01-338-9087
Aircraft Slat
01-338-9088
Aircraft Slat
01-338-9089
Aircraft Slat
01-338-9092
Structural Component Air Support
Opposite dash no. 505
01-338-9093
Structural Component Air Support
Enamel surface treated
01-338-9094
Structural Component Air Support
Enamel surface treated
01-338-9095
Structural Component Air Support
5.000" overall length 3.500" overall width opposite dash no. 1
01-338-9096
Structural Component Air Support
5.000" overall length 3.500" overall width
01-338-9097
Structural Component Air Support
6.000" overall length 6.000" overall width 0.032" material thickness
01-338-9492
Access Aircraft Door
Iff system access
01-338-9560
Structural Aircraft Plate
9.500" overall length 7.250" overall width 0.020" material thickness
01-338-9561
Aircraft Spar
Used on aircraft model sh-60. anodize surface treated
01-338-9562
Aircraft Spar
Used on aircraft model sh-60. anodize surface treated
01-338-9563
Aircraft Stiffener
18.750" overall length 4.000" overall width
01-338-9569
Aircraft Fairing
01-338-9571
Cowling
Used on aircraft model h-3.
01-338-9572
Cowling
Used on aircraft model h-3.
01-338-9573
Cowling
Used on aircraft model h-3.
01-338-9574
Structural Aircraft Panel
Used on a-6e acft.
01-338-9577
Structural Aircraft Panel
Silicon carbide tile; glass spalling; spectra backing
01-338-9578
Structural Aircraft Panel
Silicon carbide tile; glass spalling; spectra backing
01-338-9579
Structural Aircraft Panel
Silicon carbide tile; glass spalling; spectra backing
01-338-9580
Structural Aircraft Panel
Silicon carbide tile; glass spalling; spectra backing
01-338-9581
Aircraft Skin
36.000" overall length 24.000" overall width
01-338-9582
Aircraft Skin
01-338-9583
Aircraft Windshield Panel
Used on 1560-01-054-9512 windshield panel s-3a/b acft. 60313 clear chemcor chemically strengthened, modulus of rupture 16000 psi min., central tension 6500 psi max. 4000 psi min., case depth 0.017 min., anti-static coating, surface resistivity 1k-25 meg ohms per sq., face ply 0.105 in. x 41.0 xn. x 41.0 in. oxide surface treated
01-338-9584
Aircraft Windshield Panel
Used on 1560-01-054-9512 windshield panel s-3a/b acft. 60313 clear chemcor chemically strengthened, modulus of rupture 16000 psi min., central tension 6500 psi max. 4000 psi min., case depth 0.017 min., anti-static coating, surface resistivity 1k-25 meg ohms per sq., face ply 0.105 in. x 41.0 in. x 41.0 in. oxide surface treated
01-338-9585
Structural Component Air Support
Used on non-jsl item,helicopter h1.
01-338-9587
Structural Component Air Support
14.625" overall length 0.906" overall width
01-338-9588
Structural Component Air Support
01-338-9589
Structural Component Air Support
01-338-9590
Structural Component Air Bracket
1.750" overall length 1.750" overall width
01-338-9596
Structural Component Air Fitting
Used on aircraft model a-6b.
01-338-9597
Structural Component Air Fitting
Used on aircraft model a-6b.
01-338-9598
Structural Component Air Fitting
Used on aircraft model f-14.
01-339-0327
Access Aircraft Door
Used on f-16 acft. access-fuel strainer, r-h; fuselage sta 392.68, butt line 16.3
01-339-0328
Access Aircraft Door
Used on f-16 acft. access-fuel strainer, r-h; fuselage sta 392.08
01-339-0381
Structural Aircraft Plate
14.000" overall length
01-339-0382
Structural Aircraft Panel
01-339-0383
Structural Component Air Bracket
01-339-0436
Structural Aircraft Panel
14.000" overall length 14.000" overall width ventral fin core
01-339-1174
Structural Component Air Bracket
01-339-1209
Structural Component Air Support
6.000" overall length
01-339-2130
Access Aircraft Cover
Used on f-16 acft. 6.227" outside diameter access-wing upper surface; included additional 3.000 in. dia bolt hole circle w/ 6 holes anodize surface treated
01-339-2131
Access Aircraft Cover
Used on f-16 acft. 4.434" outside diameter access-wing, upper surface anodize surface treated
01-339-2132
Access Aircraft Cover
Used on f-16 acft. 0.250" hole diameter 4.077" outside diameter access-wing, upper surface anodize surface treated
01-339-2133
Access Aircraft Cover
Used on f-16 acft. 6.257" outside diameter access-wing, upper surface; includes additional 3.000 in. dia bolt hole circle w/ 6 holes anodize surface treated
01-339-2134
Access Aircraft Cover
Used on f-16 acft. 4.407" outside diameter access-wing, upper surface anodize surface treated
01-339-2183
Aircraft Fairing
C/o 13 frame instl, 1 beam, 1 lwr skin instl, 2 upp skin instl, 2 stiffener, 2 trailing edge instl, 1 channel instl, 3 skin assembly, 1 fitting, misc hardware; hci component, critical application
01-339-2184
Aircraft Fairing
