9540-00-145-7542 ( QQ-A-200/11 , 1244707 , 2-1355 , 1244707 , AMS-QQ-A-200/11 , AND10134-2002 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 9540-00-145-7542 | 9540 | 001457542 | ANGLE,STRUCTURAL | 3701 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| BRFD | WEIGHT PER UNIT MEASURE | 0.530 POUNDS PER LINEAR FOOT |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| AJJB | FIRST TIP RADIUS | 0.156 INCHES NOMINAL |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
| ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER |
| MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| CMZZ | SECOND TIP RADIUS | 0.156 INCHES NOMINAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUS |
| AJGP | BASE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLE |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| QQ-A-200/11 | 81348 | M | 9 | 5 | E | KZ | |
| 1244707 | 88277 | A | 1 | 3 | 4 | KZ | |
| 2-1355 | 38597 | A | 1 | 3 | 4 | KZ | |
| 1244707 | 18355 | A | 9 | 5 | 4 | KZ | |
| AMS-QQ-A-200/11 | 81343 | A | 1 | 3 | E | ZZ | |
| AND10134-2002 | 99237 | M | 1 | 4 | 4 | KZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS | A | M |
| 1244707 | 88277 | BOEING COMPANY THE | F | A |
| 2-1355 | 38597 | LOCKHEED MARTIN CORPORATION | A | A |
| 1244707 | 18355 | BOEING COMPANY THE | F | A |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS | A | A |
| AND10134-2002 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIG | 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 | 01/01/1 | N | 3701 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF9---V | F | ||
| DA | Z | J2200X- | A | ||
| DN | 9B----- | N | |||
| DS | N | 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 |
|---|---|---|---|---|---|---|---|---|---|
| DN | SMS | Z | 0 | FT | 0 | U | 9B----- | N | |
| DS | SMS | Z | 0 | FT | 0 | U | D | ||
| DF | SMS | Z | 0 | FT | 0 | U | SF9---V | F | |
| DA | SMS | Z | 0 | FT | 0 | U | Z | J2200X- | A |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|---|---|---|---|
| J | 2 | 2 | 00 | X |
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 013140 | X | 05390 | S | 576 | Z | R | A | B | Z | ALUMINUM ANGLES |