9535-01-531-7783 ( AMS-QQ-A-250/5-CDT3-0,016X12X36 , AMS-QQ-A-250/5-T3-0.016X12X36 , AMS-QQ-A-250/5 )

NSN Information
NSN FSC NIIN Item Name INC
9535-01-531-7783 9535 015317783 SHEET,METAL 3701
NSN Features
MRC Parameter Characteristics
CQHQ MINIMUM YIELD STRENGTH 39000 POUNDS PER SQUARE INCH
ADVM CROSS-SECTIONAL THICKNESS 0.0160 INCHES NOMINAL
ABGL WIDTH 12.000 INCHES NOMINAL
CQBC MINIMUM TENSILE STRENGTH 59000 POUNDS PER SQUARE INCH
FEAT SPECIAL FEATURES THIN LAYERS APPROXIMATELY EQUAL THICKNESS OF ALUMINUM ALLOY 1230 ANODIC TO CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
MATL MATERIAL ALUMINUM ALLOY, QQ-A-250/5
ALBY USAGE DESIGN AIRCRAFT
ABRY LENGTH 36.000 INCHES NOMINAL
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
Manufacturing Part Numbers (SKUs)
Part SKU Cage Status RNVC RNCC SADC DAC RNAAC
AMS-QQ-A-250/5-CDT3-0,016X12X36 81343 A 9 5 E 9Z
AMS-QQ-A-250/5-T3-0.016X12X36 81343 A 2 3 E 9Z
AMS-QQ-A-250/5 81343 A 1 3 E 9Z
Manufacturers
Part SKU Cage Manufacturer Type Status
AMS-QQ-A-250/5-CDT3-0,016X12X36 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/5-T3-0.016X12X36 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
AMS-QQ-A-250/5 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