N5844P

Substantial
None

PIPER PA-24-250S/N: 24-925

Accident Details

Date
Sunday, January 2, 2022
NTSB Number
CEN22LA102
Location
Grand Forks, ND
Event ID
20220118104535
Coordinates
47.947278, -97.173778
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Failure of the landing gear to properly extend before landing for reasons that could not be determined.

Aircraft Information

Registration
Make
PIPER
Serial Number
24-925
Engine Type
Reciprocating
Model / ICAO
PA-24-250PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-24-250

Registered Owner (Current)

Name
KONIAR STEVEN L
Address
1305 REDBUD LN
City
NEWCASTLE
State / Zip Code
OK 73065-6065
Country
United States

Analysis

On January 2, 2022, about 1530 central standard time, a Piper PA-24-250 airplane, N5844P, was substantially damaged when it was involved in an accident at the Grand Forks International Airport (GFK), Grand Forks, North Dakota. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the landing gear did not extend properly as he approached the intended destination airport. His attempts to extend the landing manually were not successful and he decided to divert to a tower-controlled airport. The tower controller subsequently confirmed that the landing gear appeared to be “a few inches down from the retracted position” but was not fully extended.

The pilot noted that the airplane was equipped with an aftermarket engine cowling installation with an electrically actuated nose landing gear door system. Before using the emergency gear extension system, the door must be released. The door release lever installed in the cockpit extended about one-half inch before “heavy resistance” was felt. Consultation with a mechanic via the radio and further efforts to fully extend the landing gear were not successful. He executed an emergency gear-up landing. The airframe sustained damage to the lower fuselage during the landing.

A postaccident examination of the landing gear system was performed by Federal Aviation Administration inspectors after the airplane was repositioned to a hangar at the airport. The landing motor jack screw corresponded to the retracted position at the time of the exam. Electrical power did not appear to be reaching the gear extension motor. When the nose landing gear doors were released (opened), the landing gear was able to be extended manually. Although the inspectors confirmed an anomaly with both the primary and secondary extension/retraction systems, they were not able to determine the exact source of the problem.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA102