N711HE

Substantial
None

CESSNA P210NS/N: P21000242

Accident Details

Date
Tuesday, March 11, 2025
NTSB Number
WPR25LA111
Location
Roswell, NM
Event ID
20250312199839
Coordinates
33.299878, -104.529400
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Aircraft Information

Registration
Make
CESSNA
Serial Number
P21000242
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
P210NC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
P210N

Registered Owner (Current)

Name
DESERT WEST ENTERPISES LLC
Address
PO BOX 3000
City
ROSWELL
State / Zip Code
NM 88202-3000
Country
United States

Analysis

On March 11, 2025, at 1340 mountain daylight time, a Cessna P210N, N711HE, was substantially damaged when it was involved in an accident near Roswell, New Mexico. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, he departed Roswell Air Center Airport (ROW), Roswell, New Mexico, for a cross-country flight. While climbing through about 11,000 ft mean sea level, a warning for cylinder head temperature appeared on the primary flight display (PFD) and the pilot recognized that the fuel flow was lower that expected. A short time later a “low bus voltage” message appeared on the multifunction flight display (MFD). The pilot notified the Air Traffic Control Tower at ROW that he would be returning to the airport and started descent towards the airport.

The pilot disconnected the autopilot and noted the electric trim did not appear to be working. He tried turning the trim wheel and felt resistance. The PFDs and MFD lost power during the descent and the pilot said he was “fighting the elevator control” and the airplane was descending about 2,000 ft per minute. He also stated he activated the landing gear selector, but the warning horn and gear position indicator lights were not operating. He did not visually confirm the position of the landing gear prior to landing and stated he thought the gear may have been “hanging” when he landed on runway 17. The landing gear subsequently collapsed, and the airplane slid off the right side of the runway which resulted in substantial damage to the empennage.

The airplane had a new alternator installed about 10 hours of flight time prior to the accident. The airplane was retained for examination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR25LA111