1650-01-089-6812, SERVOCYLINDER

9905-01-089-6811 PLATESET,FIREEXTINGUISHER

5130-01-089-6814 RIVETER,BLIND,PNEUMATIC

National Stock Number:
1650-01-089-6812

Federal Supply Class:
1650

National Item Identification Number:
010896812

Description:
SERVOCYLINDER

Detail:
A HYDRAULICALLY OR PNEUMATICALLY POWERED ACTUATING CYLINDER WITH PROVISIONS FOR DIRECTIONAL CONTROL (POSITIONING) IN DIRECT RELATION WITH A PRIMARY CONTROL OF COMPARATIVELY LOW LEVEL FORCE. THE PRIMARY CONTROL INPUT TO THE SERVOCYLINDER MAY BE MECHANICAL AND/OR ELECTRICAL.

Manufacturer Information:

3186800-9	0ZWK8	MOOG MILITARY AIRCRAFT LLC
3186800-9	59364	HONEYWELL INTERNATIONAL INC.
A51H9004-9	26512	NORTHROP GRUMMAN SYSTEMS CORPORATION
A51H9004-9	61174	NORTHROP GRUMMAN SYSTEMS CORPORATION
3186800-9	77068	ALLIED-SIGNAL INC DBA ALLIED-SIGNAL AEROSPACE CO ELECTRODYNAMICS DIV
A51H9004-9	79RG9	NORTHROP GRUMMAN SYSTEMS CORPORATION

Techincal Specification:

BORE DIAMETER	2.431 INCHES NOMINAL
COMPRESSED LENGTH	17.375 INCHES NOMINAL
DESIGN CHARACTERISTICS	SINGLE ACTING SINGLE CYLINDER
EXTENDED LENGTH	21.625 INCHES NOMINAL
FIRST END OUTSIDE DIAMETER	2.206 INCHES NOMINAL
FIRST END THICKNESS AT MOUNTING HOLES	0.748 INCHES MINIMUM AND 0.750 INCHES MAXIMUM
INTEGRAL VALVE OPERATION METHOD	HYDRAULIC
OVERALL WIDTH	10.000 INCHES NOMINAL
MATERIAL	STEEL BODY
PISTON ROD END SIMILARITY	NOT IDENTICAL
PRESSURE RATING	3000.0 POUNDS PER SQUARE INCH (PSI) NOMINAL
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS	AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO.
SECOND END THICKNESS AT MOUNTING HOLES	0.735 INCHES MINIMUM AND 0.745 INCHES MAXIMUM
SECOND END OUTSIDE DIAMETER	2.500 INCHES NOMINAL
SECOND PISTON ROD END STYLE	BEARING TYPE
TEMP RATING	-65.0 FAHRENHEIT
TEMP RATING	275.0 FAHRENHEIT

Click here to Register for Free 30-day Trial