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PT6A-67D Capabilities

Used in the 1900D passenger aircraft.

The PT6A-67 series of turboprop engines comprise of a 2 stage reduction gearbox, a 2 stage power turbine, a single
stage gas generator turbine and a 5 stage gas generator compressor consisting of  4 axial and 1 centrifugal. The engine produces 1,279 shp for shorter take-offs. 

  • Overhaul
  • Repair (Engine, Components or Accessories)
  • Foreign Object Damage (FOD Repair)
  • Hot Section Inspection
  • LCF Disk Change
  • TBO Extension Evaluation
  • Inspection & Test
  • OEM Approved Test Cell
  • Borescope Inspection
  • International Mobile Repair Team (MRT)

Alongside these core services, Euravia delivers an extensive range of Design and Post Design Solutions. These include component and engine life assessment, reliability studies, component improvement programs and specialist tooling. For full details click on the contact form to make a servicing enquiry.

Engine Details

Basic HSI
2000
Basic TBO
6000
Manufacturer
P&WC
Model
PT6A-67D
Part Name
Turboprop Engine
OHC Facility
Euravia, Kelbrook
Part Number/s
3044800
Technical Data Document/s
3038337 (OHM)
3072154 (IPC)
Aircraft that use this engine
Raytheon Beech 1900 Series

Approvals

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