NSN 4920-01-375-1576
Part Details | AIRCRAFT ENGINE MAINTENANCE FIXTURE
4920-01-375-1576 A fixture designed to hold/position aircraft engine/engine components to facilitate inspection, maintenance, repair, testing and/or replacement of components.
Alternate Parts: 856A1454G01, 4920-01-375-1576, 01-375-1576, 4920013751576, 013751576
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | MAY 06, 1993 | 01-375-1576 | 48925 ( FIXTURE, ENGINE MAINTENANCE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-01-375-1576
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 856A1454G01 | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 4920-01-375-1576
| Characteristic | Specifications |
|---|---|
| FUNCTIONAL DESCRIPTION | USED TO SUPPORT THE HIGH PRESSURE TURBINE ROTOR WHEN INSTALLING OR REMOVING MODULE 12 IN THE HORIZONTAL POSITION |
| REFERENCE DATA AND LITERATURE | SERD CFC3712 |
| FUNCTIONAL CLASSIFICATION | GG-7.4 |
| SPECIAL FEATURES | CONSIST OF A PLATE WITH EXTERNAL THREADS WHICH INTERFACE WITH THE INTERNAL THREADS OF THE HIGH PRESSURE TURBINE ROTOR SHAFT; A 2-1/4 IN. ALUM. TUBE WHICH ACTS AS A EXTENSION OF THE SHAFT,WHICH WILL REST ON THE SUPPORT FIXTURE,P/N 856A1453,TO PROVIDE SUPPORT FOR THE HIGH PRESSURE TURBINE ROTOR; A RAMPED CYLINDER GUIDE IS ATTACHED TO THE FORWARD FLANGE USED TO CENTER MODULE 12 DURING INSTALLATION; MATL: STEEL AND ALUMINUM; BLACK OXIDED OR ANODIZED FOR CORROSION PROTECTION |
| END ITEM IDENTIFICATION | F-108 ENGINE |