01-124-0723
Turbine Nozzle Aircraf Lock Ring
Used on acft eng tf33. 34.878" outside diameter matl ams 5731
01-124-0724
Turbine Nozzle Aircraf Lock Ring
Used on acft eng tf33. 34.878" outside diameter matl ams 5731
01-124-0725
Turbine Nozzle Aircraf Lock Ring
Used on acft eng tf33. 34.878" outside diameter matl ams 5731
01-124-0726
Turbine Nozzle Aircraf Lock Ring
Used on acft eng tf33. 34.878" outside diameter matl ams 5731
01-124-0763
Turbine Case And Nozzle Assembly
Used on acft eng f100. this nsn is an F100 fracture critical part. original name case
01-124-0764
Turbine Aircraft Ga Disk And Hub
Used on acft eng tf41. was disk
01-124-0765
Turbine Aircraft Gas T Blade Set
Used on F-100.
01-124-0915
Turbine Rotor Aircraft Gas Blade
Used on jet engine model f140. blades are preground
01-124-3243
Metallic Aircraft Gas Turbi Seal
Used on acft eng tf41. 0.355" overall length matl ams 5616
01-124-3245
Air Aircraft Gas Turbine En Seal
Used on acft eng tf41. matl ams 5703
01-124-3247
Air Aircraft Gas Turbine En Seal
Used on acft eng tf41.
01-124-4054
Compressor Ai Synchronizing Ring
Used on jet engine model f404.
01-124-4759
Combustion Chamber Aircraf Liner
Used on acft eng tf 41. 3.050" overall length
01-124-4760
Air Aircraft Gas Turbine En Seal
Used on acft eng tf-33. 1.488" overall length ring seal, turbine, 2 stage
01-124-4761
Component Mounting Aircraf Plate
Used on tf-41 aircraft gas turbine engine. 1.484" overall length 0.461" overall width original name connector, sliding liner t.o. 2j-TF41-4, fig 78a, ind 37; turbine unit assy, liner nos 2, 4, 6, 8
01-124-4768
Air Aircraft Gas Turbine En Seal
Used on acft eng tf 33. matl ams 5754
01-124-4770
Turbine Blade Aircraft Retainer
Used on acft eng tf 41. 0.072" overall length
01-124-4772
Turbine Aircraft Gas Turbi Rotor
Used on acft eng tf 41.
01-124-4776
Turbine Aircraft Gas Turbi Rotor
Used on acft eng tf 41.
01-124-4799
Turbine Component Aircraft Liner
Used on acft eng tf39. t.o. 2j-TF39-4, fig 66 ind 7; used on the turbine mid frame liner support
01-124-4876
Turbine Rotor Aircraft Gas Blade
Used on acft eng tf 41. 4.004" overall length 1.258" overall width
01-124-7403
Turbine Aircraft Gas Turbin Case
Used on acft eng f100. matl ams 5540
01-124-7500
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; 1.692-1.711 sq. in. area; turbine stator support; replaced p/ns 4045951clj, 4059191clj
01-124-8121
Component Mounting Aircraf Plate
Used on acft eng j 69. 0.308" overall length matl ams 5668
01-125-2208
Compressor Aircraft Gas Tur Vane
Used on acft eng f100. original name vane, compressor stator, turbine engine
01-125-2212
Turbine Aircraft Gas Turb Nozzle
Used on acft eng j69.
01-125-2974
Exhaust Aircraft Gas Turbi Frame
Used on engine model tf34-ge-400a.
01-125-3768
Combustion Chamber Aircraf Liner
Used on acft eng tf 34. matl ams 5536
01-125-3840
Turbine Rotor Aircraft Gas Blade
Used on acft eng f100. 3.945" overall length 0.829" overall width original name blade, turbine rotor, turbine engine
01-125-3841
Turbine Rotor Aircraft Gas Blade
Used on acft eng tf 41. 11.343" overall length 0.158" material thickness
01-125-3847
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 32; 1.730-1.749 sq. in. area; 1800 cycle; turbine stator support; replaced by p/ns 4056781cll
01-125-3848
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; turbine stator support; 1.768-1.787 sq. in. area; reid/replaced p/n 4045951cln
01-125-3849
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1.692-1.711 sq. in. area; turbine stator support; reid/replaced p/n 4045951clj
01-125-3850
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; 1.711-1.730 sq. in. area; turbine stator support; reid/replaced p/n 4045951clk
01-125-3851
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbinee ngine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; 1.730-1.749 sq. in. area; turbine stator support; reid/replaced p/n 4045951cll
01-125-3852
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; 1.747-1.768; reid/replaced p/n 4045951clm, replaced by 4056771clm
01-125-3853
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 32; 1.730-1.749 sq inch area; turbine stator support; 1800 cycle; replaces p/n 4056781cll; replaced by 4070251cll
01-125-3854
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1.711-1.730 sq. in. area; turbine stator support; 1800 cycle; replaced p/ns 4059191clk
01-125-3855
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; turbine stator support; 1.730-1.749 sq. in. area; replaced p/n 4059191cll
01-125-3856
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; 1.749-1.768 sq. in. area; turbine stator support; reid/replaced p/ns 4045951clm ad 4059191clm
01-125-3857
Turbine Aircraft Nozzle Segment
Used on acft eng f100. original name vane, compressor, aircraft gas turbine engine t.o. 2j-F100-14, fig 155, ind 30; 1800 cycle; turbine stator support; 1.768-1.787 sq. in. area; replaces p/n 4045951cln
01-125-4898
Turbo-jet Engine
01-125-7338
Lubricating Aircraft Gas Nozzle
Used on aircraft model h-53. 2.260" overall length 1.590" overall width
01-125-7339
Lubricating Aircraft Gas Nozzle
Used on aircraft model h-53. 6.547" overall length
01-125-7340
Lubricating Aircraft Gas Nozzle
Used on aircraft model h-53. 0.046 in. dia.
01-125-7341
Lubricating Aircraft Gas Nozzle
Used on aircraft model h-53.
01-125-7342
Lubricating Aircraft Gas Nozzle
Used on aircraft model h-53.
01-125-7343
Turbine Aircraft Gas Turb Nozzle
Used on aircraft model s-3a. inconel 625 AMS5599; 29.900 in.lg, 26.280 in.dia o/a; 30 holes 0.221 in.dia on a 25.860 in.dia bolt circle;
01-125-8862
Exhaust Aircraft Gas Turbin Duct
Inconel per AMS5599, composition 625
01-125-8863
Lubricating Aircraft Gas Nozzle
Used on jet engine model f404. anodize surface treated
