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3040-00-128-7430
20 Products
206-001-502-5
BELL CRANK
NSN, MFG P/N
3040001287430
NSN
3040-00-128-7430
MFG
BELL HELICOPTER TEXTRON INC.
Description
BELL CRANK
Related Searches:
206-001-502-6
BELL CRANK
NSN, MFG P/N
3040001287431
NSN
3040-00-128-7431
MFG
BELL HELICOPTER TEXTRON INC.
Description
BELL CRANK
Related Searches:
206-001-033-3
SHAFT,SHOULDERED
NSN, MFG P/N
3040001287466
NSN
3040-00-128-7466
MFG
BELL HELICOPTER TEXTRON INC.
Description
DESIGN CONTROL REFERENCE: 206-001-033-3
END SIMILARITY: NOT IDENTICAL
FIRST END ANGLE BETWEEN KEYWAYS: 45.0 DEGREES NOMINAL
FIRST END TAPER LENGTH: 0.040 INCHES NOMINAL
LARGEST STEP DIAMETER: 0.562 INCHES NOMINAL
MANUFACTURERS CODE: 97499
MATERIAL: STEEL COMP 4130
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-6736,COND N MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH: 5.460 INCHES NOMINAL
STEP QUANTITY: 3
THE MANUFACTURERS DATA:
Related Searches:
206-001-033-1
SHAFT,SHOULDERED
NSN, MFG P/N
3040001287467
NSN
3040-00-128-7467
MFG
BELL HELICOPTER TEXTRON INC.
Description
DESIGN CONTROL REFERENCE: 206-001-033-1
END SIMILARITY: NOT IDENTICAL
FIRST END DIAMETER: 0.3750 INCHES NOMINAL
FIRST END EXTERNAL THREAD LENGTH: 2.600 INCHES NOMINAL
FIRST END STYLE: 12 EXTERNAL THREADED
LARGEST STEP DIAMETER: 0.562 INCHES NOMINAL
MANUFACTURERS CODE: 97499
MATERIAL: STEEL COMP 4130
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-T-6736,CONDITION N MIL SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH: 6.660 INCHES NOMINAL
SECOND END DIAMETER: 0.5625 INCHES NOMINAL
SECOND END STYLE: 1 PLAIN
STEP QUANTITY: 4
SURFACE FINISH: 125.0 MICROINCHES
THE MANUFACTURERS DATA:
Related Searches:
206-001-159-5
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287490
NSN
3040-00-128-7490
MFG
BELL HELICOPTER TEXTRON INC.
Description
III END ITEM IDENTIFICATION: OH-58A AND/OR C, ROTARY WING AIRCRAFT
Related Searches:
206-061-714
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287582
NSN
3040-00-128-7582
MFG
BELL HELICOPTER TEXTRON INC.
Description
CONNECTING LINK,RIGID
Related Searches:
206-061-714-5
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287582
NSN
3040-00-128-7582
MFG
MASTER SWAGING INC
Description
CONNECTING LINK,RIGID
Related Searches:
206-061-714-5
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287582
NSN
3040-00-128-7582
MFG
BELL HELICOPTER TEXTRON INC.
Description
CONNECTING LINK,RIGID
Related Searches:
206-062-713-1
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287584
NSN
3040-00-128-7584
MFG
BELL HELICOPTER TEXTRON INC.
Description
CONNECTING LINK,RIGID
Related Searches:
206-061-715-1
LEVER,REMOTE CONTROL
NSN, MFG P/N
3040001287589
NSN
3040-00-128-7589
MFG
BELL HELICOPTER TEXTRON INC.
Description
BORE TYPE: SERRATED
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES: 1.880 INCHES NOMINAL
DESIGN CONTROL REFERENCE: 206-061-715-1
FEATURES PROVIDED: SPLIT END SCREW CLAMPING FEATURE
LINK END HOLE DIAMETER: 0.126 INCHES MINIMUM AND 0.129 INCHES MAXIMUM
LINK END THICKNESS: 0.090 INCHES NOMINAL
MAJOR DIAMETER: 0.2550 INCHES MINIMUM AND 0.2610 INCHES MAXIMUM
MANUFACTURERS CODE: 97499
MATERIAL: ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-601, ALLOY 356, T6 FED SPEC SINGLE MATERIAL RESPONSE
MINOR DIAMETER: 0.2300 INCHES MINIMUM AND 0.2320 INCHES MAXIMUM
SERRATION QUANTITY: 19
SHAFT END THICKNESS: 0.380 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
206-061-715-1
LEVER,REMOTE CONTROL
NSN, MFG P/N
3040001287589
NSN
3040-00-128-7589
MFG
ROTAIR INDUSTRIES INC .
Description
BORE TYPE: SERRATED
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES: 1.880 INCHES NOMINAL
DESIGN CONTROL REFERENCE: 206-061-715-1
FEATURES PROVIDED: SPLIT END SCREW CLAMPING FEATURE
LINK END HOLE DIAMETER: 0.126 INCHES MINIMUM AND 0.129 INCHES MAXIMUM
LINK END THICKNESS: 0.090 INCHES NOMINAL
MAJOR DIAMETER: 0.2550 INCHES MINIMUM AND 0.2610 INCHES MAXIMUM
MANUFACTURERS CODE: 97499
MATERIAL: ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-601, ALLOY 356, T6 FED SPEC SINGLE MATERIAL RESPONSE
MINOR DIAMETER: 0.2300 INCHES MINIMUM AND 0.2320 INCHES MAXIMUM
SERRATION QUANTITY: 19
SHAFT END THICKNESS: 0.380 INCHES NOMINAL
THE MANUFACTURERS DATA:
Related Searches:
206-062-705-1
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001287602
NSN
3040-00-128-7602
MFG
BELL HELICOPTER TEXTRON INC.
Description
(NON-CORE DATA) MATERIAL: ALUMINUM ALLOY,AMS 4260 OR ALUMINUM ALLOY,QQ-A-225/6
BODY CONSTRUCTION: SOLID
BODY WIDTH: 0.250 INCHES NOMINAL
DESIGN CONTROL REFERENCE: 206-062-705-1
LINK STYLE: A12 CLEVIS ENDS
MANUFACTURERS CODE: 97499
OVERALL LENGTH: 2.710 INCHES MINIMUM AND 2.790 INCHES MAXIMUM
THE MANUFACTURERS DATA:
Related Searches:
102635
GEARSHAFT,SPUR
NSN, MFG P/N
3040001287635
NSN
3040-00-128-7635
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
GEARSHAFT,SPUR
Related Searches:
02636
GEARSHAFT,SPUR
NSN, MFG P/N
3040001287723
NSN
3040-00-128-7723
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
GEARSHAFT,SPUR
Related Searches:
102636
GEARSHAFT,SPUR
NSN, MFG P/N
3040001287723
NSN
3040-00-128-7723
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
GEARSHAFT,SPUR
Related Searches:
102620
GEARSHAFT,SPUR
NSN, MFG P/N
3040001287724
NSN
3040-00-128-7724
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
GEARSHAFT,SPUR
Related Searches:
102619
GEARSHAFT,SPUR
NSN, MFG P/N
3040001287738
NSN
3040-00-128-7738
MFG
ASTRONAUTICS CORPORATION OF AMERICA
Description
GEARSHAFT,SPUR
Related Searches:
128CM11259
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001288113
NSN
3040-00-128-8113
MFG
NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE SYSTEMS
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.703 INCHES NOMINAL
BODY WIDTH: 1.106 INCHES NOMINAL
OVERALL LENGTH: 2.001 INCHES NOMINAL
Related Searches:
128CM11259-3
CONNECTING LINK,RIGID
NSN, MFG P/N
3040001288113
NSN
3040-00-128-8113
MFG
NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE SYSTEMS
Description
BODY CONSTRUCTION: SOLID
BODY THICKNESS: 0.703 INCHES NOMINAL
BODY WIDTH: 1.106 INCHES NOMINAL
OVERALL LENGTH: 2.001 INCHES NOMINAL
Related Searches:
9451737
ADAPTER,SPLINE
NSN, MFG P/N
3040001288928
NSN
3040-00-128-8928
MFG
GENERAL ELECTRIC COMPANY DBA GE DIV GE - AVIATION
Description
ADAPTER,SPLINE
