01-544-0614
Aircraft Stiffener
01-544-0621
Structural Component Aircraf Web
01-544-0622
Aircraft Skin
Used on A-10. 52.000" overall length 18.000" overall width skin, lower heat treat T0
01-544-0625
Structural Component Air Support
01-544-0633
Aircraft Skin
Skin-upper
01-544-0635
Structural Component Air Support
01-544-0636
Structural Aircraft Plate
7.000" overall length 4.500" overall width 0.040" material thickness baffle dim. are stock material
01-544-0807
Structural Component Air Support
Support m/f: -7 (identical except for surface treatment) ; nha: 17P6P5501
01-544-0809
Structural Component Air Support
Support m/f: -7; nha: 17P6P5501
01-544-0810
Structural Component Air Support
Support nha: 17P6P5502; make from -6 (identical except for surface treatment)
01-544-0935
Structural Component Air Support
01-544-0951
Structural Component Air Support
01-544-1064
Structural Component Air Support
01-544-1078
Structural Component Air Support
01-544-1170
Aircraft Skin
Used on f16 aircraft.
01-544-1242
Structural Aircraft Panel
Used on f-22 raptor. air dam, side fairing nha 5HF74014
01-544-1243
Structural Aircraft Panel
Used on f-22 raptor. air dam, side fairing NHA5HF74014
01-544-1246
Structural Component Air Fitting
Used on f-22 raptor. aft keel fitting assy salvaged p/n 5HT75705-107, from 5HF75700, new identity 5HP79199-405. c/o (ref 5HF75705 aft sidewall) , (ref interface 5VP99001
01-544-1263
Structural Component Air Support
Support make from 17P6P6822-6; nha 17P6P5502
01-544-1330
Structural Component Air Support
Used on A-10. 6.700" overall length 2.800" overall width 0.040" material thickness splice angle used 0n -11; ht res sh; AMS5542; inconel x-750
01-544-1392
Structural Component Air Support
Used on A-10. 6.700" overall length 2.800" overall width 0.040" material thickness splice angle used on -11; ht res sh, AMS5542, inconel X750
01-544-1776
Structural Component Air Fitting
Engine mount nha L4100102
01-544-1777
Structural Component Air Support
01-544-1789
Aircraft Hinge
Hinge half
01-544-1795
Structural Component Air Support
01-544-1803
Structural Aircraft Plate
Doubler
01-544-1808
Structural Aircraft Plate
6.000" overall length 0.800" overall width 0.063" material thickness doubler dim. are stock material
01-544-1810
Structural Aircraft Plate
4.400 " overall length 2.200" overall width 0.020" material thickness splice dim. are stock material
01-544-1824
Aircraft Stiffener
3.400" overall length dim. are stock material
01-544-1836
Structural Component Air Support
Chord lower
01-544-1845
Aircraft Skin
Used on ma0001a. skin panel make from 4T32243-101a; nha 4T31028
01-544-1847
Structural Component Air Support
Chord lower
01-544-1850
Structural Aircraft Panel
Used on F-15. panel-assy
01-544-1864
Access Aircraft Cover
Used on b-52 aircraft. plate, cover al ALLOY2024-T3; heat treat per BAC5602; 0.063 x 1.50
01-544-2112
Structural Component Air Support
Used on mv-22 aircraft. navy: panel assembly, aircraft
01-544-2153
Structural Aircraft Plate
7.100" overall length 1.800" overall width 0.102" material thickness filler dim. are stock material
01-544-2157
Structural Component Air Support
Tee
01-544-2158
Structural Aircraft Plate
0.500" overall length 0.300" overall width 0.102" material thickness filler dim. are stock material
01-544-2167
Structural Aircraft Plate
01-544-2175
Structural Aircraft Plate
01-544-2190
Structural Aircraft Plate
01-544-2193
Structural Aircraft Plate
01-544-2209
Aircraft Channel
3.000" overall length channel splice
01-544-2221
Structural Aircraft Plate
1.100" overall width 0.093" material thickness laminated filler matrl BAC1524-94
01-544-2228
Structural Component Air Support
Brace tee
01-544-2229
Structural Component Air Support
Brace tee
01-544-2231
Structural Component Aircraf Web
Bonded web
01-544-2275
Structural Aircraft Plate
Used on KC-135. 2.000" overall length 1.000" overall width 0.064" material thickness filler radius heat treat T3
