01-074-7724
Aircraft Door
Eff on-61 0013 on for netherlands a/b, 0028 on for a/b usaf; c/o door assy -37, jumper assy, hing assy, shim, plate serrated, hing half assy; nha 16L004-3
01-074-7986
Aircraft Stiffener
01-074-8021
Aircraft Skin
Used on C-141.
01-074-9226
Structural Component Aircraf Web
10.300" overall length 11.700" overall width 0.025" material thickness finish f-10.10
01-074-9254
Aircraft Rudder
01-074-9265
Bleed Air Duct Assembly
01-074-9286
Aircraft Deceleron
Function/fit
01-074-9329
Aircraft Skin
Used on acft c135. access door, station 620 to 670, lefthand only
01-074-9897
Aircraft Skin
Used on aircraft model f-14a. aluminum clad alloy
01-074-9898
Aircraft Skin
Used on aircraft model f-14a. aluminum clad alloy
01-074-9899
Aircraft Skin
Used on aircraft model f-14a. aluminum clad alloy
01-074-9900
Aircraft Skin
Aluminum alloy, AMS4077 composition 2024-T81, anodized, mil-a-8625 type 2 class 1
01-075-0490
Aircraft Former
Superseding p/n 16B5802-15 ow per 0033 on; nha 16B5250-815
01-075-0541
Aircraft Beam
01-075-0621
Structural Component Air Support
01-075-1701
Structural Aircraft Panel
01-075-1702
Structural Aircraft Panel
01-075-1703
Structural Aircraft Panel
01-075-1704
Structural Aircraft Panel
01-075-1705
Structural Aircraft Panel
01-075-1728
Structural Aircraft Plate
Used on acft model f4j. alum alloy 7178-T6 per qq-a-250/14 cond T6, stock size 0.080 in.thick, 3.35 in.wide, 24.25 in.length, left hand
01-075-1729
Structural Aircraft Plate
Used on acft model f4j. alum alloy 7178-T6 per qq-a-250/14 cond T6, stock size 0.080 in.thick, 3.35 in.wide, 24.25 in.length, right hand
01-075-1730
Structural Aircraft Plate
23.000" overall length 3.000" overall width 0.312" material thickness lefthand superseded p/n 16B1833-9ow per ecn 54625; naha 16B1931-6; eff on 0035-on
01-075-1731
Structural Aircraft Plate
Used on acft model f-16a/b usaf. alum alloy per qq-a-250/4-T62, stock size 0.312 in.thick, 3.00 in.wide, 23.00 in.length, right hand, located from fuselage station 88.0 to fs 110.50; superseded p/n 16B1833-10 ow per ecn 54625; eff on 0035-on; nha 16B1931-6
01-075-1733
Structural Component Air Support
Used on acft model f-16a/b usaf. al alloy per ams 4218-T6; 5.60 in. lg, 2.20 in. w, 5.45 in. h; used on nose radome; effective on 0117 - on; nha 16B1210-809
01-075-2644
Structural Aircraft Panel
Used on ah-1 acft.
01-075-2646
Structural Aircraft Panel
Skin, glass fabric, 299-947-076, type c, fscm 97499; cores, honeycomb, 299-947-059, type 4
01-075-2647
Structural Aircraft Panel
Used on ah-1f acft.
01-075-2648
Structural Aircraft Panel
Cores, honeycomb, aluminum alloy, 299-947-059 type 4, fscm 97499; skins, aluminum alloy, qq-a-250/12
01-075-3094
Access Aircraft Door
Used on aircraft model a-10. c/o 2 stiffener, 1 clip, nut plate, rivets a/r
01-075-3102
Structural Component Air Support
01-075-3149
Structural Aircraft Plate
Used on acft model f4.
01-075-3507
Structural Aircraft Panel
01-075-3508
Structural Aircraft Panel
01-075-3509
Structural Aircraft Panel
01-075-3510
Structural Aircraft Panel
01-075-3511
Structural Aircraft Panel
01-075-3512
Structural Aircraft Panel
01-075-3513
Structural Aircraft Panel
01-075-3514
Structural Aircraft Panel
01-075-3515
Structural Aircraft Panel
01-075-3596
Structural Component Air Fitting
Flaperon outbd hinge
01-075-3656
Structural Component Air Support
Used on acft model f4c/d. c/o support mach 1 ea p/n 32-31656-3, pin 1 ea p/n AM253-2-100
01-075-4752
Aircraft Bulkhead
01-075-4784
Aircraft Fairing
01-075-4800
Structural Aircraft Plate
3.000" overall length 3.000" overall width 0.025" material thickness cadmium plated tools not to be used on this item; TYPE1, comp b, cond a; nha 16B6312-803; eff on-0011 0034
01-075-4803
Aircraft Skin
Used on acft model f-16a/b. 60.000" overall length 23.000" overall width eff 0007 0027; nah 16L011-813
01-075-5092
Aircraft Door
Used on T-38. consists of p/n 6-24306-1 flap, p/n 6-40461-1 bracket, p/n 6-40464-1 crank, p/n 6-40465-1 roller, p/n 6-40463-1 torsion bar, p/n 6-00526-51 marking instl, p/n MS27253F1 nameplate, and assorted attaching hardware
