01-199-5250
Structural Component Air Support
Used on acft model b-1b. utitanium bar, comp 6al-4v, cond a per mil-t-9047; base 2.00 in. lg, 1.75 in. w, 0.150 in. thk; center projection from base, 1.590 in. o/a h including base thk, 0.7400 in. dia thru hole for bearing, projection 0.250 in. thk, nha L3226532
01-199-5251
Structural Component Air Support
Used on acft model b-1b. alum per mil-a-8625, cres per qq-p-35, steel per qq-p-416; 5.29 in. lg; opposite p/n -4
01-199-5253
Structural Component Air Support
Used on acft model b-1b. c/o 3 tubes, 2 release collars, 2 berring rod ends; retracted length 13.93 in.; extended length 29.5 in.
01-199-5254
Structural Component Air Support
Used on acft model b-1b.
01-199-5256
Structural Aircraft Panel
Used on acft model b-1b.
01-199-5257
Structural Aircraft Panel
Used on acft model b-1b. functional description:used as aft vane closeout nacelle door assy; nuclear hardness critical item; consists of:1 door, 1 strap, 1 seal, rivet a/r; nha L3226421;
01-199-5258
Structural Aircraft Panel
Used on acft model b-1b. functional description:used as aft vane closeout nacelle door assy; nuclear hardness critical item; c/o:1 door, 1 strap, 1 seal, rivet a/r; oppoisite p/n -012; nha L3226421;
01-199-5259
Structural Aircraft Panel
Used on acft model b-1b. functional description:used as rh crew station avionics bay panel assembly; nuclear hardness critical item; c/o:1 door, 2 half hinges, and assorted attachment hardware; located yf 372.to 422; nha L3050553-001;
01-199-5264
Aircraft Skin
Consists of 2 skin; 1 core;
01-199-5267
Thermal Special Purpo Insulation
Functional description:used as blanket assembly; end item identification:aircraft, model b-1b
01-199-5268
Thermal Special Purpo Insulation
Functional description:used as blanket; end item identification:aircraft, model b-1b
01-199-5270
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b; functional description:used as blanket
01-199-7380
Structural Component Air Support
01-199-7423
Structural Component Air Support
Used on acft model kc-135. consist of 3 angles; touch up pert.o.1c-135 (k) a-3-4; nha 458-54706
01-199-7431
Structural Aircraft Panel
01-199-7440
Aircraft Former
5.000" overall length 4.000" overall width 0.051" material thickness
01-199-8504
Structural Aircraft Panel
Used on c-5b aircraft. located fs 1303 to 1332 & fs 1523 to 1552; c/o: -106a angle (1) , -118a panel (1) , safety strip instl (1) , doubler (1) ; opposite -123a
01-199-8506
Structural Aircraft Panel
Used on c-5b aircraft. located fs 1303 to 1332 & fs 1523 to 1552; c/o: -106a angle (1) , -118a panel (1) , doubler (1) , safety strip instl (1) ; opposite -125a
01-199-8527
Aircraft Former
8.740" overall length
01-199-8528
Aircraft Former
8.760" overall length
01-199-8529
Aircraft Former
9.000" overall length
01-199-8530
Aircraft Former
9.270" overall length
01-199-8531
Aircraft Former
9.270" overall length
01-199-8532
Aircraft Former
11.200" overall length T6 temp; finish f-2.115; stock BAC1517-1055; opp -08; nha 35-2684
01-199-8533
Aircraft Former
11.200" overall length
01-199-8534
Aircraft Former
11.460" overall length type ii class 2, size .062
01-199-8535
Aircraft Former
11.460" overall length T6 temp; finish f-2.115; stock BAC1517-1055; opp -9; nha 35-2684
01-199-8536
Aircraft Former
11.660" overall length
01-199-8537
Aircraft Former
11.660" overall length
01-199-8538
Aircraft Former
10.140" overall length
01-199-8541
Aircraft Pylon
01-199-8544
Aircraft Skin
80.000" overall length 44.000" overall width opposite -10; al clad 1 side only per fms 0033-T81; finish A028; nha 12T9206
01-199-9603
Aircraft Door
Heat treatable
01-199-9685
Access Aircraft Door
01-199-9739
Access Aircraft Cover
Engine, lh lwr access FS389.80 TO446.10
01-199-9781
Structural Aircraft Plate
Used on f-16a usaf aircraft. stock size-.020X5X16 in; material-commercially pure titanium alloy per mil-t-9046, type i, comp b, cond a; finish-T100; superceded but not interchangeable with -77; nha-16B6312-805; eff on-6h 0094 0096; location-shield instl, heat, internal, fs 446.10 to 479.55
01-199-9782
Structural Aircraft Plate
Used on f-16a usaf aircraft. stock size-.020X5X16 in; material-commercially pure titanium alloy per mil-t-9046, type i, comp b, cond a, finish-T100; location-shield instl, heat, internal, fs 446.10 to 479.55; superceded -79 but not interchangeable; nha-16B6312-805; eff on-6h 0094 0096
01-199-9783
Aircraft Pylon
01-199-9808
Structural Aircraft Plate
Used on f-16d usaf aircraft. location-fuel shelf, fs 279-341; stock size-.100X26X63 in; material-al alyqq-a-250/4-T62, finish-A810; superceded-85, ow; nha-16B565-803; eff on-5d 0001 9999
01-199-9809
Structural Aircraft Plate
63.000" overall length 26.000" overall width 0.100" material thickness nha 16B565-803; eff on 5d 0001 9999
01-199-9811
Structural Component Air Support
C/o 1 strut structure, 1 plumbing instl, 1 detector insttl, 1 systems instl, 1 cable instl, 1 fairlead
01-199-9814
Structural Component Air Support
Used on acft model kc-135.
01-199-9815
Structural Component Air Support
Used on acft model kc-135. consist of 1 fitting, 2 bushing; opposite p/n -502; nha 458-58303
01-199-9816
Structural Component Air Support
Used on acft model kc-135. consist of 1 fitting, 2 bushing; opposite p/n -501; nha 458-58303
01-199-9817
Structural Component Air Support
01-199-9819
Structural Component Air Support
Used on acft model a-10a.
01-199-9820
Structural Component Air Support
Used on acft model a-10a.
01-199-9823
Aircraft Intercostal
36.000" overall length 24.000" overall width 0.125" material thickness
01-199-9827
Aircraft Skin
C/o--21 bracket (2) , -19 rib (1) , -11 rib (1) , -23 frame (1) , -33 skin (1) , sealant, -27 shim, hardware; material-of ribs-qq-a-250/4-T62, of bracket-K10A22T8511, of frame-qq-a-250/4-T62, of skin assy-qq-a-250/11-T6; skin assy, rudder fairing-vertical stabilizer-on actuator support instl-rudder fairing; superceded -1-ow; nha 16T9160-29; eff on-5c 0001 999 9
01-200-0040
Structural Component Air Support
Used on c-5b aircraft. located lh side, fs 1314.000 & fs 1534.000; nha 4H60017, eff on 0082 & up; c/o: -111a bracket (1) matl 2024-T3 alum alloy per qq-a-250/4, size .063X13.0X15.0in; -113a clip (1) matl 2024-T3 alum alloy per qq-a-250/4, size .063X2.0X2.0in
