01-542-2751
Aircraft Fairing
Used on F-16. 27.000" overall length 3.000" overall width right-hand strake for f-16 fuel tank assembly
01-542-2782
Structural Component Air Support
Used on A-10. 4.200" overall length 3.800" overall width 0.063" material thickness support used on -1, -3, -5, -7, -20, -203, -9; heat treat 0; alcd sh
01-542-2785
Structural Component Air Support
Used on A-10. 4.100" overall length 3.500" overall width 0.063" material thickness support alcd sh; heat treat 0; used on -2, -4, -8, -10, -2-2, -204
01-542-2792
Access Aircraft Cover
Used on ea-6b;cover assy, mod. navy-cover assy fuselage nadep jax dcn 314-06-04, T0000
01-542-2796
Aircraft Frame
Used on e-2c;weldment, emdu fixture. 4.120" overall length 3.100" overall width navy-gusset
01-542-2812
Acoustical Aircraft Insulation
Used on E-8. e-8 joint stars; u/o overwing emergency hatch
01-542-2817
Structural Aircraft Plate
Used on f-22 raptor. 7.000" overall length 5.000" overall width 2.220" material thickness splices lg.
01-542-2818
Structural Aircraft Plate
Used on f-22 raptor. 7.000" overall length 5.000" overall width 2.220" material thickness splices lg,
01-542-2868
Access Aircraft Cover
Used on C-130H. nha 257A475
01-542-2869
Structural Component Air Fitting
Used on b-1b spares. 20.000" overall length 7.500" overall width 7.000 " material thickness same as -001 except noted; c/o 1 bushing, 1 bearing, 1 fitting, ams 5643 cres bar, alloy 17-4 ph cond H1025
01-542-2910
Structural Component Air Support
Used on a-10a thunderbolt ii. 4.500" overall length 3.200" overall width 0.063" material thickness dim are stock matl
01-542-2914
Structural Component Air Support
Used on A-10A. 4.300" overall length 4.200" overall width 0.063" material thickness dim are stock size; heat treat 0
01-542-2919
Structural Component Air Support
Used on a-10a thunderbolt ii. 4.300" overall length 4.200" overall width 0.063" material thickness support dim are stock size; heat treat 0
01-542-2924
Structural Component Air Support
Used on a-10a thunderbolt ii. 4.500" overall length 4.200" overall width 0.063" material thickness support dim are stock size; heat treat 0
01-542-2957
Structural Component Air Support
Used on a-10a thunderbolt ii. 4.500" overall length 4.200" overall width 0.063" material thickness support dim are stock size; heat treat 0
01-542-3002
Structural Component Air Support
Used on a-10a thunderbolt ii. 4.600" overall length 4.400" overall width 0.063" material thickness support dim are stock size matl; heat treat T0
01-542-3037
Trim Aircraft Tab
New design
01-542-3096
Structural Component Air Support
Used on A-10. 4.300" overall length 3.600" overall width 0.063" material thickness support heat treat 0; alcd sh; used on -1, -3, -5, -7, -9, 201-203
01-542-3099
Structural Component Air Support
Used on A-10. 4.300" overall length 3.600" overall width 0.063" material thickness support used on -2, -4, -8, -10, -202, -204; heat treat 0; alcd sh
01-542-3104
Structural Component Air Support
Used on A-10. 4.300" overall length 4.000" overall width 0.063" material thickness support used on -2, -4, -8, -10, -202, -204; heat treat 0; alcd sh
01-542-3113
Structural Component Air Support
Used on A-10. 4.300" overall length 4.000" overall width 0.063" material thickness support alcd sh; heat treat 0; used on -1, -3, -5, -7, -9, 201, -203
01-542-3124
Aircraft Fairing
Used on A-10. 31.700" overall length 5.500" overall width 0.040" material thickness lwr fairing used on -1, -3, -5, -7, -9, ; heat treat 0; alcd sh
01-542-3125
Structural Component Air Support
Used on A-10. 12.100" overall length 1.700" overall width 0.063" material thickness support heat treat 0; alcd sh; used on -1, -3, -5, -7, -9, -201, -203
01-542-3131
Aircraft Pylon
Pylon assy opposite -4; c/o 1 head assy (-9) ; 1 pylon (16S2112-11) make from -7; 1 pylon (16S2112-15) make from -13; 4 rivets; 1 plate; 5 bolt
01-542-3146
Aircraft Pylon
Pylon assy opposite -3; 1 head assy; 1 pylon (16S2112-12) make from -7; 1 pylon (16S2112-16) make from 13; 4 rivet; 1 plate; 5 bolt
01-542-3155
Aircraft Fairing
Used on ah-64 apache helicopter. fairing assy - bonded part
01-542-3184
Structural Component Air Support
Used on A-10A. 5.300" overall length 1.680" overall width 0.246" material thickness heat treat 651; nha 160D181160-1
01-542-3195
Aircraft Stiffener
Used on mv-22 aircraft. plow beam stiffnr navy: stiffener, aircraft
01-542-3213
Structural Component Air Support
4.400" overall length 3.700" overall width 0.063" material thickness support dim are stock size material
01-542-3217
Aircraft Skin
Used on mv-22 aircraft. side skin
01-542-3229
Aircraft Stiffener
Used on mv-22 aircraft. angle stiffener bl 15.0 splice
01-542-3244
Airframe Modification Kit
Used on sikorsky s 76c helicopter. kit, window seal rhs
01-542-3286
Radome
Used on f-16a,c.
01-542-3287
Radome
Used on f-16a,c.
01-542-3288
Radome
Used on f-16a,c.
01-542-3602
Structural Component Air Support
Pan
01-542-3747
Structural Component Air Fitting
Used on B1-B. 20.000" overall length 7.500" overall width 7.500 " material thickness fitting cres bar alloy 17-4 ph cond H1025; c/o 1 -17, -18 fitting, 1 bushing, 1 bearing; finish 60AB02 except as shown on f/d; opposite -61
01-542-3755
Structural Component Air Fitting
Used on B1-B. 18.000" overall length 7.500" overall width 7.500 " material thickness fitting -62 opposite; c/o 1 -17, -18 fitting, 1 bearing, 1 bushing; cres bar alloy 17-4 ph cond H1025
01-542-3759
Structural Component Air Fitting
Used on B1-B. 20.000" overall length 7.500" overall width 7.000 " material thickness fitting
01-542-3760
Aircraft Leading Edge
72.000" overall length 1.700" overall width 0.020" material thickness fuselage fence assy & installation
01-542-3764
Structural Component Air Fitting
Used on B1-B. 18.000" overall length 7.500" overall width 7.500 " material thickness fitting cres bar alloy 17-4 ph cond H1025; c/o 1 -15, -16 fitting, 1 bearing, 1 bushing; opposite 052
01-542-3767
Airframe Modification Kit
Used on sikorsky s 76c helicopter. kit, window seal lhs
01-542-3795
Structural Component Air Fitting
Used on B1-B. 18.000" overall length 7.500" overall width 7.500 " material thickness fitting cres bar alloy 17-4 ph cond H1025; c/o 1 -13, -14 fitting, 1 bushing, 1 bearing; -41 opposite
01-542-3810
Explosion Suppressa Foam Segment
16.000" overall length 16.000" overall width void filler instl matl to be ballistic foam thermarest AX5052
01-542-3825
Access Aircraft Door
Used on c-17 acft. access-apu, inboard; nha 17P2A3800; u/o acft 17A151-17A999
01-542-3826
Access Aircraft Door
Used on c-17 acft. access-ac equipment rh; u/o acft 17A151-17A999
01-542-3827
Access Aircraft Door
Used on c-17 acft. access-apu-outboard; u/o acft 17A151-17A999
01-542-3831
Structural Aircraft Panel
24.500" overall length 14.000" overall width panel matl al plate 7050-T7451/dms 2233
01-542-3833
Aircraft Fairing
4.180" overall length 3.100" overall width fairing make from 17P2A3952-21, sh 6061-0, qq-a-250/11, dim are stock matl
01-542-3834
Aircraft Fairing
Fairing make from 17P2A3952-23; matl al 6061; qq-a-250/11
