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3040-01-057-1546
20 Products
4814128
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
4814128
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
MFG
KALMAR AC INC
Description
(NON-CORE DATA) FIRST PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
(NON-CORE DATA) SECOND PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
BODY MATERIAL: STEEL, STAINLESS
BORE DIAMETER: 3.750 INCHES NOMINAL
COMPRESSED LENGTH: 11.688 INCHES NOMINAL
DESIGN CHARACTERISTICS: DOUBLE ACTING SINGLE CYLINDER
EXTENDED LENGTH: 14.438 INCHES NOMINAL
FIRST PISTON ROD END STYLE: 7 EXTERNAL THREADED
MOUNTING TYPE AND LOCATION: TRUNNION CYLINDER HEAD END
PORT LOCATION AND QUANTITY: 1 CYLINDER HEAD END 1 PISTON ROD END
PORT STYLE: 5 GASKET SEAL
PORT THREAD CLASS: 2B
PORT THREAD DIAMETER: 0.437 INCHES NOMINAL
PORT THREAD QUANTITY PER INCH: 20
PORT THREAD SERIES DESIGNATOR: UNF
Related Searches:
4828465-1
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
4828465-1
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
MFG
KALMAR AC INC
Description
(NON-CORE DATA) FIRST PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
(NON-CORE DATA) SECOND PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
BODY MATERIAL: STEEL, STAINLESS
BORE DIAMETER: 3.750 INCHES NOMINAL
COMPRESSED LENGTH: 11.688 INCHES NOMINAL
DESIGN CHARACTERISTICS: DOUBLE ACTING SINGLE CYLINDER
EXTENDED LENGTH: 14.438 INCHES NOMINAL
FIRST PISTON ROD END STYLE: 7 EXTERNAL THREADED
MOUNTING TYPE AND LOCATION: TRUNNION CYLINDER HEAD END
PORT LOCATION AND QUANTITY: 1 CYLINDER HEAD END 1 PISTON ROD END
PORT STYLE: 5 GASKET SEAL
PORT THREAD CLASS: 2B
PORT THREAD DIAMETER: 0.437 INCHES NOMINAL
PORT THREAD QUANTITY PER INCH: 20
PORT THREAD SERIES DESIGNATOR: UNF
Related Searches:
74828465
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
74828465
CYLINDER ASSEMBLY,ACTUATING,LINEAR
NSN, MFG P/N
3040010571546
NSN
3040-01-057-1546
MFG
KALMAR AC INC
Description
(NON-CORE DATA) FIRST PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
(NON-CORE DATA) SECOND PISTON ROD END LUBRICATION FACILITY: NOT INCLUDED
BODY MATERIAL: STEEL, STAINLESS
BORE DIAMETER: 3.750 INCHES NOMINAL
COMPRESSED LENGTH: 11.688 INCHES NOMINAL
DESIGN CHARACTERISTICS: DOUBLE ACTING SINGLE CYLINDER
EXTENDED LENGTH: 14.438 INCHES NOMINAL
FIRST PISTON ROD END STYLE: 7 EXTERNAL THREADED
MOUNTING TYPE AND LOCATION: TRUNNION CYLINDER HEAD END
PORT LOCATION AND QUANTITY: 1 CYLINDER HEAD END 1 PISTON ROD END
PORT STYLE: 5 GASKET SEAL
PORT THREAD CLASS: 2B
PORT THREAD DIAMETER: 0.437 INCHES NOMINAL
PORT THREAD QUANTITY PER INCH: 20
PORT THREAD SERIES DESIGNATOR: UNF
Related Searches:
1685192-1
PAWL
NSN, MFG P/N
3040010571842
NSN
3040-01-057-1842
MFG
TELAIR INTERNATIONAL INCORPORATED DBA NORDISK AVIATION SERVICES
Description
DESIGN CONTROL REFERENCE: 1685192-1
III END ITEM IDENTIFICATION: F-16 ACFT
MANUFACTURERS CODE: 98889
MATERIAL THICKNESS: 0.150 INCHES NOMINAL
SPECIAL FEATURES: CASEHARDENED;MATERIAL DOCUMENT AND CLASSIFICATION:STEEL COMP 4130;SURFACE FINISH:PASSIVATED
THE MANUFACTURERS DATA:
Related Searches:
11507849
EXTENSION SHAFT
NSN, MFG P/N
3040010572206
NSN
3040-01-057-2206
MFG
U S ARMY AVIATION AND MISSILE COMMAND
Description
EXTENSION SHAFT
Related Searches:
7381
EXTENSION SHAFT
NSN, MFG P/N
3040010572206
NSN
3040-01-057-2206
MFG
SCHRADER-BRIDGEPORT INTERNATIONAL INC DBA SCHRADER AUTOMOTIVE
Description
EXTENSION SHAFT
Related Searches:
7381F-198
EXTENSION SHAFT
NSN, MFG P/N
3040010572206
NSN
3040-01-057-2206
MFG
SCHRADER-BRIDGEPORT INTERNATIONAL INC DBA SCHRADER AUTOMOTIVE
Description
EXTENSION SHAFT
Related Searches:
1685134-1
SHAFT,BALL SCREW
NSN, MFG P/N
3040010572299
NSN
3040-01-057-2299
MFG
TELAIR INTERNATIONAL INCORPORATED DBA NORDISK AVIATION SERVICES
Description
DESIGN CONTROL REFERENCE: 1685134-1
GENERAL CHARACTERISTICS ITEM DESCRIPTION: 45.320 IN. LG;STEEL AMS 6415;FINISH BLACK OXIDE MIL-C-13924 CL 1;SURFACE ROUGHNESS 125.0 RMS;1ST END 1ST STEP PLAIN,0.534 IN. LG,0.749 IN. DIA:1ST END 2ND STEP SPLINED,0.251 IN. LG,39 TEETH,0.825 IN. PITCH DIA,0.833 IN. MAJ DIA;1ST END 3RD STEP
MANUFACTURERS CODE: 98889
THE MANUFACTURERS DATA:
~1: PLAIN,0.155 IN. LG,0.773 IN. DIA;1ST END 4TH STEP PLAIN,0.340 IN. LG,0.835 IN. DIA;2ND END 1ST STEP THREADED,0.750-20 UNJEF-3A LH;2ND END 2ND STEP PLAIN,0.050 IN. LG,0.690 IN. DIA;2ND END 3RD STEP SPLINED,0.620 IN. LG,39 TEETH,0.825 IN. PITCH DIA,0.833
~2: IN. MAJ DIA;2ND END 4TH STEP PLAIN,0.190 IN. LG,0.773 IN. DIA;BALL BEARING SCREW DATA:0.333 LFAD RH THDS,1.002 IN. MAJ DIA,0.841 IN. MIN DIA
Related Searches:
53G970601
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
BOEING COMPANY THE DBA BOEING
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
53G970601-15
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
BOEING COMPANY THE DBA BOEING DIV DEFENSE SPACE & SECURITY - GLOBAL MOBILITY SYSTEMS
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
53G970601-15
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
AERO TECHNOLOGY COMPANY
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
53G970601-15
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
BOEING COMPANY THE DBA BOEING
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
53G970601-3
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
BOEING COMPANY THE DBA BOEING
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
CS3040-SR-0702
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
DLA LAND AND MARITIME
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
G970601-15
CONNECTING LINK,RIGID
NSN, MFG P/N
3040010572590
NSN
3040-01-057-2590
MFG
BOEING COMPANY THE DBA BOEING
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH: 0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION: FEAT
III END ITEM IDENTIFICATION: AIRCRAFT F-4 & F-5
LINK STYLE: A1 STRAIGHT
MATERIAL: ALUMINUM ALLOY
OVERALL LENGTH: 2.200 INCHES NOMINAL
SPECIAL FEATURES: NEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENT: ANODIZE
Related Searches:
53G970619-39
SHAFT,STRAIGHT
NSN, MFG P/N
3040010572592
NSN
3040-01-057-2592
MFG
BOEING COMPANY THE DBA BOEING DIV DEFENSE SPACE & SECURITY - GLOBAL MOBILITY SYSTEMS
Description
DESIGN CONTROL REFERENCE: 53G970619-39
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.4370 INCHES NOMINAL
FIRST END STYLE: 1 PLAIN
MANUFACTURERS CODE: 88277
MATERIAL: STEEL CORROSION RESISTING
OVERALL LENGTH: 1.312 INCHES NOMINAL
SECOND END DIAMETER: 0.4370 INCHES NOMINAL
SECOND END INTERNAL THREAD LENGTH: 0.625 INCHES NOMINAL
SECOND END STYLE: 9 INTERNAL THREADED
SURFACE FINISH: 10.0 MICROINCHES
THE MANUFACTURERS DATA:
Related Searches:
53G970619-39
SHAFT,STRAIGHT
NSN, MFG P/N
3040010572592
NSN
3040-01-057-2592
MFG
BOEING COMPANY THE DBA BOEING
Description
DESIGN CONTROL REFERENCE: 53G970619-39
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.4370 INCHES NOMINAL
FIRST END STYLE: 1 PLAIN
MANUFACTURERS CODE: 88277
MATERIAL: STEEL CORROSION RESISTING
OVERALL LENGTH: 1.312 INCHES NOMINAL
SECOND END DIAMETER: 0.4370 INCHES NOMINAL
SECOND END INTERNAL THREAD LENGTH: 0.625 INCHES NOMINAL
SECOND END STYLE: 9 INTERNAL THREADED
SURFACE FINISH: 10.0 MICROINCHES
THE MANUFACTURERS DATA:
Related Searches:
S108198
SHAFT,STRAIGHT
NSN, MFG P/N
3040010572593
NSN
3040-01-057-2593
MFG
CNH AMERICA LLC
Description
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.6240 INCHES NOMINAL
FIRST END INTERNAL THREAD LENGTH: ANY ACCEPTABLE
FIRST END STYLE: 9 INTERNAL THREADED
MATERIAL: STEEL
OVERALL LENGTH: 4.690 INCHES NOMINAL
SECOND END DIAMETER: 0.6240 INCHES NOMINAL
SECOND END DISTANCE FROM HOLE CENTER TO END: 1.188 INCHES NOMINAL
SECOND END HOLE DEPTH: 0.624 INCHES NOMINAL
SECOND END HOLE DIAMETER: 0.1500 INCHES NOMINAL
SECOND END STYLE: 11 UNTHREADED CROSS DRILLED
Related Searches:
CD-102116
SHAFT,SHOULDERED
NSN, MFG P/N
3040010572594
NSN
3040-01-057-2594
MFG
RAYCO WYLIE WEIGHLOAD ELECTRONIC SYSTEMS INC
Description
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.5000 INCHES NOMINAL
FIRST END EXTERNAL THREAD LENGTH: 0.750 INCHES NOMINAL
FIRST END STYLE: 12 EXTERNAL THREADED
LARGEST STEP DIAMETER: 0.999 INCHES NOMINAL
MATERIAL: STEEL
OVERALL LENGTH: 4.560 INCHES NOMINAL
SECOND END DIAMETER: 0.5000 INCHES NOMINAL
SECOND END EXTERNAL THREAD LENGTH: 1.140 INCHES NOMINAL
SECOND END STYLE: 12 EXTERNAL THREADED
STEP QUANTITY: 6
Related Searches:
D4016
SHAFT,SHOULDERED
NSN, MFG P/N
3040010572594
NSN
3040-01-057-2594
MFG
RAYCO WYLIE WEIGHLOAD ELECTRONIC SYSTEMS INC
Description
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.5000 INCHES NOMINAL
FIRST END EXTERNAL THREAD LENGTH: 0.750 INCHES NOMINAL
FIRST END STYLE: 12 EXTERNAL THREADED
LARGEST STEP DIAMETER: 0.999 INCHES NOMINAL
MATERIAL: STEEL
OVERALL LENGTH: 4.560 INCHES NOMINAL
SECOND END DIAMETER: 0.5000 INCHES NOMINAL
SECOND END EXTERNAL THREAD LENGTH: 1.140 INCHES NOMINAL
SECOND END STYLE: 12 EXTERNAL THREADED
STEP QUANTITY: 6
