01-172-0241
Structural Component Air Support
Used on acft model f-16a/b. al alloy plate 2124 per fms-3002, T851 temper; finish A461; 2.760 in.w at base, 0.360 in.w at projection, 1.000 in.h at base, 1.652 in.h end of projection, 1.951 in.o/a lg; 2 0.530 in.slots in base; serial no.effectivity 61 0001 0261; nha 16W020-846; opposite p/n -9;
01-172-0242
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha-16W020-835; nhra-16W020-843; eff on-61 0005 0027
01-172-0243
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha-16W020-836; nhra-16W020-844; eff on-61 0005 0027
01-172-0244
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha-16W020; nhra-16W020-843; eff on-61 0005 0027
01-172-0245
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha 16W020-836; nhra 16W020-844; eff on 61 0005 0027
01-172-0246
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha 16W020-835; nhra 16W020-843; eff on-61 0005 0027
01-172-0247
Structural Component Air Support
Used on f-16a/b usaf aircraft. bracket; stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha 16W020-835; nhra 16W020-843; eff on-61 0005 0027
01-172-0248
Structural Component Air Support
Used on f-16a/b aircraft. stock size-4X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha 16W020-836; nhra 16W020-844; eff on-61 0005 0027
01-172-0249
Structural Component Air Support
Used on acft model kc-135.
01-172-0261
Aircraft Former
01-172-1038
Structural Component Air Support
01-172-1451
Structural Aircraft Panel
01-172-1459
Airfoil Rib
33.000" overall length 2.750" overall width 0.063" material thickness
01-172-2751
Fuel Aircraft Tank
50.740 in. nom o/a lg; 34.810 in.nom o/a h
01-172-2752
Fuel Aircraft Tank
50.740 in. nom o/a lg; 34.810 in.nom o/a h
01-172-3193
Structural Aircraft Plate
Used on c-5 acft. matl al alloy, 7079-T6; matl size 0.050 by 7.000 by 22.000 in. lg; used as panel on leading edge wing
01-172-3506
Refueling Aircraft Probe
Used on aircraft model av-8. navyi probe assembly
01-172-3708
Attachment Molded Tank Flange
Used on aircraft model f-18.
01-172-3709
Attachment Molded Tank Flange
Used on aircraft model f-18.
01-172-3728
Fluid Aircraft Manifold
2.960" overall length 2.924" overall width
01-172-4071
Movable Canopy
01-172-4393
Aircraft Window Panel
Gu/a: window assy, cam; c/o: forward oblique glass, to meet mil-g-174; borosilicate crown type bk-7.517642, fine annealed, wedge angle max 15 aroseconds; modified pear shape; symmetrical about centerline, bottom with center to edge 3.990in. min, 4.010 in. max; top center to edge wdth 2.460 in. min, 2.480 in max; hgt 14.950 in. nom, 14.980 in. max; thk 0.375 in. nom; coating, single layer of magnesium fluoride per mil-c-675c; wedge angle per mil -w-1366
01-172-4394
Aircraft Window Panel
U/a: window assy, cam; c/o: commercial plate glass; clear; surfa quality shall be 80-50 per mil-o-13830; coating, anti-reflection, single layer of magnesium fluoride per mil-c-675c, min ref 575 nm to 600nm wave length; o/a lg 16.790 in. min
01-172-4395
Aircraft Window Panel
U/a: window assy, cam; matl: glass per mil-g-174; borosilicate crown type bk-7.517642 or equivalent; grade nh-2a, fine annealed; min 87 percent transmission between 400
01-172-4410
Structural Component Air Support
Used on acft model f-16c/d. made from rough aluminum alloy casting per ams-4218-T6, effectivity 5c 0001 9999, nha 16H1900-1
01-172-4411
Structural Component Air Support
Used on acft model b-1b. made from steel hand forging 300m per mil-s-8844. class 3; stock size 13.350 in. lg, 10.800 in. w, 6.570 in. thk; heat treated to 280-300 kips per ST0111LA0007; nha L3004050
01-172-4412
Structural Component Air Support
Used on acft model b-1b. c/o 2 fitting assemblies, 1 tube, 2 washers, 2 nuts; functional length 50.850-51.350 in., fitting hole center to tube end distance 3.930-4.170 in.; nha L3004004
01-172-4413
Structural Component Air Support
Used on acft model b-1b. cmachined steel bar 4340 per mil-s-5000; heat treated to 160-180 ksi per STO111LA0005; stock size 5.800 in. lg, 5.000 in. w, 3.500 in. thk; c/o 1 -003 fitting, 2 LD131-0028-1818 bushing; nha L3004050
01-172-4837
Structural Aircraft Plate
Doubler 14
01-172-4839
Aircraft Fairing
5.500" overall length 5.850" overall width eff 5c 0001 9999; nha 16E3147-1
01-172-4842
Structural Component Air Support
Used on acft model kc-135. al alloy extrusion 7075-T6511 per qq-a-200/11; heat treated per BAC5602; finish f-2.16; 2.000 in. lg, 2.000 in. w; s shaped cross section; 2 0.128 in. dia holes thru upper section, 0.300 in. from top, 0.440 in. in from each side; 2 pilot holes in lower section for 5/32 or 3/16 in. fasteners 0.440 in in from sides, 0.300 in. from bottom
01-172-4844
Structural Aircraft Panel
Nha 16M030-5; eff 0001-9999
01-172-4845
Structural Aircraft Panel
19.500" overall length 12.500" overall width same as -5 except replace -21 with -27; 5c 0001 9999; nha 16F4190-1; effon 4g, 4h, 4j, 4k, 5a, 5b, 5c
01-172-4994
Structural Component Air Support
Used on ah64 series helicopter.
01-172-5273
Access Aircraft Door
01-172-6652
Access Aircraft Door
Used on acft model b-1b. 2 corners opposite hinge are rounded; opposite p/n -002; nha L3011110
01-172-6803
Structural Aircraft Plate
Used on f-4 acft. used on engine air duct
01-172-6804
Structural Aircraft Plate
Used on acft model c-135. titanium compure 70 sheet per mil-t-9046, type i, comp b annealed; finish f-10.10; 4.500 in. lg, 2.300 in. w, 0.050 in. thk
01-172-6807
Structural Component Air Support
Used on acft model kc-135. al clad sheet 2024-0 per qq-a-362, 0 temp; heat treated to cond T4; finish f-2.115; 16.800 in. o/a lg, 10.000in. o/a w, 0.050 in. thk; contains 4 0.750 in. dia holes, 8 0.250 in. dia holes
01-172-6808
Structural Component Air Support
Used on acft model kc-135. al alloy clad sheet 2024-0 per qq-a-362, 0 temp; heat treated to cond T4; finish f-2.115; 8.100 in. o/a lg, 3.500 in. o/a w, 0.050 in. thk; opposite p/n -2; nha 65-19980
01-172-6809
Structural Component Air Support
Used on acft model b-1b. fitting 4340 steel bar per mil-s-5000; c/o 1 -004 fitting
01-172-6822
Aircraft Former
8.200" overall length 2.200" overall width 0.032" material thickness
01-172-6823
Aircraft Former
12.000" overall length 3.200" overall width 0.050" material thickness
01-172-6831
Aircraft Skin
Located fs 341.8 to 373.8; c/o skin, nut; 2024 alum alloy per qq-a-250/4-T62; finish A703; eff 5c on, 5d, 5c 0001 9999; nha 16B5314-803
01-172-7935
Structural Component Air Support
Used on ah64 series helicopter.
01-172-8202
Access Aircraft Door
01-172-8212
Aircraft Pylon
01-172-8676
Structural Component Air Support
Used on oh-58d aircraft. 10.910" overall length 6.700" overall width 0.032" material thickness lacquer surface treated
