logo
  • AVANTI
    • About us
    • Quality Assurance
    • Friends of Avanti
  • CATALOGUE
    • Powerplants +
      • Rolls-Royce RR250 / M250 Series
        • Compressor Section
        • Combustion Section
        • Turbine Section
        • Gearbox Section
      • PWC PT6T-3 / PT6A
        • Reduction Gearbox Section
        • Compressor Section
        • Turbine Section
        • Accessory Gearbox Section
      • GE CT58/T58
        • Air Inlet Section
        • Compressor Section
        • Combustion Section
        • Turbine Section
        • Accessory Drive Section
        • Power Turbine Section
      • GE CT64/T64
        • Compressor Section
        • Combustor Section
        • Turbine Section
        • Accessory Drive Gearbox Section
        • Speed Decreasing Gearbox Section
        • Planetary Reduction and Offset Drive Section
      • Honeywell T53
        • Output Reduction Section
        • Air Inlet Section
        • Compressor Section
        • Combustor Section
        • Turbine Section
        • Accessory Drive Section
        • Air Section
      • Honeywell T55 / T5508D
        • Air Inlet Section
        • Output Reduction Section
        • Compressor Section
        • Combustor Section
        • Turbine Section
        • Accessory Drive Section
      • PWA JT8D
        • Fan Discharge Section
        • Main Accessory Gearbox Group
        • Fan And Turbine Exhaust (Mixer) Section
        • Engine Exhaust Case Section Group
        • Front Compressor Drive Turbine Group
        • Rear Compressor Drive Turbine Group
        • Turbine Nozzle Group
        • Combustion And No. 5 Bearing Section
        • Diffuser Outer Fan Duct Group
        • Diffuser Group
        • Rear Compressor Group
        • Compressor Intermediate Group
        • Front Compressor Group
        • Front Accessory Drive Group
        • Fan Inlet Group
      • Rolls-Royce Olympus “Industrial”
      • Turbomeca Arriel 1
      • Hamilton-Sundstrand T-62T APU
      • GE LM1500 “Industrial”
      • GE LM2500 “Industrial”
      • Allison 501 KA “Industrial”
      • Rolls-Royce Avon “Industrial”
    • Airframes +
      • MDHC
      • Eurocopter AS350 / AS355
      • Bell 205
      • Bell 206
      • Bell 212
      • Bell 214
      • Bell 407
      • Sikorsky S61
      • Sikorsky S76
      • Bombardier CRJ
  • SERVICES
    • Manufacturing
    • Repair Design
    • Heat Treating
    • Plating
    • Materials Testing
    • Non Destructive Testing
    • Metallizing
    • Precision Machining
    • Welding & Brazing
  • NEWS
  • CONTACT US
  • 604-590-8013
  •  Search

Skip to Content

    • Compressor Section   +
    • Combustion Section   +
    • Turbine Section   +
    • Gearbox Section   +
    • Reduction Gearbox Section   +
    • Compressor Section   +
    • Turbine Section   +
    • Accessory Gearbox Section   +
    • Air Inlet Section   +
    • Compressor Section   +
    • Combustion Section   +
    • Turbine Section   +
    • Accessory Drive Section   +
    • Power Turbine Section   +
    • Compressor Section   +
    • Combustor Section   +
    • Turbine Section   +
    • Accessory Drive Gearbox Section   +
    • Speed Decreasing Gearbox Section   +
    • Planetary Reduction and Offset Drive Section   +
    • Output Reduction Section   +
    • Air Inlet Section   +
    • Compressor Section   +
    • Combustor Section   +
    • Turbine Section   +
    • Accessory Drive Section   +
    • Air Section   +
    • Air Inlet Section   +
    • Output Reduction Section   +
    • Compressor Section   +
    • Combustor Section   +
    • Turbine Section   +
    • Accessory Drive Section   +
    • Fan Discharge Section   +
    • Main Accessory Gearbox Group   +
    • Fan And Turbine Exhaust (Mixer) Section   +
    • Engine Exhaust Case Section Group   +
    • Front Compressor Drive Turbine Group   +
    • Rear Compressor Drive Turbine Group   +
    • Turbine Nozzle Group   +
    • Combustion And No. 5 Bearing Section   +
    • Diffuser Outer Fan Duct Group   +
    • Diffuser Group   +
    • Rear Compressor Group   +
    • Compressor Intermediate Group   +
    • Front Compressor Group   +
    • Front Accessory Drive Group   +
    • Fan Inlet Group   +
  • MDHC   +
  • Eurocopter AS350 / AS355   +
  • Bell 205   +
  • Bell 206   +
  • Bell 212   +
  • Bell 214   +
  • Bell 407   +
  • Sikorsky S76   +
  • Sikorsky S61   +
  • Bombardier CRJ   +

Home » Products » Powerplants » Honeywell T53 » Turbine Section » First Stage GP Turbine Rotor Assembly

First Stage GP Turbine Rotor Assembly

Description

Contact us for specific repair information and current pricing.

Workscope Tip Grind
IAW OHM 330.3 Sec. 72-50-07
Part # 1-101-610-01

INNOVATIVE REPAIR SOLUTIONS

Avanti Aerospace & Engineering Inc.We invite you to explore the many services that Avanti Aerospace & Engineering Inc. has to offer.

INDUSTRY CERTIFICATIONS

TC AMO 92-03
EASA 145.7162
Cage Code L0P51

CONTACT AVANTI

Address : #45 - 21330 56th Ave
Langley‎, BC V2Y 0E5
Canada
Phone: 604-590-8013
Fax: 604-590-8014
© 2023 Avanti Aerospace & Engineering Inc. - All Rights Reserved
blankCentrifugal Impeller
blankAccessory Drive Gearbox Cover