00-224-3686
Fuselage Section
Glass fabric per 299-947-057, type c, fscm 97499, and aluminum honeycomb per 299-947-053 type 2 fscm 97499
00-224-3827
Structural Aircraft Panel
00-224-3897
Radome
9.900" iii overall length
00-224-3923
Radome
5.430" overall length
00-224-4150
Aircraft Door
0.125" overall width
00-224-4154
Aircraft Door
00-224-4155
Aircraft Door
00-224-4540
Access Aircraft Cover
0.158" hole diameter
00-224-4541
Access Aircraft Cover
00-224-4557
Structural Component Air Support
Used on acft model h53. c/o support 1 ea p/n 65375-04108-101, retainer 1 ea p/n 65375-04109-102, nut 2 ea p/n ms 21042-5, washer 4 ea p/n ms 20002-5, bolt 2 ea p/n AN5c-15a, left hand
00-224-4558
Structural Component Air Support
Used on acft model h53. c/o support 1 ea p/n 65375-04107-101, retainer 1 ea p/n 65375-04109-101, washer 4 ea p/n ms 20002-5, nut 2 ea p/n ms 21042-5, bolt 1 ea p/n AN5c-15a, bolt 1 ea p/n AN5c-16a, right hand
00-224-5346
Access Aircraft Cover
Anodize surface treated
00-224-6342
Access Aircraft Door
00-225-0808
Aircraft Windshield Panel
Component parts:panel, 4-13023-3, frames, 4-13023-5, 4-13023-6, 4-13023-7, 4-13023-9, seals, 2-13019-1, 2-13019-3, 2-13019-9;
00-225-0813
Access Aircraft Cover
Used on f-5a/b aircraft.
00-225-0814
Access Aircraft Cover
00-225-0815
Access Aircraft Cover
00-225-0817
Access Aircraft Cover
00-225-0871
Aircraft Window Panel
14.323" overall length 12.682" overall width
00-225-0872
Aircraft Window Panel
Glass, 14.323 in. o/a lg, 12.276 in. o/a w, 0.300 in. thk
00-225-0940
Structural Component Air Support
Used on acft model kc135. steel 4340 per mil-s-5000, annealed heat treat to 180-200 ksi per bac 5617, 0.310 in.thk, 2.180 in.o/d, 1.380 in.bolt circle dia, 4 holes equally spaced 0.250 in.dia, left hand
00-225-0941
Structural Component Air Support
Used on acft model kc135. steel 4340 per mil-s-5000, annealed heat treat to 180-200 ksi per bac 5617, 0.310 in.thk, 2.900 in.od, 2.150 in.bolt circle dia, 4 holes equally spaced 0.380 in.dia
00-225-1012
Radome
3.318 feet overall length 2.714 feet overall width
00-225-1042
Bleed Air Duct Assembly
Used on c-141 aircraft. cres, mil-s-6721
00-225-1043
Bleed Air Duct Assembly
Used on acft model c141. 45.000" overall length used on engine air, outboard pylon cross over
00-225-1067
Bleed Air Duct Assembly
Used on c-141 acft. cres, mil-s-8840
00-225-1068
Bleed Air Duct Assembly
Used on C141.
00-225-1069
Aircraft Fairing
00-225-1757
Structural Component Air Fitting
00-225-1770
Structural Aircraft Panel
C/o core is stm 28-102 type i.o/a dim. outer skin is 0.012 by 21.000 BY94.000 in., inner skin is 0.012 BY18.000by 91.000in.
00-225-1771
Structural Aircraft Panel
00-225-1772
Structural Aircraft Panel
00-225-1905
Structural Component Air Support
00-225-3496
Aircraft Fairing
00-225-3543
Structural Component Air Support
Used on acft model f4. matl code 356-T6 per mms-132 sc, 1.920 in.h, 1.700 in.w, 2.720 in.lg, right hand, used on t.e. flap inner wing
00-225-3943
Structural Component Air Support
Used on acft model c5. al alloy 356-T6 per ams 4260, used on post, ladder emergency egress number 1
00-225-3953
Structural Component Air Support
Used on acft model c5. 5.780" overall length 2.000" overall width
00-225-4039
Access Aircraft Door
00-225-4091
Structural Component Air Support
Used on acft model c5. c/o support bearing 1 ea p/n 4J33183-103a, bushing flanged 1 ea p/n 4J33179-101b, used on upper flap number 4, 5
00-225-4382
Aircraft Fairing
00-225-4388
Aircraft Fairing
00-225-4391
Aircraft Fairing
00-225-4392
Aircraft Fairing
00-225-4455
Aircraft Former
Used on aircraft,galaxy c-5. 43.000" overall length
00-225-4503
Structural Component Air Support
Used on acft model c-5. 63.760" overall length 0.820" overall width
00-225-4663
Access Aircraft Door
00-225-5488
Structural Component Air Support
Aluminum alloy
00-225-5503
Structural Aircraft Panel
Aluminum 7075-T6, qq-a-250/13
00-225-5504
Structural Aircraft Panel
Aluminum 7075-T6, qq-a-250/12
