01-528-9415
Structural Component Air Support
24.000" overall length 4.000" overall width 0.025" material thickness strap 134a same as -124a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -106a, -114a, -124a; dim are stock material
01-528-9426
Structural Component Air Support
16.000" overall length 4.000" overall width 0.025" material thickness strap 133a same as -123a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -105a, -113a, -123a; dim are stock material
01-528-9431
Structural Component Air Support
Strap, fail safe-upper lobe heat treat T761; same as -181a except; nha 4F22034
01-528-9434
Structural Component Air Support
Strap, fail safe-upper lobe heat treat T761; same as -180a except; nha 4F22034
01-528-9440
Structural Component Air Support
93.000" overall length 4.000" overall width 0.025" material thickness strap 137a same as -127a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -108, -116, -117a, -127a; dim are stock material
01-528-9450
Structural Component Air Support
74.000" overall length 4.000" overall width 0.025" material thickness strap 135a same as -125a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -107a, -115a, -125a; dim are stock material
01-528-9479
Structural Component Air Support
4.000" overall length 0.025" material thickness strap 130 same as -120a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -102a, -110a, -120a; dim are stock matl
01-528-9483
Structural Component Air Support
16.000" overall length 4.000" overall width 0.025" material thickness strap 129a same as -119a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -101a, -109a, -119a; dim are stock matl
01-528-9485
Stiffener Aircraft Rib
Used on c-2a and e-2a; control surface-lwr outbd rudder, l.e.. navy: rib assembly
01-528-9487
Structural Component Air Support
Strap, fail safe-upper lobe heat treat T761; same as -179a except; nha 4F22034
01-528-9507
Structural Component Air Bracket
Used on e-2a; cont surface-outbd fin. 7.000" overall length 5.625" overall width 0.187" material thickness navy: strap assembly next assembly 123CS11800
01-528-9521
Structural Component Air Support
92.000" overall length 6.000" overall width 0.025" material thickness strap 132a same as -122a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -104a, -112a, -122a; dim are stock matl
01-528-9525
Structural Component Air Support
71.000" overall length 6.000" overall width 0.025" material thickness strap 131a same as -121a except use 7475-T761 bare per STM07-121 or ams 4085; spares replacement for -103a, -111a, -121a; dim are stock matl
01-528-9559
Aircraft Floor
Used on oh-58d kiowa warrior helicopter. forward floor
01-528-9563
Fuselage Section
Used on oh-58d kiowa warrior. fuel tub
01-528-9566
Structural Aircraft Panel
Frame-wing to fus fairing, fus sta 1024.00, instl of
01-528-9568
Fuselage Section
Used on oh-58d kiowa warrior helicopter. aft shell
01-528-9575
Fuselage Section
Used on oh-58d kiowa warrior helicopter. roof
01-528-9577
Structural Component Air Support
Strap, fail safe-upper lobe heat treat T761; same as -106a except; spares replacement for -102a, -104a, -106a; nha 4F40008
01-528-9580
Structural Aircraft Panel
Frame-wing to fus fairing, fus sta 1024.00, instl of
01-528-9586
Structural Component Air Support
Strap, fail safe-upper lobe heat treat T761; same as -105a except; spares replacement for -101a, -103a, -105a; nha 4F400008
01-528-9661
Aircraft Channel
01-528-9692
Structural Component Air Bracket
Used on seasprite helicopter.
01-528-9791
Aircraft Stiffener
Used on center fuselage structure, c-130 hercules aircraft. 21.000" overall length 1.000" overall width
01-528-9831
Structural Aircraft Panel
Frame-wing to fus fairing, fus sta 1084.00, instl of
01-528-9835
Structural Aircraft Panel
Frame-wing to fus fairing, fus sta 1084.00 instl of
01-528-9886
Tubing Aircraft Support
Used on f/a-22 raptor. 4.000" overall length 3.000" overall width supports, hydraulic tubing-mwd
01-528-9887
Tubing Aircraft Support
Used on f/a-22 raptor. 4.000" overall length 4.000" overall width supports, tubing-utility distr modules 2 & 3 AL6013-T4 (aluminum .063)
01-528-9888
Tubing Aircraft Support
Used on f/a-22 raptor. 4.000" overall length 2.000" overall width supports, tubing-utility distr modules 2 AL6013-T4 (aluminum .063)
01-528-9889
Tubing Aircraft Support
Used on f/a-22 raptor. 5.000" overall length 3.000" overall width supports, tubing-utility distr modules AL6013-T4; aluminum .063
01-528-9890
Structural Component Air Support
9.250" overall length 1.125" material thickness support matl bar steel 4340, ams 6414, heattreat to 160000-180000 psi per dps 5.00ams 2759 may be used subject to the restrictions of note AAZ1; dim are stock matl
01-529-0030
Access Aircraft Cover
Used on e-2a aircraft;control surfaces-outbd tab. navy: cover assembly bottom left corner squared other three are rounded. 11 holes drilled through no. 40 (.097-.102) ; material is fiberglass cloth no. 181, volan "a" finish (.040-4 layers min)
01-529-0035
Aircraft Channel
Used on c-2a and e-2a; plates, pp-nac sta57.06-sta92.88, upper cowl. 4.250" overall length 4.000" overall width 0.063" material thickness navy: channel assembly 8 holes drilled through no. 30 (.127-.133) ; next higher assembly 123P10333.
01-529-0055
Structural Component Air Bracket
Used on e-2c;straps-cont surf-inbd rud, sta3.36-7.00. 6.500" overall length 3.250" overall width 0.020" material thickness navy: angle assembly
01-529-0084
Aircraft Channel
Used on c-2a and e-2c plates-upper cowl. 4.250" overall length 4.000" overall width 0.063" material thickness navy: channel assembly
01-529-0144
Aircraft Stringer
Used on center fuselage structure, c-130 aircraft. 50.000" overall length 2.000" overall width 0.032" material thickness
01-529-0222
Tubing Aircraft Support
01-529-0223
Structural Component Air Support
01-529-0224
Tubing Aircraft Support
Used on f/a-22 raptor. 5.000" overall length 4.000" overall width support, hydraulic tubing-utility distr module iii heat treat t-4; aluminum AL6013-t-4
01-529-0225
Tubing Aircraft Support
Used on f/a-22 raptor. 4.000" overall length 3.000" overall width support, hydraulic tubing-utilitydistr module iii aluminum AL6013-4
01-529-0226
Structural Component Air Support
01-529-0227
Structural Component Air Support
01-529-0228
Structural Component Air Support
01-529-0229
Tubing Aircraft Support
01-529-0230
Structural Component Air Support
01-529-0233
Structural Component Air Support
01-529-0396
Structural Aircraft Panel
Used on c-2a and e-2c; fus-mid sect entrance door. 34.500" overall length 10.000" overall width navy: corrugation assembly
01-529-0413
Aircraft Skin
Used on c-2a and e-2c; fus-mid sect entrance door. 16.625" overall length 10.375" overall width navy: skin assembly
01-529-0425
Structural Component Air Support
14.700" overall length 6.000" overall width 0.025" material thickness support, structural component, aircraft same as -109; heat treat T761
01-529-0431
Aircraft Fairing
Used on e-2c; fairing assy-cont surf-outbd rudder upper. navy: fairing assembly next higher assembly 123CS11801 also for c-2a aircraft
