# Turbomeca TURMO IVC

- Type: Engine model (FAA registry)
- Registry code: 60077
- Manufacturer (registry): TURBOMECA
- Model: TURMO IVC
- Engine type: Turbo-shaft
- Power: 1,495 hp
- Data sheet: [TCDS E10EU](https://openairdocs.org/tcds/E10EU) (OpenAirDocs)
- Holder: Turbomeca S.A.
- Installed in: 5 registered aircraft
- Page: https://openairdocs.org/engine/turbomeca-turmo-ivc

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2016-05-08](https://openairdocs.org/ad/2016-05-08): Centrifugal compressor inducer blade loss · Turbomeca Turmo IVA and Turmo IVC. Effective Apr 21, 2016
- [AD 2010-02-08](https://openairdocs.org/ad/2010-02-08): Pipe union crack · Turbomeca Turmo IVA and Turmo IVC. Effective Feb 3, 2010
- [AD 2009-02-08](https://openairdocs.org/ad/2009-02-08): Oil-tank-to-oil-cooler flexible lubrication pipes · Turbomeca Turmo IVA and Turmo IVC. Effective Mar 4, 2009

Historical (superseded or no longer in force):

- [AD 2006-23-17](https://openairdocs.org/ad/2006-23-17) (historical): Centrifugal compressor intake wheel blades · Turbomeca Turmo IVA and Turmo IVC. Effective Dec 21, 2006
- [AD 2006-21-11](https://openairdocs.org/ad/2006-21-11) (historical): Flexible lubrication pipes · Turbomeca Turmo IVA and Turmo IVC. Effective Nov 3, 2006
- [AD 2003-11-09](https://openairdocs.org/ad/2003-11-09) (historical): Centrifugal Compressor Intake Wheel Blades · Turbomeca Turmo IVA and Turmo IVC. Effective Jul 3, 2003

## Registered aircraft (5)

- [N10248](https://openairdocs.org/aircraft/N10248): [Aeroxs Inc](https://openairdocs.org/faa-owner/AEROXS%20INC), [Swainsboro, GA](https://openairdocs.org/faa-place/GA/Swainsboro), built 1977, S/N 1502
- [N300EV](https://openairdocs.org/aircraft/N300EV): [Aeroxs Inc](https://openairdocs.org/faa-owner/AEROXS%20INC), [Swainsboro, GA](https://openairdocs.org/faa-place/GA/Swainsboro), built 1975, S/N 1301
- [N339EV](https://openairdocs.org/aircraft/N339EV): [Southern Utah University](https://openairdocs.org/faa-owner/SOUTHERN%20UTAH%20UNIVERSITY), [Cedar City, UT](https://openairdocs.org/faa-place/UT/Cedar%20City), built 1974, S/N 1285
- [N605R](https://openairdocs.org/aircraft/N605R): [Aeroxs Inc](https://openairdocs.org/faa-owner/AEROXS%20INC), [Swainsboro, GA](https://openairdocs.org/faa-place/GA/Swainsboro), built 1975, S/N 1358
- [N814AR](https://openairdocs.org/aircraft/N814AR): [First Call Helicopter Corp](https://openairdocs.org/faa-owner/FIRST%20CALL%20HELICOPTER%20CORP), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), S/N 1450

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC18LA020](https://openairdocs.org/ntsb/ANC18LA020), Jan 26, 2018: Eurocopter France SA330J Puma (N339EV), Pacific Ocean, Japan, substantial damage. Probable cause: The worn rear bearing of the freewheel unit. Contributing to the accident was the delay in analyzing an oil sample, which would have detected the increase in metal contaminants from the worn bearing.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20100316029419I](https://openairdocs.org/incident/20100316029419I), Mar 16, 2010: S.N.I.A.S SA330J (N367EV), New Bedford, MA, Minor damage. During a annual competency check (135.293) in which the check airman was being observed by a national resource for designation as a checkairman, the pilot…

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