01-190-8234
Aircraft Former
Used on acft model b-52.
01-190-8235
Aircraft Former
8.800" overall length heat treat T6; finish F2.115; opp -9; nha 35-2689
01-190-8236
Aircraft Former
7.900" overall length finish f-2.115; heat treat T6; opp-3; nha 35-2684
01-190-8237
Aircraft Former
4.370" overall length finish f-2.115; heat treat T6; opp -11; nha 35-2684
01-190-8243
Airfoil Rib
30.500" overall length 6.200" overall width 0.040" material thickness 0 temper, ht T4; finish 2.115
01-190-8967
Special Purpose E Cable Assembly
01-190-8968
Special Purpose E Cable Assembly
01-190-8969
Special Purpose E Cable Assembly
01-190-9034
Access Aircraft Door
01-190-9049
Horizontal Stabilizer
01-190-9050
Horizontal Stabilizer
01-190-9210
Air Wing Fairing Inflatable Seal
Matl: cordura fabric-nylon outer material with a thin rubber backing. nha: L3058065-102
01-190-9254
Aircraft Skin
Used on C-141.
01-190-9608
Access Aircraft Cover
Used on acft model b-1b. consist of 1 door, 6 coil insert, misc hardware; opposite p/n -002; used on lower wing panel scavenge pump mount door assy
01-190-9609
Access Aircraft Cover
Used on B-1B.
01-190-9686
Structural Aircraft Panel
Opposite -022; nha L1200901
01-190-9782
Stiffener Aircraft Rib
22.240" overall length 2.3000" overall width 2.330" material thickness made from 5-83972; finish f-2.30; opposite -503; nha 35-2684-701
01-190-9876
Aircraft Fairing
01-190-9877
Aircraft Fairing
01-190-9878
Aircraft Fairing
01-190-9879
Aircraft Fairing
01-190-9880
Aircraft Fairing
01-190-9883
Structural Component Air Fitting
Finish f-2.30; opp -5; nha 65-3741
01-190-9884
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 85.740
01-190-9885
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.91; nha 25-2329; located at pp sta. 205.00
01-190-9886
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.9132 is optional to f-1.91; nha 25-2329; located pp sta. 205.00
01-190-9887
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 111.46
01-190-9888
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 111.46
01-190-9889
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.9132 is optional to f-1.91; nha 50-5914; opposite p/n -1; located at sta. 205
01-190-9891
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 111.46
01-190-9892
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.9132, optional to f-1.91; nha 25-2329; located at pp sta. 225.00
01-190-9893
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp station 142.66
01-190-9894
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat to 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 142.66
01-190-9895
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329; located at pp sta. 142.66
01-190-9896
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat to 160, 000 to 200, 000 psi; finish f-1.91; nha 25-2329; located at station pp 179.95
01-190-9897
Structural Component Air Fitting
Finish f-2.30; opp -6; nha 65-3741
01-190-9898
Structural Component Air Support
Used on acft model b-52. made from forged block 7075-T411 per bms-7-186; heat treated to T73; stock size 52.0 in. lg, 12.000 in. w, 5.0 in. thk; opposite p/n -527; nha 35-29992
01-190-9899
Structural Component Air Support
Used on acft model b-52. aisi type 410 corrosion resistant steel per ams 5350; heat treat 160, 000 to 200, 000 psi; finish f-1.20; nha 25-2329
01-190-9906
Structural Aircraft Panel
Used on acft model c/kc-135. c/o 1 outer skin, 1 dense core, 3 light cores, 6 doublers, 1 inner skin, 4 zee members, 24 bolts, 23 collars; opposite p/n -5; nha 65C20606-4
01-190-9915
Aircraft Former
01-190-9919
Aircraft Former
9.780" overall length
01-190-9920
Aircraft Former
9.780" overall length
01-190-9921
Aircraft Former
10.002" overall length bac 1516-055; finish f-2.115; opp -16; nha 5-71864
01-190-9922
Aircraft Former
10.020" overall length BAC1517-055; opp -15; finish f-2.115; nha 5-71864
01-190-9923
Aircraft Former
10.300" overall length bac 1517-055; finish f-2.115; opp -18; nha 5-71864
01-190-9924
Aircraft Former
10.300" overall length bac 1517-055; finish f-2.115; opp -17; nha 5.71864
01-190-9925
Aircraft Former
9.140" overall length temper T6; finish f-2.115; make from BAC1517-1058; opp -8; nha 35-2689
01-190-9926
Aircraft Former
8.880" overall length finish f-2.115; temper T6; make frm bac 1517-1-58; opp -10; nha 35-2689
01-190-9927
Aircraft Former
8.610" overall length temp T6; finish-2.115; make from bac 1517-1058; opp -12; nha 35-2689
01-190-9928
Aircraft Former
8.610" overall length finish f-2.115; make from bac 1517-1058; opp -11; nha 35-2689
