01-530-0635
Aircraft Wing Assembly
Wing box assembly
01-530-0639
Aircraft Wing Assembly
Wing box assembly
01-530-0747
Structural Component Air Support
01-530-0838
Stiffener Aircraft Rib
Used on E-2C. navy: rib assembly next higher drawing AFC332
01-530-0851
Stiffener Aircraft Rib
Used on c-2a; e-2c. navy: rib assembly
01-530-0879
Structural Aircraft Plate
6.000" overall length 4.000" overall width 0.050" material thickness end plate dim. are stock material; nha 4J40102
01-530-0889
Structural Component Air Bracket
15.000" overall length 2.000" overall width 0.040" material thickness dim. are stock material; nha 4J40102
01-530-0901
Structural Component Air Bracket
15.000" overall length 2.000" overall width 0.040" material thickness dim. are stock material; nha 4J40102
01-530-0959
Aircraft Skin
Used on c-2a;entrance door. 16.700" overall length 11.200" overall width navy: skin assembly
01-530-0966
Structural Aircraft Plate
Used on E-2C. 3.300" overall length 2.600" overall width 0.080" material thickness navy: plate assembly alodize surface treated
01-530-0969
Aircraft Bulkhead
Used on E-2C. 32.000" overall length 17.000" overall width 0.025" material thickness navy: bulkhead assembly alodize surface treated
01-530-1064
Aircraft Skin
152.000" overall length 64.000" overall width skin engineering order no 2004C0001; matl AL7475-0, STM07-120 cond T761; eo creates new p/n for replacement skins; skins are to be more stress corrosion resistant than existing skins; dim are stock matl
01-530-1065
Aircraft Skin
167.000" overall length 64.000" overall width skin engineering order no 20004C0001; matl AL7475-0, STM07 cond T761; eo creates new p/n for replacement skins; skins are to be more stress corrosion resitant than existing skins; dim are stock matl
01-530-1066
Aircraft Skin
148.000" overall length 43.000" overall width skin engineering order no 2004C0001; matl AL7475-0, STM07-120 cond T761; eo creates new p/n for replacement skins, skins are to be more stress corrosion resistant than existing skins; dim are stock matl
01-530-1068
Aircraft Skin
142.000" overall length 43.000" overall width skin engineering order no 2004C0001; matl AL7475-0, STM07-120 cond T761; eo creates new p/n for replacement skins, skins are to be more stress corrosion resitant than existing skins; dim are stock matl
01-530-1069
Aircraft Skin
160.000" overall length 64.000" overall width skin engineering order 2004C0001; matl al 7475-0, STM07-120 cond T761; eo creates new p/n for replacement skins; skins are to be more stress corrosion resitant than existing skins; dim are stock matl
01-530-1085
Wing Stall Fence
Used on E-2C. navy: fence assembly aluminum spotweld
01-530-1160
Structural Aircraft Plate
Used on kc-135 stratotanker. 2.800" overall length 1.800" overall width shear plate matl 2024-T3 sheet qq-a-355 T3 temper; dim are stock matl
01-530-1169
Aircraft Stiffener
15.000" overall length 4.200" overall width 0.020" material thickness dim. are stock material; nha 5-96130
01-530-1173
Aircraft Stiffener
15.000" overall length 4.200" overall width 0.020" material thickness dim. are stock material; nha 5-96130; opposite -1
01-530-1178
Fuel Aircraft Cell
Used on helicopter,utility nsn 1520-01-492-6324.
01-530-1253
Structural Component Air Support
01-530-1265
Structural Component Air Support
01-530-1460
Structural Aircraft Plate
Used on ch47d helicopter,cargo-transport nsn 1520-01-088-3669. 16.290" overall length 0.574" overall width
01-530-1467
Structural Aircraft Plate
Used on ch47d helicopter,cargo-transport nsn 1520-01-088-3669. 16.290" overall length 0.574" overall width
01-530-1475
Structural Aircraft Plate
Used on ch47d helicopter,cargo-transport nsn 1520-01-088-3669. 16.047" overall length 0.574" overall width
01-530-1554
Winglet
M/o carbon/kevlar/epoxy
01-530-1555
Access Aircraft Door
Used on f-22 acft. access avionics
01-530-1561
Structural Aircraft Plate
Used on f/a-22 raptor. 3.000" overall length 1.000" overall width 0.063" material thickness filler, radious dim. are stock material
01-530-1637
Aircraft Window Panel
01-530-1878
Aircraft Stiffener
Used on kc 135 acft. 15.000" overall length 4.800" overall width 0.032" material thickness stiffener - balance panel, outboard aileron heat treat T4; opposite -2; used on 5-96130
01-530-1912
Fuel Aircraft Cell
Used on kc-135r/t aircraft. fuel cell bladder no. 2, center wing, nitrile const, enhanced
01-530-1913
Fuel Aircraft Cell
Used on kc-135r/t acft. fuel cell bladder no. 1, center wing, nitrile const.being modified
01-530-2048
Structural Component Air Support
Used on acft model c-135. 9.500" overall length 8.300" overall width 3.000" material thickness support fitting, flap track heat treat -T73; make from 5-7124, opposite -12, nha 5-85644
01-530-2176
Aircraft Stiffener
Used on kc-135 acft. 15.000" overall length 4.800" overall width 0.032" material thickness stiffener-balance panel, outboard ailerson heat treat T4; opposite -2 (except as shown) ; used on dwg 5-96130
01-530-2205
Aircraft Stiffener
Used on kc-135 model. 15.000" overall length 4.200" overall width 0.032" material thickness stiffener-balance panel, outboard aileron heat treat T4; used on dwg 5-96130
01-530-2211
Structural Aircraft Plate
Used on aircraft, f-16. 17.000" overall length 15.000" overall width 0.500" material thickness
01-530-2249
Fuel Aircraft Tank
Used on aircraft, beech king air c-90. cell assembly
01-530-2380
Winglet
M/o carbon/kevlar/epoxy
01-530-2390
Structural Component Air Bracket
Used on v-22 lrip 1. (navy) bracket, aft, aircraft
01-530-2395
Structural Component Air Bracket
Used on v-22 lrip 1. (navy) bracket, aft, aircraft
01-530-2403
Structural Component Air Support
01-530-2404
Structural Component Air Support
01-530-2407
Structural Component Air Support
01-530-2411
Structural Component Air Support
01-530-2415
Structural Component Air Support
01-530-2443
Structural Component Air Bracket
Used on v-22 lrip 1 e-nsn isil. navy) bracket, aircraft, ma
01-530-2504
Aircraft Frame
Used on V-22. center body assembly
01-530-2519
Structural Aircraft Panel
Used on V-22. panel assembly, aircraft essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-530-2581
Structural Aircraft Panel
Used on v22 aircraft. essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
