20070701825989I

Incident · Minor damage

FAA incident report · Mooney M20E · Wadsworth, OH · July 1, 2007

Date
July 1, 2007 · 14:30 local
Place
Wadsworth, OH
Airport
Wadsworth Municipal
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6804V
Reported as
Mooney M20E
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,760 total1,680 in this make and model8 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Witness statements support pilot's claim that the landing gear was fully extended upon touch down. Toward the end of landing roll-out all three landing gear retracted with selector in down position. During retrieval the landing gear freely extended and locked in down position, with electrical power on the landing gear actuator could be heard running. Considering the number of airworthiness directives and manufacturer's service bulletins involving the landing gear actuator, there is a distinct possibility an internal failure caused the landing gear collapse. When owner makes future arrangements for repairs, actuator identity, time in service, AD compliance status, and area of failure will be determined. A malfunction or defect report will be submitted and this 8020-23 updated.

As the FAA filed it

(-23) WITNESS STATEMENTS SUPPORT PILOT'S CLAIM THAT THE LANDING GEAR WAS FULLY EXTENDED UPON TOUCH DOWN. TOWARD THE END OF LANDING ROLL-OUT ALL THREE LANDING GEAR RETRACTED WITH SELECTOR IN DOWN POSITION. DURING RETRIEVAL THE LANDING GEAR FREELY EXTENDED AND LOCKED IN DOWN POSITION, WITH ELECTRICAL POWER ON THE LANDING GEAR ACTUATOR COULD BE HEARD RUNNING. CONSIDERING THE NUMBER OF AIRWORTHINESS DIRECTIVES AND MANUFACTURER'S SERVICE BULLETINS INVOLVING THE LANDING GEAR ACTUATOR, THERE IS A DISTINCT POSSIBILITY AN INTERNAL FAILURE CAUSED THE LANDING GEAR COLLAPSE. WHEN OWNER MAKES FUTURE ARRANGEMENTS FOR REPAIRS, ACTUATOR IDENTITY, TIME IN SERVICE, AD COMPLIANCE STATUS, AND AREA OF FAILURE WILL BE DETERMINED. A MALFUNCTION OR DEFECT REPORT WILL BE SUBMITTED AND THIS 8020-23 UPDATED.