01-202-9147
Structural Component Air Support
Used on acft model kc-135. opposite p/n -505
01-202-9148
Structural Component Air Support
Used on acft model kc-135. opposite p/n -508
01-202-9151
Structural Aircraft Panel
01-202-9152
Structural Aircraft Panel
Used on acft model kc-135. consists of 1 insulation core, 1 lwr skin, 1 upr skin, 2 foil washer, 1 upper skin assy, 20 spacer grommet; nha 65C18764
01-202-9215
Access Aircraft Door
01-202-9216
Access Aircraft Door
Used on aircraft model 4-14a.
01-203-0960
Structural Aircraft Plate
5.180" overall length 3.660" overall width 0.078" material thickness
01-203-1565
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket assembly
01-203-1721
Access Aircraft Cover
Used on b-1b aircraft. 0.256" hole diameter nuclear hardness critical item; holes counterbored 0.126 by 0.415 in. dia; nha L3010827; used as fuel tank access door
01-203-1723
Access Aircraft Door
Used on acft model b-1b. used as envirmental control system ground air service door; nha L3010790-101
01-203-1882
Structural Aircraft Plate
12.000" overall length 8.000" overall width 0.020" material thickness
01-203-1885
Structural Component Air Support
Used on acft model b-1b. 6al-4v titanium extrusion annealed LS043-1347 by 8.500 in. lg per mil-T81556, type iii, comp a; nha L3207040
01-203-1886
Structural Component Air Support
Used on kc-135 aircraft.
01-203-1887
Structural Component Air Support
Used on acft model b-1b. stainless steel, finish per qq-p-35; max length 20.08, min length 13.33; max load 1200 lbs
01-203-1888
Structural Component Air Support
Used on acft model b-1b. alum per mil-a-8625, cres per qq-p-35, steel per qq-p-416; max length 21.00 min length 12.50, stow length 12.87, weight cal 0.55 lb.
01-203-1889
Structural Component Air Support
Used on acft model b-1b. alum per mil-a-8625, cres per qq-p-35, steel per qq-p-416; max. length 29.00 min. length 16.75, stow length 16.90, weight cal 0.62 lb.
01-203-1890
Structural Component Air Support
Used on acft model b-1b. 6al-4v T1 die forging comp 6, cond a per mil-f-83142; nha L3207040
01-203-1891
Structural Component Air Support
Used on acft model b-1b. 6al-4v T1 die forging comp 6, cond a per mil-f-83142; nha L3207040
01-203-1892
Structural Component Air Support
Used on acft model b-1b. 6al-4v alloy plate T1, comp c, cond a, type iii per mil-t-9046; 15.00 in. long, 10.50 in. wide, 3.25 in. thick; nha L3226004; located at yn 247.000
01-203-1893
Structural Component Air Support
Used on acft model b1b. al aly 2024-T8511 per ST0170LB0052; shape LS043-1380 by 2.50 in. long; nha L3206249; located at yn 249.00
01-203-1895
Structural Component Air Support
Used on acft model a-10a. aluminum alloy forging per qq-a-367, 7075-T73
01-203-1899
Aircraft Former
9.440" overall length
01-203-1901
Airfoil Rib
10.500" overall length 7.900" overall width 0.032" material thickness
01-203-1902
Airfoil Rib
20.200" overall length 7.700" overall width 0.032" material thickness
01-203-1904
Aircraft Skin
69.000" overall length 22.000" overall width
01-203-1906
Horizontal Stabilizer
C/o hinge ay, panel ay, 2 angle, 4 pin hi-lok, 4 collar hi-lok, 6 plate nutss, rivets as required
01-203-1914
Thermal Special Purpo Insulation
Vc/o insulation blanket 1; support inboard door 1; clip 9; washer 2; nut 9; cement 1; vinyl tape 1; finish f-9.05; nha 458-53003; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical ass
01-203-1915
Thermal Special Purpo Insulation
7c/o insulation blanket 1; clip 16; fwd panel liner 1; fwd door support 1; washer 22; nut 16; cement 1; vinyl tape 1; finish f-9.05; nha 458-53004; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical assy
01-203-1916
Thermal Special Purpo Insulation
C/0 insulation blanket 1; clips 17; outboard panel liner 2; outboard panel support 1; washer 40; nut 17; cement 1; vinyl tape 1; finish f-9.05; nha 458-53001; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical assy
01-203-1917
Thermal Special Purpo Insulation
C/o insulation blanket 1; clips 18; outboard panel liner 3; outboard panel support 1; cement 1; washer 40; nut 18; vinyl tape 1; finish f-9.05; nha 458-53001; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical assy
01-203-1918
Thermal Special Purpo Insulation
7c/o insulation blanket 1; clip 9; top panel liner 2; top panel support 1; washer 10; nut 10; cement 1; vinyl tape 1; finish f-9.05; nha 458-53001; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical assy
01-203-1919
Thermal Special Purpo Insulation
9c/o insulation blanket 1; clip 12; washer 11; top panel liner 2; top panel support 1; nut 12; cement 1; vinyl tape 1; finish f-9.05; nha 458-530091; end item identification:aircraft, model kc-135; functional description:used as mod apu enclosure acoustical assy
01-203-2195
Vertical Stabilizer
Used on e-2c aircraft. cognizant service:navy;
01-203-4213
Structural Component Air Support
Used on c-5b aircraft.
01-203-4579
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-2.0 dia x 9.0 l; matl per fms-1111, cond sta, fin D450; mounting hole one end-.595, champhered to 1.002; hole drilled lengthwise into other end-5.75 in l, .901 dia; nha-16P3100-3; superceded 16P1104-7, ni; eff on-178, 180, 182, 188, 190, 192, 194, 202, 204, 206, 208, 212, 214, 216, 218, 220, 222, 224, 226, 228-231, 0233-9999
01-203-4586
Aircraft Former
6.000" overall length
01-203-4587
Aircraft Former
5.700" overall length
01-203-4588
Aircraft Former
5.600" overall length
01-203-4589
Aircraft Former
5.300" overall length
01-203-4590
Aircraft Former
5.200" overall length
01-203-4591
Aircraft Former
5.000" overall length
01-203-4592
Aircraft Former
4.900" overall length
01-203-4593
Aircraft Former
4.300" overall length
01-203-4594
Aircraft Former
11.200" overall length 3.560" overall width 1.100" material thickness
01-203-4595
Airfoil Rib
12.000" overall length 6.000" overall width 0.050" material thickness
01-203-4596
Airfoil Rib
12.000" overall length 6.000" overall width 0.050" material thickness
01-203-4597
Airfoil Rib
22.500" overall length 9.000" overall width 0.040" material thickness
01-203-4598
Airfoil Rib
22.500" overall length 9.000" overall width 0.040" material thickness
01-203-4599
Airfoil Rib
22.500" overall length 9.000" overall width 0.032" material thickness
01-203-4600
Aircraft Skin
79.000" overall length 28.000" overall width
