01-318-8829
Structural Aircraft Panel
Used on helicopter model ch-53e.
01-318-8830
Aircraft Skin
Used on aircraft model s-3.
01-318-8836
Aircraft Engine Build- Parts Kit
Used on aircraft model ea-6b.
01-318-9267
Structural Aircraft Plate
01-318-9268
Structural Aircraft Panel
01-318-9917
Access Aircraft Door
Used on a-4 aircraft.
01-318-9957
Structural Aircraft Panel
17.400" overall length 1.100" overall width
01-318-9958
Structural Aircraft Plate
Used on b-52 aircraft. 14.200" overall length 1.200" overall width 0.200" material thickness
01-318-9965
Cutter Cable Blade
01-318-9966
Cutter Cable Blade
01-318-9967
Fuel Cell Aircraft Plate
Used on 1520-01-125-5476.
01-319-1208
Aircraft Fairing
01-319-1210
Aircraft Skin
37.000" overall length 23.000" overall width
01-319-1251
Structural Component Air Bracket
C/o 3 wire cable assy, 1 support center, 1 structure assy
01-319-3089
Aircraft Skin
Used on ea-6b acft.
01-319-3714
Aircraft Fairing
01-319-3715
Aircraft Fairing
01-319-3716
Aircraft Fairing
01-319-3717
Aircraft Fairing
01-319-3721
Structural Aircraft Panel
C/o 1 panel, 2 baffle; nha DAA3132B950; opposite -002; finish f-25.01; nuclear hardness critical item
01-319-3722
Structural Aircraft Panel
Nha DAA3132B950; c/o 1 panel, 2 baffle; opposite -001; finish f-25.01; nuclear hardness critical item; smoothness critical item
01-319-3723
Structural Aircraft Panel
C/o 1 panel, 1 baffle; opposite -004; nha DAA3132B950; finish f-25.01; nuclear hardness critical item
01-319-3724
Structural Aircraft Panel
C/o 1 panel, 1 baffle; opposite -003; nha DAA3132B950; finish 25.01; nuclear hardness critical item
01-319-3725
Structural Aircraft Panel
Opposite -006; finish f-14.67 plusf-19.62; c/o 1 core; nha DAA3132B700; nucear hardness critical item, smoothnesscritical item
01-319-3726
Structural Aircraft Panel
Opposite -005; finish f-14.67 plusf-19.62; nha DAA3132B700; nuclear hardness critical item; smoothness critical item
01-319-3727
Structural Aircraft Panel
Finish f-14.67 plus f-19.62; c/o 1core; nha DAA3132B700; nuclear hardness critical item, smoothness critical item
01-319-3728
Structural Aircraft Panel
Finish f-14.67 plus f-19.62; nha DAA3132B700; opposite -006; c/o 1 core; nuclear hardness critical item, smoothness critical item
01-319-3729
Structural Aircraft Panel
Finish f-14.67 plue f-19.62; nha DAA3132B700; opposite -005; c/o 1 core; nuclear hardness critical item, smoothness critical item
01-319-3730
Structural Aircraft Panel
Finish f-14.67 plus f-19.62; nha DAA3132B700; opposite -006; c/o 1 core; nuclear critical item, smoothness critical item
01-319-3731
Structural Aircraft Panel
Finish f-14.67 plus f-19.62; nha DAA3132B700; opposite -005; c/o 1 core; nuclear hardness critical item, smoothness critical item
01-319-3732
Structural Aircraft Panel
Used on pacer special. 33.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -006; dimensions listed are stock size
01-319-3733
Structural Aircraft Panel
Used on pacer special. 33.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerence plus or minus .006; opposite -005; dimensions listed are stock size
01-319-3734
Structural Aircraft Panel
Used on pacer special. 56.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -010; dimensions listed are stock size
01-319-3735
Structural Aircraft Panel
Used on pacer special. 56.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -009; dimensions listed are stock size
01-319-3736
Structural Aircraft Panel
Used on pacer special. 59.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -010; dimensions listed are stock size
01-319-3737
Structural Aircraft Panel
Used on pacer special. 59.000" overall length 13.000" overall width hnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -009; dimensions listed are stock size
01-319-3738
Structural Aircraft Panel
Nuclear hardness critical item
01-319-3739
Structural Aircraft Panel
Nuclear hardness critical item
01-319-3740
Structural Aircraft Panel
Used on pacer special. 47.000" overall length 11.000" overall width nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -002
01-319-3742
Aircraft Skin
01-319-3743
Aircraft Skin
01-319-3790
Access Aircraft Cover
Used on b-2 pacer special. nha DAA3234A422; oppositie -040
01-319-4525
Aircraft Skin
01-319-4993
Elevator Balance Weight
01-319-4994
Elevator Balance Weight
Used on acft model e-3a.
01-319-5483
Thermal Insulation Pipe Covering
