Material determines chemical compatibility Standard durometer is 70 Shore A
Wrong material = catastrophic seal failure
PRODUCT OVERVIEW
The STRAINER ELEMENT,SEDIMENT is a the manufacturer industrial component. Key specifications include material: STEEL OVERALL, head_style: PAN, fastener_length: 0.500 INCHES NOMINAL IN, surface_treatment: ZINC OVERALL, internal_drive_style: TORX, end_item_identification: MRAP-MAXXPRO RECOVERY VEHICLE;MRAP - MAXXPRO DASH ISS W/OGPK AND W/CROWS. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5331-00-297-7106, 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
11845-1
NSN:5331-00-297-7106 FSC:5331 — O-RING CAGE:34623 — AM GENERAL LLC (USA)
SPECIFICATIONS
material
STEEL OVERALL
head_style
PAN
fastener_length
0.500 INCHES NOMINAL IN
surface_treatment
ZINC OVERALL
internal_drive_style
TORX
end_item_identification
MRAP-MAXXPRO RECOVERY VEHICLE;MRAP - MAXXPRO DASH ISS W/OGPK AND W/CROWS
nonmachine_thread_style
DOG TYPE (TYPE B OR C)
nonmachine_nominal_thread_diameter
0.1380 INCHES IN
part_name_assigned_by_controlling_agency
SCREW, TORX, THREAD CUTTING
NSN
5331-00-297-7106
COMPONENT DIAGRAM
KEY FEATURES
•
MATERIAL: RUBBER ISOBUTYLENE-ISOPRENE CLASS IIR
•
CENTER HOLE DIAMETER: 4.1155 INCHES MINIMUM AND 4.2395 INCHES MAXIMUM IN
•
CROSS-SECTIONAL HEIGHT: 0.120 INCHES MINIMUM AND 0.135 INCHES MAXIMUM IN
TECHNICAL CHARACTERISTICS (FLIS)
END ITEM IDENTIFICATION
HIGH-MOBILITY ARTILLERY ROCKET SYSTEM (HIMARS)
MATERIAL
RUBBER ISOBUTYLENE-ISOPRENE CLASS IIR
CENTER HOLE DIAMETER
4.1155 INCHES MINIMUM AND 4.2395 INCHES MAXIMUM IN