N451M is a 2005 Lancair Intl LANCAIR IV P. It is a fixed-wing single-engine aircraft with 4 seats, powered by a Cont Motor TSIO-550 SER rated at 280 horsepower. The registration is active, with the registrant based in Glenwood, MO. Its experimental airworthiness certificate was issued in Mar 2005. It has been registered to its current owner since Sep 2025. This page also carries 1 NTSB event.
- 21 years old
- 1 of 133 Lancair Intl LANCAIR IV P
2025
2005
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N451M's record changes.
The pilot reported that he was hired to fly the airplane to another airport following a pre-purchase inspection. The preceding pilot informed the pilot of several issues with the airplane including the propeller control and the cabin door. The pilot said he familiarized himself with the airplane and after about three hours of inspections and ground tests determined the airplane was in a safe condition and proceeded with the flight. He reported that during the descent to the destination airport, the turbulence became severe, noting that his head hit the cabin roof twice even though the lap seat belt was secured. The cockpit was loud and as he advanced the throttle after lowering the flaps 10 degrees, the cabin noise increased, and the propeller indications became erratic. Several engine instruments were giving erratic readings as well and the pilot was additionally concerned about the cabin door latches becoming loose in the turbulence. The airplane was operating properly and after a minute the propeller indications stabilized. All these events added to his workload.
The pilot said that while approaching to land and after lowering the flaps, he reached for the landing gear handle, noting that these checks were performed in severe turbulence. He visually confirmed that the flaps were fully extended by looking out the side window and believed that he looked at the gear indicator lights but didn’t clearly remember this. He also did not remember shading the landing gear position indicator with his hand as he had done previously.
During the landing, the airplane settled onto its belly and the airplane slid to a stop. He noted that after the accident, the landing gear handle and flap handle were both in the mid-position.
The airplane sustained substantial damage to the fuselage.
When the airplane was being recovered from the runway, aircraft power was turned on and the landing gear selector placed in the fully down position. The landing gear extended and locked into the fully extended position with no anomalies noted.
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