01-161-0564
Structural Component Air Support
Used on acft model kc-135r. al alloy clad 2024-0 per qq-a-250/5; heat treated to cond T42; 6.300 in. lg, 3.800 in. w, 0.080 in. thk; opposite p/n -8; located nacelle station 213.88; nha 458-58075-4
01-161-0565
Structural Component Air Support
Used on acft model kc-135r. al alloy clad 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 6.300 in. lg, 3.800 in. w, 0.080 in. thk; opposite p/n -7; located nacelle station 213.88; nha 458-58075-4
01-161-0566
Structural Component Air Support
Used on acft model kc-135r. al alloy clad 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 7.000 in. lg, 4.000 in. w, 0.080 in. thk; opposite p/n -8; nha 458-58067-4
01-161-0567
Structural Component Air Support
Used on acft model kc-135r. al alloy clad 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 7.000 in. lg, 4.000 in. w, 0.080 in. thk; opposite p/n -7; nha 458-58067-4
01-161-0568
Structural Component Air Support
4.500" overall length 3.400" overall width 2.800" material thickness used on inboard/outboard forward engine mount
01-161-0569
Structural Component Air Support
4.500" overall length 3.400" overall width 2.800" material thickness used on inboard/outboard forward engine mount
01-161-0570
Structural Component Air Support
4.000" overall length 3.700" overall width 2.200" material thickness used on inboard/outboard forward engine mount
01-161-0571
Structural Component Air Support
4.000" overall length 3.700" overall width 2.200" material thickness used on inboard/outboard forward engine mount
01-161-0585
Aircraft Former
2.500" overall length nha 458-58067-4
01-161-0586
Aircraft Former
12.400" overall length 4.200" overall width 0.050" material thickness
01-161-0587
Aircraft Former
12.400" overall length 4.200" overall width 0.050" material thickness
01-161-0588
Aircraft Former
Used on acft model b52.
01-161-0589
Aircraft Former
1.500" overall length make froma BAC1505-100155
01-161-0590
Aircraft Former
1.500" overall length make from BAC1505-100155
01-161-0591
Aircraft Former
1.800" overall length make from BAC1514-1312
01-161-0592
Aircraft Former
1.800" overall length make from BAC1514-1312
01-161-1089
Aircraft Fairing
Form, fit, function
01-161-1102
Structural Aircraft Plate
9.500" overall length 7.400" overall width 0.050" material thickness
01-161-1105
Structural Aircraft Plate
4.500" overall length 2.800" overall width 0.220" material thickness
01-161-1106
Structural Aircraft Plate
4.500" overall length 2.800" overall width 0.220" material thickness
01-161-1107
Structural Aircraft Plate
14.200" overall length 2.900" overall width 0.250" material thickness
01-161-1110
Structural Aircraft Plate
12.480" overall length 3.000" overall width includes spring
01-161-1112
Structural Component Air Support
Used on acft model kc-135r. al alloy extruded 2024-T3511 per qq-a-200/3; finish f-2.03; AND10134-1407 x 4.900 in. lg; located nacelle station 224.465; nha 458-58077-2
01-161-1113
Structural Component Air Support
Used on acft model kc-135r. al alloy clad sheet 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 6.300 in. lg, 3.800 in. w, 0.080 in. thk; located nacelle sta. 224.465; opposite p/n-8; nha 458-58077-4
01-161-1114
Structural Component Air Support
Used on acft model kc-135r. al alloy extrusion 7075-0 per qq-a-200/11; heat treated to cond T73; finish f-12.37; stock BAC1514-2750; 33.380 in. contour radius, 85.430 in. contour lg; opposite p/n -3; nha 458-58042
01-161-1117
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-601 comp 3; 1.970 in. lg; 0.158 dia tap drill 100 deg csk by 0.220 in. dia, tap 10-32 nf-3b; used as fitting, rod end on upper emergency door, fuselage station 1074.75
01-161-1531
Access Aircraft Cover
Used on c-130 aircraft. has deflector at fs 196.00
01-161-1617
Aircraft Beam
01-161-1630
Structural Aircraft Plate
Used on B-52. make from BAC1513-68 x 2.900 in.
01-161-1631
Structural Aircraft Plate
Used on B-52. make from BAC1513-13 x 2.400 in.
01-161-1632
Structural Aircraft Plate
1.000" overall length 0.700" overall width 0.040" material thickness
01-161-1633
Structural Aircraft Plate
2.660" overall length 1.660" overall width 0.250" material thickness used as spacer; finished dim. 2.66 x 1.81 x 2.66 x 1.66-4 sides; 2 holedia. .594 &.406 in dia
01-161-1634
Structural Aircraft Plate
2.640" overall length 1.330" overall width 0.250" material thickness used as spacer; finished dim. 4 sides 2.36 x 1.33 x 2.64 x 1.05 in.; 2 hole dia. .594 in.
01-161-1636
Structural Component Air Support
Used on C-130.
01-161-1637
Structural Component Air Support
Used on c-130e aircraft. used as strut, main landing gear fairing, left hand
01-161-1641
Aircraft Former
Opposite -1; nha 458-58066
01-161-1642
Aircraft Former
7.100" overall length 3.000" overall width 0.080" material thickness
01-161-1643
Aircraft Former
7.100" overall length 3.000" overall width 0.080" material thickness
01-161-1644
Aircraft Former
1.500" overall length make from BAC1506-902
01-161-1645
Aircraft Former
1.500" overall length make from BAC1506-902
01-161-1646
Aircraft Former
1.800" overall length make from BAC1505-24231
01-161-1647
Aircraft Former
1.800" overall length make from BAC1505-24231
01-161-1648
Aircraft Former
1.700" overall length make from BAC1505-35050
01-161-1649
Aircraft Former
1.700" overall length make from BAC1505-35050
01-161-2062
Structural Aircraft Panel
C/o 1 honeycomb panel assy, 1 aft panel assy, 1 forward mid fireshield, 1 aft fireshield, 2 spacers, 1 splice strap, 1 angle, 1 strap, 204 rivets; featgnya 458-58023; opposite -1
01-161-2064
Structural Aircraft Panel
C/o 1 honeycomb panel, 1 aft panel assy, 1 forward mid fireshield, 1 aff fireshield, 2 spacers, 1 splice strap, 1 angle, 1 strap, 204 rivets; nha 458-58023; opposite -2
01-161-2065
Structural Aircraft Panel
Used on acft model kc-135r. used as honeycomb panel assy on outer barrel assy of fan duct; bonded with BMS5-104, type ii, class 1, grade 10 supported film adhesive; opposite p/n -4; nha 458-58048-1
01-161-2081
Structural Component Air Support
2.600" overall length 2.200" overall width 0.050" material thickness
01-161-2082
Structural Component Air Support
2.500" overall length 2.300" overall width 0.050" material thickness
