01-579-2280
Structural Component Air Support
Used on APU. apu support strut
01-579-2291
Structural Component Air Support
Used on APU. apu support strut assembly
01-579-2301
Structural Component Air Support
Used on APU. apu support strut assembly
01-579-2310
Structural Component Air Support
Fairing flap support installation components
01-579-2311
Radome Panel
Used on 77 foot radome398-08. 72.120" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 77.500"; fiberglass material is sandwiched around a resin core
01-579-2347
Structural Aircraft Plate
Used on 1520-01-355-8250. 5.750" overall length 3.720" overall width front panel assembly
01-579-2367
Radome Panel
Used on 77 foot radome398-08. 80.800" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 82.000"; fiberglass material is sandwiched around a resin core
01-579-2370
Radome Panel
Used on 77 foot radome398-08. 77.750" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 80.800"; fiberglass material is sandwiched around a resin core
01-579-2426
Wing Landing Flap
Used on f-22 raptor.
01-579-2427
Structural Aircraft Plate
Used on f-22 raptor.
01-579-2429
Access Aircraft Door
Used on c-17 acft.
01-579-2430
Structural Aircraft Plate
Used on f-22 raptor.
01-579-2433
Structural Aircraft Panel
Used on f-22 raptor. nha 5HW83030; left
01-579-2435
Structural Aircraft Panel
Used on f-22 raptor. NHA5HW83032; right
01-579-2436
Wing Landing Flap
Used on f-22 raptor.
01-579-2442
Structural Aircraft Panel
Used on REAPER. bottom closeout, pylon
01-579-2642
Structural Component Air Support
Used on B-52. 7.700" overall length 2.100" overall width 0.050" material thickness 26-3161-2 opposite; clad sheet, t-3
01-579-2643
Stiffener Aircraft Rib
Used on f-22 raptor. 8.000" overall length 4.000" overall width 3.750" material thickness 6-2222 cond f titanium 3.750 plate
01-579-2659
Structural Aircraft Panel
01-579-2665
Structural Aircraft Panel
Used on V-22.
01-579-2689
Inner Wing Section
01-579-2704
Inner Wing Section
01-579-2707
Radome Panel
Used on 77 foot radome398-08. 82.180" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 81.000"; fiberglass material is sandwiched around a resin core
01-579-2708
Radome Panel
Used on 77 foot radome398-08. 81.000" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 77.600"; fiberglass material is sandwiched around a resin core
01-579-2710
Radome Panel
Used on 77 foot radome398-08. 77.500" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 72.250"; fiberglass material is sandwiched around a resin core
01-579-2717
Radome Panel
Used on 77 foot radome398-08. 72.250" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 65.000"; fiberglass material is sandwiched around a resin core
01-579-2721
Structural Component Air Support
Fan cowl hold open rod temp range: -65 to 250 deg f
01-579-2722
Radome Panel
Used on 77 foot radome398-08. 65.000" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 56.000"; fiberglass material is sandwiched around a resin core
01-579-2728
Radome Panel
Used on 77 foot radome398-08. 56.000" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 45.250"; fiberglass material is sandwiched around a resin core
01-579-2730
Radome Panel
Used on 77 foot radome398-08. 45.370" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 33.620"; fiberglass material is sandwiched around a resin core
01-579-2736
Radome Panel
Used on 77 foot radome398-08. 65.250" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 40.500"; fiberglass material is sandwiched around a resin core
01-579-2740
Aircraft Door
Used on CH-47.
01-579-2742
Structural Component Air Support
Used on CH-47.
01-579-2745
Radome Panel
Used on 77 foot radome398-08. 77.620" overall length 78.000" overall width radome panel 398-01/rosas top of panel measures 26.500"; fiberglass material is sandwiched around a resin core
01-579-2767
Radome Panel
Used on 77 foot radome398-08. radome panel cap 398-01/rosas featgfiberglass_material_is_sandwiched_around_a_resin_core_and_then_gel_coated_ (2_skins-core-2 skins) ; yellow green in color
01-579-2774
Radome Panel
Special combination panel consisting of the aa
01-579-2782
Structural Component Air Support
Used on CH-47.
01-579-2788
Radome Panel
Used on 77 foot radome398-08. radome door 398-01/rosas door panel; fiberglass material is sandwiched around a resin core
01-579-2789
Structural Component Air Support
Used on CH-47.
01-579-2790
Aircraft Bulkhead
Used on KC-135. 8.000" overall length 5.000" overall width 0.040" material thickness bulkhead finish srf-2.115; heat treat T4; clad-0 sht; dim. are stocksize matl
01-579-2791
Structural Component Air Support
Used on CH-47.
01-579-2812
Access Aircraft Cover
Used on ef-18a aircraft.
01-579-2818
Structural Aircraft Plate
01-579-2819
Structural Aircraft Panel
Used on CH-47.
01-579-2824
Structural Component Air Support
Used on CH-47.
01-579-2866
Structural Aircraft Plate
Used on 1520-01-355-8250. ecu blank assembly
01-579-2922
Radome Cover
Protective radome boot abrasion, erosion, scratch, puncture, moisture
01-579-2940
Radome Cover
Used on embraer 145-32391-401. abrasion, erosion, scratch, puncture, moisture
01-579-2992
Aileron
Used on f-22 raptor.
01-579-2993
Aileron
Used on f-22 raptor.
