9535-01-531-7793 ( AMS-QQ-A-250/5 , AMS-QQ-A-250/5-CDT3-0,125X12X48 , AMS-QQ-A-250/5-T3-0.125X12X48 )

NSN Information
NSN FSC NIIN Item Name INC
9535-01-531-7793 9535 015317793 SHEET,METAL 3701
NSN Features
MRC Parameter Characteristics
CQBC MINIMUM TENSILE STRENGTH 61000 POUNDS PER SQUARE INCH
ABRY LENGTH 48.000 INCHES NOMINAL
ABGL WIDTH 12.000 INCHES NOMINAL
CQHQ MINIMUM YIELD STRENGTH 40000 POUNDS PER SQUARE INCH
ADVM CROSS-SECTIONAL THICKNESS 0.1250 INCHES NOMINAL
MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5
ALBY USAGE DESIGN AIRCRAFT
HEAT HEAT TREATMENT T-3 SOLUTION HEAT TREATED
AGTA BASIC SHAPE STYLE SOLID
AARN FABRICATION METHOD ROLLED
AGAV END ITEM IDENTIFICATION FUSELAGE F4F JET AIRCRAFT
FEAT SPECIAL FEATURES THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS
Manufacturing Part Numbers (SKUs)
Part SKU Cage Status RNVC RNCC SADC DAC RNAAC
AMS-QQ-A-250/5 81343 A 1 3 E 9Z
AMS-QQ-A-250/5-CDT3-0,125X12X48 81343 A 9 5 E 9Z
AMS-QQ-A-250/5-T3-0.125X12X48 81343 A 2 3 E 9Z
Manufacturers
Part SKU Cage Manufacturer Type Status
AMS-QQ-A-250/5 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/5-CDT3-0,125X12X48 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/5-T3-0.125X12X48 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 07/21/2 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