Lycoming TIO-540-C1A Aircraft Engine | 250 HP | 1,077.7 SMOH




Lycoming TIO-540-C1A Aircraft Engine | 250 HP | 1,077.7 SMOH
Lycoming TIO-540-C1A, 250 HP aircraft piston engine removed from the right-hand engine position of a 1977 Piper PA-23-250 Aztec.
Detailed Description
Condition Disclosure: The engine has experienced a propeller strike. The seller reports crankshaft flange runout of 0.000 inches. The turbo system is not included.
Engine Highlights
- Lycoming TIO-540-C1A, 250 HP
- Serial Number: L-4542-61A
- Removed from 1977 Piper PA-23-250 Aztec
- Right-Hand Engine Position
- 13,118.9 Hours Total Engine Time
- 1,077.7 Hours Since Major Overhaul
- Overhauled July 12, 2018, by Aero Recip Canada
- Complete Engine Logbooks
- Last Annual Inspection: May 16, 2022
- Fuel Injected, Bottom Draft
- Dynafocal Engine Mount
- Prop Strike History
- Crankshaft Flange Runout: 0.000"
- Sky-Tec Starter, Alternator and Bendix Magnetos Included
- Turbo System Not Included
Engine Specifications
| SpecificationDetails | |
| Manufacturer | Lycoming |
| Model | TIO-540-C1A |
| Alternate P/N | TIO540 / 0540 |
| Serial Number | L-4542-61A |
| Horsepower | 250 HP |
| Fuel System | Fuel Injection, Bottom Draft |
| Engine Mount | Dynafocal |
| Aircraft Removed From | 1977 Piper PA-23-250 Aztec |
| Engine Position | Right-Hand |
| Aircraft Hobbs Reading | 72.5 Hours |
| Total Engine Time (TTE) | 13,118.9 Hours |
| Time Since Major Overhaul (TSMO) | 1,077.7 Hours |
| Last Major Overhaul | July 12, 2018 |
| Overhaul Facility | Aero Recip Canada |
| Last Annual Inspection | May 16, 2022 |
| Logbooks | Complete |
| Prop Strike | Yes |
| Crankshaft Flange Runout | 0.000" |
| Turbo System | Not Included |
Compression Readings
Last reported cylinder compression readings:
| CylinderCompression | |
| #1 | 70/80 |
| #2 | 75/80 |
| #3 | 73/80 |
| #4 | 74/80 |
| #5 | 69/80 |
| #6 | 68/80 |
These are historical, seller-reported readings and should be verified against the maintenance records.
Prop Strike Disclosure
This engine has a documented propeller strike.
The seller reports that the crankshaft flange measures 0.000 inches runout.
This measurement does not establish airworthiness or eliminate applicable prop strike inspection requirements. Buyers should independently determine the required inspections, repairs, and return-to-service procedures.
Included Accessories
- Engine Baffling, As Photographed
- Flywheel and Ring Gear
- Sky-Tec Starter
- Alternator
- Engine-Mounted Fuel System
- Bendix Magnetos
- Air Pump
Not Included
- Propeller
- Air Box
- Engine Mount
- Exhaust System
- Turbo System
Accessories not specifically listed as included are excluded from the sale.
Engine Documentation
Complete engine logbooks are reported to be available.
Engine Logbook:
http://www.texasairsalvage.com/Log_books/N22387RHEngine.pdf
Buyers should review the overhaul documentation, maintenance history, engine times, and prop strike records before purchase.
Condition and Sale Terms
This Lycoming TIO-540-C1A was removed from a salvaged aircraft and is offered in as-removed, as-is condition.
- Condition: As Removed, Prop Strike History
- Warranty: No warranty expressed or implied
- Returns: Aircraft engines are not returnable
- Deposit: No deposit required or accepted
- Payment: Cash or bank wire transfer
- Inspection: Independent pre-purchase inspection strongly recommended
Cashier's checks, credit cards, and PayPal are not accepted.
The seller can provide contact information for a local A&P mechanic to assist with a pre-purchase inspection.
Shipping Information
- Commercial delivery within the lower 48 states: $1,000
- Residential delivery surcharge: $250
- Liftgate service surcharge: $250
- Buyer-arranged shipping permitted
- Shipping Origin ZIP Code: 75556
Buyer Applications
This Lycoming TIO-540-C1A may interest Piper Aztec owners, aircraft maintenance facilities, engine overhaul shops, and aviation restoration projects seeking a 250 HP Lycoming engine with complete logbooks and included accessories.
Buyers should independently verify engine configuration, aircraft compatibility, turbo system requirements, prop strike inspection requirements, and eligibility for return to service.
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