For Sale
APU Model RE100-XL (S/N: P-549)
This APU was inducted to Gulfstream where it was inspected, tested and long-term preserved on February 12, 2025. The 450 hour / 1-year & 900 hour / 2-year inspections were carried out and the APU was issued an 8130 Dual release with no outstanding AD’s. The APU has operated 363.1 hours and 555 cycles since the last major shop visit by Honeywell where LLP replacement was performed and is currently available for outright sale in Serviceable condition. Contact your Sales Manager at C&L Aerospace for additional
information.
| Summary | |
|---|---|
| Serial Number: | P-549 |
| Model: | RE100-XL |
| Aircraft: | Cessna 560XL |
| TSN: | 8,535.1 |
| TSO: | |
| LSV Date: | May 22, 2023 |
APU
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 3842340-2 | 363.1 | 555 | 4,000 | 3,445 |
| Compressor Impeller | 3822523-003 | 363.1 | 555 | 12,000 | 11,445 |
| Fuel Control | 3883900-1 | Inspected | |||
| Ignition Unit | 3888000-7 | Inspected | |||
| Oil Level Sensor | 3876318-3 | Inspected | |||
| Lube Pump | 3881825-1 | Inspected | |||
| Start Counter | 3876317-1 | Inspected | |||
| Lop Switch | 3876351-1 | Inspected | |||
For Sale
APU Model: APS2300 S/N: HSC-E0823604
This APU was last inducted to Standard Aero on February 18, 2020, where it was cleaned, inspected, and repaired IAW the Pratt & Whitney Standard Practices manual. It has operated 2,541.1 hours and 2,288 cycles since this shop visit. The APU was sent to NExT MRO where it was inspected, repaired, tested and released with no LLP replacement on July 17, 2024. Long term preservation was accomplished and is good
until January 16, 2026
*Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | HSC-E0823604 |
| Model: | APS2300 |
| Aircraft: | E170/175/190/195 |
| TSN: | 22,762.1 |
| TSO: | |
| LSV Date: | July 17, 2024 |
Cold Section
Life Limited Parts
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Impeller | 4509329 | 6,014.6 | 5,191 | 50,000 | 44,809 |
| 1st Turbine Rotor Disk | 4520419 | 2,542.2 | 2,288 | 60,000 | 57,712 |
| 1st Turbine Blade Set | 4507016 | 2,542.2 | 2,288 | 17,500 | 15,212 |
| 2nd Turbine Rotor Disk | 4520421 | 2,542.2 | 2,288 | 35,000 | 32,712 |
| 2nd Turbine Blade Set | 4520010 | 2,542.2 | 2,288 | 17,500 | 15,212 |
LRUs
LRU ACCESSORIES:
| Item | P/N | Condition at LSV |
|---|---|---|
| Powerhead Assembly | 4505011R | REPAIRED |
| Gearbox Assembly | 4505015G | REPAIRED |
| Fuel Module | 4505008F | NO WORK ACCOMPLISHED |
| Anti-Surge Valve | 4953195-1 | INSPECTED / TESTED |
| BSG Stator Assembly | 4952826 | NO WORK ACCOMPLISHED |
| Oil Cooler | 4951700 | NO WORK ACCOMPLISHED |
| Ignition Unit | 4952793 | NO WORK ACCOMPLISHED |
| Oil Pressure Sensor | 4951695 | NO WORK ACCOMPLISHED |
| Oil Temp Sensor | 4950760 | NO WORK ACCOMPLISHED |
| Speed Sensor | 4951694 | NO WORK ACCOMPLISHED |
| Thermocouple (x2) | 4951690-1, -2 | NO WORK ACCOMPLISHED |
| Deprime Solenoid | 756722B | NO WORK ACCOMPLISHED |
| Data Memory Module | 4505576 | NO WORK ACCOMPLISHED |
| Electrical Harness | 4505113B | REPAIRED |
| Fuel Injector Simplex (x6) | 4951948 | INSPECTED / TESTED |
| Fuel Injector Duplex (x6) | 4951949 | INSPECTED / TESTED |
| Fuel Manifold – Primary | 4951707 | NO WORK ACCOMPLISHED |
| Fuel Manifold – Secondary | 4951708 | NO WORK ACCOMPLISHED |
| Lube/Scavenge Oil Pump | 4951727 | NO WORK ACCOMPLISHED |
No airworthiness directives applicable to this engine model.
SB / AD EMBODIMENT
| SB | Description | Status |
|---|---|---|
| 230025 | REWORK OF COMPRESSOR IMPELLER ASSY TO P/N: 4509329 |
EMBODIED |
| 230026 | REPLACEMENT OF CARBON SEAL O-RING | N/A TO DATE |
| 230058 | REPLACEMENT OF OIL FILTER ELEMENT | EMBODIED |
| 230061 | REPLACEMENT OF FIRST STAGE TURBINE DISK | EMBODIED |
| 230062 | REPLACEMENT OF SECOND STAGE TURBINE DISKS | EMBODIED |
| 230063 | REPLACEMENT OF TURBINE WHEEL ASSEMBLIES (FIRST AND SECOND STAGES) |
EMBODIED |
| 230066 | REPLACEMENT OF THE FIRST STAGE TURBINE WHEEL ASSEMBLY |
EMBODIED |
| 230067 | REPLACEMENT / MODIFICATION OF THE SECOND STAGE TURBINE WHEEL AND SECOND STAGE TURBINE NOZZLE ASSEMBLY |
EMBODIED |
For Sale
APU Model: GTCP131-9B
This APU was inducted to Honeywell on October 25, 2021, where it was cleaned, inspected, repaired, and released. The APU has operated 2,571.8 hours and 2,755 cycles since the last shop visit and has been long-term preserved, due in August 2026. The APU has been inspected, issued a CASA SV tag and is available for outright sale.
Contact your Regional Sales Manager at C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | P-6233 |
| Model: | GTCP131-9B |
| Aircraft: | B737-800 |
| TSN: | 30,657.6 |
| TSO: | |
| LSV Date: | October 25, 2021 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | APU Cycles Remaining |
|---|---|---|---|---|---|
| Comp. Rotor EC | 3822391-6 | 1,795.6 | 1,384 | 29,065 | 27,245 |
| 1st Stage Turbine Disk | 3840310-3 | 10,524.1 | 10,882 | 29,065 | 18,461 |
| 2nd Stage Turbine Disk | 3840165-4 | 10,524.1 | 10,882 | 29,065 | 18,461 |
| Turbine Shaft | 3822504-3 | 10,524.1 | 10,882 | 29,065 | 18,461 |
APU
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Comp. Rotor EC | 3822391-6 | 1,795.6 | 1,384 | 29,065 | 27,245 |
| 1st Stage Turbine Disk | 3840310-3 | 10,524.1 | 10,882 | 29,065 | 18,461 |
| 2nd Stage Turbine Disk | 3840165-4 | 10,524.1 | 10,882 | 29,065 | 18,461 |
| Turbine Shaft | 3822504-3 | 10,524.1 | 10,882 | 29,065 | 18,461 |
For Sale
APU Model: RE100-CS (S/N: P-294)
This APU was last inducted to Honeywell, where it was inspected, repaired, and released on June 7, 2022. The APU has operated 1,242.7 hours and 1,550 cycles since the last shop visit and is currently available for outright sale in As-Removed condition. Contact your Sales Manager at C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | P-294 |
| Model: | RE100-CS |
| Aircraft: | Cessna 680 |
| TSN: | 11,354.5 |
| TSO: | |
| LSV Date: | June 7, 2022 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 3842340-2 | 1,242.7 | 1,550 | 12,000 | 10,450 |
| Compressor Impeller | 3822523-003 | 10,786.2 | 13,521 | 36,000 | 22,479 |
| Fuel Control | 3883900-1 | ||||
| Ignition Unit | 3888000-7 | ||||
| Lube Pump | 3881825-1 | ||||
| Start Counter | 3876317-1 |
APU
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 3842340-2 | 1,242.7 | 1,550 | 12,000 | 10,450 |
| Compressor Impeller | 3822523-003 | 10,786.2 | 13,521 | 36,000 | 22,479 |
| Fuel Control | 3883900-1 | ||||
| Ignition Unit | 3888000-7 | ||||
| Lube Pump | 3881825-1 | ||||
| Start Counter | 3876317-1 |
For Sale
APU Model: RE100-XL (S/N: P-373)
This APU was last inducted to Honeywell for LLP replacement, where it was inspected, repaired, and released on March 31, 2022. The APU has operated 1,533.9 hours and 2,340 cycles since the last shop visit and is currently available for outright sale in As-Removed condition. Contact your Sales Manager at C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | P-373 |
| Model: | RE100-XL |
| Aircraft: | Cessna 560XL |
| TSN: | 11,793.5 |
| TSO: | |
| LSV Date: | March 31, 2022 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 70722360-2 | 1,533.9 | 2,340 | 4,000 | 1,660 |
| Compressor Impeller | 3822523-003 | 6,011.4 | 9,889 | 12,000 | 2,111 |
| Fuel Control | 3883900-1 | Inspected | Inspected | Inspected | Inspected |
| Ignition Unit | 3888000-7 | Inspected | Inspected | Inspected | Inspected |
| Lube Pump | 3881825-2 | Inspected | Inspected | Inspected | Inspected |
| Start Counter | 3876317-1 | Inspected | Inspected | Inspected | Inspected |
| Oil Level Sensor | 3876318-3 | New | New | New | New |
| Lop Switch | 3876351-1 | Inspected | Inspected | Inspected | Inspected |
For Sale
CF34-3A Engine 350109
| Summary | |
|---|---|
| Serial Number: | 350109 |
| Model: | CF34-3A |
| Aircraft: | Challenger 601 |
| TSN: | 8853.9 |
| TSO: | 2858.7 |
| LSV Date: | |
Hot Section
| FAN MODULE | |||||
|---|---|---|---|---|---|
| Item | Part Number | S/N | CSN | 3A Cycles Remain | 3A Cycles Remain |
| Disk, Fan | 5921T54G01 | GATT4735 | 5774 | 9000 | 3226 |
| Shaft, Forward Fan | 6017T63P05 | GATT2366 | 5774 | 38280 | 32506 |
| Shaft, Fan Drive | 6036T78P02 | CWE1935 | 5774 | 15000 | 9226 |
| COMPRESSOR MODULE | |||||
| Blisk, Stage 1 Compressor Motor | 6040T79G01 | GATR2212 | 5675 | 6000 | 325 |
| Shaft, Compressor Forward | 5037T01P03 | GATS3652 | 5675 | 11836 | 6161 |
| Disk, Stage 2 Compressor Rotor | 6036T91P01 | GATR6467 | 5675 | 15000 | 9325 |
| Spool, Stage 3-8 Compressor Rotor | 6036T75P03 | GATR8768 | 5774 | 6000 | 226 |
| Spool, Stage 10-14 Compressor Rotor Rear | 6037T83P04 | GATS3336 | 5774 | 6000 | 226 |
| Seal, Compressor Discharge Rotating | 4019T38P01 | APV15206 | 5675 | 14495 | 8820 |
| Shaft, Compressor Rotor Rear | 6016T83P01 | GATP9346 | 5675 | 6000 | 325 |
| Disk, Stage 9 Compressor Rotor | 6016T43P03 | GATP0705 | 5774 | 6000 | 226 |
| HTP MODULE | |||||
| Seal, Balance Piston Air | 3921T56P01 | GATT6888 | 5757 | 7200 | 1443 |
| Shaft, HPT Rotor | 6017T00P04 | GATU0810 | 5658 | 6000 | 342 |
| Plate, Stage 1 Front Cooling | 3921T52P01 | GATU6868 | 5757 | 6000 | 243 |
| Disk, Stage 1 Turbine | 3922T54P01 | GATP3555 | 5757 | 6000 | 243 |
| Plate, Stage 1 Aft Cooling | 5041T70P03 | GAT7588E | 2554 | 6000 | 3446 |
| Plate, Stage 2 Rear Cooling | 3921T54P01 | GATV9119 | 5757 | 6000 | 243 |
| Disk, Stage 2 Turbine | 3921T51P01 | GATW2451 | 5757 | 6000 | 243 |
| Plate, Stage 2 Front Cooling | 3921T53P01 | GATT5154 | 5757 | 6000 | 243 |
| Coupling, Outer Torque | 3921T61P01 | GATV7852 | 5757 | 6000 | 243 |
| LPT MODULE | |||||
| Shaft, Turbine Rear | 4922T19P01 | GATS4459 | 5774 | 34708 | 28934 |
| Disk, Stage 3 Turbine | 4922T14P01 | GATT0273 | 5774 | 6000 | 226 |
| Seal, Stage 3 and 4 Turbine | 4922T20P01 | ABIA2459 | 5774 | 29948 | 24174 |
| Disk, Stage 4 Turbine | 4922T15P01 | GATS5002 | 5774 | 6000 | 226 |
| Disk, Strage 6 Turbine | 6078T89P03 | GATHF45W | 1221 | 15000 | 13779 |
| Seal, Stage 5 and 6 Turbine | 4922T22P01 | ABIA4180 | 5774 | 29948 | 24174 |
| Disk, Stage 5 Turbine | 6078T92P02 | GATHF22M | 1221 | 15000 | 13779 |
| Cone, Turbine Drive | 4922T18P01 | GATP8014 | 5774 | 15000 | 9226 |
| Seal, Stage 4 and 5 Turbine | 4922T21P01 | HAAB0709 | 5774 | 29948 | 24174 |
For Sale
CF34-3B/-3B1 Engine 872046
| Summary | |
|---|---|
| Serial Number: | 872046 |
| Model: | CF34-3B/-3B1 |
| Aircraft: | Challenger 604 |
| TSN: | 6104.5 |
| TSO: | |
| LSV Date: | |
Hot Section
| FAN MODULE | ||||||
|---|---|---|---|---|---|---|
| Item | Part Number | S/N | TSN | CSN | 3B Cycles Remain | 3B1 Cycles Remain |
| Disk, Fan | 6078T57G04 | GEE09277 | 6104.5 | 4131 | 25869 | 21558 |
| Shaft, Forward Fan | 6078T51P02 | GATCEN02 | 6104.5 | 4131 | 15869 | 19836 |
| Shaft, Fan Drive | 6036T78P02 | BCM40321 | 6104.5 | 4131 | 15869 | 19836 |
| COMPRESSOR MODULE | ||||||
| Blisk, Stage 1 Compressor Motor | 5087T84P01 | GLHK1319 | 6104.5 | 4131 | 15869 | 17,615 |
| Shaft, Compressor Forward | 5037T01P03 | GATCDL49 | 6104.5 | 4131 | 25869 | 25869 |
| Disk, Stage 2 Compressor Rotor | 6078T56P04 | GATCEA16 | 6104.5 | 4131 | 10869 | 18115 |
| Spool, Stage 3-8 Compressor Rotor | 5087T46P04 | GATCEM83 | 6104.5 | 4131 | 15869 | 17456 |
| Seal, Compressor Discharge Rotating | 4019T38P01 | PAMU2323 | 6104.5 | 4131 | 25869 | 25869 |
| Shaft, Compressor Rotor Rear | 6087T03P03 | GEE08415 | 6104.5 | 4131 | 10869 | 18115 |
| Disk, Stage 9 Compressor Rotor | 6087T01P03 | GATCEG99 | 6104.5 | 4131 | 10869 | 18115 |
| Spool, Stage 10-14 Compressor Repair | 5087T46P02 | GATCEM74 | 6104.5 | 4131 | 10869 | 18115 |
| HTP MODULE | ||||||
| Seal, Balance Piston Air | 5079T63P02 | GATCER37 | 6104.5 | 4131 | 10869 | 13043 |
| Shaft, HPT Rotor | 5079T62P02 | GEE09300 | 6104.5 | 4131 | 15869 | 23804 |
| Plate, Stage 1 Front Cooling | 5079T65P06 | NCE7933E | 6104.5 | 4131 | 15869 | 23804 |
| Disk, Stage 1 Turbine | 5079T52P09 | GATCEL09 | 6104.5 | 4131 | 10869 | 13043 |
| Plate, Stage 1 Aft Cooling | 5123T02P01 | NCE7991E | 6104.5 | 4131 | 9869 | 12689 |
| Plate, Stage 2 Rear Cooling | 5079T56P02 | NCE8170E | 6104.5 | 4131 | 15869 | 23804 |
| Disk, Stage 2 Turbine | 5079T73P02 | GATCFE58 | 6104.5 | 4131 | 10869 | 13043 |
| Plate, Stage 2 Front Cooling | 5079T55P04 | NCE6552E | 61041.5 | 4131 | 10869 | 21738 |
| Coupling, Outer Torque | 5079T64P05 | GATCFA12 | 6104.5 | 4131 | 15869 | 23804 |
| LPT MODULE | ||||||
| Shaft, Turbine Rear | 6030T72P02 | PAMV3252 | 5584.1 | 3755 | 11245 | 18742 |
| Disk, Stage 3 Turbine | 6078T91P01 | GATCTH60 | 5584.1 | 3755 | 11245 | 18742 |
| Seal, Stage 3 and 4 Turbine | 5023T59P02 | PAMU9643 | 5584.1 | 3755 | 11245 | 11245 |
| Disk, Stage 4 Turbine | 6078T02P03 | GATCTH7R | 5584.1 | 3755 | 11245 | 18742 |
| Disk, Strage 6 Turbine | 6078T89P03 | GATHNC51 | 3038.6 | 2029 | 12971 | 21618 |
| Seal, Stage 5 and 6 Turbine | 5023T64P02 | PAMV9129 | 3058.9 | 2077 | 12923 | 12923 |
| Disk, Stage 5 Turbine | 6078T92P02 | GATHNCOW | 3038.6 | 2029 | 12971 | 21618 |
| Cone, Turbine Drive | 5023T40P03 | BCM50251 | 5584.1 | 3755 | 11245 | 18742 |
| Seal, Stage 4 and 5 Turbine | 5023T67P02 | WES41137 | 3052.7 | 2039 | 12961 | 21602 |
For Sale
CF34-3B/-3B1 Engine 872049
| Summary | |
|---|---|
| Serial Number: | 872049 |
| Model: | CF34-3B/-3B1 |
| Aircraft: | Challenger 604 |
| TSN: | 5968.7 |
| TSO: | |
| LSV Date: | |
Hot Section
| FAN MODULE | ||||||
|---|---|---|---|---|---|---|
| Item | Part Number | S/N | TSN | CSN | 3B Cycles Remain | 3B1 Cycles Remain |
| Disk, Fan | 6078T57G04 | GEE09282 | 5968.7 | 4047 | 25953 | 21022 |
| Shaft, Forward Fan | 6078T51P02 | GATCEM95 | 5968.7 | 4047 | 15953 | 19941 |
| Shaft, Fan Drive | 6036T78P02 | BCM42198 | 5968.7 | 4047 | 15953 | 19941 |
| COMPRESSOR ROTOR | ||||||
| Blisk, Stage 1 Compressor Rotor | 5087T84P01 | GLHK2257 | 5968.7 | 4047 | 15953 | 17708 |
| Shaft, Compressor Forward | 5037T01P03 | GATCEU60 | 5968.7 | 4047 | 25953 | 25953 |
| Disk, Stage 2 Compressor Rotor | 6036T91P02 | GATCGL10 | 5968.7 | 4047 | 10953 | 18255 |
| Spool, Stage 3-8 Compressor Rotor | 6078T56P04 | GATCFN45 | 5968.7 | 4047 | 15953 | 17548 |
| Spool, Stage 10-14 Compressor Rotor Rear | 5087T46P02 | GATCEU05 | 5968.7 | 4047 | 10953 | 18255 |
| Seal, Compressor Discharge Rotating | 4019T38P01 | PAMU2313 | 5968.7 | 4047 | 25953 | 25953 |
| Shaft, Compressor Rotor Rear | 6087T03P03 | GEE08439 | 5968.7 | 4047 | 10953 | 18255 |
| Disk, Stage 9 Compressor Rotor | 6087T01P03 | GATCFH68 | 5968.7 | 4047 | 10953 | 18255 |
| HP TURBINE ROTOR | ||||||
| Seal, Balance Piston Air | 5079T63P02 | NCU48243 | 832.9 | 501 | 14499 | 17399 |
| Shaft, HPT Rotor | 5079T62P02 | GEE09829 | 5968.7 | 4047 | 15953 | 23930 |
| Plate, Stage 1 Front Cooling | 5079T65P06 | NCE7931E | 5968.7 | 4047 | 15953 | 23930 |
| Disk, Stage 1 Turbine | 5079T52P09 | GATCGL02 | 5968.7 | 4047 | 10953 | 13144 |
| Plate, Stage 1 Aft Cooling | 5123T02P01 | UKT07085 | 5968.7 | 4047 | 9953 | 10664 |
| Plate, Stage 2 Rear Cooling | 5079T56P02 | NCE8128E | 5968.7 | 4047 | 15953 | 23930 |
| Disk, Stage 2 Turbine | 5079T73P02 | GATCGK84 | 5968.7 | 4047 | 10953 | 13144 |
| Plate, Stage 2 Front Cooling | 5079T55P04 | NCE8041E | 5968.7 | 4047 | 10953 | 21906 |
| Coupling, Outer Torque | 5079T64P05 | NCU41348 | 832.9 | 501 | 19499 | 29249 |
| LP TURBINE ROTOR | ||||||
| Shaft, Turbine Rear | 6030T72P02 | PAMU1951 | 5968.7 | 4047 | 10953 | 18255 |
| Disk, Stage 3 Turbine | 6078T91P01 | GATCEE04 | 5968.7 | 4047 | 10953 | 18255 |
| Seal, Stage 3 and 4 Turbine | 5023T59P06 | WES51174 | 2916.9 | 1955 | 13045 | 21742 |
| Disk, Stage 4 Turbine | 6078T02P03 | GATCDW08 | 5968.7 | 4047 | 10953 | 18255 |
| Disk, Stage 6 Turbine | 6078T89P03 | GATHNC61 | 2902.8 | 1945 | 13055 | 21758 |
| Seal, Stage 4 and 5 Turbine | 5023T64P02 | WES37183 | 4920.8 | 3894 | 11106 | 18510 |
| Disk, Stage 5 Turbine | 6078T92P01 | GATCHNC4C | 2902.8 | 1945 | 13055 | 21758 |
| Cone, Turbine Drive | 5023T40P03 | BCM40829 | 5968.7 | 4047 | 10953 | 18255 |
| Seal, Stage 5 and 6 Turbine | 5023T67P01 | PAMT7691 | 5968.7 | 4047 | 10953 | 10953 |
For Sale For Lease
CT7-5A2 PT Module s/n GE-L-067432
| Summary | |
|---|---|
| Serial Number: | GE-L-067432 |
| Model: | CT7-5A2 |
| Aircraft: | Saab 340A |
| TSN: | 22731 |
| TSO: | N/A |
| LSV Date: | January 1, 2010 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| PT Rotor Assy | 5043T75G21 | 22731 | 23252 | N/A | N/A |
| Stage 3 Disk | 6055T98P01 | 13501 | 12403 | 22800 | 10397 |
| Stage 4 Disk | 6038T34P05 | 501 | 594 | 24000 | 23406 |
| PT Drive Shaft | 5121T01G01 | 15770 | 14795 | 30000 | 15205 |
| Stage 3 Blades | 6038T39P09 | 501 | 594 | N/A | N/A |
| Turbine Case | 6044T55G13 | 501 | 594 | N/A | N/A |
Note: This engine is up to the following SB standard as a minimum. There are no outstanding FAA AD’s or Service Bulletins as of January 2010:
Service Bulletin / AD Compliance Record
| SB Number | Description |
|---|---|
| 72-363R1 | Introduction of PT Drive Shaft P/N 512T01G01 with Omni Seal |
| 72-000 | Hardware exposed to abnormal operating events |
| 72-111R2 | Turbine Case rework |
| 72-395 | Introduction of Omni Seal Configuration |
| 72-401 | Exhaust Frame Drain Hole |
| 72-153 | No. 5 & 6 Bearing packing replacement |
| 72-294 | Introduction of Radiation Heat Shield P/N 5078T26P01 |
| 72-438R1 | 72-438R2 Introduction of New No. 5 Carbon Seal assembly |
| 72-365 | Elimination of Asbestos material |
For Sale
CT7-9C S/N GE-E-309132A
The engine has been fitted with a 6068T72P25 HMU and stored in a pressurized storage container per GE Maintenance Manual SEI 576 since the last shop visit. Optional configuration including PGB is available. All mandatory AD’s have been accomplished and the engine is offered with a fresh 8130-3 from GE Engine Services. Contact you Regional Sales Manager at C&L Aerospace for more information.
| Summary | |
|---|---|
| Serial Number: | GE-E-309132A |
| Model: | CT7-9C |
| Aircraft: | CASA CN235 |
| TSN: | 17782.9 |
| TSO: | 0 |
| LSV Date: | December 18, 2015 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 0 | 0 | 26900 | 26900 |
| Stage 2 Blisk | 6055T84P10 | 0 | 0 | 20800 | 20800 |
| Stage 3/4 Blisk | 6055T15P10 | 0 | 0 | 18000 | 18000 |
| Stage 5 Blisk | 6044T42P11 | 0 | 0 | 35100 | 35100 |
| Impeller | 5123T51P02 | 0 | 0 | 21600 | 21600 |
| Tie Rod | 5043T04P03 | 0 | 0 | 40000 | 40000 |
| Rear Shaft | 5086T47P03 | 0 | 0 | 31800 | 31800 |
| GG Shaft | 6068T44P02 | 0 | 0 | 28200 | 28200 |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 0 | 0 | 10000 | 10000 |
| Stage 2 Disk | 6064T12P03 | 0 | 0 | 15000 | 15000 |
| Stage 2 Fwd C/P | 4106T80P01 | 0 | 0 | 13200 | 13200 |
| Stage 1 Aft C/P | 6064T09P01 | 0 | 0 | 15000 | 15000 |
| Stage 1 Disk | 6064T06P03 | 0 | 0 | 15000 | 15000 |
| Stage 1 Fwd C/P | 6064T08P03 | 0 | 0 | 10000 | 10000 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 0 | 0 | 18600 | 18600 |
| Stage 4 Disk | 6068T32P05 | 0 | 0 | 18600 | 18600 |
| PT Shaft | 5121T01G01 | 9702.6 | 10342 | 30000 | 19658 |
| Turb. Int. Seal | 5060T86P05 | 0 | 0 | 16000 | 16000 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| MAX CONT | 40°C± |
| TAKEOFF | TBD |
Ohms Resistance = N/K Ω
For Sale
GTCP30-92C s/n P-150
Engine Details:
Hobbs Meter Reading: 4891.5
Time since repair: 0 Hours
Last repair facility: Piedmont aviation W/O# AN20801
8130-Dual release included
Dated: NOV -15 -2012
| Summary | |
|---|---|
| Serial Number: | P-150 |
| Model: | GTCP30-92C |
| Aircraft: | Hawker 800A |
| TSN: | 4891.5 |
| TSO: | 0 |
| LSV Date: | November 15, 2012 |
Note: This engine is up to the following SB standard:
Accessory Inventory Listing
| P/N | |
|---|---|
| 369945-6 | Atomizer |
| 394206-5 | FCU |
| 370854 | EGT |
| 694890-1 | Overspeed Switch |
| 693012 | Tach Generator |
| 379908 | Fuel Solenoid |
| 354972-6 | Oil Pressure Regulator |
| 305179-1 | Wiring Harness |
| 107996-81-1 | Load Stat |
For Sale
PW127M FOR SALE ESN: ED0092
| Summary | |
|---|---|
| Serial Number: | ED0092 |
| Model: | PW127M |
| Aircraft: | ATR |
| TSN: | 9,981 |
| TSO: | First Run |
| LSV Date: | November 2022 |
Hot Section
| Item | CSN | Cycles Remaining | % Time Remaining |
|---|---|---|---|
| L.P. Impeller | 4,171 | 10,829 | 72% |
| H.P. Impeller | 4,171 | 10,829 | 72% |
| H.P. Front Cover | 4,797 | 8,872 | 59% |
| Seal, Air Interstage* | 5,214 | 7,829 | 52% |
| H.P. Rear Cover* | 4,171 | 10,829 | 72% |
| H.P. Blades | – | 15,000 | 100% |
| H.P. Disk | 4,171 | 10,829 | 72% |
| L.P. Disk | 4,171 | 10,829 | 72% |
| 1st P.T. Disk | 4,171 | 25,829 | 86% |
| 2nd P.T. Disk | 4,171 | 25,829 | 86% |
Limiter: Seal, Air Interstage – 7,829 CR
- FCU used to calculate the CR
For Sale
PW127M FOR SALE ESN: ED0294
| Summary | |
|---|---|
| Serial Number: | ED0294 |
| Model: | PW127M |
| Aircraft: | ATR |
| TSN: | 6,596 |
| TSO: | First Run |
| LSV Date: | March 2024 |
Hot Section
| Item | CSN | Cycles Remaining | % Time Remaining |
|---|---|---|---|
| L.P. Impeller | 7,307 | 7,693 | 51% |
| H.P. Impeller | 7,307 | 7,693 | 51% |
| H.P. Front Cover | – | 15,000 | 100% |
| Seal, Air Interstage | – | 15,000 | 100% |
| H.P. Rear Cover | 7,307 | 7,693 | 51% |
| H.P. Blades | – | 15,000 | 100% |
| H.P. Disk | 7,307 | 7,693 | 51% |
| L.P. Disk | 7,307 | 7,693 | 51% |
| 1st P.T. Disk | 7,307 | 22,693 | 76% |
| 2nd P.T. Disk | 7,307 | 22,693 | 76% |
Limiter: various – 7,693 CR
For Sale
PW306C S/N: PCE-CG0023
| Summary | |
|---|---|
| Serial Number: | |
| Model: | |
| Aircraft: | |
| TSN: | |
| TSO: | |
| LSV Date: | |
For Sale
PW306C: S/N: PCE-CG0023
This engine was inducted to Dallas Airmotive, where it was inspected, overhauled, tested, and released with an 8130 Dual Release certificate on August 24, 2022. The engine has operated 263.2 hours and 103 cycles since its last shop visit and is being offered for sale in As-Removed condition.
CSN: 10,363
CSO: 1,317
| Summary | |
|---|---|
| Serial Number: | CE-CG0023 |
| Model: | PW306C |
| Aircraft: | Cessna Sovereign 680 |
| TSN: | 15,423.1 |
| TSO: | 1,952.8 |
| LSV Date: | August 24, 2022 |
Since Repair
| Item | Part Number | TSR | CSR | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 4923T37G23 | 68 | 256 | 87 | 83 |
| Stage 1 Blisk | 4923T37G23 | 68 | 256 | 87 | 83 |
Sold
APU Model: APS500 S/N: SP-E974057
This APU was inducted to NExT MRO in March 2023 where it was inspected, repaired, and preserved with an FAA 8130-3 Dual
Release. There are no outstanding Airworthiness Directives or Alert Service Bulletins due at this time.
| Summary | |
|---|---|
| Serial Number: | SP-E974057 |
| Model: | APS500 |
| Aircraft: | ERJ 135/145 |
| TSN: | UNK |
| TSO: | |
| LSV Date: | March 22, 2023 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 45045744923T37G23 | N/A | N/A | ||
| Stage 1 Blisk | 4923T37G23 | N/A | N/A |
LRUs
| Item | P/N | S/N | TSN |
|---|---|---|---|
| Engine Control Harness | 4504051B | V28-S109UNK | UNK |
| Gearbox Assy | 4501979B | V51D0139 | UNK |
| Surge Valve | 4950899 | 0279 | UNK |
| Ignition Exciter | 4950745 | 01174029 | UNK |
| High Oil Temperature Switch | 4952459-2 | 311 | UNK |
| Fuel Pump | 4951545 | V48-T0519 | UNK |
| Servo Control Bleed Air Valve | 4950958 | 0136A | UNK |
| Ignitors | 26519-1, 26519-1 | N/A | UNK |
| Ignition Cable | 115352-4 | N/A | UNK |
| Ignition Cable | 115352-1 | N/A | UNK |
| Filter Assy. | 4950769 | 0086 | UNK |
| Fuel Nozzle | 4504401A | N/A | UNK |
| Fuel Nozzle | 4504401A | NHSA405 | UNK |
| Fuel Nozzle | 4504401A | HSA9072 | UNK |
| Fuel Solenoid Valve | 4952316-2 | 1364 | UNK |
| Fuel Solenoid Valve | 4952316-2 | 2048 | UNK |
| Fuel Solenoid Valve | 4952316-1 | 0015 | UNK |
| Filter Assy. | 4950769 | 0086 | UNK |
| Magnetic Plug | 4950868 | N/A | UNK |
SB EMBODIMENT:
No SB incorporated during this shop visit.
AD EMBODIMENT:
None apply to the APS 500 at this time
Sold
APU Model: RE100-CS (S/N: P-358)
This APU was inducted to Honeywell PHX in February 2022, where it was upgraded IAW CMM 49-24-65, as well as SB 49-7997 and SB 49-8303. Turbine rotor was newly replaced at this shop visit and the APU was repaired and released with no outstanding AD’s. The APU has operated 920.2 hours since the last shop visit and is currently in the process of receiving a fresh test cell run, long term preservation and 8130 Dual Release. Contact your Sales Manager at C&L Aerospace for additional information.
*Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | P-358 |
| Model: | RE100-CS |
| Aircraft: | Cessna 680 |
| TSN: | 9362.7 |
| TSO: | |
| LSV Date: | 02/10/2022 |
Cold Section
Inspections (Hourly)
*Indicative of April 2023 Test & Long Term Preservation
| Description | Interval | C/W APU TSN | TSR | Next Due | Hours Remaining |
|---|---|---|---|---|---|
| Chip Detector | 450 (12 MO) | 9362.7 | 504.7 | 9812.7 (*04/2024) | 0 |
| Ignitor Plug | 900 (24 MO) | 9362.7 | 920.2 | 10262.7 (*04/2025) | 0 |
| Lubricating Oil System | 900 (24 MO) | 9362.7 | 920.2 | 10262.7 (*04/2025) | 0 |
| Oil Filter Element | 900 (24 MO) | 9362.7 | 920.2 | 10262.7 (*04/2025) | 0 |
| Fuel Filter element | 900 (24 MO) | 9362.7 | 920.2 | 10262.7 (*04/2025) | 0 |
Inspections (Cyclical)
| Description | Interval | C/W APU CSN | CSR | Next Due | Hours Remaining |
|---|---|---|---|---|---|
| Combustor Chamber | 12000 | 11757 | 959 | 23757 | 11041 |
| Interstage Seal | 12000 | 11757 | 959 | 23757 | 11041 |
| Retainer | 12000 | 11757 | 959 | 23757 | 11041 |
| Shim | 12000 | 11757 | 959 | 23757 | 11041 |
| Fuel Nozzle Assy. | 12000 | 11757 | 959 | 23757 | 11041 |
| Deswirl Deflector | 12000 | 11757 | 959 | 23757 | 11041 |
| Turbine Housing Assy. | 12000 | 11757 | 959 | 23757 | 11041 |
| Turbine Nozzle | 12000 | 11757 | 959 | 23757 | 11041 |
| Turbine Rotor Replacement | 12000 | 11757 | 959 | 23757 | 11041 |
| Compressor Rotor | Next Exposure | — | — | At Access | — |
| Compressor Rotor Replacement | 36000 | 11757 | 959 | 23757 | 11041 |
Since Repair
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 70722360-1 | 920.2 | 959 | 12000 | 11041 |
| Compressor Rotor | 3822523-003 | 3205.4 | 3628 | 36000 | 32372 |
| Fuel Control | 3883900-1 | ||||
| Ignition Unit | 3888000-7 | ||||
| Lube Pump | 3881825-1 | ||||
| Start Counter | 3876317-1 |
Note: This engine is up to the following SB standard:
Service Bulletin / *AD Embodiment
| Cold Section | Hot Section | Bulletin |
|---|---|---|
| SB 49-7992 | 06/02/2012 | Remove and replace electronic control unit (P/N: 2119552-2 or P/N: 2119552-3) with electronic control unit (P/N: 2119552-4) |
| SB 49-7997 | 07/26/2018 02/10/2022 |
Standard storage and preservation guidelines |
| SB 49-8303 | 02/08/2022 | Rework and repair of engine for incorporation of improved compressor or carbon seal and related components on the RE100 APU |
| SB 49-7976 | 07/25/2018 | Install fuel flow deflector, P/N: 70720001-1 on the fuel control differential pressure (delta P) sleeve |
| SB 49-8139 | 07/25/2018 | Increase the installation torque and add the use of locking compound during carbon seal assembly on the RE100 APU |
* No airworthiness directives applicable to this engine model.
Sold
APU Model: RE100-XL (S/N: P-664)
This APU was last inducted to Honeywell for LLP replacement in May 2022. The Turbine Rotor and Compressor Rotor were replaced with zero-time units and the APU was inspected, repaired, and released on May 18, 2022. The APU has operated 4,331.7 hours and 1,289 cycles since the last shop visit under an approved maintenance program and is currently available for outright sale in As-Removed condition. Contact your Sales Manager at C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | P-664 |
| Model: | RE100-XL |
| Aircraft: | Cessna 560XLS |
| TSN: | 10,974.6 |
| TSO: | |
| LSV Date: | May 18, 2022 |
Hot Section
INSPECTIONS (HRS): Per approved maintenance program
| DESCRIPTION | INTERVAL | C/W APU TSN | NEXT DUE | HOURS REMAINING |
|---|---|---|---|---|
| Chip Detector | 642 or 12 MO | 11470.6 | 12112.6 | 451.1 |
| APU Oil Servicing | 11470.6 | |||
| APU Inspection | 1285 or 24M | 11470.6 | 12755.6 | 1064.1 |
INSPECTIONS (CYC): May 18, 2022 Shop Visit at APU TSN: 6642.9 / CSN: 11380
| DESCRIPTION | INTERVAL | C/W APU CSN | CSR* | NEXT DUE | REMAINING |
|---|---|---|---|---|---|
| Combustor Chamber | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Interstage Seal | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Retainer | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Shim | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Fuel Nozzle Assy. | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Deswirl Deflector | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Turbine Housing Assy. | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Turbine Nozzle | 4,000 | 11380 | 1289 | 15380 | 2711 |
| Turbine Rotor Replacement | 4,000 | 11380 | 1289 | 15380 | 2711 |
NDC / LIFE LIMITED PARTS: May 18, 2022 Shop Visit at APU TSN: 6642.9 / CSN: 11380
| ITEM | P/N | TSN | CSR* | LIFE LIMIT | CYCLES REMAINING |
|---|---|---|---|---|---|
| Turbine Rotor | 70722360-1 | 4,331.7 | 1,289 | 4,000 | 2,711 |
| Compressor Impeller | 70722359-1 | 4,331.7 | 1289 | 9,000 | 7,711 |
| Fuel Control | 3883900-1 | Repaired at May 2022 Shop Visit | |||
| Ignition Unit | 3888000-7 | Tested at May 2022 Shop Visit | |||
| Oil Level Sensor | 3876318-3 | Tested at May 2022 Shop Visit | |||
| Lube Pump | 3881825-2 | Serviceable Unit Installed at 2022 Shop Visit | |||
| Time Meter | 3876317-1 | Tested at May 2022 Shop Visit | |||
| Lop Switch | 3876351-1 | Tested at May 2022 Shop Visist | 271 |
SB / AD EMBODIMENT:
| SB Number | C/W | Bulletin |
|---|---|---|
| 49-7997 (R2) 49-7997 (R3) 49-7997 (R4) 49-7997 (R6) |
3NOV2011 23FEB2013 9JAN2012 11APR2017 18MAY2022 14JUL2022 |
STANDARD STORAGE AND PRESERVATION GUIDELINES |
| RE100-49-8139 | 8APR2017 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – INCREASE THE INSTALLATION TORQUE AND ADD THE USE OF LOCKING COMPOUND DURING CARBON SEAL ASSEMBLY ON THE RE100 APU |
| 3883900-49-7976 (R1) | 10APR2017 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – INSTALL FUEL FLOW DEFLECTOR P/N: 70720001-1 ON THE FUEL CONTROL DIFFERENTIAL PRESSURE (DELTA P) SLEEVE |
| 3883900-49-8297 (R00) | 18MAY2022 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – REPLACE OIL SEAL P/N: 3883905-1 WITH P/N: 70722907-1 ON THE FUEL CONTROL UNIT (FCU), P/N: 3883900-1 FOR THE RE100 APU |
| RE100-49-8250 (R2) | 18MAY2022 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – REPLACE LUBE MODULE P/N: 3881825-1 WITH P/N: 3881825-2 FOR THE RE100[CS] AND RE100[XL] AUXILIARY POWER UNIT (APU) |
| RE100-49-8303 (R3) | 18MAY2022 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – REWORK AND REPAIR OF ENGINE FOR INCORPORATION OF IMPROVED COMPRESSOR OR CARBON SEAL AND RELATED COMPONENTS ON THE RE100 AUXILIARY POWER UNIT (APU) |
| RE100-49-8360 (R1) | 18MAY2022 |
AIRBORNE AUXILIARY POWER – GAS TURBINE ENGINE – REPLACE RIVET P/N: M24243/6A401H WITH P/N: 627-504-9209 ON ENGINES RE100[CS], RE100[LJ], AND RE100[XL] MODELS |
No airworthiness directives applicable to this engine model.
Sold
APU Model: T-62T-40C14
| Summary | |
|---|---|
| Serial Number: | SP-E0314547 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ-135 |
| TSN: | 13133.7 |
| TSO: | |
| LSV Date: | June 5, 2018 |
Since Repair
| Item | Part Number | TSN | CSR | Life Limit | Hours Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 4504847 | 408.5 | 749 | 15000 | 14251 |
| Compressor Wheel | 4504253 | 408.5 | 749 | On Condition | N/A |
LRUs
LRU ACCESSORIES
| ITEM | P/N | TSN |
| Fuel Solenoid Valve | 4952316-2 | UNK |
| Servo Control Bleed Air Valve | 4952829 | UNK |
| Anti-Surge Valve | 4950899 | UNK |
| Low Oil Pressure Switch | 4952366 | UNK |
| High Oil Temperature Switch | 4952459-1 | UNK |
| Speed Sensor Assy | 4504185C | UNK |
| Secondary Fuel Manifold | 4951610 | UNK |
| Primary Fuel Manifold | 4951609 | UNK |
| Indicator Pressure Differential | 179349-1 | UNK |
| Ignitors | 4952382 | 0 |
| Engine Control Harness | 45042308 | UNK |
| Fuel Control Assy | 45046168 | UNK |
| Flow Divider | 4951486 | UNK |
| Fuel Filter | 4952505 | 0 |
| Ignition Exciter | 4950745 | UNK |
| Data Memory Module | 4505576 | 13132.6 |
| Air/Oil Cooler | 4950929 | UNK |
| Ignition Cable | 4951491 | UNK |
| Ignition Cable | 4950581-1 | UNK |
| Ambient Pressure | 4504196A | 13132.6 |
Sold
APU Model: T-62T-40C14 S/N SP-E0014016
| Summary | |
|---|---|
| Serial Number: | SP-E0014016 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ 145 |
| TSN: | 17600 |
| TSO: | |
| LSV Date: | May 2021 |
Since Repair
| Item | Part Number | TSN | CSR | Life Limit | Hours Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 4504847 | 3580 | 6240 | 15000 | 8760 |
| Compressor Wheel | 4504253 | 3580 | 6240 | 50000 | 43760 |
LRUs
LRUs
| ITEM | P/N | TSN |
| Fuel Solenoid Valve | 4952316-2 | UNK |
| Servo Control Bleed Air Valve | 4952829 | UNK |
| Anti-Surge Valve | 4950899 | UNK |
| Low Oil Pressure Switch | 4952366 | UNK |
| High Oil Temperature Switch | 4952459-1 | UNK |
| Speed Sensor Assy | 4504185D | 0 |
| Secondary Fuel Manifold | 4951610 | 3580 |
| Ignitors | CH34834 | 0 |
| Engine Control Harness | 4504230B | UNK |
| Fuel Control Assy | 4504616A | UNK |
| Flow Divider | 4951486 | UNK |
| Fuel Filter | 4952505 | 0 |
| Ignition Exciter | 4950745 | UNK |
| Data Memory Module | 4505576 | UNK |
| Air/Oil Cooler | 4950929 | UNK |
| Ambient Pressure | 4504196A | UNK |
SM EMBODIMENT
| SB Number | SB Description | CW Date |
|---|---|---|
| 4504112-49-1 | Fuel filter cap assy replacement | 1/4/2003 |
| 4504112-49-5 | Intro. of engine control harness assy | 1/4/2003 |
| 4504112-49-6 | Intro. of fuel control assy | 1/4/2003 |
| 4504112-49-8 | Intro. of quill shaft PN 4504407A | 1/4/2003 |
| 4504112-49-10 | Intro. of servo controlled bleed valve | 1/4/2003 |
| 4504112-49-11 | New engine configuration | 11/3/2006 |
| 4504112-49-15R1 | Intro. of reinforced drain lines | 12/26/2003 |
| 4504112-49-19 | Improved servo controlled bleed air valve | 12/26/2003 |
| 4504112-49-20 | Intro. of improved hot switch | 12/26/2003 |
| 450112-49-21 | AI housing with rounded bosses | 11/3/2006 |
| 4504112-49-22R3 | Fuel filter assy replacement | 5/22/2012 |
| 4504112-49-24 | Large mod. plate | 11/3/2006 |
| 4504112-49-27 | Add shims, cold start bypass valve | 11/3/2006 |
| 4504112-49-29 | Improved combustor housing | 11/3/2006 |
| 4504112-49-30 | AI hsg w/ improved shroud coat | 11/3/2006 |
| 4504112-49-32 | Improved speed sensor | 11/3/2006 |
Sold
APU Model: T-62T-40C14 S/N SP-E0114167
This APU was inducted into NExT MRO where it was repaired, tested, and released on July 28th, 2023. The unit was long-term preserved in accordance with the manufacturer’s procedures, and preservation is good until July 27th, 2024.
There are no outstanding Airworthiness Directives or Alert Service Bulletins due at this time.
*Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | SP-E0114167 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ 135/145 |
| TSN: | |
| TSO: | |
| LSV Date: | July 28, 2023 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 4504847 | N/A | 4 | 15000 | 14996 |
| Compressor Wheel | 4504253 | N/A | 11182 | 50000 | 38818 |
LRUs
| Item | P/N | Tested |
|---|---|---|
| Fuel Solenoid Valve | 4952316-2 | Yes |
| Servo Control Bleed Air Valve | 4956056 | Yes |
| Anti-Surge Valve | 4950899 | Yes |
| Low Oil Pressure Switch | 4952366 | Yes |
| High Oil Temperature Switch | 4952397-1 | Yes |
| Speed Sensor Assy | 4504185C | Yes |
| Ignitors | 4952382 | Yes |
| Engine Control Harness | 4504230B- | Yes |
| Fuel Control Assy | 4504616B | Yes |
| Flow Divider | 4951486 | Yes |
| Ignition Exciter | 4950745 | Yes |
| Data Memory Module | 4505576 | Yes |
| Air/Oil Cooler | 4950929 | Yes |
| Ambient Pressure | 4504196 | Yes |
| Gearbox Assy | 4504235C | Yes |
Service Bulletin Embodiment
ASB 4504112-49-44
AD EMBODIMENT:
No ADs apply to the APS 500 at this time.
Sold
APU Model: T-62T-40C14 S/N SP-E0114217
| Summary | |
|---|---|
| Serial Number: | SP-E0114217 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ 145 |
| TSN: | 28151.0 |
| TSO: | |
| LSV Date: | January 6, 2022 |
Since Repair
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 4504847 | 0.0 | 0 | 15000 | 15000 |
| Compressor Wheel | 4504253 | 9095.7 | 15050 | On Condition | N/A |
LRUs
LRU
| ITEM | P/N | TSN |
| Fuel Solenoid Valve | 4952316-2 | UNK |
| Servo Control Bleed Air Valve | 4956056 | UNK |
| Anti-Surge Valve | 4950899 | 0.0 |
| Low Oil Pressure Switch | 4952366 | UNK |
| High Oil Temperature Switch | 4952397-1 | UNK |
| Speed Sensor Assy | 4504185D | UNK |
| Ignitors | 4952382 | UNK |
| Engine Control Harness | 4504230B | UNK |
| Fuel Control Assy | 4504616B | UNK |
| Flow Divider | 4951486 | UNK |
| Fuel Filter | 4953126 | 0.0 |
| Ignition Exciter | 4950745 | UNK |
| Data Memory Module | 4505576A | UNK |
| Air/Oil Cooler | 4950929 | UNK |
| Ambient Pressure | 4504196A | UNK |
Note: This engine is up to the following SB standard:
Service Bulletin / AD Compliance Record
| 4504112-49-8 | 4504112-49-22 | 72-4504112-49-27 | 4504112-49-35 |
| 4504112-49-11 | 4504112-49-23 | 4504112-49-29 | 4504112-49-36 |
| 4504112-49-19 | 4504112-49-24 | 4504112-49-30 | 4504112-49-2 |
| 4504112-49-21 | 4504112-49-26 |
Sold
APU Model: T-62T-40C14 S/N SP-E0414657
This APU was inducted to NExT MRO in September 2022 where it was inspected, repaired, nd preserved with an FAA 8130-3 Dual Release. There are no outstanding Airworthiness Directives or Alert Service Bulletins due at this time.
| Summary | |
|---|---|
| Serial Number: | SP-E0414657 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ 135/145 |
| TSN: | 10866.7 |
| TSO: | |
| LSV Date: | Oct. 3, 2022 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Hours Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 4504847 | UNK | 9830 | 15000 | 5170 |
| Compressor Wheel | 4504253 | UNK | 9830 | 50000 | 40170 |
LRUs
| Item | P/N | TSN |
|---|---|---|
| Fuel Solenoid Valve | 4952316-2 | UNK |
| Servo Control Bleed Air Valve | 4952829 | UNK |
| Anti-Surge Valve | 4950899 | UNK |
| Low Oil Pressure Switch | 4951510 | UNK |
| High Oil Temperature Switch | 4952397-1 | UNK |
| Speed Sensor Assy | 4504185D | UNK |
| Secondary Fuel Manifold | 4951610 | UNK |
| Primary Fuel Manifold | 4951609 | UNK |
| Gearbox Assy | 4504235C | UNK |
| Ignitors | 4952382 | UNK |
| Engine Control Harness | 4504230B | UNK |
| Fuel Control Assy | 4504616A | UNK |
| Flow Divider | 4951486 | UNK |
| Fuel Filter | 4951960 | UNK |
| Ignition Exciter | 4950745 | UNK |
| Data Memory Module | 4505576 | UNK |
| Air/Oil Cooler | 4950929 | UNK |
| Ignition Cable | 4951491 | UNK |
| Ignition Cable | 4950581-1 | UNK |
| Ambient Pressure | G4504196A | UNK |
Service Bulletin Embodiment:
4504112-49-27
ASB 4504112-49-22
Sold
APU Model: T-62T-40C14 S/N SP-E1328147
This APU was inducted to NExT MRO in February 2024 where it was inspected, repaired, and preserved with an FAA 8130-3 Dual Release. There are no outstanding Airworthiness Directives or Alert Service Bulletins due at this time.
*Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate
to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained
in this document. Parties interested in the products shown in this document are responsible for verifying
the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | SP-E1328147 |
| Model: | T-62T-40C14 |
| Aircraft: | ERJ 135/145 |
| TSN: | 4,364 |
| TSO: | |
| LSV Date: | February 2024 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Cycles Remaining |
|---|---|---|---|---|---|
| Turbine Wheel | 450847 | 4,364 | 10,356 | 15,000 | 4,644 |
| Compressor Wheel | 4504253 | 4,364 | 10,356 | 50,000 | 39,644 |
LRUs
| Item | P/N | Tested |
|---|---|---|
| Fuel Solenoid Valve | 4952316-2 | UNK |
| Servo Control Bleed Air Valve | 4952829 | UNK |
| Anti-Surge Valve | 4950899 | UNK |
| Low Oil Pressure Switch | 4952366 | UNK |
| High Oil Temperature Switch | 4952397-1 | UNK |
| Speed Sensor Assy | 4504185D | UNK |
| Ignitors (x2) | 4952382 | UNK |
| Engine Control Harness | 4504230B | UNK |
| Fuel Control Assy | 4504616B | UNK |
| Flow Divider | 4951486 | UNK |
| Ignition Exciter | 4950745 | UNK |
| Data Memory Module | 450505576A | UNK |
| Air/Oil Cooler | 4950929 | UNK |
| Ambient Pressure | 4504196A | UNK |
| Gearbox Assy | 4504235E | UNK |
SB EMBODIMENT:
No service bulletins apply to the APS 500 at this time.
AD EMBODIMENT:
No airworthiness directives apply to the APS 500 at this time.
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ATR 72 Engine PW127 PCE-127085
This engine has operated 1,916.8 hours and 3,344 cycles since its last repair and will be delivered with an 8130 Dual Release.
Contact your Regional Sales Manager at C&L Aerospace for more information.
Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | PCE-127085 |
| Model: | PW127 |
| Aircraft: | ATR |
| TSN: | 36,408.5 |
| TSO: | |
| LSV Date: | June 8, 2016 |
Cold Section
| Item | Part Number | CSN | Life Remaining |
|---|---|---|---|
| HP Centrifugal Impeller | 3072766-01 | 13,295 | 1,705 |
| LP Centrifugal Impeller | 3072764-01 | 7,468 | 7,532 |
| 2nd Stage PT Disk | 3033914 | 13,295 | 16,705 |
| 1st Stage PT Disk | 3038513 | 13,295 | 16,705 |
| LPT Disk | 3039412 | 13,295 | 1,705 |
| HPT Front Cover | 3039640 | 13,158 | 1,842 |
| Air Interstage Seal | 3039639 | 12,161 | 2,839 |
| HPT Rear Cover | 3039639 | 13,295 | 1,705 |
| HPT Disk | 3041511 | 12,443 | 2,557 |
| HPT Blades | 3115601-01 | 7,468 | 7,532 |
Hot Section
| Description | Last OH | TSO | CSO |
|---|---|---|---|
| Turbomachine | July 2014 | 3,786.1 | 7,468 |
| Reduction Gearbox | Feb. 2010 | 8,229.9 | 13,295 |
| Hot Section Inspection | July 2014 | 3,786.1 | 7,468 |
Sold
ATR 72 Engine PW127 PCE-127089
This engine has operated 4,116.7 hours and 8,510 cycles since its last repair and will be delivered with an 8130 Dual Release.
Contact your Regional Sales Manager at C&L Aerospace for more information.
Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | PCE-127089 |
| Model: | PW127 |
| Aircraft: | ATR |
| TSN: | 34,060.1 |
| TSO: | |
| LSV Date: | October 9, 2013 |
Cold Section
| Item | Part Number | CSN | Life Remaining |
|---|---|---|---|
| HP Centrifugal Impeller | 3072766-01 | 12,807 | 2,193 |
| LP Centrifugal Impeller | 3072764-01 | 12,807 | 2,193 |
| 2nd Stage PT Disk | 3033914 | 12,807 | 17,193 |
| 1st Stage PT Disk | 3038513 | 12,807 | 17,193 |
| LPT Disk | 3039412 | 12,807 | 2,193 |
| HPT Front Cover | 3039640 | 12,807 | 2,193 |
| Air Interstage Seal | 3039639 | 8,510 | 6,490 |
| HPT Rear Cover | 3039639 | 12,807 | 2,193 |
| HPT Disk | 3041511 | 12,807 | 2,193 |
| HPT Blades | 3115601-01 | 8,510 | 6,490 |
Hot Section
| Description | Last OH | TSO | CSO |
|---|---|---|---|
| Turbomachine | March 2010 | 7,943.7 | 12,807 |
| Reduction Gearbox | March 2010 | 7,943.7 | 12,807 |
| Hot Section Inspection | March 2010 | 7,943.7 | 12,807 |
Sold
ATR 72 Engine PW127 PCE-127100
This engine has operated 199.7 hours and 292 cycles since its last repair at Vector Aerospace in September 2016. All FAA AD’s were confirmed to have been previously complied with and the engine will be delivered with an 8130 Dual Release.
Contact your Regional Sales Manager at C&L Aerospace for more information.
Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | PCE-127100 |
| Model: | PW127 |
| Aircraft: | ATR |
| TSN: | 36,375 |
| TSO: | |
| LSV Date: | September 6, 2016 |
Cold Section
| Item | Part Number | CSN | Life Remaining |
|---|---|---|---|
| HP Centrifugal Impeller | 3072766-01 | 10,501 | 4,499 |
| LP Centrifugal Impeller | 3072764-01 | 10,501 | 4,499 |
| 2nd Stage PT Disk | 3033914 | 10,501 | 19,499 |
| 1st Stage PT Disk | 3038513 | 15,498 | 14,502 |
| LPT Disk | 3039412 | 10,501 | 4,499 |
| HPT Front Cover | 3039640 | 10,501 | 4,499 |
| Air Interstage Seal | 3039172 | 6,628 | 8,372 |
| HPT Rear Cover | 3039639 | 10,501 | 4,499 |
| HTP Disk | 3041511 | 664 | 14,336 |
| HPT Blades | 311561-01 | 3,560 | 11,440 |
Hot Section
| Description | Last OH | TSO | CSO |
|---|---|---|---|
| Turbomachine | Nov. 2010 | 6,333.2 | 10,501 |
| Reduction Gearbox | Nov. 2010 | 6,333.2 | 10,501 |
| Hot Section Inspection | Nov. 2010 | 6,333.2 | 10,501 |
Sold
ATR 72 Engine PW127F PCE-127122
This ATR 72 engine has operated 421.1 hours and 692 cycles since its last repair and will be delivered freshly converted to PW127F configuration with an 8130 Dual Release.
Contact your Regional Sales Manager at C&L Aerospace for more information.
Note:
The information contained in this document has been provided by C&L Aerospace, LLC and is accurate to the best of their knowledge. C&L Aerospace, LLC is not liable for any errors which may be contained in this document. Parties interested in the products shown in this document are responsible for verifying the accuracy of all subject matter.
| Summary | |
|---|---|
| Serial Number: | PCE-127122 |
| Model: | PW127 |
| Aircraft: | ATR |
| TSN: | 33,669.8 |
| TSO: | |
| LSV Date: | July 12, 2016 |
Cold Section
| Item | Part Number | CSN | Life Remaining |
|---|---|---|---|
| HP Centrifugal Impeller | 3072766-01 | 7,369 | 7,631 |
| LP Centrifugal Impeller | 3072764-01 | 7,369 | 7,631 |
| 2nd Stage PT Disk | 3033914 | 23,946 | 6,054 |
| 1st Stage PT Disk | 3038513 | 22,092 | 7,908 |
| LPT Disk | 3039412 | 7,369 | 7,631 |
| HPT Front Cover | 3039640 | 2,097 | 12,903 |
| Air Interstage Seal | 3039639 | 8,037 | 6,963 |
| HPT Rear Cover | 3039639 | 7,369 | 7,631 |
| HPT Disk | 3041511 | 7,369 | 7,631 |
| HPT Blades | 3115601-01 | 7,369 | 7,631 |
Hot Section
| Item | Last OH | TSO | CSO |
|---|---|---|---|
| Turbomachine | June 212 | 3,606.4 | 7,369 |
| Reduction Gearbox | June 2012 | 3,606.4 | 7,369 |
| Hot Section Inspection | June 2012 | 3,606.4 | 7,369 |
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Challenger GTCP36-150CL
| Part Number | Serial Number | Date of Overhaul | Current Assy TSN | Current Acft TAT | Date Installed | Assy TSN @ Install | Acft SN | Acft Reg | Acft TAT @ Install | Current Assy TSO |
| 3800804-1 | P-292C | June-96 | 6742.0 | 6104.5 | 27-Mar-15 | 4697 | 5314 | 2-CLES | 4617.8 | 2045.0 |
| Summary | |
|---|---|
| Serial Number: | P-292C |
| Model: | GTCP36-150CL |
| Aircraft: | Bombardier CL-604 |
| TSN: | 6742 |
| TSO: | |
| LSV Date: | March 30, 2022 |
Since Repair
| Item | Part Number | TSN | CSN | Life Limit | Hours Remaining |
|---|---|---|---|---|---|
| Turbine Rotor | 3822632-1 | 2045.0 | N/A | 10000 | 7955.0 |
| Compressor Rotor | 3822632-1 | 2045.0 | N/A | 20000 | 17955.0 |
LRUs
| Item | P/N | TSR |
| Starter Motor | 2704458-1 | 2045.0 |
| Fuel Control Valve | 3883964-3 | 2045.0 |
| Load Control Valve | Not installed | |
| LOP Switch | Not INstalled | |
| Harness | 3888524-3 | 2045.0 |
Service Bulletin
| Servcie Bulletin | Rev. | Description | Date C/W |
|---|---|---|---|
| 49-7997 | 6 | Standard storage and preservation guidelines | 30-Mar-22 |
| D201408000053 | 0 | Workscope planning guide (WPG 36-150 series) | 8-Mar-15 |
| 49-7885 | 0 | Conversion of GTCP36-100E to 36-150CL configuration | 27-Mar-15 |
| 49-8048 | 1 | Replacement of load control valve coupling | 26-Mar-15 |
| 49-8121 | 2 | Rotating group balancing procedure | 26-Mar-15 |
Inspections
| Description | Interval | C/W APU TSN | Hours Since | Next Due | Hours Remaining |
| Clean LCV Filter | 500 HR | ||||
| Insp Fuel Components | 750 HR | 6742.0 | 0 | 7492.0 | 750.0 |
| Magnetic Chip Detector | 750 HR | 6742.0 | 0 | 7492.0 | 750.0 |
| Fuel Filter Diff Press Indicator | 750 HR | 6742.0 | 0 | 7492.0 | 750.0 |
| Discard Oil | 1000 HR | 6742.0 | 0 | 7492.0 | 750.0 |
| Oil Filter Element | 1000 HR | 6631.0 | 111 | 8631.0 | 889.0 |
| Fuel Filter | 1000 HR | Due at APU fitment to airframe | |||
| Igniter Plug | 2000 HR | 6631.0 | 111 | 8631.0 | 1889.0 |
| Insp Inlet Screens | 2250 HR | 4697.0 | 2045.0 | 6947.0 | 205.0 |
| Rest Starter Motor | 2500 HR | 4697.0 | 2045.0 | 7197.0 | 455.0 |
| Insp Inlet Ducts | 3000 HR | 4697.0 | 2045.0 | 7697.0 | 955.0 |
Sold
CT7-9B Engine S/N GE-E-785254
SUMMARY:
This engine was inducted to H+S Aviation where it was repaired and released on October 14, 2011. The engine received major work scopes to the Cold Section, Hot Section and PTM and has operated 4,272.1 hours and 3,987 cycles since the last major repair. The engine will be long term preserved and released with no outstanding AD’s. Please contact C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | GE-E-785254 |
| Model: | CT7-9B |
| Aircraft: | Saab 340B |
| TSN: | 30,907.5 |
| TSO: | |
| LSV Date: | October 14, 2011 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 4272.1 | 3987 | 26900 | 22913 |
| Stage 2 Blisk | 6055T84P10 | 4272.1 | 3987 | 20800 | 16813 |
| Stage 3/4 Blisk | 6055T15P10 | 4272.1 | 3987 | 18000 | 14013 |
| Stage 5 Blisk | 6044T42P11 | 9372.9 | 8662 | 35100 | 26438 |
| Impeller | 5123T51P02 | 4272.1 | 3987 | 18600 | 17613 |
| Tie Rod | 5043T04P03 | 4272.1 | 3987 | 40000 | 36013 |
| Rear Shaft | 5086T74P03 | 4272.1 | 3987 | 31800 | 27813 |
| GG Shaft | 6068T44P02 | 12483.9 | 15670 | 28200 | 12530 |
| Midframe Case | 6055T47G08 | 4272.1 | 3987 | N/A | N/A |
| Midframe Assy | 6071T77G13 | 4272.1 | 3987 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 4272.1 | 3987 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 4272.1 | 3987 | 10000 | 6013 |
| Stage 2 Disk | 6064T12P03 | 4272.1 | 3987 | 15000 | 11013 |
| Stage 2 Fwd C/P | 4106T80P01 | 4272.1 | 3987 | 13200 | 9213 |
| Stage 1 Aft C/P | 6064T09P01 | 6847.1 | 6431 | 15000 | 8569 |
| Stage 1 Disk | 6064T06P03 | 4272.1 | 3987 | 15000 | 11013 |
| Stage 1 Fwd C/P | 6064T08P04 | 4272.1 | 3987 | 10000 | 6013 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 4272.1 | 3987 | 18600 | 14613 |
| Stage 4 Disk | 6068T32P05 | 4272.1 | 3987 | 18600 | 14613 |
| PT Shaft | 5121T01G02 | 15456.5 | 16587 | 30000 | 13413 |
| Turb. Int. Seal | 5060T86P05 | 4272.1 | 3987 | 16000 | 12013 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 38.4°C |
| MAX CONT | 54°C |
Ohms Resistance = TBD Ω
Performance Summary Results
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CT7-9B GE-E-785752
| Summary | |
|---|---|
| Serial Number: | GE-E-785752 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 33920.7 |
| TSO: | |
| LSV Date: | June 19, 2018 |
Cold Section
| Item | Part Number | TSN | CSN | LIFE LIMIT | LIFE REMAINING |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 10610.5 | 11837 | 26900 | 15063 |
| Stage 2 Blisk | 6055T84P10 | 10610.5 | 11837 | 20800 | 8963 |
| Stage 3/4 Blisk | 6055T15P10 | 10610.5 | 11837 | 18000 | 6163 |
| Stage 5 Blisk | 6044T42P11 | 10610.5 | 11837 | 35100 | 23263 |
| Impeller | 5123T51P02 | 10610.5 | 11837 | 35100 | 23263 |
| Tie Rod | 5043T04P03 | 27411.5 | 33150 | 40000 | 6850 |
| Rear Shaft | 5086T74P03 | 10610.5 | 11837 | 31800 | 19963 |
| GG Shaft | 6068T44P02 | 19104.5 | 21447 | 28200 | 6753 |
| Midframe Case | 6055T47G08 | 1876.8 | 1847 | N/A | N/A |
| Midframe Assy | 5922T43G05 | 1876.8 | 1847 | N/A | N/A |
| Diffuser Case | 5922T38G05 | 1876.8 | 1847 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | LIFE LIMIT | LIFE REMAINING |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 1876.887 | 1847 | 10000 | 8153 |
| Stage 2 Disk | 6064T12P03 | 9799.0 | 10407 | 15000 | 4593 |
| Stage 2 Fwd C/P | 4106T80P01 | 5940.0 | 6464 | 13200 | 6736 |
| Stage 1 Aft C/P | 6064T09P01 | 7497.8 | 7887 | 15000 | 7113 |
| Stage 1 Disk | 6064T06P03 | 1876.8 | 1847 | 15000 | 13153 |
| Stage 1 Fwd C/P | 6064T08P03 | 1876.8 | 1847 | 1000 | 8153 |
Power Turbine Module
| Item | Part Number | TSN | CSN | LIFE LIMIT | LIFE REMAINING |
|---|---|---|---|---|---|
| Stage 3 Blisk | 6068T21P02 | 1876.8 | 1847 | 18600 | 16753 |
| Stage 4 Blisk | 6068T32P05 | 7929.1 | 8849 | 18600 | 9751 |
| PT Shaft | 5121T01G2 | 6724.3 | 7293 | 30000 | 22707 |
| Turb. Int. Seal | 5060T86P05 | 8659.0 | 9601 | 16000 | 6399 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 30.3°C |
| MAX CONT | 45.6°C |
Ohms Resistance = N/K Ω
Sold
CT7-9B S/N GE-E-785382
This engine was recently inducted to H+S Aviation for LLP replacement where major work scopes were carried out to the Cold, Hot, PTM and Accessory Section. The engine was repaired, tested and released by H+S Aviation on April 17th 2018 with no outstanding AD’s. The engine has been long term preserved and will be released with a fresh 8130 dual release.
| Summary | |
|---|---|
| Serial Number: | GE-E-785382 |
| Model: | CT7-9B |
| Aircraft: | Saab 340B |
| TSN: | 35,466.5 |
| TSO: | N/A |
| LSV Date: | April 17, 2018 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 897.2 | 1262 | 26900 | 25638 |
| Stage 2 Blisk | 6055T84P10 | 7377.9 | 8793 | 20800 | 12007 |
| Stage 3/4 Blisk | 6055T15P10 | 897.2 | 1262 | 18000 | 16738 |
| Stage 5 Blisk | 6044T42P11 | 897.2 | 1262 | 35100 | 33838 |
| Impeller | 5123T51P02 | 897.2 | 1262 | 21600 | 20338 |
| Tie Rod | 5043T04P03 | 24972.3 | 17949 | 40000 | 12051 |
| Rear Shaft | 5086T74P03 | 12087.6 | 16717 | 31800 | 15083 |
| GG Shaft | 6068T44P02 | 897.2 | 1262 | 28200 | 26938 |
| Midframe Case | 6055T47G08 | 897.2 | 1262 | N/A | N/A |
| Midframe Assy | 5922T43G05 | 897.2 | 1262 | N/A | N/A |
| Diffuser Case | 5922T38G01 | 897.2 | 1262 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 897.2 | 1262 | 10000 | 8738 |
| Stage 2 Disk | 6064T12P03 | 897.2 | 1262 | 15000 | 13738 |
| Stage 2 Fwd C/P | 4106T80P01 | 897.2 | 1262 | 13200 | 11938 |
| Stage 1 Aft C/P | 6064T09P01 | 897.2 | 1262 | 15000 | 13738 |
| Stage 1 Disk | 6064T06P03 | 897.2 | 1262 | 15000 | 13738 |
| Stage 1 Fwd C/P | 6064T08P03 | 897.2 | 1262 | 10000 | 8738 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 897.2 | 1262 | 18600 | 17338 |
| Stage 4 Disk | 6068T32P05 | 3616.5 | 4588 | 18600 | 14012 |
| PT Shaft | 5121T01G02 | 8799.5 | 9790 | 30000 | 20210 |
| Turb. int. Seal | 5060T86P05 | 897.2 | 1262 | 16000 | 14738 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 57.0°C |
| MAX CONT | 72.5°C |
Ohms Resistance = 2150 Ω
Performance info from April 17, 2018 shop visit
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CT7-9B S/N GE-E-785410
Performance info from March 8, 2021 shop visit
SUMMARY:
This engine was inducted to H+S Aviation for LLP Replacement where major work scopes were carried out to the Hot and Cold Section. The PTM and Accessory Section received minor work scopes. The engine was repaired, tested, and released by H+S Aviation on March 8, 2021 with no outstanding AD’s. The engine has been long-term preserved and will be released with a fresh 8130 dual release.
| Summary | |
|---|---|
| Serial Number: | GE-E-785410 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 33,841.3 |
| TSO: | |
| LSV Date: | March 8, 2021 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 11276.8 | 17814 | 26900 | 9086 |
| Stage 2 Blisk | 6055T84P10 | 7696.2 | 12236 | 20800 | 9086 |
| Stage 3/4 Blisk | 6055T15P10 | 7679.2 | 12236 | 18000 | 5764 |
| Stage 5 Blisk | 6044T42P11 | 9914.1 | 16086 | 35100 | 19014 |
| Impeller | 5123T51P02 | 11872.3 | 12971 | 21600 | 8629 |
| Tie Rod | 5043T04P03 | 10576.6 | 17619 | 40000 | 22381 |
| Rear Shaft | 6068T44P02 | 10576.6 | 17619 | 28200 | 10581 |
| Item | P/N | TSR | CSR | Life Limit |
Life Remaining |
| Midframe Case | 5922T42G04 | 36.0 | 6 | N/A | N/a |
| Midframe Assy | 5922T43G05 | 36.0 | 6 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 36.0 | 6 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 36.0 | 6 | 10000 | 9994 |
| Stage 2 Disk | 6064T12P03 | 4568.2 | 7689 | 15000 | 7311 |
| Stage 2 Fwd C/P | 4106T80P01 | 4568.2 | 7689 | 13200 | 5511 |
| Stage 1 Aft C/P | 6064T09P01 | 4568.2 | 7689 | 15000 | 7311 |
| Stage 1 Disk | 6064T06P03 | 4568.2 | 7689 | 15000 | 7311 |
| Stage 1 Fwd C/P | 6064T08P03 | 36.0 | 6 | 10000 | 9994 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 2265.2 | 3811 | 18600 | 14789 |
| Stage 4 Disk | 6068T32P05 | 2265.2 | 3811 | 18600 | 14789 |
| PT Shaft | 5121T01G02 | 2265.2 | 3811 | 30000 | 26189 |
| Turb. Int. Seal | 5060T86P05 | 2265.2 | 3811 | 16000 | 12189 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 49.2°C |
| MAX CONT | 64.1°C |
Ohms Resistance = 2270 Ω
Performance info from March 8, 2021 shop visit
Sold
CT7-9B S/N GE-E-785489
SUMMARY:
This engine was inducted to GE Strother for LCF Replacement where major work scopes were carried out to the Hot, PTM & Accessory Section, and a Cold Section minor work scope. The engine was repaired, tested, and released by GE Strother on January 8, 2007, with no outstanding ADs. The engine has been long-term preserved and will be released with a fresh 8130 dual release.
| Summary | |
|---|---|
| Serial Number: | GE-E-785489 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 23,613.6 |
| TSO: | |
| LSV Date: | January 8, 2007 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 9252.9 | 12391 | 26900 | 14509 |
| Stage 2 Blisk | 4923T38P08 | 16294.9 | 19095 | 20800 | 1705 |
| Stage 3/4 Blisk | 6055T15P10 | 6179.9 | 9749 | 18000 | 8251 |
| Stage 5 Blisk | 4923T40P09 | 12297.9 | 14742 | 35100 | 20358 |
| Impeller | 5123T51P02 | 6179.9 | 9749 | 21600 | 11851 |
| Tie Rod | 5043T04P03 | 17990.9 | 22902 | 40000 | 17098 |
| Rear Shaft | 5086T74P03 | 6179.9 | 9749 | 31800 | 22051 |
| GG Shaft | 6068T44P02 | 9045.9 | 12225 | 28200 | 15975 |
| Item | P/N | TSR | CSR | Life Limit |
Life Remaining |
| Midframe Case | 5922T38G05 | 6179.9 | 9749 | N/A | N/A |
| Midframe Assy | 5922T43G05 | 6179.9 | 9749 | N/A | N/A |
| Diffuser Case | 5922T38G01 | 6179.9 | 9749 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P01 | 6932.3 | 8741 | 15000 | 6259 |
| Stage 2 Disk | 6064T12P03 | 6932.3 | 8741 | 15000 | 7311 |
| Stage 2 Fwd C/P | 4106T80P01 | 7424.3 | 10037 | 13200 | 3163 |
| Stage 1 Aft C/P | 6064T09P01 | 8869.3 | 9647 | 15000 | 5353 |
| Stage 1 Disk | 6064T06P03 | 6932.3 | 8741 | 15000 | 6259 |
| Stage 1 Fwd C/P | 6064T08P01 | 6932.3 | 8741 | 15000 | 6259 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P01 | 2517.3 | 3767 | 18600 | 14833 |
| Stage 4 Disk | 6068T32P01 | 10854.3 | 12756 | 18600 | 5844 |
| PT Shaft | 5121T01G02 | 9408.3 | 11376 | 30000 | 18624 |
| Turb. Int. Seal | 5060T86P05 | 2517.3 | 3767 | 16000 | 12233 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 39.3°C |
| MAX CONT | N/A |
Ohms Resistance = 1874 Ω
Performance info from July 2021 Capped GPA
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CT7-9B S/N GE-E-785547
SUMMARY:
This engine was input to H+S Aviation and received major work scopes to the Cold Section, Hot Section, and PT Module. The engine was repaired, tested and released with no outstanding AD’s by H+S Aviation on July 31, 2018. The engine operated 1,211.1 hours and 1,031 cycles since the last shop visit, has been long-term preserved and will be released with a fresh 8130 dual release.
| Summary | |
|---|---|
| Serial Number: | GE-E-785547 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 37,366.6 |
| TSO: | |
| LSV Date: | July 31, 2018 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 1211.1 | 1031 | 26900 | 25869 |
| Stage 2 Blisk | 6055T84P10 | 1211.1 | 1031 | 20800 | 19769 |
| Stage 3/4 Blisk | 6055T15P10 | 1211.1 | 1031 | 18000 | 16969 |
| Stage 5 Blisk | 6044T42P11 | 11117.1 | 12096 | 35100 | 23004 |
| Impeller | 5123T51P02 | 1211.1 | 1031 | 21600 | 20569 |
| Tie Rod | 5043T04P03 | 11791.9 | 10879 | 40000 | 29121 |
| Rear Shaft | 5089T74P03 | 1211.1 | 1031 | 31800 | 30769 |
| CG Shaft | 6068T44P02 | 1211.1 | 1031 | 28200 | 27169 |
| Item | P/N | TSR | CSR | Life Limit |
Life Remaining |
| Midframe Case | 6055T47G08 | 1211.1 | 1031 | N/A | N/A |
| Midframe Assy | 6071T77G11 | 1211.1 | 1031 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 1211.1 | 1031 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 1211.1 | 1031 | 10000 | 8969 |
| Stage 2 Disk | 6064T12P03 | 1211.1 | 1031 | 15000 | 13969 |
| Stage 2 Fwd C/P | 4106T80P01 | 6685.4 | 6249 | 13200 | 6951 |
| Stage 1 Aft C/P | 6064T09P01 | 6640.3 | 7498 | 15000 | 7502 |
| Stage 1 Disk | 6064T06P03 | 7484.4 | 8067 | 15000 | 6933 |
| Stage 1 Fwd C/P | 6064T08P03 | 1211.1 | 1031 | 10000 | 8969 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 1211.1 | 1031 | 18600 | 17569 |
| Stage 4 Disk | 6068T32P05 | 1211.1 | 1031 | 18600 | 17569 |
| PT Shaft | 5121T01G01 | 7393.7 | 5199 | 30000 | 24801 |
| Turb. Int. Seal | 5060T86P05 | 1211.1 | 1031 | 16000 | 14969 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | Estimated +45 deg. |
| MAX CONT | – |
Ohms Resistance = TBDΩ
NOte: To be determined upon engine installation
Sold
CT7-9B S/N GE-E-785562
SUMMARY:
This engine was inducted to H+S Aviation for LLP Replacement where major work scopes were carried out to the Hot and Cold Section. The PTM and Accessory Section received minor work scopes. The engine was repaired, tested, and released by H+S Aviation on February 4, 2021 with no outstanding AD’s. The following items were installed with zero time at this shop visit.
• Stage 1 Blisk
• Stage 2 Blisk
• Stage ¾ Blisk
• GG Shaft
• Midframe Case
• Diffuser Case
• Centrifugal Diffuser
• Stage 1 Disk
• Stage 1 FCP
• Stage 2 ACP
• Stage 1 Blades (Qty. 38)
• PT Shaft
The engine was kept in storage since its last repair and will receive a fresh preservation run then released with a CAA & EASA Form One from H+S Aviation in July 2022.
| Summary | |
|---|---|
| Serial Number: | GE-E-785562 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 34,389.4 |
| TSO: | |
| LSV Date: | February 4th, 2021 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 0 | 0 | 26900 | 26900 |
| Stage 2 Blisk | 6055T84P10 | 0 | 0 | 20800 | 20800 |
| Stage 3/4 Blisk | 6055T15P10 | 0 | 0 | 18000 | 18000 |
| Stage 5 Blisk | 4923T40P09 | 13995.1 | 20300 | 35100 | 14800 |
| Impeller | 5123T51P02 | 4619.7 | 4395 | 21600 | 17205 |
| Tie Rod | 5043T04P03 | 10628.2 | 16951 | 40000 | 23049 |
| Rear Shaft | 5086T74P03 | 10628.2 | 16951 | 31800 | 14849 |
| GG Shaft | 6068T44P02 | 0 | 0 | 28200 | 28200 |
| Item | P/N | TSR | CSR | Life Limit |
Life Remaining |
| Midframe Case | 6055T47G08 | 0 | 0 | N/A | N/A |
| Midframe Assy | 6071T77G11 | 0 | 0 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 0 | 0 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 0 | 0 | 10000 | 10000 |
| Stage 2 Disk | 6064T12P03 | 4103.9 | 7059 | 15000 | 7941 |
| Stage 2 Fwd C/P | 4106T80P01 | 5869.0 | 3892 | 13200 | 9308 |
| Stage 1 Aft C/P | 6064T09P01 | 4103.9 | 7059 | 15000 | 7941 |
| Stage 1 Disk | 6064T06P03 | 0 | 0 | 15000 | 15000 |
| Stage 1 Fwd C/P | 6064T08P03 | 0 | 0 | 10000 | 10000 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 4103.9 | 7059 | 18600 | 11541 |
| Stage 4 Disk | 6068T32P01 | 4103.9 | 7059 | 18600 | 11541 |
| PT Shaft | 5121T01G02 | 0 | 0 | 30000 | 30000 |
| Turb. Int. Seal | 5060T86P05 | 4103.9 | 7059 | 16000 | 8941 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 53.3°C |
| MAX CONT | TBD |
Ohms Resistance = 3200 Ω
Performance info from Feb 4, 2021 shop visit
Sold
CT7-9B S/N GE-E-785794
This engine was recently inducted to H+S Aviation for LLP replacement where major work scopes were carried out to the Cold and Hot Section as well as a minor work scope on the Accessory Section and PTM replacement. The engine was repaired, tested and released on January 29th 2020 with no outstanding AD’s. The engine has been long term preserved and will be released with a fresh 8130 dual release.
| Summary | |
|---|---|
| Serial Number: | GE-E-785794 |
| Model: | CT7-9B |
| Aircraft: | Saab 340 |
| TSN: | 29,689.4 |
| TSO: | N/A |
| LSV Date: | January 29, 2020 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 9593.3 | 12061 | 26900 | 14839 |
| Stage 2 Blisk | 6055T84P10 | 35.2 | 7 | 20800 | 20793 |
| Stage 3/4 Blisk | 6044T42P11 | 35.2 | 7 | 18000 | 17993 |
| Stage 5 Blisk | 6044T42P11 | 4654.9 | 4402 | 35100 | 30698 |
| Impeller | 5123T51P02 | 8265.2 | 8930 | 21600 | 12670 |
| Tie Rod | 5043T04P03 | 14162.8 | 21604 | 40000 | 18396 |
| Rear Shaft | 5086T74P03 | 13234.4 | 17144 | 31800 | 14656 |
| GG Shaft | 6068T44P02 | 35.2 | 7 | 28200 | 28193 |
| Midframe Case | 6055T47G08 | 35.2 | 7 | N/A | N/A |
| Midframe Assy | 6071T77G11 | 35.2 | 7 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 35.2 | 7 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 35.2 | 7 | 10000 | 9993 |
| Stage 2 Disk | 6064T12P03 | 35.2 | 7 | 15000 | 14993 |
| Stage 2 Fwd C/P | 4106T80P01 | 35.2 | 7 | 13200 | 13193 |
| Stage 1 Aft C/P | 6064T09P01 | 35.2 | 7 | 15000 | 14993 |
| Stage 1 Disk | 6064T06P03 | 3644.4 | 6090 | 15000 | 8910 |
| Stage I Fwd C/P | 6064T08P03 | 35.2 | 7 | 10000 | 9993 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 35.2 | 7 | 18600 | 18593 |
| Stage 4 Disk | 6068T32P05 | 9845.7 | 13772 | 18600 | 4828 |
| PT Shaft | 5121T01G02 | 35.2 | 7 | 30000 | 29993 |
| Turb. Int. Seal | 5060T86P05 | 35.2 | 7 | 16000 | 15993 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 48.0°C |
| MAX CONT | 63.6°C |
Ohms Resistance = 1630 Ω
Performance info from January 29, 2020 shop visit
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CT7-9C3 S/N GE-E-785254A
SUMMARY:
This engine was inducted to H+S Aviation where it was repaired and released on October 14, 2011. The engine received major work scopes to the Cold Section, Hot Section and PTM and has operated 4,272.1 hours and 3,987 cycles since the last major repair. The engine is being offered in CT7-9C3 configuration without HMU and will be released with a fresh CAA and EASA Form One after SB 72-0255 R02 and 72-0412 R01 are carried out. The engine will be long term preserved and released with no outstanding AD’s. Please contact C&L Aerospace for additional information.
| Summary | |
|---|---|
| Serial Number: | GE-E-785254A |
| Model: | CT7-9C3 |
| Aircraft: | CN 235 |
| TSN: | 30,907.5 |
| TSO: | |
| LSV Date: | October 14, 2011 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G16 | 4272.1 | 3987 | 26900 | 22913 |
| Stage 1 Blisk | 6055T84P10 | 4272.1 | 3987 | 20800 | 16813 |
| Stage 3/4 Blisk | 6055T15P10 | 4272.1 | 3987 | 18000 | 14013 |
| Stage 5 Blisk | 6044T42P11 | 9372.9 | 8662 | 35100 | 26438 |
| Impeller | 5123T51P02 | 4272.1 | 3987 | 18600 | 17613 |
| Tie Rod | 5043T04P03 | 4272.1 | 3987 | 40000 | 36013 |
| Rear Shaft | 5086T74P03 | 4272.1 | 3987 | 31800 | 27813 |
| GG Shaft | 6068T44P02 | 12483.9 | 15670 | 28200 | 12530 |
| Midframe Case | 6055T47G08 | 4272.1 | 3987 | N/A | N/A |
| Midframe Assy | 6071T77G13 | 4272.1 | 3987 | N/A | N/A |
| Diffuser Case | 6071T54G05 | 4272.1 | 3987 | N/A | N/A |
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P04 | 4272.1 | 3987 | 9800 | 5813 |
| Stage 2 Disk | 6064T12P03 | 4272.1 | 3987 | 15000 | 11013 |
| Stage 2 Fwd C/P | 4106T80P01 | 4272.1 | 3987 | 13200 | 9213 |
| Stage 1 Aft C/P | 6064T09P01 | 6847.1 | 6431 | 15000 | 8569 |
| Stage 1 Disk | 6064T06P03 | 4272.1 | 3987 | 15000 | 11013 |
| Stage 1 Fwd C/P | 6064T08P04 | 4272.1 | 3987 | 10000 | 6013 |
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P02 | 4272.1 | 3987 | 18600 | 14613 |
| Stage 4 Disk | 6068T32P05 | 4272.1 | 3987 | 18600 | 14613 |
| PT Shaft | 5121T01G02 | 15456.5 | 16587 | 30000 | 13413 |
| Turb. Int. Seal | 5060T86P05 | 4272.1 | 3987 | 16000 | 12013 |
Test Performance Summary
| Rating Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | 18.8°C |
| MAX CONT | 28.1°C |
Ohms Resistance = TBD Ω
Estimated Performance
Sold
Engine Model: CT7-9B (P/N 6058T83G01)
This engine was inducted into Standard Aero for a return to service workscope. The engine will be borescoped, the lower nine fuel injectors replaced, tested, long-term preserved, and issued a fresh dual release by Standard Aero. The engine is expected to be available late May 2025 and has operated 1,797.3 hours and 1,496 cycles since its 2016 shop visit at H+S Aviation. Contact your Regional Sales Manager at C&L Aerospace for more information.
| Summary | |
|---|---|
| Serial Number: | |
| Model: | CT7-9B |
| Aircraft: | Saab 340B |
| TSN: | 10,554 |
| TSO: | |
| LSV Date: | August 4, 2016 |
Cold Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 1 Blisk | 6055T83G15 | 10,554 | 9,899 | 26,900 | 17,001 |
| Stage 2 Blisk | 6055T84P09 | 10,554 | 9,899 | 20,800 | 10,901 |
| Stage 3/4 Blisk | 6055T84P09 | 10,554 | 9,899 | 18,000 | 8,101 |
| Stage 5 Blisk | 6044T42P09 | 10,554 | 9,899 | 35,100 | 25,201 |
| Impeller | 6071T86P03 | 10,554 | 9,899 | 18,600 | 8,701 |
| Tie Rod | 5043T04P03 | 10,554 | 9,899 | 40,000 | 30,101 |
| Rear Shaft | 5086T74P01 | 10,554 | 9,899 | 31,800 | 21,901 |
| GG Shaft | 6068T44P01 | 10,554 | 9,899 | 28,200 | *8,401 |
*Denotes SB 72-A0550 Limits
Hot Section
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 2 Aft C/P | 6068T36P01 | 10,554 | 9,899 | 15000 | 5,101 |
| Stage 2 Disk | 6064T12P01 | 10,554 | 9,899 | 15000 | *3,600 |
| Stage 2 Fwd C/P | 4106T80P01 | 11,848.9 | 11,100 | 13200 | 2,100 |
| Stage 1 Aft C/P | 6064T09P01 | 10,521.2 | 11,260 | 15000 | *3,600 |
| Stage 1 Disk | 6064T06P01 | 8,190.9 | 7,701 | 15000 | *4,800 |
| Stage 1 Fwd C/P | 6064T08P01 | 10,554 | 9,899 | 15000 | 5,101 |
*Denotes SB 72-A0550 Limits
Power Turbine Module
| Item | Part Number | TSN | CSN | Life Limit | Life Remaining |
|---|---|---|---|---|---|
| Stage 3 Disk | 6068T21P010 | 10,554 | 9,899 | 18600 | 8,701 |
| Stage 4 Disk | 6068T32P01 | 10,554 | 9,899 | 18600 | 8,701 |
| PT Shaft | 5121T01G02 | 12,525.9 | 12,806 | 30000 | 17,194 |
| Turb. Int. Seal | 5060T86P05 | 5,223.9 | 4,458 | 16000 | 11,542 |
Test Performance Summary
| Rate Point | T4.5 Margin Deg.C |
|---|---|
| TAKEOFF | +/- 25 |
| MAX CONT | TBD |
