01-572-8183
Aircraft Skin
Used on c-130 aircraft. 46.000" overall length 37.000" overall width skin cond a rc 70; dim. are stocksize
01-572-8189
Aircraft Intercostal
Used on c-130 aircraft. 8.000" overall length 5.000" overall width 0.032" material thickness intercostal T3 clad; cond-T3; dim. are stocksize; finish f-1
01-572-8212
Aircraft Skin
Used on c-130 acft. 43.000" overall length 7.000" overall width skin finish s-26; dim. are stocksize matl; cond-T3; T3 clad
01-572-8242
Aircraft Fairing
Used on f-15 acft. 19.000" overall length 3.400" overall width 0.050" material thickness fairing assy (rh) al sh-0; dim. are stocksize; nha 9767115 per eo
01-572-8248
Aircraft Fairing
Used on f-15 acft. 19.000" overall length 3.400" overall width 0.050" material thickness fairing assy (lh) al sh-0; c/o fairing, clips, rivets, shims; dim. are stocksize; nha 9767115 per eo
01-572-8361
Door Aircraft Hinge
Used on airbus a-310 nacelle turbine engine starter outside air induction panel door.
01-572-8362
Door Aircraft Hinge
Used on airbus a-310 nacelle turbine engine starter outside air induction panel door.
01-572-8363
Access Aircraft Door
Airbus a-310 nacelle turbine engine starter outside air induction door
01-572-8462
Exhaust Pipe
Used on P-3C. filler, inboard nacelle, tail pipe assembly/installation; drawing 285E11-101-04; size 0.050 x 2 x 1
01-572-8484
Exhaust Pipe
Used on P-3C. tail pipe assembly/installation, inborad nacelle; drawing 285E11-101-04; size 142.48" long
01-572-8485
Exhaust Pipe
Used on P-3C. tail pipe assembly/installation, outboard nacelle; drawing 285E11-101-04; size 108.99" long
01-572-8625
Aircraft Window Panel
01-572-8628
Aircraft Window Panel
01-572-8659
Aircraft Stiffener
Used on c-130 acft. 10.000" overall length 3.000" overall width 0.032" material thickness stiffiner dim. are stocksize; 0 al clad; T4 heat treat; cond-0
01-572-8663
Structural Aircraft Plate
Used on c-130 acft. 133.000" overall length strip m/f LS4267; dim. are stocksize; T3 clad; cond-T3
01-572-8668
Structural Component Air Support
Used on bell 206b-1.
01-572-8672
Structural Aircraft Plate
Used on c-130 acft. 5.000" overall length 2.000" overall width 0.032" material thickness gusset T3 clad; cond-T3; dim. are stocksize matl; finish f-1
01-572-8706
Access Aircraft Door
Used on B-1B. access-actuator, inboard, upper, wing leading edge horn
01-572-8710
Access Aircraft Door
Used on b-1b bomber. access-actuator, inboard, upper, wing leading edge horn
01-572-8717
Access Aircraft Door
Used on B-1B. access-actuator, outboard, upper, wing leading edge horn
01-572-8722
Access Aircraft Door
Used on b-1b bomber. access-actuator, outboard, upper, wing leading edge horn
01-572-8729
Structural Component Aircraf Web
0.040" material thickness finish per F2.115
01-572-8732
Structural Component Aircraf Web
0.040" material thickness finish per F2.115
01-572-8775
Aircraft Skin
01-572-8823
Aircraft Pylon
01-572-8841
Structural Aircraft Plate
Used on c-130 acft. 9.000" overall length 3.000" overall width 0.051" material thickness gusset T3 clad al; dim. are stocksize; cond-T3; finish f-1; NHA375456
01-572-8868
Structural Aircraft Panel
Used on c-130 aircraft. 6.000" overall length 6.000" overall width closure 0-clad alum; dim. are stocksize matl; heat treat T6; used on 4P52070-123a
01-572-8873
Structural Aircraft Panel
Used on c-5 acft. 6.000" overall length 6.000" overall width closure 0-clad alum; dim. are stocksize matl; heat treat T6; used on 4P52070-123a
01-572-8937
Aircraft Skin
Used on c-130 acft. 66.000" overall length 26.000" overall width skin cond-T3; finish s-19; dim. are stocksize matl.; T3 clad al; rightside
01-572-8944
Aircraft Skin
Used on c-130 acft. 66.000" overall length 26.000" overall width skin cond-T3; finish s-19; dim. are stocksize matl; T3 clad alum
01-572-9076
Aircraft Skin
Used on c-130h acft. 52.000" overall length 26.000" overall width skin T3 clad; dim. are stocksize matl; finish s-19; cond-T3
01-572-9101
Aircraft Skin
Used on c-130 acft. 32.000" overall length 26.000" overall width skin T3 clad alum; dim. are stocksize matl; cont-T3; finish s-19
01-572-9109
Aircraft Skin
Used on c-130 acft. 32.000" overall length 26.000" overall width skin T3 clad alum; dim. are stocksize matl; cond-T3; finish s-19
01-572-9162
Aircraft Skin
Used on c-130 acft. 26.000" overall length 16.000" overall width skin T3 clad; dim. are stocksize matl; finish s-19; cond-T3
01-572-9222
Structural Component Air Support
Used on c-130 acft. 14.000" overall length cap nha 343597; dim. are stocksize matl; m/f LS2045; heat treat T42; finish f-19
01-572-9251
Aircraft Skin
Used on c-130 acft. 71.000" overall length 26.000" overall width skin cond-T3; dim. are stocksize matl; T3 clad al; finish s-19; no heat treat; -26r opposite
01-572-9309
Structural Component Air Support
Used on c-130 acft. 331.000" overall length cap finish f-19-19; dim. are stocksize matl; next assy 343538l
01-572-9592
Airfoil Rib
Used on c-130 acft. 44.000" overall length 8.000" overall width 0.032" material thickness rib assy finish f-54; heat treat T42; al-0 clad; c/o 1 rib, 1 stiffener, 1 former; dim. are stocksize matl
01-572-9637
Airfoil Rib
Used on c-130 acft. 44.000" overall length 8.000" overall width 0.032" material thickness rib finish f-54; heat treat T42; alum-0 clad; dim. are stocksize matl; u/o 345196-12
01-572-9651
Structural Component Air Support
Used on c-130 acft. 5.000" overall length 1.250" overall width 0.025" material thickness angle finish F1; dim. are stocksize; heat treat none; cond a; rc 70
01-572-9692
Structural Aircraft Plate
Used on c-130 acft. 4.000" overall length 3.000" overall width 0.032" material thickness gusset cond T3; dim. are stocksize matl; heat treat/none; next assy 342328; T3 clad alum
01-572-9773
Structural Aircraft Plate
2.120" overall length 1.900" overall width 0.800" material thickness filler 1.26 in. dia. center hole, finish per f-1.1929
01-572-9775
Structural Component Air Fitting
01-572-9776
Structural Component Air Fitting
01-572-9779
Structural Aircraft Plate
4.330" overall length 2.560" overall width 0.040" material thickness gusset
01-572-9782
Structural Aircraft Plate
4.330" overall length 4.120" overall width 0.040" material thickness gusset
01-572-9789
Structural Component Air Support
Cap m/f LS2045 14.0 in. lg
01-572-9810
Structural Component Air Support
Used on c-130 acft. clip LS3216 x 2; used on 343596-35, -36; finish f-1-1; heat treat none
01-572-9817
Airfoil Rib
Used on c-130 acft. 43.000" overall length 6.000" overall width 0.032" material thickness rib heat treat T42; finish f-19; dim. are stocksize matl; 0-clad alum; next assy 342328
01-572-9830
Fuel Tank Parts Kit
Used on f-16 acft. u/o 300 gal. tank
