P/N: 6055t40p01
Category: Baffles & Engine Cooling
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 2 Available |
The 6055T40P01 is a front frame shroud for aircraft gas turbine engines, directing inlet airflow toward the compressor section. This component shields upstream hardware and manages entry conditions at the engine front frame. Manufactured to General Electric specifications (CAGE 99207) and identified by NSN 2840-01-241-7467, the shroud maintains airflow integrity during engine operation.
Installation requires torque verification per the applicable engine maintenance manual and part identification confirmation against the aircraft's engine IPC.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 6055T40P01 is a front frame shroud for aircraft gas turbine engines, directing inlet airflow toward the compressor section. This component shields upstream hardware and manages entry conditions at the engine front frame.
Depending on condition, the 6055t40p01 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: Serviceable. Contact us for specific documentation details on the condition you need.
Yes, the SHROUD,IMP can be used in engine overhauls and maintenance events. Always verify part compatibility against your engine's Type Certificate Data Sheet (TCDS) and Illustrated Parts Catalog (IPC) before installation.
In-stock items ship same business day when ordered before 3 PM EST. We also offer 24/7 AOG (Aircraft on Ground) support at (904) 998-9101 for urgent engine part needs.