01-113-9468
Structural Aircraft Plate
Used on c-5a acft. 5.380" overall length 4.780" overall width
01-113-9469
Structural Component Air Support
Used on c-5a acft. matl al alloy, qq-a-250/12, 7075-T651; used on front inboard flap no. 1
01-113-9470
Structural Component Air Support
Used on c-5a acft. matl al alloy, qq-a-250/12, 7075-T651; opposite to p/n 4J41174-101a; used on front inboard flap no. 1
01-113-9471
Structural Component Air Support
Used on c-5a acft. matl al alloy, qq-a-250/12, 7075-T651; used on inboard, flap no 1
01-113-9472
Structural Component Air Support
Used on c-5a acft. matl al; 16.050 in. lg; 6.000 in. w; four holes, 0.376 in. dia; 0.188 in. dia pin rivets, 41 places; used as shim, rib closure inboard flap 2
01-113-9473
Structural Component Air Fitting
Opposite -104c
01-113-9475
Structural Component Air Support
Used on acft model f4.
01-113-9483
Aircraft Window Panel
01-113-9484
Canopy Forward Transparency
Transparency, canopy, fwd
01-113-9485
Canopy Transparency
Fwd clear transparency
01-113-9486
Canopy Aft Transparency
Transparency, canopy, aft
01-113-9489
Aircraft Door
Used on C-5. c/olongeron 2; frame installation 9; panel assy 3; torque box installation; ramp installation; miscellaneous hardware
01-114-0333
Structural Component Air Bracket
5.500" overall length 3.250" overall width
01-114-0375
Aircraft Beam
Strake fuel tank beam
01-114-0379
Access Aircraft Door
Used on f-16a/b usaf aircraft. on elec access, nacelle, fs 224-236; nha 16B410-99; eff on 61 0262 9999
01-114-0395
Structural Component Air Support
C/o: bracket (16P286-73) , bracket (16P286-81) , rivets (as required)
01-114-0396
Structural Component Air Support
11.000" overall length 7.000" overall width 4.000" material thickness matl: steel per FMS1111
01-114-0398
Structural Component Air Support
Used on acft model f-16.
01-114-0402
Aircraft Skin
Used on F-16. 27.000" overall length 13.000" overall width
01-114-1755
Aircraft Leading Edge
01-114-2043
Aircraft Windshield Panel
84.000" overall length 60.000" overall width part of 3150220-601-107 canopy assy
01-114-2135
Structural Aircraft Panel
Used on uh-60a helicopter.
01-114-2138
Structural Component Air Fitting
Used on uh-60l helicopter. 4.135" overall width 0.100 " material thickness u/o support instl vibration absorber forward rh 70219-02109-012. includes 2 bushings
01-114-3499
Structural Component Air Bracket
2.250" overall length 1.250" overall width
01-114-3505
Structural Component Air Bracket
01-114-3530
Aircraft Fairing
3.800" overall length 3.300" overall width 0.020" material thickness
01-114-3531
Aircraft Fairing
Used on A-10. splice, wing center
01-114-3532
Aircraft Fairing
Used on A-10. splice, wing center
01-114-3533
Structural Component Air Support
Used on acft model f4e. steel 301 1/2 hard per mil-s-5059, 0.045 in.thk, 2.340 in.w, 4.280 in.lg, right hand
01-114-4621
Aircraft Door
01-114-4645
Aircraft Latch Assembly
Used on f-15a acft. ams 6411; 3.250 in. lg; 2.250 in. wd; 0.500 in. thk
01-114-4697
Access Aircraft Door
Used on F-16. lh main landing gear
01-114-4703
Radome
Used on F-16. 73.500" overall length nose radome
01-114-4711
Aircraft Door
C/o 1 door assy, misc hardware
01-114-4717
Aircraft Former
Used on F-15.
01-114-4727
Aircraft Former
9.000" overall length 5.410" overall width 0.080" material thickness function-spar to rib-intermedeate, lower forward
01-114-4745
Structural Component Air Support
Used on acft model f-16. c/o flange p/n 39219-7, bolting ring p/n 39214-1, bolting ring 39090-1
01-114-4746
Structural Component Air Support
Used on acft model f-16. c/o flange p/n 39220-7, bolt ring p/n 39226-1, bolting ring p/n 39217-1
01-114-4747
Structural Component Air Support
Used on acft model f-16. c/o flange p/n 39221-7, bolt ring p/n 39224-1, bolting ring p/n 39216-1
01-114-4748
Structural Component Air Support
3.000" overall length 3.000" overall width 1.015" material thickness u/a: arm; matl:1.015in dia hole; temper T651; alum alloy, bare
01-114-4749
Structural Component Air Support
Used on acft model f-16. used on inboard console, right hand; eff 61 0262 9999; nha 16F0145-817; superseded 16F0143-805 ni
01-114-4750
Structural Component Air Support
Used on f-15a/tf-15a acft. function-engine removal
01-114-4765
Aircraft Skin
57.030" overall length 5.750" overall width c/0 bolt 132, bolt 95, rivet 3, strap 1, washer 65; cond 1/2 hard
01-114-4766
Aircraft Skin
27.200" overall length 11.500" overall width
01-114-4767
Aircraft Skin
27.200" overall length 11.500" overall width
01-114-4768
Aircraft Skin
57.030" overall length 5.750" overall width cond 1/2 hard; c/0 bolt 132, jo bbolt 95, washer 66, rivet 3, strap 1
01-114-4769
Aircraft Skin
36.000" overall length 33.000" overall width
01-114-4770
Aircraft Spar
01-114-4771
Vertical Stabilizer
Nha: 16T7101-1 eff 61 0293 9999
01-114-6009
Structural Component Air Support
Used on c-5 acft. MA7l al alloy, qq-a-367; 11.319 in. lg; 2.900 in. n; 1.251 in. dia two holes, chamfer 0.015 by 45 deg outer faces; used as fitting hinge, no 6 aileron station 264.945
