01-200-0041
Structural Component Air Support
Used on acft model c-18a. used with 66-13301-3; used on 65-18421-15; optional to 69-15480-6
01-200-0043
Structural Component Air Support
Used on acft model f-111t. die forging D6ac steel per fms-1011; forge per fps-1041
01-200-0044
Structural Component Air Support
01-200-0047
Structural Aircraft Panel
Used on c-5b aircraft. located fs 1353 to 1383 & fs 1573 to 1603; c/o: -107a doubler (1) , -117a angle (1) , -123a panel (1) , safety strip instl (1) ; opposite -130a
01-200-0048
Structural Aircraft Panel
Used on c-5b aircraft. located fs 1353 to 1383 & fs 1573 to 1603; c/o: -107a doubler (1) , -118a angle (1) , -124a panel (1) , safety strip (1) ; opposite -129a
01-200-0050
Structural Aircraft Panel
Used on c-130 acft. floor; fuselage station 196.0 to 228.66; water line 146.0
01-200-0062
Aircraft Former
Used on aircraft c-18a.
01-200-0063
Aircraft Former
16.600" overall length 2.800" overall width 0.032" material thickness
01-200-0065
Aircraft Former
37.000" overall length 4.000" overall width 3.400" material thickness PO23-1l; finish A028; nha 12T9212-1
01-200-0075
Aircraft Skin
Used on C-141.
01-200-0076
Aircraft Skin
Used on C-141.
01-200-0078
Aircraft Skin
Used on C-141.
01-200-0080
Aircraft Skin
Used on c-141 acft. no. 4 upper surface outer wing
01-200-0082
Aircraft Skin
Used on C-141.
01-200-0083
Aircraft Skin
Used on C-141. no. 5 upper surface; outer wing
01-200-0084
Aircraft Skin
Used on C-130.
01-200-0085
Aircraft Skin
Used on C-130.
01-200-2382
Structural Aircraft Plate
Nha 65-1348-53
01-200-2383
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7944-92; used as forward cargo door angle retainer
01-200-2384
Structural Component Air Support
01-200-3521
Structural Component Air Support
Used on acft model kc-135. consists of 1 fitting, 4 bushing
01-200-3522
Structural Component Air Support
Used on acft model kc-135. consists of 1 fitting, 4 bushing; nha 65C18235
01-200-3523
Structural Component Air Support
Used on acft model kc-135. consists of 1 fitting, 4 bushing; nha 65C18235
01-200-3524
Structural Component Air Support
Used on acft model kc-135. 15-5ph forged block per AMS5659; heat treat 150-170 ksi per BAC5619; finish f-8.07; nha 65C18248; stationed at 223.50
01-200-3531
Aircraft Former
01-200-3532
Aircraft Former
Used on acft model kc-135.
01-200-4518
Aircraft Pylon
Used on aircraft model f-18. cognizant service:navy;
01-200-4519
Aircraft Pylon
Used on aircraft model f-18. cognizant service:navy;
01-200-5441
Structural Aircraft Plate
Nha 5-84477-3058
01-200-5446
Structural Aircraft Panel
C/o: -105a core (1) , -111a face sheet (2) , -113a trim (1) ; nha 4E22048
01-200-5447
Structural Aircraft Panel
Used on c-5b aircraft. dnha 4E23002; consist of two splice, p/n 4E23200-107a & 4E23200-119a, two panel p/n 4E23200-115a & p/n 4E23200-117a, twelve pad, one edge, twenty-five insert, sixteen screw, thirty-two washer, sixteen nuts
01-200-5448
Structural Aircraft Panel
Used on c-5b aircraft. consist of one panel, p/n 4E23216-109a; seven insert; six pad; nha 4E23227
01-200-5449
Structural Aircraft Panel
Used on c-5b aircraft. consist of one core, -103a; one edge member, -107a, one face sheet, -109a; two doublers, -111a; one angle; eight pads; two nuts; five insert; nha 4E23227
01-200-5450
Structural Aircraft Panel
Used on c-5b aircraft. material fiberglass prepreg per stm 22-401, form ii, class i; nha 4E32261
01-200-6452
Aircraft Fairing
01-200-6508
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -107a panel assembly (1) , insert (27) ; nha 4E32302, eff on 0082 & up
01-200-6509
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -125a panel assembly (1) , insert (15) ; nha 4E32302, eff on 0082 & up
01-200-6510
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a edging (2) , -107a strap (1) , -109a strap (2) , insert (70) ; nha 4E32302, eff on 0082 & up
01-200-6511
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a edging (1) , -107a strap (1) , -109a strap (1) , -111a strap (1) , -113a strap (1) , insert (45) ; nha 4E32302, eff on 0082 & up; opposite -102a
01-200-6512
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a edging (1) , -107a strap (1) , -109a strap (1) , -111a strap (1) , -113a strap (1) , insert (45) ; nha 4E32302, eff on 0082 & up; opposite -101a
01-200-6513
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a edging (2) , -107a strap (4) , -109a strap (2) , -111a strap (1) , -113a strap (2) , -115a strap (1) , insert (131) ; nha 4E32302, eff on 0082 & up
01-200-6514
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a strap (1) , -107a strap (2) , -109a strap (1) , -111a strap (1) , insert (46) ; nha 4E32302
01-200-6515
Structural Aircraft Panel
Used on c-5b aircraft. consist of one panel, -103a; sixteen nut plates; nha 4E32261
01-200-6516
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a frame (1) , insert (26) ; nha 4E32302, eff on 0082 & up
01-200-6517
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a cover (1) size .062X21.0X72.0in, nut (36) ; nha 4E32302, eff on 0082 & up
01-200-6518
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel (1) , -105a support (1) , nut plate (1) ; nha 4E32281
01-200-6519
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -105a seal (1) , -107a plate (1) , -111a angle (1) , -117a seal (1) , nut (6) , -103e channel (1) , -119a seal (1) , -121a seal (1) , -123a seal (1)
01-200-6529
Aircraft Pylon
01-200-7168
Aircraft Skin
38.500" overall length 35.000" overall width opposite p/n -802
01-200-8571
Access Aircraft Door
Used on acft model b-1b. opposite p/n -042; nha L3206634-201; used as lower nacelle hydraulic access door assembly
