Part identity

A1-4001

Clevis Rod End

Aviation Industries Corp

Avg quote: 14 minFulfilled from Anaheim, CAAS9120:2025 · ISO 9001 · FAA AC 00-56BC of C, lot & date code with every line

Part description

Clevis Rod End

ASAP supports this specific part for replacement, spare-pool replenishment, retrofit, and urgent maintenance requirements. Quote requests can include alternate MPN, condition preferences, certification needs, and plant-specific receiving instructions so procurement gets a clear sourcing response before purchase.

Specifications

MPN
A1-4001
Item name
Clevis Rod End
Manufacturer code
30918
Manufacturer
Aviation Industries Corp

Certifications & documentation

  • UL Recognized
  • CE
  • C of C available on request
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Manufacturer

Aviation Industries Corp

Authorized-distributor or qualified-aftermarket source. Parts shipped from this manufacturer include full traceability paperwork and counterfeit-mitigation per SAE AS6081.

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NSN Information for Part Number A1-4001 with NSN 5340-00-596-4923, 5340005964923

NSNFSCNIINCLSHazmatDEMILCancelled NSN
5340005964923

Item PartTypeName:

CLEVIS,ROD END

53400059649230P
CIICHCCESDPMICCriticalityENAC
UU
Part NumberISCRNVCRNCCHCCMSDSSADC
A1-4001695

Characteristics Data of NSN 5340-00-596-4923, 5340005964923

MRCCriteriaCharacteristic
AAJDTHREAD CLASS2A ROD CONNECTION
AAJFTHREAD DIRECTIONRIGHT-HAND ROD CONNECTION
AASATHREAD LENGTH2.750 INCHES NOMINAL ROD CONNECTION
AATRSHANK LENGTH3.100 INCHES NOMINAL
AAUBHOLE DIAMETER0.312 INCHES MINIMUM AND 0.318 INCHES MAXIMUM
AAZESHANK DIAMETER0.739 INCHES MINIMUM AND 0.748 INCHES MAXIMUM
ABKWOVERALL HEIGHT1.750 INCHES NOMINAL
ABMKOVERALL WIDTH1.750 INCHES NOMINAL
ABPZEND RADIUS0.940 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONUAIRCRAFT,B-2 BOMBER (ATB),SUPPORT EQUIPMENT,T-37AIRCRAFT,SUPPORT EQUIPMENT,T-38 AIRCRAFT,ENGINE,AIRCRAFT,F110-GE-100/129 (F-16C/D),AIRCRAFT,STRATOLIFTER C-135,SUPPORT EQUIPMENT,F-106 AIRCRAFT,AIRCRAFT,THUNDERBOLT II,A-10
AJSDFORK SPAN WIDTH0.995 INCHES MINIMUM AND 1.010 INCHES MAXIMUM
AKYESECURING PIN HOLE DIAMETER0.312 INCHES MINIMUM AND 0.318 INCHES MAXIMUM
AKYHDISTANCE FROM CENTER OF SECURING PIN HOLE TO ROD END5.880 INCHES NOMINAL
AKYVDISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END5.880 INCHES NOMINAL
AKYWFORK ARM THICKNESS0.377 INCHES NOMINAL
AKYXFORK DEPTH2.000 INCHES NOMINAL
CQJXNOMINAL THREAD SIZE0.750 INCHES ROD CONNECTION
MATTMATERIALSTEEL COMP 1212 OR STEEL COMP 5015 OVERALL
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAISI/SAE ASSN STD 1ST MATERIAL RESPONSE OVERALL
SFTTSURFACE TREATMENTCADMIUM OVERALL
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416,TYPE 2,CLASS 1 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
STYLSTYLE DESIGNATORCLEVIS
THSDTHREAD SERIES DESIGNATORUNF ROD CONNECTION
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Certifications

  • AS9120:2025
  • ISO 9001:2015
  • FAA AC 00-56B
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