Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE LOCK
2840-01-198-7358 An item used to maintain the position of a BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 1277M27G01, 1277M27G01, 1277M27G01, 1277M27G01, 1277M27G01, 1277M27G01, 1277M27G01, 2840-01-198-7358, 01-198-7358, 2840011987358, 011987358
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 11, 1985 | 01-198-7358 | 50456 ( LOCK, FAN BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-198-7358
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1277M27G01 | 32317 | BARNES GROUP INC.DBA BARNES AEROSPACE |
| 1277M27G01 | 92541 | CUSTOM CRAFT PRODUCTS INC |
| 1277M27G01 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 1277M27G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1277M27G01 | 03350 | GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV |
| 1277M27G01 | 28884 | TSS TECHNOLOGIES, INC.DBA TSS MEDICAL |
| 1277M27G01 | 32543 | WHITCRAFT LLCDBA WHITCRAFT |
Technical Data | NSN 2840-01-198-7358
| Characteristic | Specifications |
|---|---|
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.111 INCHES MINIMUM AND 0.115 INCHES MAXIMUM |
| OVERALL WIDTH | 0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM |
| OVERALL LENGTH | 23.000 INCHES MINIMUM AND 23.200 INCHES MAXIMUM |
| SPECIAL FEATURES | RETAINER WHEN COMPRESSED MEASURES21.464 MIN. 21.466 MAX. INCHES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
