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MRC | Criteria | Characteristic |
---|---|---|
AGAV | III END ITEM IDENTIFICATION | F-108 ENGINE |
SR-5 | DESIGN CONTROL REFERENCE | 856A1454G01 |
FTLD | FUNCTIONAL DESCRIPTION | USED TO SUPPORT THE HIGH PRESSURE TURBINE ROTOR WHEN INSTALLING OR REMOVING MODULE 12 IN THE HORIZONTAL POSITION |
SR-5 | MANUFACTURERS CODE | 58828 |
RDAL | REFERENCE DATA AND LITERATURE | SERD CFC3712 |
FEAT | 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 |
FCLS | FUNCTIONAL CLASSIFICATION | GG-7.4 |
SR-5 | THE MANUFACTURERS DATA |
856-0014-235 | 856-0014-235 | 856-0006 | 856-003-001 |
856-0014-235 | 856-0010 | 856-0012 | 856-0013 |
856-000-5011 | 856.002.4 | 856-000-5011 | 856-0003 |
856-0008 | 856-003-001 | 856-0013 | 856-00 |
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