PartsTable
Technical Data Sheet
424848 ✓ Verified by PartsTable
· NUT WASHER
WHAT YOU NEED TO KNOW
Match nut grade to bolt grade for full strength Lock nuts prevent loosening under vibration
Don't mix grades — weakens the joint
PRODUCT OVERVIEW

IGNITER,SPARK,GAS TURBINE ENGINE. Key specifications include component_quantity: 24, nonsupply_items_and_quantities: PACKING,PREFORMED 10;BACKUP RING 9;DISK SUB-ASSY 1;SEAL SPRING 4. This product is currently in active production with full OEM support.

This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5315-00-042-4848, 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
424848
NSN: 5315-00-042-4848
FSC: 5315
CAGE: 24617 — GENERAL MOTORS CORP (USA)
SPECIFICATIONS
component_quantity24
nonsupply_items_and_quantitiesPACKING,PREFORMED 10;BACKUP RING 9;DISK SUB-ASSY 1;SEAL SPRING 4
NSN5315-00-042-4848
COMPONENT DIAGRAM
NUT & WASHER — GRADE MATCHING REQUIRED Hex NUT CROSS-SECTION WASHER OD: — SIZE: — MATERIAL: — PN: 424848 · OEM ⚠ VERIFY BEFORE ORDERING Grade matters for torque spec — don't mix grades. A Grade 5 nut on a Grade 8 bolt weakens the joint. Lock nuts, wing nuts, and castle nuts are NOT interchangeable with standard hex ✓ BROKER TIP Match nut to bolt thread class and material. Stainless bolt + zinc nut = galvanic corrosion. Always verify finish matches (plain, zinc, hot-dip galvanized) PARTSTABLE TECHNICAL DRAWING — NOT TO SCALE
KEY FEATURES
SECOND END RELATIONSHIP WITH FIRST END: IDENTICAL
FIRST END TAPER ANGLE: 25.0 DEGREES NOMINAL
PIN OVERALL DIAMETER: 0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM IN
MATERIAL DOCUMENT AND CLASSIFICATION: MIL-B-994 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL
FIRST END TAPER LENGTH: 0.016 INCHES NOMINAL IN
MATERIAL: COPPER ALLOY 464 OVERALL
PIN OVERALL LENGTH: 0.738 INCHES MINIMUM AND 0.762 INCHES MAXIMUM IN
FIRST END STYLE: CHAMFERED
TECHNICAL CHARACTERISTICS (FLIS)
SECOND END RELATIONSHIP WITH FIRST ENDIDENTICAL
FIRST END TAPER ANGLE25.0 DEGREES NOMINAL
PIN OVERALL DIAMETER0.2480 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM IN
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-B-994 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL
FIRST END TAPER LENGTH0.016 INCHES NOMINAL IN
MATERIALCOPPER ALLOY 464 OVERALL
PIN OVERALL LENGTH0.738 INCHES MINIMUM AND 0.762 INCHES MAXIMUM IN
FIRST END STYLECHAMFERED
VERIFIED SUBSTITUTES & CROSS-REFERENCES 9
252533R91Interchangeable
interchangeable cross-reference
interchangeable
748SInterchangeable
interchangeable cross-reference
interchangeable
BB26246Interchangeable
interchangeable cross-reference
interchangeable
AA33SCInterchangeable
interchangeable cross-reference
interchangeable
AA33SDInterchangeable
interchangeable cross-reference
interchangeable
AA33SInterchangeable
interchangeable cross-reference
interchangeable
LIFECYCLE
StatusACTIVE
AvailabilityOEM and secondary market
RoHS CompliantEAR99Not HAZMAT
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FREQUENTLY ASKED QUESTIONS
What is 424848?
424848 is a IGNITER,SPARK,GAS TURBINE ENGINE.
What parts can replace 424848?
There are 9 known substitutes for 424848: 252533R91, 748S, BB26246 and 6 more. Substitute compatibility should be verified for your specific system.
What is the NSN for 424848?
424848 is cataloged in the Federal Logistics Information System (FLIS) under NSN 5315-00-042-4848. This indicates validated use in U.S. government and defense supply chains.
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