01-161-5658
Structural Aircraft Plate
Used on acft model kc-135r. corrosion resistant steel sheet 15-5ph per BMS7-240, type i; heat treated to 150-170 ksi per BAC5619; finish f-12.37 plus 12.100 (gray) ; 58.000 in. lg, 5.000 in. w, 0.032 in. thk; opposite p/n -507; nha 458-58023-502
01-161-5659
Structural Aircraft Plate
Used on acft model kc-135r. al alloy bar 2024-T62 per qq-a-225/6; finish f-2.16; 4.000 in. lg, 1.300 in. w, 0.800 in thk; contains 4 MS21209F4-25 inserts; opposite p/n -15; nha 458-58057-2
01-161-5660
Structural Aircraft Plate
Used on acft model kc-135r. corrosion resistant steel sheet 15-5ph per BMS7-240, type i; heat treated to 150-170 ksi per BAC5619; finish f-12.37 plus 12.100 (gray) ; 58.000 in. lg, 5.000 in. w, 0.032 in. thk; opposite p/n -507; nha 458-58023-501
01-161-5661
Structural Aircraft Plate
2.400" overall length 1.000" overall width 0.250" material thickness comp 4335
01-161-5662
Structural Aircraft Plate
2.600" overall length 1.000" overall width 0.250" material thickness comp 4335
01-161-5663
Structural Aircraft Plate
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; 11.900 in. lg, 7.400 in. w, 0.063 in. thk; nha 458-58066-29
01-161-5664
Structural Aircraft Plate
4.200" overall length 3.600" overall width 0.080" material thickness comp 4335
01-161-5667
Structural Aircraft Plate
3.000" overall length 1.300" overall width 0.100" material thickness comp 4335
01-161-5668
Structural Aircraft Plate
3.700" overall length 2.900" overall width 0.125" material thickness
01-161-5669
Structural Aircraft Plate
Used on b-52 acft. matl magnesium alloy, qq-m-44, cond a or al alloy, qq-a-250, ht treat T42; matl size 0.050 by 2.000 by 51.000 in. lg; used as circular splice plate on nose cowl assy
01-161-5671
Structural Aircraft Plate
2.900" overall length 1.820" overall width 0.250" material thickness used as spacer; retrofit-spar beef-up
01-161-5672
Structural Aircraft Plate
Used on F-15. 0.150" material thickness 1.50 dia.; as plug
01-161-5673
Structural Aircraft Plate
Used on BF-15. 0.150" material thickness 1.75 dia.; as plug
01-161-5674
Aircraft Fairing
58.000" overall length 5.000" overall width 0.071" material thickness opposite -505; nha -502 & -504
01-161-5675
Aircraft Fairing
58.000" overall length 5.000" overall width 0.071" material thickness opp -506; nha -501
01-161-5676
Structural Component Air Support
Used on acft model c/kc-135. titanium 6al-4v forging per AMS4928, condition annealed; finish desoto high temp primer per BAC5710; 3.640 in. lg, 3.460 in. w, 3.620 in. h; opposie p/n -1; contains 2 bushings
01-161-5677
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0; matl size 0.071 by 4.000 by 4.000 in. lg; opposite to p/n 25-2365-20; used as bracket on frame installation, nose cowl
01-161-5678
Structural Component Air Support
5.700" overall length 2.900" overall width 0.050" material thickness
01-161-5679
Structural Component Air Support
Forge per mil-f-7190 grade b
01-161-5680
Structural Component Air Support
C/o: pad 35-10747-3, pad 35-10747-4, stiffener 35-10747-6, stiffener 35-10747-8, web 35-10747-803
01-161-5681
Structural Component Air Support
C/o: web 35-10748-3, pad 35-10748-4, pad 35-10748-5
01-161-5682
Structural Component Air Support
C/o: web 35-10748-3, pad 35-10748-4, pad 35-10748-5
01-161-5683
Structural Component Air Bracket
01-161-5684
Structural Component Air Bracket
01-161-5686
Structural Component Air Support
2.530" overall length 1.580" overall width 0.250" material thickness
01-161-5687
Structural Component Air Support
2.510" overall length 1.580" overall width 0.250" material thickness
01-161-5688
Structural Component Air Support
4.800" overall length 8.100" overall width 0.060" material thickness
01-161-5689
Structural Component Air Support
6.300" overall length 3.700" overall width 0.063" material thickness
01-161-5690
Structural Component Air Support
Used on acft model kc-135r. hal alloy extrusion 7075-0 per qq-a-200/11; heat treated to cond T73; finish f-2.20 plus desoto hitemp primer per BAC5710; stock AND10134-2004 x 3.000 in. lg; opposite p/n -13; nha 458-58023-2
01-161-5691
Structural Component Air Support
Used on acft model kc-135r. hal alloy extrusion 7075-0 per qq-a-200/11; heat treated to cond T73; finish f-2.20 plus desoto hitemp primer per BAC5710; stock AND10134-2004 x 3.000 in. lg; opposite p/n -14; nha 458-58023-1
01-161-5692
Structural Component Air Support
Used on acft model kc-135r. c/o 1 stop fitting, 1 spacer, 1 shim, washer, bolt, nut 2 of each; finish f-2.20 plus desoto hitemp primer per BAC5710
01-161-5693
Structural Component Air Support
C/o: support bracket 29-2512-5, nut plate-floating F2000-10-1032
01-161-5694
Structural Component Air Support
C/o: bracket (1 ea) 36-3908-1, nutplate (1 ea) MK2000-3
01-161-5695
Structural Component Air Support
C/o: bracket (1 ea) 36-3908-5, nutplate (1 ea) MK1000-3; used on rib closure, fire detector harness
01-161-5696
Structural Component Air Support
8.800" overall length 1.300" overall width 0.063" material thickness
01-161-5697
Structural Component Air Support
2.100" overall length 1.200" overall width 0.063" material thickness
01-161-5698
Structural Component Air Support
1.500" overall length 1.400" overall width 0.063" material thickness
01-161-5699
Structural Component Air Support
Used on b-52 acft. used as weld assy on nose cowl assy
01-161-5700
Structural Component Air Support
1.700" overall length 1.000" overall width 0.063" material thickness
01-161-5701
Structural Component Air Support
Used on f-15 aircraft. same as -2005 except for additional fastener pattern; location-support-lower, aft section, inboard pylon
01-161-5702
Structural Component Air Support
Interchangeable with -2001, -2003, -2005, -2007, -2009, -2011, -2013, -2015, -2017
01-161-5703
Structural Component Air Support
Used on f-15 aircraft. same as -2004 except for some dimensions; stock size-3.00 x 6.62 x 6.75; material spec mil-t-9047 type iii comp c condition annealed; function.support, pivot-variable inlet, ramp outboard
01-161-5710
Aircraft Former
14.300" overall length 2.500" overall width 0.063" material thickness
01-161-5711
Aircraft Former
10.200" overall length 3.000" overall width 0.040" material thickness
01-161-5712
Aircraft Former
10.400" overall length nha -10
01-161-5714
Aircraft Former
3.500" overall length 3.100" overall width 0.063" material thickness nha -4
01-161-5715
Aircraft Former
6.400" overall length 4.100" overall width 0.063" material thickness nha 458-58066-3
01-161-5716
Aircraft Former
01-161-5717
Aircraft Former
01-161-5722
Aircraft Skin
Used on F-16. 4.000" overall length 3.000" overall width finish A666
