01-185-0866
Aircraft Former
9.800" overall length 1.800" overall width 0.050" material thickness
01-185-0867
Aircraft Former
9.900" overall length 1.800" overall width 0.050" material thickness
01-185-1046
Structural Aircraft Plate
01-185-1055
Structural Aircraft Panel
Used on F-15.
01-185-1056
Structural Aircraft Panel
Used on F-15.
01-185-2745
Access Aircraft Door
Used on e-3a aircraft. 2, -18, -21, &-23 replaceable assy (interchangeable at attaching points only) ; part of -19 door & doubler instl-waste water drain, section 43; c/o skin door:stock size-.090X6.2X11.6in, finish srf-2.130 (1) ; half hinge:finish srf-12.205 (faying surface only) stock made from MS20001-PH4 & PH6-1088 (2) ; clip (1) ; latch-flush:finish install per srf-8.51 (2) ; pin-hinge (1) ; pin-spring:finish install per f-12.44 (2)
01-185-2987
Aircraft Skin
Used on F-15. 9.500" overall length 6.500" overall width
01-185-3809
Structural Component Air Bracket
14.510" overall length 0.500" overall width canopy mounted body positioning hfeatgandle
01-185-3899
Structural Component Air Support
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 7.700 in. lg, 4.400 in. w, 0.050 in. thk; c/o 1 support, 4 nutplates; nha 458-54745
01-185-3900
Structural Component Air Support
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 7.300 in. lg, 4.600 in. w, 0.050 in. thk; c/o 1 support, 10 nutplates; nha 458-54745
01-185-3901
Structural Component Air Support
C/o 1 tube support, 1 end fitting, 8 rivets
01-185-3921
Fuel Aircraft Tank
01-185-4945
Access Aircraft Cover
Sixteen no. 21 holes
01-185-5802
Wiring Harness
Conductor identification no.:mil-w-5088 1W11P46m/W1W38J46; first end component controlling agency
01-185-5936
Vertical Stabilizer
Item is made up one structural assy p/n 11557840; one rudder assy p/n 11557842; one support p/n 11557820; ar washer p/n AN960-616l; one bolt p/n NAS1226-9l; two screws p/n MS35206-243; two lock washer p/n MS35338-42; ar dp seal sn 11557823-1; one washer p/n AN960-616;
01-185-5937
Control Surface Aircraft Fairing
Acrylic-pvc aly flat sheet 0.125 in.thk per 11558018-6; finish iaw MIS26332, white;
01-185-5938
Wing Aircraft Fairing
Used on targets surface to air missiles.
01-185-5960
Fuselage Section
Bracket 5; rivet 81; channel 2; tank 1; washer 22; bolt 22; insert 48; grommet 1; nut 17; nutplate 30; screw 14;
01-185-5961
Fuselage Section
Rpart dim 44.1250 x 15.1875 x 14.8750 in.; wt 14 lbs 2 oz; material alum alloy alclad 2024 plate
01-185-5965
Center Wing Section
Part dim:63X54X3.125 in.; wt:46 lbs; section comp of 43 types of items; sections o/a material comp al alclad 2024; qtys are dp skin 4, dp doubler 20, dp honeycomb 5, bracket assy 3, rib 2, rib assy 5, grommet 28, door access 2, dp conduit 2, dp channel 2, nut plat 4;
01-185-6320
Access Aircraft Cover
Used on acft model b-1b. 0.250" hole diameter 4 additiona rows of screw holes along with; sealed with rubber strips
01-185-6323
Access Aircraft Door
Used on acft model b-1b.
01-185-6324
Access Aircraft Door
Used on b-1b aircraft. 4nuclear hardness critical item; p/o: door, avionics bay-fuselage; sta YF737.000 to sta YF875.500; c/o: lru door, channels, skupports, door hinges, emp shield, stud nuts, retaining rings, rivets, clip & corner clip, shield, spacer; opposite -172
01-185-6326
Access Aircraft Door
Used on b-1b aircraft. 3nuclear hardness critical item; p/o: door, avionics bay-fuselage; sta YF737.000 to sta YF875.500; c/o: lru door; channels, supports, door hinges, emp shield, stud nuts, retaining rings; rivets, clip & corner clip, shield, spacer; opposite -162
01-185-6415
Access Aircraft Cover
Used on e-3a acft. overhead air conditioning nozzle gap cover; make from 6061 per qq-a-250; heat treat T4; finish srf-2.30 7.000 in lg, 4.500 in wd, 0.016 in thk; nha 204-67020-1
01-185-6416
Access Aircraft Cover
Used on e-3a aircraft. overhead air conditioning nozzle gap cover; nha 204-67016-2; 4.500 in lg, 1.40 in wd, 0.016 in thk; make from 6061 per qq-a-250; heat treat T4; finish srf-2.30
01-185-6452
Aircraft Fairing
15.900" overall length 9.300" overall width 7.725" material thickness
01-185-6453
Structural Component Air Support
Used on acft model b-1b. machined AMS5629 corrosion resistant steel bar; 3.212 in. lg, 3.000 in. w, 1.808 in. h; clevis angled 3.5 deg to base; 3 pilot holes for 3/16 in. fasteners in corners of triangular base; c/o 1 fitting, 1 plain cres bushing, 1 flanged cres bushing; opposite p/n -002; nha L3223550
01-185-6454
Structural Component Air Support
Used on acft model b-1b. machined AMS5629 corrosion resistant steel bar; 3.212 in. lg, 3.000 in. w, 1.808 in. h; clevis angled 3.5 deg to base: 3 pilot holes for 3/16 in. fasteners in corners of triangular base; c/o 1 fitting, 1 plain cres bushing, 1 flanged cres bushing; opposite p/n -001; nha L3223550
01-185-6456
Structural Component Air Support
Used as engine access door fitting
01-185-6459
Structural Component Air Support
01-185-6460
Structural Component Air Support
Used as engine access door assembly
01-185-6461
Structural Component Air Support
Used as engine access door fitting
01-185-6932
Access Aircraft Door
01-185-7340
Access Aircraft Door
Used on b-1b aircraft. 5nuclear hardness critical item; p/o: door, avionics bay-fuselage; sta YF737.000 to sta YF875.500; c/o: lru door, channels, skupports, door hinges, emp shield, stud nuts, retaining rings, rivets, clip & corner clip, shield, spacer; opposite -182;
01-185-7552
Structural Aircraft Plate
2.590" overall length 1.000" overall width 0.050" material thickness nha 8427100-10
01-185-7555
Structural Component Air Support
Corrosion resistant steel; stock size 1.60 in. lg, 1.06 in. w, 0.83 in. thk; 0.295 in. dia centered hole 0.88 in. deep; 2 thru holes 0.191 in. dia csk .381 dia by 100 deg; nha L3223454
01-185-7556
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel; stock size 1.06 in. lg, 1.06 in. w, 0.83 in. thk; 0.295 in. dia centered hole 0.583 in. deep; 2 thru holes 0.191 in. dia csk .381 dia by 100 deg; nha L3223454
01-185-7557
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel; stock size 1.60 in. lg, 1.21 in. w, 0.73 in. thk; 0.295 in. dia center hole 0.265 in. deep; 2 holes .1900-32 unjf-3b; nha L3223454
01-185-7558
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel; stock size 1.60 in. lg, 1.21 in. w, 0.75 in. thk; 0.295 in. dia centered hole 0.265 in. deep; 2 thru holes 0.191 in. dia csk .381 dia by 100 deg; nha L3223454
01-185-7559
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 -8 fitting, 1 bushing; opposite p/n -9; nha 65-6140
01-185-7560
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 -7 fitting, 1 bushing; opposite p/n -10; nha 65-6140
01-185-7561
Structural Component Air Support
Finish f-2.30; opposite -1; nha 65-3148-9; c/o 2 hinge side, 1 base plate
01-185-7562
Structural Component Air Bracket
C/o 1 support bracket, 1 clip, 1 angle, 1 filler, 1 floating nutplate; finish f-2.115; opp -1; nha 65-8303
01-185-7571
Structural Aircraft Panel
C/o 1 upper doubler, 1 lower doubler, 1 skin, 1 beaded doubler; al alloy 2024 per qq-a-250/5; finish f-2.10
01-185-7572
Structural Aircraft Panel
C/o 1 access door, 1 doubler, 1 upper doubler, 1 lower doubler, 1 skin, 1 beaded doubler; al alloy 2024 per qq-a-250/5; finish f-2.10
01-185-7573
Structural Aircraft Panel
C/o 1 upper doubler, 1 lower doubler, 1 skin, 1 beaded doubler; al alloy 2024 per qq-a-250/5; finish f-2.10
01-185-7574
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 access door, 1 doubler, 1 upper doubler, 1 lower doubler, 1 skin, 1 beaded doubler; al alloy 2024 per qq-a-250/5; finish f-2.10
01-185-7575
Structural Aircraft Panel
Used on acft model kc-135. royalite sheet, color medium gray no. 36251 per fed std 595; 5000 series hardness, solid color, haircell grain, dull finish; opposite p/n -1; nha 50-3729
01-185-7589
Aircraft Former
4.200" overall length 3.100" overall width 0.050" material thickness
