00-000-0048
Aircraft Turbo-shaft Engine
Used on t-55 engines series.
00-000-0049
Engine Modification Kit
Used on t-55 series engines.
00-001-1741
Turbine Case And Nozzle Assembly
Used on acft eng tf-41. vanes: 100 eq sp except one offset
00-001-2114
Compressor Aircraft Gas Tur Vane
Used on acft eng tf-39. 1.345" overall length 0.935" overall width 63 aa microinch surface finish
00-001-4903
Air Aircraft Gas Turbine En Seal
00-001-4908
Air Aircraft Gas Turbine En Seal
00-001-8342
Metallic Aircraft Gas Turbi Seal
Used on acft eng tf-39. t.o. 2j-TF39-4
00-001-8343
Turbine Aircraft Gas Turb Nozzle
Used on engine assembly,turbo-jet,model no. j85-ge-21..
00-001-8347
Turbine Rotor Aircraft Gas Blade
Used on acft eng tf-39. 63 aa microinch finish all surfaces
00-001-9579
Compressor Aircraft Gas Tur Vane
00-003-0843
Air Aircraft Gas Turbine En Seal
Used on acft eng tf-39.
00-003-1297
Air Aircraft Gas Turbine En Seal
00-003-1326
Air Aircraft Gas Turbine En Seal
00-003-3437
Air Aircraft Gas Turbine En Seal
00-003-4276
Gearbox Turbine Engine Housing
Used on f-5 freedom fighter.
00-003-5604
Antifriction Bearing Air Housing
Used on tf33 aircraft engine. 2.348" overall length
00-003-5607
Antifriction Bearing Air Housing
Used on tf33 aircraft engine.
00-003-5608
Bearing Aircraft Gas Tur Support
Used on acft eng tf33.
00-003-9754
Component Mounting Aircraf Plate
Used on tf-30 aircraft gas turbine engine. 1.590" overall length original name boss, combustion chamber, turbine engine
00-004-2625
Air Aircraft Gas Turbine En Seal
00-005-1307
Fan Aircraft Gas Turbine E Rotor
Used on acft eng tf-39.
00-005-1795
Compressor Aircraft Gas Tur Vane
Used on tf-41 acft engine.
00-005-3764
Compressor Component Air Support
Used on acft eng. for front compressor casing bellcrank
00-005-6753
Compressor Aircraft Gas Tur Disk
Used on acft eng j57. 2.882" overall length 6.995-7.005 in id.; 28 blade slots eq sp around od, 16 0.420-0.423 in. dia. holes eq sp on 8.0000 in centerline rad.; 16 0.437-0.440 in. dia. holes eq sp on 8.000 centerline rad.
00-005-6754
Compressor Aircraft Gas Tur Disk
Used on acft eng j57. 2.348" overall length 6.995-7.005 in. id.; 37 blade slots eq sp around od; 16 0.437-0.440 in. dia holes eq sp on 8.000 in. centerline rad.; 16 0.420-0.423 in. dia holes eq sp on 8.0000 in. centerline rad. AGAVGJ57 aircraft engine
00-005-6755
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 2.039" overall length 7.995-8.005 in. id.; 51 blade slots eq sp around od; 16 0.420 in. dia holes eq sp on 8.000 in. centerline rad.; 16 0.437-0.440 in. dia holes eq sp on 8.000 in. centerline rad.
00-005-6766
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 0.971" overall length 5.995-6.005 in. id; 16 0.437-0.440 in. holes eq sp on 9.000 in. centerline rad.; 16 0.498-0.501 in. holes eq sp on 9.000 in. centerline rad.
00-005-6768
Turbine Aircraft Gas Turbin Disk
Used on j57 engine.
00-005-6772
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 0.971" overall length 5.995-6.005 in. id; 85 blade slots eq sp around od; 16 0.498-0.501 in. holes eq sp on 9.000 in. centerline rad.; 16 0.437-0.440 in. holes eq sp on 9.000 in. centerline rad.
00-005-6773
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 1.790" overall length 8.995-9.005 in. id; 69 blade slots eq sp around od; 16 0.437-0.440 in. holes eq sp on 8.000 in. centerline rad.; 16 0.420-0.423 in. holes eq sp on 8.000 in. centerline rad.
00-005-6775
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 1.629" overall length 8.995-9.005 in. id; 91 blade slots eq sp around od; 16 0.420-0.423 in. holes eq sp on 8.000 in. centerline rad.; 16 0.437-0.440 in. holes eq sp on 8.000 in. centerline rad.
00-005-6776
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 1.518" overall length was disk, axial compressor, turbineengine
00-005-6777
Turbine Aircraft Gas Turbin Disk
Steel, ams 6415, rockwell C35-40 hardness, 1.354-1.365 in. thk, 20.017-20.027 in. od, 11.995-12.005 in. id, 103 blade slots equallyspaced around od, sixteen 0.437-0.440 in. holes equally spaced on 8.000in. centerline radius, 32 scallops equally spaced on 7.260 in.centerline radius, thirty-two 0.108-0.113 in. holes equally spaced ON7.260 in. centerline radius
00-006-2791
Turbine Aircraft Gas Turbin Disk
Rockwell C35-40 hardness; 1.482-1.493 inch thickness; 19.825-19.835 inch od; 101 blade slots equally spaced around od; 16 0.4205-0.4235 inch holes equally spaced on 8 inch centerline radius; 16 0.437-0.440 inch holes equally spaced on 8.0 inch centerline radius
00-006-5305
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 1.482" overall length 10.995-11.005 in. id.; 101 blade s lots eq sp around od; 16 0.420-0.423 holes eq sp on 8.000 in. c/l rad.; 16 0.433-0.440 in. holes eq sp on 8.000 in. c/l rad.
00-006-5308
Turbine Aircraft Gas Turbin Disk
Steel, ams 6415, rockwell C35-40 hardness, 3.210-3.221 in. thk, 19.825-19.835 in. od, 6.995-7.005 in. id, 27 blade slots equally spacedaround od, sixteen 0.437-0.440 in. holes equally spaced on 8.000 in.centerline radius, thirty-two 0.101-0.113 in. holes equally spaced ON7.260 in. centerline radius, thirty-two scallops equally spaced on 7.260in. centerline radius
00-006-5309
Turbine Aircraft Gas Turbin Disk
Steel, ams 6415, rockwell C35-40 hardness, 2.028-2.039 in. thk, 19.825-19.835 in. od, 7.995-8.005 in. id, 51 blade slots equally spacedaround od, sixteen 0.4205-0.4235 in. holes equally spaced on 9.000 in.centerline radius, sixteen 0.437-0.440 in. holes equally spaced on 9.000in.centerline radius
00-006-5311
Compressor Aircraft Gas Tur Disk
Used on j57 aircraft engine. 1.096" overall length 5.995-6.005 in. id cadmium disk surface treated
00-007-5636
Turbine Aircraft Nozzle Segment
Used on aircraft engine model t56.
00-007-5637
Turbine Nozzle Turbine Engi Vane
00-007-5638
Turbine Nozzle Turbine Engi Vane
00-007-5639
Turbine Aircraft Nozzle Segment
Used on model t56 engine.
00-007-9782
Combustion Aircraft Gas Chamber
00-008-0007
Gearbox Turbine Engine Housing
Used on J85.
00-008-0009
Turbine Component Aircraft Liner
Used on acft eng j85. 15.440" overall length original name liner, afterburner t.o. 2j-J85-94, fig 22, ind 81; liner, mid front; 2nd end dia. 17.230
00-008-0010
Augmentor Component Aircra Liner
Used on acft engine j85.
00-008-0032
Compressor Aircraft Gas Tu Rotor
Used on acft eng. tf-39.
00-008-0033
Air Aircraft Gas Turbine En Seal
Used on tf39 eng. 1.956" overall length id 9.04 min/9.06 max in.
00-008-6164
Combustion Chamber Aircraft Case
Used on acft eng. j-85. 16.000" overall length t.o. 2j-J85-94; includes stages 1-9; original name casing, compressor
00-008-6165
Compressor Aircraft Gas Tu Rotor
Used on j85 model aircraft engine. 6.076" overall length rotor spool, rear-compressor
