01-206-9021
Access Aircraft Door
Used on t-37a acft. tunnel wall aft
01-206-9064
Aircraft Door
01-206-9102
Access Hole Frame
Used on c-130 acft. structure emergency depressurization door
01-206-9103
Access Hole Frame
Used on c-130 acft. structure emergency depressurization door
01-206-9131
Pylon Aircraft Fairing
Used on aircraft model sh-60b. cognizant service:navy;
01-206-9132
Aircraft Fairing
Nuclear hardness critical item; opposite pn -021; nha L3223771-012
01-206-9134
Structural Component Air Support
Used on c-5a acft. p/o: door assy, sliding-bunk compartment, flight station
01-206-9136
Structural Component Air Support
Used on acft model b-1b. al extr bar. alloy 2024-T8511; 0.8120 in. dia hole, cen; 7.608 in. lg, 2.220 in. w; 4.350 in. o/a h; opposite p/n -003; nha L3226828-002
01-206-9137
Structural Component Air Support
Used on acft model b-1b. al alloy 2024-T4; shape LS043-0791 by 26.40 in. lg; opposite p/n -009; nha L3203627-102
01-206-9138
Structural Component Air Support
Used on c-130 acft. aluminum alloy 2024-0 clad qq-a-362; 17.760 in. lg, 1.920 in. w, 1.160 in. h
01-206-9139
Structural Component Air Support
Used on c-130 acft. bulkhead, ramp, forward
01-206-9142
Aircraft Floor
Used on aircraft model sh-60b,lamps mark 3.
01-206-9144
Airfoil Rib
Used on aircraft model a-6.
01-206-9145
Aircraft Spar
68.000" overall length 5.400" overall width 0.051" material thickness
01-206-9846
Structural Component Air Support
Used on acft model b-1b. machined from al alloy extruded bar, alloy 2024-T8511; stock size 2.860 in. lg, 2.500 in. w, 2.000 in. thk; opposite p/n -003; nha L3226835-002
01-206-9847
Structural Component Air Support
Used on acft model b-1b. al alloy 2024-T4; shape LS043-0791 by 15.000 in. lg; finish 10AB01; opposite p/n -003; nha L3203627-202
01-207-0583
Structural Component Air Support
Consists of p/n 65C18770-619, p/n 65C18770-620
01-207-0994
Airframe Modification Kit
Used on ch-47d,helicopter.
01-207-1638
Access Aircraft Door
01-207-1639
Access Aircraft Door
01-207-1818
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d plate matl cres uns S17700 /17-7ph/ mil-s-25043; triangular shape; preformed cross section; w/ stud p/n 34003; w/o rivet holes; left hand appl
01-207-1819
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d plate matl cres uns S17700 /17-7ph/ mil-s-25043; triangular shape; preformed cross section; w/ stud p/n 34003; w/o rivet holes; right hand appl
01-207-1821
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.020 in. thk by 1.800 in. w by 15.000 in. lg, right hand bow ski shape; l cross section; w/o holes
01-207-1823
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T4; t
01-207-1824
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T3; 0.040 in. matl thk by 2.500 in. w by 8.000 in. lg; w/o rivet holes
01-207-1825
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T4; t
01-207-1826
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.063 in. matl thk by 6.000 in. w by 18.000 in. lg; bowed shape; u cross section; w/o rivet holes; right hand appl
01-207-1827
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7079 ams 4136; 0.156 in. matl thk; l cross section; prebent; w/o holes
01-207-1828
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7079 ams 4136; l cross section; prebent; 0.156 in. matl thk; w/o rivet holes
01-207-1835
Aircraft Floor
Used on 1520-859-2670. component qty 6; p/ns 205-030-279-41, 205-030-279-39, 205-030-279-37, 205-030-279-27, 205-030-279-21, 205-030-279-19, w/o rivet holes
01-207-1836
Aircraft Floor
Used on 1520-00-859-2670. component qty 6; 205-030-260-11, 205-030-260-1, 205-030-260-13, 204-031-322-69, 205-030-322-63; w/o attaching rivet holes
01-207-1837
Aircraft Floor
Used on 1520-00-859-2670. component qty 6; 205-030-260-3, 205-030-260-7, 205-030-260-5, 205-030-260-9, 205-030-260-13, 205-030-322-77; w/o attaching rivet holes
01-207-1840
Former
Used on 1520-00-859-2670. functional description:bulkhead assy left hand STA63.38; reference data
01-207-1841
Former
Used on 1520-00-859-2670. functional description:bulkhead section fuselage; reference data
01-207-1842
Vertical Stabilizer Rib
Used on 1520-00-859-2670. 9.700" overall length 7.000" overall width 0.020" material thickness modified u cross section; flanged aperature located in center member; w/o rivet holes; rectangular shaped
01-207-2047
Structural Aircraft Panel
Used on helicopter model sh-60b.
01-207-2513
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5; w/o rivet holes; made from p/n 205-030-186-001 nsn 1560-00-103-0035 cap beam
01-207-2514
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, T6; 0.094 in. matl thk; 1.000 in. w both legs; 13.000 in. o/a lg; l cross section; w/o rivet holes
01-207-2515
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11; l cross section; w/o rivet holes
01-207-2530
Aircraft Pylon
Used on 1520-00-859-2670. 5aluminum alloy; u cross section; w/stiffener, bearing plate
01-207-2531
Aircraft Pylon
Used on 1520-00-859-2670. aluminum alloy 2024 qq-a-250/5; 0.025 in.matl thk; 11.430 in.o/a lg; u cross section; w/bearing plate
01-207-2532
Aircraft Pylon
Used on 1520-00-859-2670. aluminum alloy 2024 qq-a-250/5; 0.025 in.matl thk; 11.430 in.o/a lg; u cross section, with bearing plate
01-207-3215
Structural Aircraft Plate
63.000" overall length 26.000" overall width 0.100" material thickness nha 16B565-803; eff on 5c 0001 9999
01-207-3216
Structural Aircraft Plate
63.000" overall length 26.000" overall width 0.100" material thickness aaaaa; nha-16B565-803; eff on-5c 0001 9999
01-207-3217
Structural Aircraft Plate
63.000" overall length 26.000" overall width 0.100" material thickness nha 16B565-801; eff 0n 6d 0009 9999
01-207-3218
Structural Aircraft Plate
Used on kc-135 aircraft.
01-207-3219
Structural Aircraft Plate
01-207-3220
Structural Aircraft Plate
Used on kc-135 aircraft.
01-207-3221
Structural Aircraft Plate
Used on kc-135 aircraft.
01-207-3222
Structural Aircraft Plate
Used on kc-135 aircraft.
