Catalog item
Request a quoteBRACKET,DOUBLE ANGLE
5340FSC
01NCB code
488-7233Item number
NIIN 01-488-7233
- Unit price
- $24.50
- Unit of issue
- EA
- Source of supply
- F01
- DEMIL code
- D
Identification
- Item name code
- 20354
- PINC
- 0020354
- Criticality code
- X
- II
- 0
- DEMIL code
- D
- DEMIL integrity code
- 1
- NIIN assigned
- 31-AUG-01
- Precious metals indicator
- A
- ADP equipment code
- 0
- Hazardous material indicator
- P
- ESD/EMI code
- A
Management
| Effective date | Major organizational entity | Acquisition advice code | Source of supply | Unit of issue | Unit of measure quantity | Unit price | Quantity per unit pack | Controlled inventory item code | Shelf-life code | Recoverability code | Management control | Net price | USC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 01-NOV-2025 | DF | D | F01 | EA | 0.0000 | $24.50 | 1 | 7 | 0 | N | --SFR-E | $0.00 | F |
| 01-NOV-2025 | DF | D | F01 | EA | 0.0000 | $24.50 | 1 | 7 | 0 | N | --SFR-E | $0.00 | I |
Part numbers
- Part number
- 5HM40053-171
- CAGE
- 81755LOCKHEED MARTIN CORPORATION DIV LOCKHEED MARTIN AERONAUTICS COMPANY
- CAGE status
- A
- RNCC
- 3
- RNVC
- 2
- Document availability code
- D
- RNAAC
- ZZ
Characteristics
| MOUNTING HOLE TYPE | PLAIN |
|---|---|
| FIRST LEG LENGTH | INCHES NOMINAL 0.800 |
| SECOND LEG LENGTH | INCHES NOMINAL 1.240 |
| END ITEM IDENTIFICATION | F-22 RAPTOR |
| FIRST LEG THICKNESS | INCHES NOMINAL 0.080 |
| SECOND LEG THICKNESS | INCHES NOMINAL 0.080 |
| CENTER SECTION HEIGHT | INCHES NOMINAL 1.620 |
| CENTER SECTION WIDTH | INCHES NOMINAL 2.000 |
| CENTER SECTION THICKNESS | INCHES NOMINAL 0.080 |
| FIRST LEG STYLE | |
| FIRST LEG HOLE ARRANGEMENT STYLE | |
| SECOND LEG STYLE | |
| SECOND LEG HOLE ARRANGEMENT STYLE | |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| FIRST LEG ANGLE | DEGREES NOMINAL 90.0 |
| SECOND LEG ANGLE | DEGREES NOMINAL 90.0 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DETAILS-SHEET METAL BRACKET HARNESS SUPPORT |
| SPECIAL FEATURES | NAME AND FSC CHANGED-FROM 1560 BRACKET, STRUCTURAL COMPONENT AIRCRAFT TO 5340 BRACKET DOUBLE ANGLE;ITEM REQUIRES NTU, SELF-LOCKING PLATE P/N 204F3 AND RIVETS P/N MS20426AD3-5 |
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-250 TO 4 |
| PROPRIETARY CHARACTERISTICS | PACS |
| STYLE DESIGNATOR |
MOE rules
- MOE rule
- FLL5
- MOE CD
- DF
- AMC
- 0
- AMSC
- 0
- Date assigned
- 01-AUG-01
- IMC
- B
- PICA
- TL
- PICA LOA
- 06
- Auth collab
- TL TU
Service data
Air Force
- Budget
- S
- MMAC
- FR
- PVC
- E
- ERRC
- N
Freight
- ACTY CD
- TK
Related items
Standardization
- Item standardization code
- 5
- Orig stdzn dec
- 97
- Dt stdzn dec
- 31-AUG-2001
- NIIN status code
- 0
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