01-110-6508
Structural Aircraft Plate
5.300" overall length 0.900" overall width 0.050" material thickness finish f-8.07; heat treat 130ksi
01-110-6509
Structural Aircraft Plate
3.300" overall length 1.400" overall width 0.050" material thickness finish f-2.30
01-110-6510
Structural Aircraft Plate
70.000" overall length 57.000" overall width 0.040" material thickness heat treat T62; finish f-8.05
01-110-6511
Structural Aircraft Plate
70.000" overall length 57.000" overall width 0.040" material thickness heat treat T62; finish f-8.05
01-110-6512
Structural Aircraft Plate
70.000" overall length 65.000" overall width 0.040" material thickness finish f-8.05; heat treat T62
01-110-6515
Longeron
54.500" overall length 4.200" overall width 0.050" material thickness heat treat to 130ksi (min) per bac 5619; finish f-8.07
01-110-6516
Longeron
74.500" overall length 3.700" overall width 0.050" material thickness heat treat T62; finish srf-2.30
01-110-6518
Aircraft Skin
70.000" overall length 57.000" overall width cond 0; finish F8.05
01-110-6519
Aircraft Skin
70.000" overall length 65.000" overall width cond 0; finish F8.05
01-110-6520
Aircraft Skin
70.000" overall length 57.000" overall width cond 0; finish F8.05
01-110-6521
Aircraft Skin
70.000" overall length 65.000" overall width C0nd 0; finish F8.05
01-110-6523
Aircraft Skin
Used on F-111.
01-110-6524
Aircraft Spar
76.190" overall length
01-110-8042
Aircraft Frame
Nacelle aft inlet section
01-110-8072
Aircraft Fairing
01-110-8073
Aircraft Fairing
01-110-8091
Structural Aircraft Plate
70.000" overall length 65.000" overall width 0.040" material thickness heat treat T62; finish f-8.05
01-110-8099
Aircraft Skin
01-110-8100
Aircraft Skin
Used on a-10 airplane.. 70.000" overall length 24.000" overall width matt; clad sheet
01-110-8101
Aircraft Skin
Used on a-10 airplane.. 70.000" overall length 24.000" overall width matt; clad sheet
01-110-8103
Aircraft Skin
Used on a-10 airplane.. 48.000" overall length 12.000" overall width matt; clad sheet
01-110-8981
Thermal Special Purpo Insulation
End item identification:aircraft, model F4c
01-110-9428
Structural Component Air Support
Used on c-5a acft. matl al casting, A356-T61; 3.750 in. lg; 2.000 in., w; 1.500 in. h; opposite to p/n 4F37124-991a; used on step, upper, crew entry door
01-110-9429
Structural Component Air Support
Used on c-5a acft. matl al casting, A356-T61; 3.750 in. lg; 2.000 in. w; 1.500 in. h; used on step, upper, crew entry door; opposite to p/n 4F73124-992a
01-110-9702
Structural Component Air Support
01-111-1568
Structural Component Air Fitting
01-111-1961
Structural Component Air Support
C/o 1 support, 1 pad, rivets a/r
01-111-2037
Structural Aircraft Plate
Used on f-5 acft.
01-111-2041
Structural Component Air Support
Used on acft model f111. material per fms-0131, 6.000 in. lg, 3.000 in. w, 1.75 in. thk, used on pave tack cradle
01-111-2042
Structural Component Air Support
Used on acft model f111. material per fms-0131, 6.000 in. lg, 3.000 in. w, 1.750 in. thk, used on pave tack cradle
01-111-2046
Aircraft Former
33.020" overall length opposite p/n 4034583-1
01-111-2047
Aircraft Former
10.900" overall length three holes, 0193 in. dia.
01-111-2057
Airfoil Rib
3.370" overall length 2.600" overall width 0.020" material thickness
01-111-2058
Airfoil Rib
6.330" overall length opposite pn 4034534-3
01-111-2059
Airfoil Rib
5.360" overall length opposite pn 4034535-2
01-111-2060
Airfoil Rib
4.600" overall length 2.500" overall width 0.025" material thickness
01-111-2062
Airfoil Rib
15.000" overall length 5.000" overall width 0.032" material thickness
01-111-2063
Airfoil Rib
7.000" overall length 5.500" overall width 0.063" material thickness part of balance weight attachment, elevator
01-111-2064
Aircraft Skin
Used on F-111.
01-111-2065
Aircraft Spar
76.190" overall length heat treat T42; opposite 4023800-3
01-111-3003
Access Aircraft Door
Used on acft e3a. inflight refueling; finish f-14.9865-707 on exterior surface only
01-111-3004
Access Aircraft Door
Used on acft e3a. inflight refueling; finish f-14.9865-707 on exterior surface only
01-111-3021
Aircraft Former
8.000" overall length 5.700" overall width 0.025" material thickness
01-111-3024
Exhaust Pipe
N8.810 in. lg; 1.510-1.535 in. dia; 0.035 in. wall thk; tube material steel, cres cmpsn 321 or 347, spec mil-t-8606 or steel, cres, spec mil-t-8808; weld in accordance w/class 3 mil-std-126; braze in accordance w/mil-b-7883
01-111-3025
Airfoil Rib
10.500" overall length 8.300" overall width 0.050" material thickness
01-111-3775
Exhaust Pipe
13.750 in. lg; 1.510-1.535 in.dia; tubing, cres, cmpsn 321 or 347 mil-t-8606 or steel, cres mil-t-8808; 1.500 in. od; 0.035 in. wall thk; weld mil-std-1261; braze mil-b-7883
01-111-4412
Aircraft Fairing
Used on C-141.
01-111-4617
Access Aircraft Cover
01-111-6067
Aircraft Floor
Used on ch-53 super jolly helicopter....
