Catalog item
Request a quotePLATE,METAL
9535FSC
01NCB code
531-2513Item number
NIIN 01-531-2513
- DEMIL code
- A
Identification
- Item name code
- 37013
- PINC
- 0037013
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- DEMIL integrity code
- 1
- NIIN assigned
- 29-JUN-05
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- N
- ESD/EMI code
- A
Part numbers
| Part number | CAGE | CAGE status | RNCC | RNVC | Document availability code | RNAAC | RNFC | RNSC |
|---|---|---|---|---|---|---|---|---|
| QQ-A-225/9-T6-1.00X3.00X10 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 3 | 9 | 4 | 9Z | 4 | A |
| AMS-QQ-A-225/9T6-1,00X3,00X10 | 81343 SOCIETY OF AUTOMOTIVE ENGINEERS INC | R | 5 | 9 | 4 | 9Z | 4 | D |
| QQ-A-225/9-T6-1.00X3.00X10 | 0U583 SAE INTERNATIONAL DBA SAE INTERNATIONAL | A | 3 | 2 | 5 | ZZ |
Characteristics
| FABRICATION METHOD | COLD FINISH |
|---|---|
| WIDTH | INCHES NOMINAL 3.000 |
| LENGTH | FEET NOMINAL 10.000 |
| CROSS-SECTIONAL THICKNESS | INCHES NOMINAL 1.0000 |
| END ITEM IDENTIFICATION | FUSELAGE, F4F JET AIRCRAFT |
| BASIC SHAPE STYLE | |
| MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 77000 |
| MINIMUM YIELD STRENGTH | POUNDS PER SQUARE INCH 66000 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-225 TO 9 |
MOE rules
- MOE rule
- ZG01
- MOE CD
- ZG
- Date assigned
- 01-JUN-05
- PICA
- ZG
- PICA LOA
- 81
- Auth collab
- ZG
Freight
- ACTY CD
- LI
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 29-JUN-2005
- NIIN status code
- 0
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