N722CF

Substantial
None

PIPER PA 31-310S/N: 31-7300968

Accident Details

Date
Monday, December 4, 2017
NTSB Number
CEN18LA048
Location
Jeffersonville, IN
Event ID
20171206X43704
Coordinates
38.365554, -85.738052
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The right main landing gear’s failure to fully extend for reasons that could not be determined because postaccident testing revealed no mechanical anomalies that would have precluded normal operation.

Aircraft Information

Registration
N722CF
Make
PIPER
Serial Number
31-7300968
Engine Type
Turbo-shaft
Year Built
1973
Model / ICAO
PA 31-310M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LUFTLADDER INC
Address
2265 OLD GARLAND RD
Status
Deregistered
City
PITTSFIELD
State / Zip Code
PA 16340-4431
Country
United States

Analysis

On December 3, 2017, about 1910 eastern standard time, a Piper PA-31-310, N722CF, was damaged during a wheels-up landing on runway 18 at the Clark Regional Airport (JVY), Jeffersonville, Indiana. The pilot and two passengers were not injured. The airplane received substantial damage to fuselage longerons and the aft flange of the main wing spar carry through. The aircraft was registered to Luftladder Inc. and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions existed at the time of the accident. A visual flight rules flight plan had been filed. The flight originated from the Wellsville Municipal Airport (ELZ), near Wellsville, New York, about 1630, with JVY as the intended destination.

The pilot reported that when the airplane was about 5 miles from JVY, he lowered the landing gear and the right main landing gear was slow to extend, but within a few seconds all three gear down indicator lights illuminated. A normal descent was made and when the airplane was over the runway about to flare, the right main landing gear light went out. The pilot initiated a go-around, increasing engine power, pitching for climb, and retracting the landing gear and flaps. He stated that the airplane may have settled after the flaps were retracted and he heard a noise as if a propeller blade had contacted something. He decided to discontinue the go-around and landed the airplane straight ahead, coming to a stop on the runway with the landing gear retracted.

After the accident the airplane landing gear was tested under the supervision of Federal Aviation Administration inspectors. Before the test, an o-ring was replaced on the hydraulic reservoir, but this would not have prevented the right main landing gear from extending. The gear retraction tests were performed satisfactorily, with no defects in the landing gear operation noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN18LA048