01-580-5723
Aircraft Channel
Used on e-2c aircraft. size is 0.020 x 3-3/16 x 10-3/16 inch
01-580-5738
Structural Component Air Support
Used on e-2c aircraft. strap
01-580-5769
Structural Component Air Support
Used on e-2c aircraft. channel
01-580-5988
Structural Component Air Bracket
Used on f-22 raptor. c/o (1) -125 bracket (m/f ann. titanium plate) and (ar) urethane; dim. are stocksize matl
01-580-5989
Structural Component Air Bracket
Used on f-22 raptor. 14.000" overall length 7.000" overall width tit. sht; dim. are stocksize matl
01-580-5990
Structural Component Air Bracket
Used on f-22 raptor. 5.000" overall length 5.000" overall width 0.071" material thickness dim. are stocksize matl; 0-alum sheet
01-580-5991
Structural Component Air Bracket
Used on f-22 raptor. 6.000" overall length 4.000" overall width c/o (1) -287 bracket, 4 rivet, 2 nut; dim. are stocksize matl; tit sht
01-580-5992
Structural Component Air Bracket
Used on f-22 raptor. 5.000" overall length 5.000" overall width 0.072" material thickness sheet al-0; dim. are stocksize matl
01-580-5993
Structural Component Aircraf Web
Used on f-22 raptor. 28.000" overall length 15.000" overall width tit. plate; 5PTM7T01 6-2222 sta; dim. are stocksize matl
01-580-6104
Tubing Aircraft Support
Used on c-2a aircraft. 2.750" overall length 2.280" overall width 0.380" material thickness clamp assy, tube-hyd line support
01-580-6223
Aircraft Scoop
Air scoop
01-580-6301
Structural Component Air Bracket
Attaching angle, radome latch. measures 2.25 x 1.04 x 1.00.
01-580-6306
Structural Component Air Bracket
Attching angle, radome latch. measures 2.25 x 1.04 x 1.00.
01-580-6311
Aircraft Frame
Frame assembly includes filler, seal, beams, formers, stiffeners,
01-580-6331
Structural Aircraft Panel
Panel. lower assembly includes stringers, doubler skin,
01-580-6348
Structural Aircraft Plate
Fillet installation; horizontal stabilizer to tailcone splice. .032 x 2 x 4.
01-580-6612
Structural Aircraft Panel
Used on f-22 raptor. c/o (ref) smoothness, panel instl, coating appl, fill & fair, ident. mark; 4 rivets, 32 bolt, (sub) rivets, 20 nut, 2 nut plate, 1 nut element; (ar) titanium
01-580-6613
Structural Aircraft Panel
Used on f-22 raptor. c/o (ref) smoothness, mds index, loft, surface texture, fin. organ, ident marks, windswept part, temp protection; (ar) epoxy; (bkm) carbon/bmi
01-580-6616
Structural Aircraft Panel
Used on f-22 raptor. c/o (ref) smoothness, mds indes, loft, surface texture, finishes, organ, windswept part, temp protection; (bkm) carbon/bmi; (ar) epoxy
01-580-6623
Aircraft Fairing
Used on f-22 raptor. (mf) -111 fairing, labels; (ref) 5HF70006 smoothness; (ar) primer
01-580-6624
Structural Component Air Bracket
Used on f-22 raptor. 4.000" overall length 3.000" overall width alum plate; dim. are stocksize matl
01-580-6625
Aircraft Fairing
Used on f-22 raptor. mf (-112 fairing) , labels; ref (smoothness) ; primer (ar)
01-580-6626
Structural Component Aircraf Web
Used on f-22 raptor. 28.000" overall length 15.000" overall width dim. are stocksize matl; 5PTM7T01 6-2222 sta tit. plate
01-580-6627
Structural Component Air Bracket
Used on f-22 raptor. 6.000" overall length 5.000" overall width c/o (1) -113 bracket (m/f -103 casting, ams-a-21180 a 356.0-T6 al) , (sub) nut, 2 nuts, 4 rivets, (ar) sealant
01-580-6691
Structural Aircraft Panel
Used on c-5 acft. 41.000" overall length 12.000" overall width panel dim. are stocksize matl; AL7079-T6 clad; c/o skin, facing sheet, doublers, edge member, cores
01-580-6772
Structural Aircraft Panel
Used on c-5 acft. 12.000" overall length 7.000" overall width end closure-outbd heat treat T42; temper-0; 0 clad; dim. are stocksize matl
01-580-6827
Structural Component Air Bracket
Used on c-5 acft. 12.000" overall length 2.000" overall width 0.063" material thickness bracket 0 clad; heat treat T42; dim. are stocksize matl
01-580-6866
Aircraft Channel
Used on c-5 acft. 38.000" overall length 6.000" overall width 0.025" material thickness channel heat treat-T6; dim. are stocksize matl; used on 4J11183-103a panel assy; 0 clad; temper-0;
01-580-6871
Structural Component Air Bracket
Used on c-5 acft. 4.000" overall length 3.000" overall width 0.032" material thickness clip inconel 718 steel; dim. are stocksize matl; used on 4P51036-139a
01-580-6882
Structural Aircraft Plate
Used on c-5 acft. 13.000" overall length 4.000" overall width 0.020" material thickness closure dim. are stocksize matl; 0 clad
01-580-6987
Fuselage Parts Kit
Used on f-16 acft. u/o bulkhead segment-upper fuselage station 341.8
01-580-6988
Fuselage Parts Kit
Used on f-16 acft. u/o web details, fuel shelf FS331 to 352
01-580-7005
Aircraft Frame
01-580-7010
Structural Component Air Fitting
01-580-7044
Structural Component Air Bracket
Used on c-5 acft. 10.000" overall length 4.000" overall width 0.040" material thickness bracket used on 4J41352-110a; dim. are stocksize matl; 0 clad alum
01-580-7045
Structural Aircraft Plate
Used on c-5 acft. 8.000" overall length 6.000" overall width 0.080" material thickness end plate used on 4J41325-178a; dim. are stocksize matl
01-580-7050
Door Aircraft Hinge
Used on kc-135 acft. hinge used on 527-12528-1 door
01-580-7254
Aircraft Frame
Used on CH-47.
01-580-7261
Aircraft Frame
Used on CH-47.
01-580-7268
Aircraft Frame
Used on CH-47.
01-580-7277
Aircraft Frame
Used on CH-47.
01-580-7282
Aircraft Frame
Used on CH-47.
01-580-7290
Aircraft Frame
Used on CH-47.
01-580-7293
Aircraft Frame
Used on CH-47.
01-580-7296
Aircraft Frame
Used on CH-47F.
01-580-7304
Aircraft Frame
Used on CH-47.
01-580-7343
Aircraft Skin
01-580-7346
Aircraft Skin
01-580-7347
Structural Aircraft Plate
Filler
01-580-7350
Aircraft Hinge
