9540-01-468-0130 ( CVC10001-331CJ , AMS-QQ-A-200/15 , QQ-A-200/15 )

NSN Information
NSN FSC NIIN Item Name INC
9540-01-468-0130 9540 014680130 ANGLE,STRUCTURAL 3701
NSN Features
MRC Parameter Characteristics
AARN FABRICATION METHOD EXTRUDED
HEAT HEAT TREATMENT T76511 SOLUTION HEAT TREATED
ABMK OVERALL WIDTH 2.500 INCHES NOMINAL
ADXL LEFT SIDE FLANGE THICKNESS 0.320 INCHES NOMINAL
AJGP BASE FLANGE THICKNESS 0.320 INCHES NOMINAL
AJJB FIRST TIP RADIUS 0.032 INCHES NOMINAL
CNQK SECOND TIP STYLE UPPER RADIUS
CQHP LEFT INSIDE ANGLE 90.0 DEGREES NOMINAL
CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY ANGLE, UNEQUAL LEGS AND THICKNESSES
CMZY FIRST TIP STYLE RIGHT QUARTER RADIUS
AJGL FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE 0.125 INCHES NOMINAL
ABKW OVERALL HEIGHT 2.000 INCHES NOMINAL
AGAV END ITEM IDENTIFICATION B-2 AIRCRAFT
CMZZ SECOND TIP RADIUS 0.032 INCHES NOMINAL
CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
AGTA BASIC SHAPE STYLE ANGLE
MATL MATERIAL ALUMINUM ALLOY, AMS-QQ-A-200/15, ALLOY 7075
ABRY LENGTH 12.000 INCHES NOMINAL
Manufacturing Part Numbers (SKUs)
Part SKU Cage Status RNVC RNCC SADC DAC RNAAC
CVC10001-331CJ 80378 A 2 3 E ZZ
AMS-QQ-A-200/15 81343 A 1 3 E ZZ
QQ-A-200/15 81348 M 9 5 E ZZ
Manufacturers
Part SKU Cage Manufacturer Type Status
CVC10001-331CJ 80378 TRIUMPH AEROSTRUCTURES, LLC A A
AMS-QQ-A-200/15 81343 SOCIETY OF AUTOMOTIVE ENGINEERS A A
QQ-A-200/15 81348 FEDERAL SPECIFICATIONS A M
FLIS Identification
PMIC ADPE Code CRITL Code DEMIL Code DEMIL INTG NIIN Asgt ESD HMIC ENAC Schedule-B INC
A 0 X A 1 09/24/1 N 3701
FLIS Management
MOE REC Rep Code Mgmt Ctl USC Phrase Code Phrase Statement
DF ------- I
DF N --SBQ-E F
Demilitarization Codes & Management
DML PMI HMIC ADP CC ESDC
A A N 0 X
Miscellaneous Management
MOE (S_A) SOS AAC QUP UI SLC CIIC RC MCC SVC
DF F59 J 0 FT 0 U --SBQ-E D
DF F59 J 0 FT 0 U ------- D
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