# Pratt & Whitney PW6124A

- Type: Engine model (FAA registry)
- Registry code: 51507
- Manufacturer (registry): P & W
- Model: PW6124A
- Engine type: Turbo-fan
- Power: 23,800 lb thrust
- Data sheet: [TCDS E00064EN](https://openairdocs.org/tcds/E00064EN) (OpenAirDocs)
- Holder: Pratt & Whitney Division
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-pw6124a

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 2015-12-10](https://openairdocs.org/ad/2015-12-10): High-pressure compressor (HPC) 7th stage integrally bladed (IB) rotor aft integral arm · Pratt & Whitney Division PW6122A and PW6124A. Effective Jul 6, 2015

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

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