/a w, 1.250 in. o/a thk; nha L6312001
01-173-3157
Structural Component Air Support
Used on acft model b-1b. al investment casting, alloy A356.0; 3.750 in. o/a lg, 3.750 in. o/a w, 1.500 in. h; nha L6312001
