N3020M

Substantial
None

PIPER PA 44-180S/N: 44-7995220

Accident Details

Date
Friday, June 9, 2017
NTSB Number
ERA17LA204
Location
Gaithersburg, MD
Event ID
20170609X91950
Coordinates
39.168334, -77.166114
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The failure of the right main landing gear trunnion bracket due to an undetermined overstress event.

Aircraft Information

Registration
Make
PIPER
Serial Number
44-7995220
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
PA 44-180M600
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
4
FAA Model
PA-44-180

Registered Owner (Current)

Name
WIFA (WASHINGTON INTERNATIONAL FLIGHT ACADEMY) LLC
Address
7940 AIRPARK RD
City
GAITHERSBURG
State / Zip Code
MD 20879-4176
Country
United States

Analysis

On June 8, 2017, about 2110 eastern daylight time, a Piper PA-44-180 airplane, N3020M, was substantially damaged during landing rollout at Montgomery County Airpark (GAI), Gaithersburg, Maryland. The flight instructor and two student pilots were not injured. The instructional flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the local flight.According to the flight instructor, he was returning to home base after a training flight that consisted of basic maneuvers, as well as two takeoffs and landings to a full stop. During the final approach the flight instructor configured the airplane for landing and briefed the student pilot. The touchdown was uneventful and during the landing roll the airplane began veering to the right of centerline. The airplane came to a full stop and the instructor performed an engine shutdown before exiting the airplane. On inspection of the airplane the flight instructor noted that the right main landing gear was collapsed and bent backwards towards the aft of the airplane.

Examination of the airplane by a Federal Aviation Administration inspector revealed that the aft right wing spar web was damaged during the landing sequence. Further examination of the landing gear revealed that the right aft main landing gear trunnion bracket failed. A visual examination of the fracture surfaces by the NTSB Materials laboratory revealed that there were no signs of fatigued failure within the trunnion, and the bracket failed during an overstress event. A review of the logbooks did not reveal any recent maintenance to the landing gear assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA17LA204