9540-01-438-1222 ( AMS-QQ-A-200/11 , CVC10050-114CA , QQ-A-200/11 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 9540-01-438-1222 | 9540 | 014381222 | STRUCTURAL SECTION,SPECIAL SHAPE | 3088 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| HEAT | HEAT TREATMENT | 0-ANNEALED |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| AMS-QQ-A-200/11 | 81343 | A | 1 | 3 | E | ZZ | |
| CVC10050-114CA | 80378 | A | 2 | 3 | E | ZZ | |
| QQ-A-200/11 | 81348 | M | 9 | 5 | E | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS | A | A |
| CVC10050-114CA | 80378 | TRIUMPH AEROSTRUCTURES, LLC | A | A |
| QQ-A-200/11 | 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 | 10/31/1 | N | 3088 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | --SBQ-E | F | ||
| DF | ------- | I |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|