01-203-9677
Airfoil Rib
19.600" overall length 7.300" overall width 0.032" material thickness
01-203-9678
Airfoil Rib
19.600" overall length 7.300" overall width 0.032" material thickness
01-203-9679
Airfoil Rib
21.200" overall length 8.400" overall width 0.032" material thickness
01-203-9680
Airfoil Rib
21.200" overall length 8.400" overall width 0.032" material thickness
01-203-9681
Airfoil Rib
21.900" overall length 8.700" overall width 0.032" material thickness
01-203-9682
Airfoil Rib
21.900" overall length 8.700" overall width 0.032" material thickness
01-203-9683
Airfoil Rib
11.000" overall length 8.000" overall width 0.040" material thickness
01-203-9685
Airfoil Rib
11.000" overall length 8.000" overall width 0.040" material thickness
01-203-9686
Aircraft Skin
Used on acft model kc-135. 2024-T3 clad sheet per qq-a-250/5; finish f-2.59; 24.5 in. long, 4.0 in.wide, 0.080 in. thick; opposite p/n -610
01-203-9687
Aircraft Skin
Used on acft model kc-135. 2024-T3 clad sheet per qq-a-250/5; finish f-2.59; 24.5 in. long, 5.0 in. wide, 0.080 in. thick; opposite p/n-624
01-203-9688
Aircraft Skin
Used on acft model kc-135. 2024-T3 clad sheet per qq-a-250/5; finish f-2.59; 24.5 in. long, 5.0 in. wide, 0.080 in. thick; opposite p/n -623
01-203-9689
Aircraft Skin
Used on acft model kc-135. 2024-T3 clad sheet per qq-a-250/5; finish f-2.59; 25.0 in. long, 4.5 in. wide, 0.080 in. thick; opposite p/n -628
01-203-9690
Aircraft Skin
69.000" overall length 27.000" overall width
01-203-9691
Aircraft Spar
78.000" overall length 9.500" overall width 0.063" material thickness
01-203-9692
Aircraft Stringer
76.500" overall length
01-203-9693
Aircraft Stringer
42.000" overall length
01-204-1529
Structural Component Air Bracket
01-204-1551
Structural Aircraft Plate
Used on acft model b-1b. functional description:used as apu start module serrated mtg plate; nuclear hardness critical item; PH15-7mo cres sheet plate per AMS5520; 1.90 in.long, 0.750 in.wide, 0.125 in.thick; nha L5802631;
01-204-1554
Structural Component Air Support
Used on c-130 acft.
01-204-1573
Bleed Air Duct Assembly
Used on acft model f-111. material is inconel 625, 7.000 in. lg, 2.000 in. w, 0.032 in. thk
01-204-1578
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -107a seal (1) , -111a panel (1) ; nha 4E20080
01-204-1580
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -101a panel assembly (1) , -105a door (1) , marker (1) , screw (8) , washer (8) ; nha 4E23227
01-204-1581
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -101a panel assembly (1) , -107a door (1) , screw (8) , washer (1) , marker (1) ; nha 4E23227
01-204-1583
Structural Aircraft Panel
Used on acft model b-1b. c/o 1 fiberglass epoxy prepreg, 2 non-flammable adhesive backed piles; 17.190 in. lg, 8.220 in. w; 19 holes around edge 0.219 in. dia; nha L5338210
01-204-1584
Structural Aircraft Panel
Used on acft model b-1b.
01-204-1587
Structural Aircraft Panel
Used on acft model b-1b.
01-204-1588
Structural Aircraft Panel
01-204-1592
Fuselage Section
C/o bulkhead p/n 12B10809-7, bushing p/n 12B10616-7, bushing p/n 12B9743-9
01-204-1599
Aircraft Skin
49.000" overall length 41.000" overall width superceded -803 ow; nha-16B5313-803; eff on-0001 9999; c/0 -27 skin, nuts, rivets, sealant
01-204-1600
Aircraft Skin
80.000" overall length 24.000" overall width
01-204-1601
Aircraft Skin
Used on F-15.
01-204-1602
Aircraft Skin
Used on C-130.
01-204-1604
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b
01-204-1605
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b
01-204-1606
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b
01-204-1608
Aircraft Door
C/o: door panel assembly (1) , slam strip (3) , channel (5) , latch assembly (1) , indicator lock (1) , screw (32) ; nha 4E32085
01-204-1706
Thermal Insulation Pipe Covering
Acft c-130
01-204-1709
Fluid Aircraft Manifold
C/o: duct half (4) , duct (3) , flange (2) , nut (2) ; manifold assembly-madar cooling air, fus sta 471.70; nha 4A31112, eff on 0082 & up; c-5b aircraft
01-204-1961
Access Aircraft Door
Used on acft model b-1b. material temper T851; stock size 11.250 in. lg., 6.380 in. w, 0.875 in.thk; nha L3226649-001; used as idg access lh nacelle door; hinge included with nha
01-204-2419
Structural Aircraft Plate
12.000" overall length 8.000" overall width 0.020" material thickness
01-204-2420
Structural Aircraft Plate
01-204-2421
Structural Aircraft Plate
01-204-2422
Structural Component Air Support
Used on f-15 acft.
01-204-2423
Structural Component Air Support
Used on f-15 acft. fuselage station 672.680
01-204-2433
Aircraft Former
01-204-2434
Aircraft Former
01-204-2435
Fuselage Section
C/o bulkhead p/n 12B10809-8, bushing p/n 12B16616-7, bushing p/n 12B09743-9
01-204-3016
Structural Component Air Support
Used on b-1b se. support assembly; aluminum alloy; 12.460 in. min, 12.540 in. max o/a lg, 1.180 in. nom w; 2 holes 0.620 in. nom dist between ctr holes along lg; hardness critical item
01-204-3452
Access Aircraft Door
Used on acft model b-1b. nha L3202814-011; used as nacelle center beam apu fire access door
