191C532 — STARTER,ENGINE,ELECTRICAL

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

191C532: STARTER,ENGINE,ELECTRICAL.

The STARTER,ENGINE,ELECTRICAL is a the manufacturer industrial component. Key specifications include special_features: SUPPORTS GRUMMAN A10 AIRCRAFT, voltage_in_volts: 12.0, mounting_hole_diameter: 0.406 INCHES MINIMUM AND 0.407 INCHES MAXIMUM IN, engaging_mechanism_style: PERIPHERAL OUTBOARD GEAR DRIVE W/WORM SHAFT AND TORSION DRIVE SPRING W/DRIVE HOUSING, shaft_rotation_direction: COUNTERCLOCKWISE, terminal_type_and_quantity: 1 THREADED STUD. This part is cataloged in the U.S.

Government catalog under NSN 2920-00-132-4683, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS

191C532

NSN: 2920-00-132-4683
FSC: 2920 — Engine Electrical System Components, Nonaircraft
CAGE: 44940 — CUMMINS POWER GENERATION INC. (USA)

SPECIFICATIONS

special_features	SUPPORTS GRUMMAN A10 AIRCRAFT
voltage_in_volts	12.0
mounting_hole_diameter	0.406 INCHES MINIMUM AND 0.407 INCHES MAXIMUM IN
engaging_mechanism_style	PERIPHERAL OUTBOARD GEAR DRIVE W/WORM SHAFT AND TORSION DRIVE SPRING W/DRIVE HOUSING
shaft_rotation_direction	COUNTERCLOCKWISE
terminal_type_and_quantity	1 THREADED STUD
mounting_flange_shape_style	TRIANGULAR
mounting_hole_circle_radius	2.062 INCHES NOMINAL IN
lock_test_current_rating_in_amps	235.0
mounting_flange_angular_deviation_in_deg	158.0
engaging_mechanism_opening_angular_deviation_in_deg	112.0
engaging_mechanism_to_armature_positional_relationship	STRAIGHT
NSN	2920-00-132-4683

COMPONENT DIAGRAM

KEY FEATURES

•

VOLTAGE IN VOLTS: 12.0

•

ENGAGING MECHANISM OPENING ANGULAR DEVIATION IN DEG: 112.0

•

MOUNTING HOLE DIAMETER: 0.406 INCHES MINIMUM AND 0.407 INCHES MAXIMUM IN

•

SHAFT ROTATION DIRECTION: COUNTERCLOCKWISE

•

MOUNTING FLANGE SHAPE STYLE: TRIANGULAR

•

ENGAGING MECHANISM TO ARMATURE POSITIONAL RELATIONSHIP: STRAIGHT

•

MOUNTING FLANGE ANGULAR DEVIATION IN DEG: 158.0

•

MOUNTING HOLE CIRCLE RADIUS: 2.062 INCHES NOMINAL IN

TECHNICAL CHARACTERISTICS

VOLTAGE IN VOLTS	12.0
ENGAGING MECHANISM OPENING ANGULAR DEVIATION IN DEG	112.0
MOUNTING HOLE DIAMETER	0.406 INCHES MINIMUM AND 0.407 INCHES MAXIMUM IN
SHAFT ROTATION DIRECTION	COUNTERCLOCKWISE
MOUNTING FLANGE SHAPE STYLE	TRIANGULAR
ENGAGING MECHANISM TO ARMATURE POSITIONAL RELATIONSHIP	STRAIGHT
MOUNTING FLANGE ANGULAR DEVIATION IN DEG	158.0
MOUNTING HOLE CIRCLE RADIUS	2.062 INCHES NOMINAL IN
SPECIAL FEATURES	SUPPORTS GRUMMAN A10 AIRCRAFT
LOCK TEST CURRENT RATING IN AMPS	235.0

SUBSTITUTES & CROSS-REFERENCES 2

MBG4134ATReference document

Same NSN cross-reference

Reference document — Secondary reference

191-0532Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 191C532?

191C532 is a STARTER,ENGINE,ELECTRICAL.

What parts can replace 191C532?

There are 2 known substitutes for 191C532: MBG4134AT, 191-0532. Substitute compatibility should be verified for your specific system.

What is the NSN for 191C532?

191C532 is cataloged in the U.S. Government catalog under NSN 2920-00-132-4683. This indicates validated use in U.S. government and defense supply chains.

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191C532 — STARTER,ENGINE,ELECTRICAL

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