01-254-3221
Hydraulic Motor-pump Piston
Used on b-1b aircraft.
01-254-3222
Hydraulic Motor-pump Piston
Used on b-1b aircraft.
01-254-4619
Hydraulic Drive Unit
Used on b-1b aircraft. consist of gearbox sub-assembly 2, pid assembly 1, washer flat 45, bolt hex 24, bolt 12 point 4, lockwire ar, grease ar, expoxy primer ar, acrylic lacquer ar, locking compound ar, topcoat, type ur ar, nameplate 1, washer csk 4, screw cap, socket HEAD17, cam, emergency switch 1, dowel special 1, wire retaining 1, screw machine 4, adhesive ar, motor, hydraulic assy rlds 2, valve control hyd 2, tube assembly hydraulic 2, tube transfer 6, shim set 4, seal ring assembly 12, plug threaded 4, bracket elec.cable 1, clamp assy cush saddle 1, screw machine F1lh 2, nut hex 2; ref dimensions 41.500 long, 23.375 high, 8.85 wide
01-254-6833
Valve Cap
Used on b-1b aircraft hydraulic vacuum deicing systems.
01-254-6886
Linear Actuating Cylinder Piston
Used on b-1b aircraft. 440c, per qq-s-763; 1.953 in. min., 1.957 in. max. lg.; 1st end dia. 0.497 in. min., 0.498 in. max.; 2nd end dia. 0.454 in. min., 0.484 in. max.; heat treated per sunstrand spec PN09.440-hfd; hardness is 56 hrc min.; fsc application data:aircraft hydraulic system
01-254-6887
Hydraulic Motor-pump Head
Used on pump,sundstrand aerospace,model b1b. assembly includes:736364 tube 1, 736358 race bearing, outer roller 1; 1739868-1 port, plate 1
01-254-6888
Directional Control Linea Sleeve
Used on b-1b aircraft. 0.695" overall length steel, corrosion resistant, 302, per mil-s-7720, cond a; 0.939 in.min, 0.940 in.max o/a dia; 0.500 in.min, 0.501 in.max i/s dia; passivate per mil-s-5002; fsc application data:aircraft hydraulic system
01-254-7450
Hydraulic Pump-motor Cover
Steel; 2.000 in. dia; 0.250 in. thk; used on numerous hydraulic pump models
01-254-7470
Actuating Line Cylinder Assembly
01-254-9911
Hydraulic Manifold Assembly
01-255-1398
Hydraulic Servovalve
Used on b-1b aircraft. igv actuator positions the igv flaps; used on F110-ge-100 engine; dimensions in": 2.260 long, 2.480 wide; mounted with 4 screws 0.211" diameter hole; action electro-hydraulic
01-255-1400
Directional Control Linear Slide
01-255-1401
Directional Control Linear Slide
Used on c5b aircraft. 2.580" overall length 2cres steel per ams 5630; 1st end dia 0.483/0.484 in.; 2nd end dia 0.309/0.310 in.; 1st end drilled 0.312 in. dia to 0.906 in. depth, drilled 0.125 to 0.594 in. depth; 2nd end has number 2 center, drilled to 0.125 in. depth; aircraft hydraulic system
01-255-2942
Hydraulic Pump-motor Cover
Aluminum alloy, 6061T6 per qq-a-200/8d; anodize per mil-a-8625, type 1; 0.230 in. thk; 2.125 in. dia; 0.520 in. dia hole thru; 1st counterbore .505 min 1.525 max in. dia, 0.045 in. deep; 2nd counterbore 0.755 min 0.775 max in. dia, 0.065 in. deep; stepped on one side 0.043 in.
01-255-4409
Linear Actuating Cylinder Head
1.750" overall length 8 holes 0.256 in.dia, equally spaced parallel to cylinder end; 1.020 in.bore dia same end with 0.815 in.conter bore dia; 0.520 in.bore dia second end
01-255-5486
Mechanical Drive Housing
Used on 1650012511153. matl is C3867055-1; acft hyd system anodize surface treated
01-255-5509
Linear Actuating Cylinder Piston
Used on 1650-01-251-1153. 3.171" overall length 1st end, 0.840 in. dia; 2nd end, 0.750 iin. dia; 16 thds per in. series unjf, class 3b; heat treat, passivate, chrome plated
01-255-5510
Linear Actuating Cylinder Piston
Used on 1650-01-251-1153. 2nd end dia is 1.246 in.heat treat; passivate
01-255-7567
Linear Actuating Cylinder Piston
1.000" overall length hard chrome plated; used on f-18 aircraft
01-255-8128
Hydraulic Manifold Assembly
Inlet/outlet valve-not provided; u/o actuator of f-15 acft
01-256-2030
Linear Actuating Cylinder Piston
Used on b-1b aircraft.
01-256-2031
Linear Actuating Cylinder Piston
Used on 1650-01-251-1153. 3.644" overall length heat treat; chrome plate
01-256-2032
Linear Actuating Cylinder Piston
Used on 1650-01-251-1153.
01-256-2033
Linear Actuating Cylinder Piston
Used on 1650-01-251-1153. 1.625-16 unj-3b int thd, under head hex 2.120 in.; heat treat; passivate
01-256-2034
Piston Linear Actuating Cyli Rod
Used on 1650012511153. 4.011" overall length 1.360 in.od, outside stepped, 1.059 in.; 1.020 in.next dia; 0.599 in.on one end, inside dia stepped, 1st end stepped 0.440 in., 2nd step 0.780 in.; 3rd step 0.500 in.; 4th step 0.440 in.; 5th step 0.500 in.; 6th step 0.500 in.; 7th step 0.533 in.; material document
01-256-2039
Directional Control Linea Sleeve
Used on 1650012511153. 6.105" overall length steel, corrosion resistant, ams 5659; heat treated per ps-15227; passivated per ps-13001; 0.547 in.min, 0.548 in.max o/a dia; fsc application data:aircraft hydraulic system
01-256-2040
Directional Control Linea Sleeve
Used on 1650-01-251-1153. 0.884" overall length aluminum alloy, qq-a-225/9, 7075-T73 or 7075-T7351; anodized per ps-13201, ty 2, cl 1; o/a dia is 0.672 in.min, 0.673 in.max; i/s dia 0.375 in.; fsc application data:aircraft hydraulic system
01-256-2041
Directional Control Linea Sleeve
Used on 1650012511153. 10.856" overall length steel, qq-s-763, 440c sst; 1.864 in.o/s dia stepped; 1.489-22 in.dia places, 1.244 in.dia 11 places; 0.9914 in.i/s dia; heat treated 56-61 rc per ps-15151, mcair approved sources must be used; finish passivate per ps-13001; fsc application data:aircraft hydraulic system
01-256-2042
Directional Control Linear Slide
Used on 1650012511153. 5.765 in. lg, 0.6126 in. dia 19 places, 0.440 in. relief dia 8 places, 0.550 in. dia both ends; 0.095 in. dia holes (2 ea end) 1st end 3.250 in. deep
01-256-2043
Directional Control Linear Slide
Used on acft hydraulic system.
01-256-2044
Directional Control Linear Slide
Used on 1650012511153. U3.095 in. lg, 0.673 in. od, stepped diameters, 0.380 in. od, 0.400 in. dia, 0.3125-24 unjf-3a thd; matl-sst PH13-8mo per ams 5629; heat treat H1000 per ps-15238; mcair approved sources must be used; passivate per ps-13001; acft hyd system
01-256-2451
Linear Actuating Cylinder Piston
Used on 1650-01-251-8480. 1.181" overall length 2nd end, 0.124 in. dia; heat treated; passivated
01-256-4344
Hydraulic Pump-motor Cover
Used on b-1b aircraft. 7-holes equally spaced 0.1970 diameter thru on 0.663 diameter bolt circle
01-256-4345
Hydraulic Pump-motor Cover
Used on b-1b aircraft. 7 holes 0.198 diameter thru equally spaced on 0.663 diameter bolt circle
01-256-4346
Hydraulic Pump-motor Cover
Used on b-1b aircraft. 7 holes equally spaced on 0.663 diameter bolt circle; hole diameter 0.1970
01-256-4347
Valve Body
Used on 1650012518480. fsc application data:aircraft hydraulic system
01-257-1030
Actuating Linear Cylinder
3.917" overall length 1.790" bore diameter
01-257-1042
Pneumatic Accumulator
Used on 70167/19d22454-5 escape slide assembly. 18.310" overall length
01-257-1687
Actuating Line Cylinder Assembly
Used on f-14 acft.
01-257-2783
Hydraulic Aircraf Valve Assembly
Used on b-1b aircraft.
01-257-4875
Servocylinder
01-257-4948
Linear Actuating Cylinder Piston
01-257-6756
Dust And Moisture Seal Boot
01-257-6883
Directional Control Linea Sleeve
01-257-7588
Actuating Line Cylinder Assembly
Used on f-14 acft.
01-258-1705
Linear Actuating Cylinder Piston
1.870" overall length hard chrome plated; used on ground support for f-18 aircraft
01-258-2301
Linear Actuating Cylinder Piston
Used on c-141 a, b aircraft
01-258-3029
Hydraulic Pump-motor Cover
01-258-8182
Fluid Filter Body
01-258-8339
Hydraulic Pump-motor Cover
Used on b-1b aircraft. 7-equally spaced holes 0.198 diameter thru
