01-046-5686
Structural Aircraft Panel
01-046-5694
Structural Component Air Bracket
01-046-5713
Aircraft Fairing
01-046-5736
Structural Aircraft Panel
Effective on 0004 - on; nha 16B111-61
01-046-5743
Longeron
Used on acft model f-4. aluminum alloy, qq-a-200/13 cond T651; 3
01-046-5744
Aircraft Pylon
01-046-5746
Aircraft Skin
Used on acft model f-16a/b usaf. eff 0004 on; NHA16B1920-1
01-046-5748
Aircraft Skin
Used on acft f16. 100.000" overall length 30.000" overall width
01-046-7557
Structural Component Air Support
1.8000" overall length 1.500" overall width
01-046-7595
Structural Component Air Fitting
Fuel pylon attachment ball
01-046-7685
Structural Component Air Support
Used on model no. f-16 acft. steel, mil-s-6721, 3.000 in.lg, 3.000 in.w, 0.050 in.thk;
01-046-7686
Structural Component Air Support
C/o: 1 rough casting; eff 0012 & on; superseded 16F0144-21 ow; nha: 16F0146-1
01-046-7698
Longeron
Used on aircraft model t-39. located at fuselage station 357 to 457.406, aluminum alloy 7178-0;
01-046-7699
Longeron
Used on aircraft model t-39. aluminum alloy 7178-0, located at fuselage station 357 to ctd station 457.406;
01-046-7701
Aircraft Skin
Used on F-16. 39.000" overall length 23.000" overall width
01-046-7702
Aircraft Skin
Used on F-16.
01-046-7703
Aircraft Skin
Used on F-16.
01-046-7704
Aircraft Skin
Used on acft f16. 56.000" overall length 27.000" overall width
01-046-7705
Aircraft Skin
Used on acft f16. 56.000" overall length 27.000" overall width
01-046-8143
Access Aircraft Door
01-046-8258
Aircraft Leading Edge
Used on aircraft model a-7e.
01-046-8301
Bell Crank
0.193" bore diameter
01-046-8436
Structural Component Air Fitting
Wg to fuslg shear
01-046-8566
Structural Component Air Support
01-046-8586
Structural Component Air Bracket
5.300" overall length 1.000" overall width nlg steering input potentiometer arm
01-046-8589
Structural Component Air Bracket
Used on f-16 aircraft. 14.000" overall length 5.000" overall width 0.071" material thickness
01-046-8590
Structural Aircraft Panel
Used on F-16. c/o panel p/n 16F0195-7
01-046-8591
Structural Aircraft Panel
Used on F-16. c/o panel p/n 16F0195-8
01-046-8618
Structural Component Air Fitting
6.190" overall length
01-046-8637
Aircraft Wing Assembly
Wing box assembly
01-046-8638
Aircraft Wing Assembly
01-046-8690
Structural Aircraft Panel
20.000" overall length 9.000" overall width matl spec P5327-3; eff 0007 on; nha F0170-1
01-046-8691
Fuselage Aircraft Fairing
Used on acft model f-16.
01-046-8692
Fuselage Aircraft Fairing
Used on acft model f-16.
01-046-8693
Structural Component Air Support
Used on acft model f-16. alum.alloy, per qq-a-367, comp.7075, temp T73, located at fuselage station 267.4
01-046-8694
Structural Component Air Support
Used on acft model f-16. consists of support 1 ea.pn.16P103-7, nut 1 ea.pn.MS21061L4, nut 3 ea.pn.MS21075L4
01-046-8695
Structural Component Air Support
Used on aircraft model f-16. aluminum alloy qq-a-250/4-T81; , eff 0001 on; nha 16B4825-2
01-046-8720
Longeron
Used on acft model f-16a/b. matl qq-a-250/4-T67; 8.0 in.lg, 0.35 in.wd, 0.071 in.thk; nha 16B110-5; eff 0007 on; superseded p/n 16B1112-3 ni per ecn 39230;
01-046-8721
Longeron
Used on aircraft model t-39. 7178-T6 aluminum alloy formed to fuselage contour, fuselage station 357 to ctd station 457.406;
01-046-8722
Aircraft Skin
31.000" overall length 4.000" overall width eff 0001-on; nha pn 16B510-1
01-046-8723
Aircraft Skin
31.000" overall length 4.000" overall width nha 16B510-1; eff 0001-on
01-046-8724
Aircraft Skin
Used on F-16.
01-046-8725
Aircraft Skin
Used on F-16.
01-046-8726
Aircraft Skin
Eff 0004-on; nha pn 16B1323-1
01-046-8727
Aircraft Skin
Used on f-16a/b aircraft. 63.000" overall length 32.000" overall width inner skin; opp -19
01-046-8728
Aircraft Skin
67.000" overall length 32.000" overall width outer skin; opp -7; finish A464a
01-046-8729
Aircraft Skin
Used on F-16. 46.000" overall length 14.000" overall width
01-046-8730
Aircraft Skin
Used on F-16. eff 0008-on; nha 16B5311-5; superseded 16B5301-3 ni
01-046-8731
Aircraft Skin
Used on acft f16.
