01-101-1906
Structural Aircraft Panel
Used on h-3 aircraft.
01-101-1907
Structural Aircraft Panel
Used on h-3 aircraft.
01-101-2085
Structural Component Air Bracket
2.800" overall length
01-101-2086
Structural Component Aircraf Web
20.500" overall length 4.500" overall width 0.025" material thickness ht T4; finish f-2.115; 0 temper
01-101-2087
Structural Component Aircraf Web
11.000" overall length 4.200" overall width 0.025" material thickness 0 temper; ht T4; finish f-2.115
01-101-2088
Airframe Aircraft Rail
Used on acft c135. track installation, windshield, sliding
01-101-2092
Structural Component Air Bracket
25.500" overall length heat treat T42; finish f-2.30
01-101-2109
Structural Aircraft Panel
Used on acft model f111. aluminum alloy per qq-a-250/5, 13.000 in. lg, 5.000 in. w, 0.063 in. thk
01-101-2110
Structural Aircraft Panel
Used on F-111. 47.000" overall length 4.000" overall width
01-101-2111
Structural Aircraft Panel
Used on F-111. 44.000" overall length 5.000" overall width
01-101-3115
Structural Component Air Bracket
01-101-3647
Structural Component Air Bracket
3.000" overall length 3.000" overall width 0.050" material thickness
01-101-3649
Structural Component Air Support
24.500" overall length 1.800" overall width 0.015" material thickness inconel sheet per ANS5542d, f-1 finish; silver plate per BAC5715
01-101-3650
Structural Component Air Support
24.500" overall length 1.800" overall width 0.015" material thickness inconel per AMSS5420; heat treat 1625 degree; f-1 finish silver plate
01-101-3655
Structural Component Aircraf Web
32.500" overall length 16.000" overall width 0.032" material thickness 0 temper; ht T4; finish f-2.115
01-101-3656
Structural Component Aircraf Web
20.000" overall length 16.000" overall width 0.032" material thickness 0 temper; ht T4; finish f-2.115
01-101-3685
Aircraft Frame
C/o modified frame assy, former
01-101-3706
Aircraft Fairing
Superseded p/n 16T7260-109, i/c code ow, effectivity 41 0001 9999, ecn 97657, nha spares only
01-101-3708
Structural Component Air Support
Eff 0001; nha 16U10074-1
01-101-3717
Aircraft Skin
Used on B-52. 26.000" overall length 13.000" overall width 0 temper; finish F2.130
01-101-3718
Aircraft Skin
Used on B-52. 51.500" overall length 13.000" overall width heat treat T4; finish F2.130
01-101-4072
Fuel Aircraft Tank
01-101-4965
Acoustical Aircraft Insulation
Used on uh-60 blackhawk helicopter, 1520-01-035-0266. soundproofing instl - sta 265.5 - sta 295
01-101-5298
Aircraft Door
C/o 6 bracket instl, 9 rivets, 25pin, 9 coating, 1 stud, 1 bracket
01-101-8883
Airfoil Rib
Used on F-15. 7.500" overall length 5.000" overall width 0.050" material thickness cond 0 alclad
01-101-8884
Airfoil Rib
Used on F-15. 7.500" overall length 5.000" overall width 0.050" material thickness
01-101-8885
Aircraft Skin
Used on F-15. 24.500" overall length 18.750" overall width
01-101-8886
Aircraft Skin
Used on F-15. 24.500" overall length 18.750" overall width
01-101-9715
Structural Component Air Support
Used on uh-60a helicopter. aluminum alloy, qq-a-250-18
01-101-9724
Structural Component Air Bracket
Used on uh-60 blackhawk helicopter.
01-101-9731
Structural Component Air Fitting
Used on uh-60l helicopter. 2.630" overall width 0.100 " material thickness u/o support instl vibration absorber forward lh 70219-02109-013. includes 2 bushings
01-101-9843
Fuselage Aircraft Fairing
01-101-9844
Fuselage Aircraft Fairing
01-101-9849
Aircraft Window Panel
Used on uh-60black hawk helicopter.
01-101-9851
Aircraft Window Panel
01-102-0536
Aircraft Door
01-102-0588
Structural Aircraft Plate
C/oplate p/n 12E45215-19, plate p/n 12E45215-15, plate p/n 12E45215-13
01-102-0590
Structural Component Air Support
Used on acft model f4.
01-102-0598
Airfoil Rib
C/o 3 channel, 1 clip, 2 rib, 1 doubler, 1 angle, 1 support, 2 plate, 2fitting, misc hardware
01-102-1167
Structural Component Air Support
3.000" overall length 2.210" overall width c/o:support, bracket, rivets; 0.620 in. dia hole; 2 holes 0.155 in dia; 4 holes 0.250 in dia
01-102-1168
Structural Component Air Support
Used on c-141 acft. matl al alloy, 2024.0 T6; opposite to p/n 3W22000-295; used as a pan onleading edge assy
01-102-2250
Structural Component Air Fitting
2.870" overall length 0.625" overall width
01-102-2251
Structural Component Air Fitting
2.870" overall length 0.375" overall width
01-102-2267
Structural Component Air Support
Used on bqm-34a acft. matl st, mil-s-5059, cond a, type 302; 2.800 in. w with 0.250 radius in 2 places; 2.250 in. lg; 2 holes 0.217 in. dia; used on engine shroud aft
01-102-2415
Structural Component Air Support
Used on uh-60 helicopter. aluminum alloy, qq-a-250-13, composition 7075-0
01-102-2953
Structural Component Air Bracket
5.040" overall length 3.900" overall width 0.050" material thickness
01-102-3015
Aircraft Beam
C/o 4 channel, 4 bracket, 2 cap, misc hardware
01-102-3038
Structural Aircraft Plate
17.600" overall length 7.750" overall width 0.040" material thickness cover 1 ea p/N53-64039-4spacer 1 ea p/n 53-64039-5, 0.063 in.thk, 0.820in. w, 3.000 in.lg, right hand
01-102-3774
Aircraft Door
01-102-3781
Aircraft Door
C/o skin, doubler, a/r sealant, rivets
