edited borescope inspection report 9-26-2013 - salvex...compressor gv a) nicks and dents. quantity...

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  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 1 of 14

    Ie H

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 2 of 14

    E

    D

    C B

    A Air inlet Air Inlet Duct Air Inlet Screen Compressor Inlet GV 00 Stage Blades 00 Stage GV

    Borescope Port 4th Stage Blades 4th Stage GV 5th Stage Blades

    Borescope Port 11th Stage Blades 11th Stage GV 12th Stage Blades

    Fuel Injectors Compressor Exit GV Injectors Combustor Interior Combustor Pins Torch Tube Sliding Ring 1st Stage Nozzle 1st Stage Blades

    Thermocouple Port 2nd Stage Nozzle 2nd Stage Blades 2nd Stage Tip Shoe Blade Retaining Pins 3rd Stage Nozzle 3rd Stage Tip Shoe 3rd Stage Blades

    VGV

    External Variable Guide Vanes IGV 00 Stage VGV 0 Stage VGV 1st Stage VGV 2nd Stage VGV

    RGB Inspection Port Pinion & Star Gear Star Gear 2nd stage Accessory Gear Low Speed Brg

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 3 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Air Inlet

    A

    Air Inlet Duct a) Potential FOD

    b) Corrosive Pitting

    c) Cracks

    d) Excessive

    fouling

    None

    None

    None

    None

    Air Inlet

    A

    Air Inlet Screen a) Potential FOD b) Cracks,

    damaged mesh

    None None

    Air Inlet

    A

    Inlet Guide Vanes a) Nicks and dents. Quantity and size b) Excess of

    fouling

    c) Corrosive pitting. Affected

    area

    None None

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 4 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Air Inlet

    A

    00 Stage

    Compressor Blades

    a) Nicks and

    dents. Quantity and size.

    b) Excessive fouling

    c) Corrosive

    pitting. Affected area. d) Tip rub. Gap width and metal curling.

    None

    None

    None

    None

    Air Inlet

    A

    00 Stage Guide

    Vanes

    a) Nicks and

    dents. Quantity and size.

    b) Excessive fouling

    c) Corrosive

    pitting. Affected area.

    Superfici

    al nicks

    None

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 5 of 14

    Access Location

    Picture Description Inspection for Severity

    Borescope Port

    B

    4th Stage Compressor Blades

    a) Nicks and dents. Quantity and size. b) Excessive fouling

    c) Corrosive

    pitting. Affected area.

    d) Tip rub. Gap width and metal

    curling.

    None None

    None

    None

    Borescope Port

    B

    4th Stage Compressor GV

    a) Nicks and dents. Quantity

    and size.

    b) Excessive fouling c) Corrosive pitting. Affected area.

    None

    None None

    Borescope Port

    B

    5th Stage Compressor Blades

    a) Nicks and dents. Quantity

    and size.

    b) Excessive fouling

    c) Corrosive pitting. Affected area. d) Tip rub. Gap width and metal

    curling.

    None

    None

    None None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 6 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Borescope

    Port

    C

    11th Stage

    Compressor Blades

    a) Nicks and

    dents. Quantity and size. b) Excessive fouling

    c) Corrosive pitting. Affected

    area.

    d) Tip rub. Gap width and metal curling.

    None

    None

    None

    None

    Borescope

    Port

    C

    11th Stage

    Compressor GV

    a) Nicks and

    dents. Quantity and size.

    b) Excessive

    fouling c) Corrosive pitting. Affected area.

    None

    Rust on

    both sides None

    Borescope Port

    C

    12th Stage Compressor Blades

    a) Nicks and dents. Quantity and size.

    b) Excessive

    fouling

    c) Corrosive pitting. Affected area. d) Tip rub. Gap width and metal curling.

    None

    None

    None None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 7 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Fuel

    Injectors

    D

    Compressor Exit GV a) Nicks and

    dents. Quantity and size. b) Excessive fouling.

    c) Corrosive pitting. Affected

    area.

    None

    None

    Quite advance

    d rust

    Fuel Injectors

    D

    Injectors a) Pilot Centerbody

    erosion. b) Fuel hole contamination or blockage.

    c) Cracks.

    Quantity and size.

    d) Liquid only: broken main fuel spokes.

    None

    Sulfidation

    None

    None

    Fuel Injectors

    D

    Combustor Interior a) Cracks. Quantity and size b) Thermal

    Erosion.

    c) Hot spots.

    d) Buckling or warpage.

    None None

    None

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 8 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Fuel

    Injectors

    D

    Combustor Pins a) Cracks. None

    Fuel

    Injectors

    D

    Torch Tube a) Thermal

    erosion.

    None

    Fuel Injectors

    D

    Clamp ring/Sliding Ring

    a) Thermal erosion. Depth and affected area.

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 9 of 14

    Access

    Location

    Picture Description Inspection for Severity

    Fuel

    Injectors

    D

    1st Stage Turbine

    Nozzle: - Leading edge - Airfoil surface

    - Trailing edge

    a) Cracks.

    Quantity, length, and orientation.

    b) Thermal erosion. Depth

    and affected area.

    c) F.O.D. Affected area

    None

    None

    None

    Fuel Injectors

    D

    1st Stage Turbine Blades:

    - Leading edge - Airfoil surface

    - Trailing edge - Blade Tip

    a) Cracks. Quantity, length,

    and orientation.

    b) Thermal erosion. Depth

    and affected area. c) F.O.D. Affected area d) Tip rub. Gap

    width.

    None

    None

    None None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 10 of 14

    Access

    Location

    Picture Description Inspection for Severity

    T5 Port

    E

    2nd Stage Turbine

    Nozzle: - Leading edge - Airfoil surface - Trailing edge

    a) Cracks.

    Quantity, length, and orientation. b) Cracks. c) Thermal

    erosion. Depth and affected area.

    None

    None None

    T5 Port

    E

    2nd Stage Turbine

    Blades: - Leading edge - Airfoil surface - Trailing edge - Blade Tip

    a) Cracks.

    Quantity, length, and orientation. b) Thermal erosion. Depth and affected area.

    c) F.O.D. Affected

    area

    d) Tip rub. Gap width.

    None

    None

    None

    None

    T5 Port

    E

    3rd Stage Turbine Nozzle:

    - Leading edge - Airfoil surface - Trailing edge

    a) Cracks. Quantity, length,

    and orientation. b) Cracks. c) Thermal erosion. Depth and affected area.

    None

    None None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 11 of 14

    Access

    Location

    Picture Description Inspection for Severity

    T5 Port

    E

    3rd Stage Turbine

    Blades: - Leading edge - Airfoil surface

    - Trailing edge - Blade Tip

    a) Cracks.

    Quantity, length, and orientation.

    b) Thermal erosion. Depth

    and affected area.

    c) F.O.D. Affected area d) Tip rub. Gap width.

    None

    None

    None None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 12 of 14

    Access

    location

    Picture Description Inspection for Severity

    External

    VGV

    VGV

    IGV a) Cracks

    b) Lever arms bent c) Grommet out of position on

    unison ring

    d) Corrosion

    None

    None None

    None

    External VGV

    VGV

    00 Stage VGV a) Cracks

    b) Lever arms bent

    c) Grommet out of position on unison ring d) Corrosion

    None

    None

    None None

    External

    VGV

    VGV

    0 Stage VGV a) Cracks

    b) Lever arms bent c) Grommet out of position on

    unison ring d) Corrosion

    None

    None None

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 13 of 14

    Access location

    Picture Description Inspection for Severity

    External VGV

    VGV

    1st Stage VGV a) Cracks

    b) Lever arms bent c) Grommet out of position on unison ring

    d) Corrosion

    None

    None None

    None

    External VGV

    VGV

    2s Stage VGV a) Cracks b) Lever arms bent c) Grommet out

    of position on unison ring

    d) Corrosion

    None None None

    None

  • Borescope Inspection Report Taurus 70 CED

    MO-S-113

    24.05.2012

    Page 14 of 14

    Access location

    Picture Description Inspection for Severity

    Inspection Port

    RGB

    Pinion Double Helical & Star Gear

    a) Gear wear

    b) Teeth Cracks

    None

    None

    Inspection Port

    RGB

    Star Gear 2nd Stage – Ring Gear

    a) Gear wear b) Teeth Cracks

    None None

    Inspection Port

    RGB

    Accessory Gear a) Gear wear

    b) Teeth Cracks

    None

    None

    Inspection Port

    RGB

    Low Speed Bearing a) Wear

    None