The Fixture,engine Maintenance,aircr, cataloged under National Stock Number 4920-01-336-6601, is classified within Federal Supply Class 4920 (Aircraft Maintenance and Repair Shop Specialized Equipment) of the Maintenance and Repair Shop Equipment group. The manufacturer of record is General Electric Co. Government technical data includes 2 specifications, cited from the U.S. Government catalog. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 4920-01-336-6601 |
| Primary Part Number | 3C4206G01 |
| Item Name | Fixture,engine Maintenance,aircr |
| FSC / FSG | 4920 / 49 — Aircraft Maintenance and Repair Shop Specialized Equipment |
| Manufacturer | General Electric Co |
| Status | ACTIVE |
| Reference Data and Literature | SERD NO. 1832 |
| Functional Description | USED TO INSTALL/REMOVE THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL WITH THE COMPRESSOR ROTOR SHAFT IN POSITION AND TO TURN THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL FROM THE HORIZONTAL TO THE VERTICAL PLANE |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL A — No Demilitarization Required |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Part Number | Manufacturer |
|---|---|
| 3C4206G01 PRIMARY | General Electric Co (USA) |
NSN 4920-01-336-6601 is a Fixture,engine Maintenance,aircr, manufactured by General Electric Co, classified under FSC 4920, Aircraft Maintenance and Repair Shop Specialized Equipment. Status: active.
NSN 4920-01-336-6601 has 1 manufacturer part number on file: 3C4206G01 (General Electric Co).
Key specifications for 3C4206G01: Reference Data and Literature: SERD NO. 1832; Special Features: C/0 WYE SHAPED PLATE WITH ITS LEGS SPACED 120.0 DEG APART AND OF EQUAL LENGTH; CLEVIS MOUNTING BLOCK AT THE CENTER OF THE PLATE ON ONE SIDE AND THREE EQUALLY SPACED SUPPORT BLOCKS ON THE OPPOSITE SIDE OF THE CLEVIS MOUNTING BLOCK; Functional Description: USED TO INSTALL/REMOVE THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL WITH THE COMPRESSOR ROTOR SHAFT IN POSITION AND TO TURN THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL FROM THE HORIZONTAL TO THE VERTICAL PLANE; End Item Identification: F110-GE-129 ENGINE AGE. 2 specifications are documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.