9535-01-532-0507 ( AMS-QQ-A-250/8-CDH34-0,02X12X36 , AMS-QQ-A-250/8 , AMS-QQ-A-250/8-H34-0.020X12X36 )

NSN Information
NSN FSC NIIN Item Name INC
9535-01-532-0507 9535 015320507 SHEET,METAL 3701
NSN Features
MRC Parameter Characteristics
MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/8
ADVM CROSS-SECTIONAL THICKNESS 0.0200 INCHES NOMINAL
CQHQ MINIMUM YIELD STRENGTH NOT RATED
ABGL WIDTH 12.000 INCHES NOMINAL
ALBY USAGE DESIGN AIRCRAFT
ABRY LENGTH 36.000 INCHES NOMINAL
FEAT SPECIAL FEATURES MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH
AGTA BASIC SHAPE STYLE SOLID
CQBC MINIMUM TENSILE STRENGTH 34000 POUNDS PER SQUARE INCH
AGAV END ITEM IDENTIFICATION FUSELAGE, F4F JET AIRCRAFT
HEAT HEAT TREATMENT H-34 STRAIN HARDENED
AARN FABRICATION METHOD ROLLED
Manufacturing Part Numbers (SKUs)
Part SKU Cage Status RNVC RNCC SADC DAC RNAAC
AMS-QQ-A-250/8-CDH34-0,02X12X36 81343 A 9 5 E 9Z
AMS-QQ-A-250/8 81343 A 1 3 E 9Z
AMS-QQ-A-250/8-H34-0.020X12X36 81343 A 2 3 E 9Z
Manufacturers
Part SKU Cage Manufacturer Type Status
AMS-QQ-A-250/8-CDH34-0,02X12X36 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/8 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/8-H34-0.020X12X36 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
FLIS Identification
PMIC ADPE Code CRITL Code DEMIL Code DEMIL INTG NIIN Asgt ESD HMIC ENAC Schedule-B INC
A 0 X A 1 07/26/2 A N 3701
FLIS Management
MOE REC Rep Code Mgmt Ctl USC Phrase Code Phrase Statement
Demilitarization Codes & Management
DML PMI HMIC ADP CC ESDC
Miscellaneous Management
MOE (S_A) SOS AAC QUP UI SLC CIIC RC MCC SVC
Management Control Army
MATCAT 1 MATCAT 2 MATCAT 3 MATCAT 4 5 ARC
Freight
NMFC NMFC SUB UFC HMC LTL LCL WCC TCC SHC ADC ACC ASH NMF DESC