100 Gallons Fuel Capacity
Speed Brakes
Wheel Pants
Factory Oxygen (Recertified)
Static Wicks
Dual Alternators
Wingtip Strobes
Polished Spinner
Turbo System Overhauled in 2022
Useful Load: 1050 Lbs
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2005 Lancair Columbia 400
Single-engine Piston-Used
$349,000
$300,000
(-14%)
10/31/2023
Registration no. N25281Serial no. 41089
1,709 VIEWS
563 DAYS ON FLYING
13 SAVES
Aircraft Listing Type
For Sale
Seller location
Placerville, California, United States
Aircraft location
Placerville, California, United States
Airframe & Propulsion
Airframe Total time
1,435 hours
ESTIMATED TIME BEFORE OVERHAUL (TBO)
Remaining engine hours before the factory recommended Time Before Overhaul (TBO).
Airframe Description
Propulsion
TSIO-550
Since Major IRAN: 750
Since Prop OH: 200
Avionics
Flight rules
Instrument Flight Rules
Navigation equipment
Dual Avidyne Flightmax Integra PFD's
Garmin 340 Audio Panel with 3LMB
Garmin GNS 430 WAAS Color IFR Moving Map GPS
Garmin GNS 430 Color IFR Moving Map GPS
S-Tec 55X Fully Coupled Autopilot
Garmin 345 Transponder with ADS-B in and out
Airspeed Back-up Gyro
Altimeter Back-up Gyro
Artificial horizon Back-up Gyro
Induction Air
Interior & Exterior
Number of seats
4
Interior Condition
Tan leather seats with matching carpet. Generally very good condition. Overall rated 8 out of 10.
Interior Year
2005
Interior Score
8
Exterior Condition
Overall white with black major accent and silver gray minor accents in excellent original condition. Overall rated 8 out of 10.
Paint Year
2005
Paint Score
8
Maintenance
Inspection Expiry
Sat, Jun 1, 2024
Damage history
One owner since new. Excellent maintenance since new. California based. Famous owner. Trading to a different plane. Complete logs, no damage. Turbo IO-550 engine, 185 kt cruise. The engine was torn down and overhauled 750 hours ago. The owner opted to "continue the time" rather than zero it. All he had to do to make it a complete overhaul was the fuel servo. This was not done, but it did get a new crankshaft and cylinder, turbo's and everything else that an overhaul requires. Call Nevada Aircraft Engines in Henderson Nevada and they will verify this.
Price Change history
Date
Event
Price
06/28/2024
Sold
N/A
12/27/2023
Listed for Sale
$300,000
12/21/2023
Closed
N/A
10/31/2023
Price Change
$349,000$300,000
(-14%)
08/18/2023
Listed for Sale
$349,000
Learn More about the Lancair Columbia 400
August 27, Bend, Ore. / Lancair 400
At approximately 1045 Pacific time, a Lancair LC41, prototype for the Lancair 400, crashed about 15 miles east of Bend during spin testing. The pilot bailed out and was not injured. The pilot had been conducting a series of spin entry and recovery tests, and had intentionally entered a fully developed spin. During the final spin, the flight controls were insufficient to recover, so he deployed the spin recovery/stabilization drogue parachute. After he recovered from the spin, he was unable to jettison the drogue chute with either the manual or backup system. He attempted to establish controlled flight with the chute attached, but was unable. He then bailed out. Initial examination of the wre...
As seen on: 
Squawk Box: 06/04
The following information is derived from the FAAs Service Difficulty Reports and Aviation Maintenance Alerts.<P>----------<P><B>Lycoming IO-540 Engines<BR>Crankshaft Gear Bolts</B><BR>A new AD supercedes AD 2002-23-06 regarding certain zinc plated crankshaft gear retaining bolts installe d in Lycoming AEIO-540, IO-540, LTIO-540, and TIO-540 series engines. The AD retains the original requirement but expands the population of affected engines by 161. In addition, it AD adds five additional kits (alternative method of complia nce) for replacing the crankshaft gear retaining bolts.<P><B>Lancair 400<BR>Fuel Pressure Transducer</B><BR>AD 2004-06-09, Fuel Pressure Transducer Inspection,...
As seen on:
August 27, Bend, Ore. / Lancair 400
At approximately 1045 Pacific time, a Lancair LC41, prototype for the Lancair 400, crashed about 15 miles east of Bend during spin testing. The pilot bailed out and was not injured. The pilot had been conducting a series of spin entry and recovery tests, and had intentionally entered a fully developed spin. During the final spin, the flight controls were insufficient to recover, so he deployed the spin recovery/stabilization drogue parachute. After he recovered from the spin, he was unable to jettison the drogue chute with either the manual or backup system. He attempted to establish controlled flight with the chute attached, but was unable. He then bailed out. Initial examination of the wre...
As seen on:
