LM2500 BORESCOPE INSPECTION REPORT
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1 LM2500 BORESCOPE INSPECTION REPORT UC DAVIS CUSTOMER UNIT NAME/NUMBER: N/A ENGINE SERIAL NUMBER: TCT SALES ORDER NUMBER: US DATE INSPECTED: SERVICEABILITY AT DATE OF INSPECTION: UNSERVICEABLE
2 BACKGROUND Customer: UC Davis Location: Sacramento, Ca Work Order: US Performed by: Keith Enox Package S/N and Manufacturer: S/N: N/A Manufacturer: S&S Engine Model: LM2500 NGW Engine Hours: Operating hours: 165,413 Starts: Fired starts: 558 Start attempts: 353 Purpose of Visit: Perform routine borescope inspection in accordance with GEK 97310, Vol 1, Chapter 5. Inspect Lube and Scavenge Finger Screens in accordance with GEK 97310, Volume 1, Ch. 5, Inspect Magnetic Chip detectors in accordance with GEK 97310, Volume 1, Chapter 5, A Inspection of engine externals I.A.W. GEK 97310, Volume 1, chapter 5, Inspection of igniters I.A.W. GEK 97310, Volume 1, chapter 5, Summary of Overall Condition: was found to be UNSERVICEABLE HPC: Blades viewed in dirty condition. Serviceable Combustor: Normal discoloration. Serviceable Stage 1 HPT: Unserviceable damage found to HPT stage 1 blades beyond limits of GEK Volume 1 Chapter 5, Table 5-8 Item 3e. 5 HPTN1 nozzle segments found with serviceable T/E cracks. One HPTN1 nozzle found with trailing edge erosion and crack- Unserviceable. Stage 2 HPT: Unserviceable damage found to Stage 2 HPT blades- 3 blades found with leading edge holes, 2 blades found with L/E tip tears- unserviceable IAW Volume 1, Chapter 5 Table 5-8 Items 2a and b. TMF: Strut crack found within serviceable limits. LPT: The borescope inspection was completed with the below recommendations: Page 2
3 Recommendations: It is recommended to send to depot for repairs to damaged hot section components prior to further operation. It is also recommended to perform a compressor water wash to maintain compressor efficiency and power. It is recommended to repair TMF strut crack at time of hot section repair. Page 3
4 High Pressure Compressor: High Pressure Compressor Rotor Blades Stage 1 Blade Mid-Spans Stage 1&2 Blade Retainers HPC Rotor Weep Holes IGV & Stator Vanes IGV, 1 & 2 VSV Shrouds Rotor Spool Rub Coat Additional Comments Comments: Blades viewed in dirty condition. Serviceable No further comment Page 4
5 HPC Stage 1 L/E Tip HPC Stage 1 Root HPC Stage 1 Carboloy wear pads HPC Stage 1 Carboloy wear pads HPC Stage 1 Blade retainers HPC Stage 1 Blade retainers Page 5
6 HPC Stage 2 L/E Blades HPC Stage 2 T/E Blades HPC Stage 3 L/E Blades HPC Stage 3 L/E Blades HPC Stage 4 L/E Blades HPC Stage 4 L/E Blades Page 6
7 HPC Stage 5 L/E Blades HPC Stage 5 T/E Blades HPC Stage 6 L/E Blades HPC Stage 6 T/E Blades HPC Stage 9 L/E Blades HPC Stage 9 T/E Blades Page 7
8 HPC Stage 10 L/E Blades HPC Stage 10 T/E Blades HPC Stage 11 Blades HPC Stage 12 Blades HPC Stage 15 Blades HPC Stage 16 Blades Page 8
9 Combustor: Combustor All Surfaces Cowl Dome Assembly Primary & Secondary Swirlers Inner & Outer Liner Fuel Nozzles Igniters Additional Comments Comments: Normal discoloration. Serviceable Normal discoloration. Serviceable Normal discoloration. Serviceable Minor TBC loss normal discoloration. Serviceable Normal discoloration. Serviceable Not removed per customer request. No further comment Page 9
10 Combustor Overview Combustor Dome Assembly Primary and secondary swirler Combustor Dome Band Combustor Outer Liner Combustor Inner Liner Page 10
11 Combustor Splash Plates Combustor Splash Plates Combustor Splash Plates Combustor Splash Plates Upper Igniter Lower Igniter Page 11
12 High Pressure Turbine: High Pressure Turbine HPT Stage 1 Nozzles HPT Stage 1 Shrouds HPT Stage 1 Rotor Blades HPT Stage 2 Nozzles HPT Stage 2 Shrouds HPT Stage 2 Rotor Blades Additional Comments Comments: Trailing edge impacts and missing material. Unserviceable Tip Rub- serviceable Impact with missing material. Unserviceable Minor serviceable impacts throughout Impacts on shrouds- within serviceable limits. Leading edge impacts/ holes/ tip tears. Unserviceable Recommend HPT repair prior to further operation. Page 12
13 HPTN1 L/E HPTN1 L/E HPTN1 T/E impact HPTN1 T/E impact and missing material. HPT Stage 1 L/E Tip HPT Stage 1 L/E Root Page 13
14 HPT Stage 1 L/E Tip HPT Stage 1 L/E Root HPT Stage 1 Blades shroud and blade Impact. HPT Stage 2 Blades shroud impact. HPT Stage 2 L/E impact T/E nozzle impact. HPT Stage 2 L/E impact. Page 14
15 HPT Stage 2 L/E impact. HPT Stage 2 L/E impact and cracked. HPT Stage 2 L/E impact. HPT Stage 2 L/E impact. HPT Stage 2 L/E Tip crack. HPT Stage 2 L/E Tip crack. Page 15
16 Turbine Mid Frame: Turbine Mid Frame Inner Liner (shifting, cracks) Casing (outer liner) welds Comments: T5.4 bosses C-Sump Housing Struts & End caps Strut crack found to be within serviceable limits (est.250 ) T5.4 Probes P5.4 Probe S1 LPT Nozzle Support Additional Comments It is recommended to repair TMF strut crack at time of engine repair. Page 16
17 TMF Strut minor crack. TMF Strut minor crack. TMF Outer Liner T5.4 Thermocouple T5.4 Thermocouple T5.4 Thermocouple Page 17
18 Power Turbine: Power Turbine Stage 1 Nozzle Vanes Stage 1 LPT Shrouds Stg 1 & 6 Rotor Blades Case Turbine Rear Frame D-Sump Manifold Additional Comments Comments: LPT Stage 1 Blades Shroud impact- serviceable. No further comment Page 18
19 LPT Stage 1 Blades L/E Tip LPT Stage 1 Blades L/E Root LPT Stage 1 Blades L/E Tip LPT Stage 1 Blades L/E Root LPT Stage 1 Blades Shroud impact. LPT Stage 1 Blades Shroud impact. Page 19
20 Lube and Scavenge Finger Screens and Chip Detectors: Chip Detector and Finger Screen as Found Condition Location Chip Detector Finger Screen TGB/A Scavenge Not Equipped A Scavenge Not Equipped B Scavenge Not Equipped C Scavenge Not Equipped D Scavenge Not Equipped Lube Inlet Not Equipped Lube & Scavenge Finger Screens Lube & Scavenge Finger Screens Lube & Scavenge Finger Screens Lube & Scavenge Finger Screens Page 20
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