01-047-6531
Structural Component Air Fitting
01-047-6533
Structural Component Air Fitting
01-047-6536
Access Aircraft Door
Used on e-3a acft. vert. tail access
01-047-6560
Structural Component Air Fitting
Bulkhead penetration dual detonation transfer assembly
01-047-6561
Structural Component Air Fitting
Bulkhead penetration dual detonation transfer assembly
01-047-6568
Access Aircraft Door
Used on f-16a/b aircraft. c/o-plate, latch, cover, 2 buttons for latching
01-047-6570
Structural Component Air Fitting
1.900" overall length 1.250" overall width 0.180 " material thickness hinge bolt keeper
01-047-6613
Longeron
Used on acft model f-16b usaf. effective on 0003 - on; nha 16B2931-801;
01-047-7142
Structural Component Air Fitting
01-047-7165
Aircraft Door
01-047-7330
Structural Aircraft Plate
Used on acft model f-16. 160 in. dia, 5 in. hgt, 5 in. lg, stock size, alum. alloy per qq-a-25084-T81
01-047-7337
Longeron
Used on acft model f-16. 16.000" overall length 5.000" overall width 0.080" material thickness
01-047-7338
Longeron
Used on acft model f-16. 16.000" overall length 5.000" overall width 0.080" material thickness
01-047-7339
Longeron
Used on acft model f-16. 16.000" overall length 5.000" overall width 0.080" material thickness
01-047-7340
Longeron
Used on acft model f-16. alum alloy per qq-a-250/4-T6, 0.100 in.thick, 6.00 in.wide, 62.00 in.length, located from fs 279.66 to 341.36;
01-047-7341
Longeron
Used on acft model f-16. alum alloy, per qq-a-250/4-T62, 0.100 in.thick, 6.00 in.wide, 62.00 in.length, located from fs 279.66 to 341.36;
01-047-7344
Aircraft Skin
Used on acft model f-16. consists of 1 ea. skin p/n C061-02-11, 38 ea. nut p/n C061-02, 135 ea. nut C061-048
01-047-8197
Aircraft Bulkhead
Main landing gear well, fwd
01-047-8199
Aircraft Bulkhead
Used on acft model f-16. 34.000" overall length 32.000" overall width 3.500" material thickness
01-047-8204
Former
Used on acft model f-16a/b usaf. located at lower fuselage station 344.24; superseded p/n 16B5802-17 ow per ecn 54896
01-047-8206
Structural Component Air Support
Used on acft model f-16a/b usaf. alum.alloy 7075-T73, per qq-a-367, comp 7075, located at fuselage station 344.24; eff 0007 on; nha 16B560-1
01-047-8218
Structural Component Air Support
Used on acft model f-16.
01-047-8221
Aircraft Skin
Used on acft model f-16. 65.000" overall length 19.000" overall width located from fuselage station 279.00 to fs 344.00
01-047-9039
Access Aircraft Door
Used on F-16. rh ammo loading access
01-047-9042
Structural Component Air Fitting
Mlg drag support
01-047-9043
Structural Component Air Fitting
Mlg drag support
01-047-9057
Structural Aircraft Panel
C/o 1 fiberglass assy, 1 seal, 1 retainer
01-047-9058
Structural Aircraft Panel
C/o 1 fiberglass assy, 1 seal, 1 retainer
01-047-9073
Structural Component Air Support
Used on acft model f-16. alum.alloy 7075, per qq-a-367, comp 7075-T73, located at external stores station 286.60
01-047-9074
Structural Component Air Support
Used on acft model f-16. alum.alloy, per qq-a-367, comp 7075-T73, located at external stores station 286.60;
01-047-9075
Structural Component Air Support
Used on acft model f-16. located at external stores station 333.80
01-047-9076
Structural Component Air Support
Used on acft model f-16. located at external stores station 333.80
01-047-9082
Longeron
Used on acft model f-16. alum alloy, per qq-a-250/4-T62, 0.080 in.thick, 6.00 in.wide, 24.00 in.length, located from fs 279 to fs 309;
01-047-9083
Longeron
Used on acft model f-16. alum alloy, per qq-a-250/4-T62, 0.080 in.thk, 6.00 in.wide, 24.00 in.length, located from fs 279 to 309;
01-047-9084
Longeron
Used on acft model f-16. alum alloy, per qq-a-250/4-T62, 0.080 in.thk, 6.00 in.wide, 8.00 in.length, located from fuselage station 279 to fs 309;
01-047-9085
Longeron
Used on acft model f-16. alum alloy, per qq-a-250/4-T62, 0.080 in.thk, 6.00 in.wide, 8.00 in.length, located from fuselage station 279 to 309;
01-047-9086
Longeron
Used on acft f16. 32.000" overall length 6.000" overall width 0.071" material thickness
01-047-9087
Longeron
Used on acft f16. 32.000" overall length 6.000" overall width 0.071" material thickness
01-047-9088
Aircraft Skin
Nha 16B5611-1; to. 1f-16a-4-51
01-047-9089
Aircraft Skin
63.000" overall length 55.000" overall width eff 0001-0n; nha 16B5611-1
01-047-9090
Aircraft Skin
35.000" overall length 20.000" overall width
01-047-9091
Aircraft Skin
Used on acft f16. 35.000" overall length 20.000" overall width
01-047-9092
Aircraft Skin
Used on acft model f-16a/b usaf. 38.000" overall length 20.000" overall width eff 61 00019999; nha 16B5612-1; superseded p/n 16B5602-9 ow per ecn 87094
01-047-9603
Former
Used on f-16a/b aircraft. 55.000" overall length 26.000" overall width 1.750" material thickness used as bulkhead on lower fuselage station 417.40
01-047-9604
Structural Aircraft Plate
15.000" overall length 5.000" overall width 0.020" material thickness eff 6h 0001 0055; nha 16B6312-803; not interchangeable with supercedingpn -69
01-047-9605
Structural Aircraft Plate
16.000" overall length 5.000" overall width 0.020" material thickness superceded pn 16B6312-25; nha 16B6312-1, 0007-on
01-047-9611
Structural Aircraft Plate
15.000" overall length extension, internal heat shield
01-047-9612
Structural Aircraft Plate
39.000" overall length 34.000" overall width 0.020" material thickness superceded by pn 16B6312-63; nha 16B6312-803; 0009-0021
01-047-9613
Structural Aircraft Plate
Used on f-16a/b aircraft. used on internal heat shield installation fuselage station 446.10 to 479.55, dimensions-39.00 in. lg, 34.00 in. w, 0.020 in. thk, supercedes p/n 16B6312-28, nha 16B6312-803, 0009-on
01-047-9614
Structural Aircraft Plate
Used on f-16a/b aircraft. used as doubler on internal heat shield, fuselage station 446.10 to 479.55; dimensions-4.00 in. lg, 1.00 in. w, 0.025 in. thk, nha 16B6312-803, 0001-on
