01-251-5161
Aircraft Trailing Edge
C/o t.e. assembly p/n 12W7925-951, rub strip p/n 12W7905-41, hinge assembly p/n 12W7949-5, support p/n 12W7948-9
01-251-5162
Aircraft Trailing Edge
C/o t.e. assembly p/n 12W7905-852, rub strip p/n 12W7905-41, hinge assembly p/n 12W7949-6, support p/n 12W7948-10
01-251-6550
Structural Component Air Support
Used on c-135 aircraft. support for aft engine ay
01-251-6551
Access Aircraft Door
01-251-6624
Structural Aircraft Plate
01-251-6813
Structural Aircraft Plate
Used on acft,model f18. left hand side brace assy
01-251-7114
Access Aircraft Door
Used on aircraft model f-18.
01-251-7218
Fuselage Aircraft Fairing
Used on aircraft model f-18. aluminum alloy per qq-a-250/13, cond o;
01-251-7219
Fuselage Aircraft Fairing
Used on aircraft model f-18. aluminum alloy per qq-a-250/13, cond o;
01-251-7226
Movable Canopy
Used on aircraft model av-8.
01-251-7230
Aircraft Leading Edge
Used on aircraft model e-2c.
01-251-7231
Aircraft Leading Edge
Used on e2c special electronic aircraft.
01-251-7232
Airfoil Rib
Used on acft model c-2/e-2.
01-251-7233
Airfoil Rib
Used on acft model c-2/e-2.
01-251-7872
Metal Molding
Color orange yellow no. 13538 fed std 595
01-251-8447
Structural Aircraft Plate
Used on acft model e-3a. fansteel 77, cadmium plate per qq-p-416 type ii; 9.5 in. lg, 1.1 in. wd, 0.20 in. thk; nha 65-5347
01-251-8448
Structural Aircraft Plate
Used on acft model e-3a. 1020 or 1025 steel plate per qq-s-698 per mil-s-18/29; stock 24.2 in. lg, 3.0 in. wd, 0.87 in. thk
01-251-8469
Aircraft Former
Used on F-15.
01-251-8471
Aircraft Skin
Used on b-52 bomber airplane.... 70.000" overall length 30.000" overall width opppsite p/n -208, finish f-10.10
01-251-8473
Aircraft Skin
90.000" overall length oppsite p/n -211, finish f-10.10
01-251-9297
Access Aircraft Door
Used on ea-6b aircraft. color yellow primer zinc chromate surface treated
01-251-9405
Structural Component Air Support
Primer epoxy-polyamide surface treated
01-252-0363
Structural Component Air Support
Used on 1520-01-088-3669 heilcopter,cargo-transport. material metallic; o/a lg 2.930 in., with round base plate on one end, base plate has 3 ea mounting holes evenly spaced, id 0.190 in.
01-252-0377
Structural Aircraft Plate
Used on uh-60a helicopter. aluminum alloy, qq-a-250/5, comp 2024-T3
01-252-0378
Structural Aircraft Plate
Used on uh-60a helicopter. aluminum alloy, qq-a-250/5, c/o component quantity, 1
01-252-1098
Structural Aircraft Panel
Used on c-5a/b aircraft. panel assembly-keel beam closure, mlg fairing; nha 4F75001; opposite -104d
01-252-1100
Structural Aircraft Panel
Used on acft model e-3a. located at sta. 259-5 to 302
01-252-1101
Structural Aircraft Panel
Used on acft model e-3a. located at 259.5 to 302
01-252-1102
Structural Aircraft Panel
Used on acft model e-3a. located on sta. 259.5 to 302
01-252-1103
Structural Aircraft Panel
Consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upr doubler, 1 doubler; nha 65-3495; opposite p/n -2
01-252-1104
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upr doubler, 2 doubler, 1 bonded panel assy, 1 door; opposite p/n -1; nha 65-3495; located on sta.30.31
01-252-1105
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upr doubler, 1 skin assy, 1 doubler, 1 access door; opposite p/n -1; finish srf-12.915; nha 65-3495; located on station 30.31 to 48.67
01-252-1471
Structural Component Air Support
Used on c-5b aircraft. 6.420" overall length 1.685" overall width chromate surface treated
01-252-1472
Structural Component Air Support
Used on e-3a aircraft.
01-252-3394
Structural Aircraft Plate
Used on F-15.
01-252-3395
Structural Aircraft Plate
Used on F-15.
01-252-3396
Structural Aircraft Plate
Used on F-15.
01-252-3397
Structural Aircraft Plate
Used on F-15.
01-252-3398
Structural Aircraft Plate
Used on F-15.
01-252-3399
Structural Aircraft Plate
Used on F-15. 1MA160B04-10333 x 22.10 in.; opposite -2031
01-252-3400
Structural Aircraft Plate
7.450" overall length 4.150" overall width 0.032" material thickness opp -2025; made from -2004
01-252-3401
Aircraft Fairing
9.000" overall length 5.000" overall width 0.080" material thickness nha 16W048-2
01-252-3403
Structural Component Air Support
Used on f-15 acft. tee u/o fuselage section, upper panel fuselage station 712.310 to 749.000
01-252-3404
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9047 type 3 comp a annealed; u/o keel, web fuselage station 712.310 to 730.350
01-252-3408
Structural Aircraft Panel
Consist of 2 skin; same as -2035; nha 68A324000
01-252-3419
Aircraft Former
Used on F-15.
01-252-3420
Fuselage Section
01-252-3421
Fuselage Section
01-252-3422
Fuselage Section
