01-171-2671
Structural Aircraft Plate
Used on acft model kc-135. al alloy plate 2024-T3 per qq-a-250/5; 2.100 in. lg, 2.100 in. w, 0.063 in. thk; 4 concave corners 0.530 in. radius; 1 0.218-0.219 in. dia hole centered 1.050 in. in from top
01-171-2672
Aircraft Fairing
01-171-2675
Structural Component Air Support
Used on acft model kc-135. al alloy extr 2024-T4 per qq-a-267, T4 temper; finish f-2.30; bac stock AND10134-1001 by 11.300 in. lg; nha 5-84012-2; opposite p/n -301
01-171-2676
Structural Component Air Support
Used on acft model kc-135. al alloy extr 2024-T4 per qq-a-267, T4 temper; finish f-2.30; bac stock AND10134-1001 by 11.200 in. lg, nha 5-84012-2; opposite p/n -303
01-171-2677
Structural Component Air Support
Used on acft model b-1b. made from 2763499-101 casting; 18.400 in. functional lg, 2.000 in. w at center hole, tappered to 1.270 in. w at both ends, 3.070 in. o/a h; 1st arm end slot 0.260 in. w, 2 in-line holes 0.250 in. dia, 10.300 in. functional arm lg; 2nd arm end slot 0.205 in. w, 2 in-line holes 0.500 in. dia, 8.100 in. functional arm lg; center hole (fulcrum) 0.323 in. dia; nha 2761046
01-171-2709
Aircraft Skin
Used on F-15. 11.000" overall length 9.000" overall width
01-171-2710
Aircraft Skin
Used on F-15. 36.000" overall length 33.000" overall width
01-171-2711
Aircraft Skin
Used on F-15. 36.000" overall length 33.000" overall width
01-171-3038
Structural Aircraft Panel
Used on kc-135 aircraft.
01-171-3039
Structural Aircraft Panel
Used on acft model kc-135.
01-171-3040
Structural Aircraft Panel
Used on acft model kc-135.
01-171-3041
Structural Aircraft Panel
Used on kc-135 aircraft.
01-171-3042
Structural Aircraft Panel
Used on kc-135 aircraft.
01-171-3044
Structural Component Air Support
01-171-3045
Structural Component Air Support
01-171-3051
Aircraft Former
01-171-3052
Aircraft Former
01-171-3968
Access Aircraft Cover
01-171-4097
Attachment Molded Tank Flange
0.257" hole diameter
01-171-5835
Access Cover
Used on aircraft model f-18.
01-171-5836
Access Cover
Used on aircraft model f-18.
01-171-5841
Attachment Molded Tank Flange
01-171-5842
Attachment Molded Tank Flange
Flange
01-171-5843
Attachment Molded Tank Flange
01-171-6466
Fuselage Aircraft Fairing
01-171-7263
Aircraft Fairing
Nha 35-35387-54, -55
01-171-7265
Structural Component Air Support
Used on moving island nose door,landing edge c-5a acft. 8.000" overall length 3.000" overall width 0.080" material thickness
01-171-9120
Vertical Stabilizer
Used on ch-47d,cargo hel.
01-171-9263
Access Aircraft Cover
01-171-9264
Access Aircraft Door
01-172-0220
Structural Component Air Support
Used on c-5b acft. matl al alloy, qq-a-250/12, 7075-T651; matl size 2.000 by 5.000 by 5.000 in. lg; opposite to p/n 4F53460-102c; used as fitting-winch support, aft ramp
01-172-0221
Structural Component Air Fitting
5.000" overall length 5.000" overall width 2.000 " material thickness opposite -101c
01-172-0223
Structural Component Air Support
Used on acft model f-16a/b. 5corrosion resistant steel bar PH13-8mo per ams-5629; heat treated to H1000 condition per fps-3014; finish S457; base 2.320 in.lg, 2.000 in.w, .135 in.thk tappered .021 in., 4 slots in base .468 in.lg, .198 in.w; forked projection perpendicular to base 2.345 in.lg, 2.220 in.between fork centers, end radius .38 in., center radius .73 in., .250 in.thk at base, .200 in.thk at ends; serial no.effectivity 61 0001 9999; nha 16W020-845; opposite p/n -10; functional description:used as le flap actuator attachment bracket;
01-172-0225
Structural Component Air Bracket
01-172-0226
Structural Component Air Bracket
01-172-0227
Structural Component Air Bracket
01-172-0228
Structural Component Air Bracket
3.000" overall length 3.000" overall width
01-172-0229
Structural Component Air Support
Used on f-16a/b usaf aircraft. bbracket; stock size-2X3X3 in.; material-aluminum alloy per fms-3002-T851, finish-A466; nha 16W020-836; nhra 16W020-844, 16W030-4; eff on-61 0001 0027, 61 0125 0125, 61 0128 0128, 61 0130 0130, 61 0132 0132
01-172-0230
Structural Component Air Support
3.000" overall length 3.000" overall width 2.000" material thickness eff on 61 0001 0027
01-172-0231
Structural Component Air Support
3.000" overall length 3.000" overall width 2.000" material thickness nha 16W020-836; eff on 61 0001 0027
01-172-0232
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, 1.580 in. lg, 1.650 in. w, 0.410 in. thk at base, 0.110 in. thk slot centered in thk 1.090 in. deep; serial no. effectivity 61 0007 0261; nha 16W020-846; opposite p/n -7
01-172-0233
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., 0.920 in. w., 0.162 in. thk.; contains 2 slots, 0.530 in.; forked projection perpendicular to base, 1.640 in. l., 1.650 in. w., 0.410 in. thk at base, 0.110 in. thk slot centered, 1.150 in. deep; nha-16W020-845; opp -10; eff on-61 0028 0124, 61 0126 0127, 61 0129 0129, 61 0131 0131, 61 0133 0261
01-172-0234
Structural Component Air Support
Used on acft model f-16a/b. steel ams-5343; made from -15 casting; finish S409; 2.760 in. o/a lg at base, 1.300 in. h at base, 1.612 in. h at end of fork, 1.011 in. o/a w, base thk 0.150; 0.110 in. thk slot in fork; 0.280 in. r. hole centered through fork; nha 16W020-835; opp--18; eff on-61 0007 0027
01-172-0235
Structural Component Air Support
Used on acft model f-16a/b. steel ams-5243; made from -16 casting; finish-S409; 2.760 in. o/a lg. at base, 1.300 in. h. at base, 1.612 in. h. at end of fork, 1.011 in. o/a w., base thk o.150; 0.110 in. thk slot in fork; 0.280 in. r hole centered through fork; nha 16W020-836; opposite -17; eff on-61 0007 0027
01-172-0236
Structural Component Air Support
Used on acft model f-16a/b. tsteel ams-5343; made from -19 casting; finish S409; 2.760 in. lg at base, 1.300 in. h at base; 0.951 in. o/a w, 1.620 in. h at end of attachment projection; 2-0.530 in. lg. slots in base; nha 16W020-835; opposite -22; eff on-61 0007 0027
01-172-0237
Structural Component Air Support
Used on acft model f-16a/b. steel ams-5343; made from -20 casting; finish S409; 2.760 in. lg at base, 1.300 in. h at base; 0.951 in. o/a w. 1.620 in. h at h at end of attachment projection; 2-0.530 in. lg slots in base; nha 16W020-835; opposite p/n -21; eff ON61 0007 0027
01-172-0238
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, 2.011 in. o/a lg; 2 0.530 in. slots in base; effective on 28 thru 116 type 6.1
01-172-0239
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, 2.011 in. o/a lg; 2 0.530 in. slots in base; serial no. effectivity 61 0001 0261; nha 16W020-846; opposite p/n -7
01-172-0240
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 16W020-845; opposite p/n -10
