Catalog item
Request a quoteANGLE,STRUCTURAL
9540FSC
01NCB code
478-9725Item number
NIIN 01-478-9725
- DEMIL code
- A
Identification
- Item name code
- 37017
- PINC
- 0037017
- Criticality code
- X
- II
- 0
- DEMIL code
- A
- DEMIL integrity code
- 1
- NIIN assigned
- 04-OCT-00
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- N
- ESD/EMI code
- A
Part numbers
- Part number
- HS1004DD63-0525
- CAGE
- 8V613THE BOEING COMPANY
- CAGE status
- A
- RNCC
- 3
- RNVC
- 2
- Document availability code
- 2
- RNAAC
- 9Z
- RNFC
- 4
- RNSC
- A
Characteristics
| FABRICATION METHOD | EXTRUDED |
|---|---|
| OVERALL HEIGHT | INCHES NOMINAL 1.000 |
| OVERALL WIDTH | INCHES NOMINAL 1.500 |
| LENGTH | INCHES NOMINAL 5.781 |
| LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.063 |
| END ITEM IDENTIFICATION | APACHE HELICOPTER |
| BASIC SHAPE STYLE | |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.062 |
| BASE FLANGE THICKNESS | INCHES NOMINAL 0.063 |
| FIRST TIP STYLE | |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| LEFT INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUDED ANGLE - UNEQUAL LEG, ALUMINUM ALLOY |
| HEAT TREATMENT | T-4 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED |
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-200 TO 3 |
MOE rules
- MOE rule
- ZK01
- MOE CD
- ZK
- Date assigned
- 01-OCT-00
- PICA
- ZK
- PICA LOA
- 81
- Auth collab
- ZK
Freight
- ACTY CD
- QE
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 04-OCT-2000
- NIIN status code
- 0
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