19961023036459I

Incident · Minor damage

FAA incident report · Mooney M20E · Kansas City, MO · October 23, 1996

Date
October 23, 1996 · 09:53 local
Place
Kansas City, MO
Airport
Richards-Gebaur Airport
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N5578Q
Reported as
Mooney M20E
Reported engine
Continental IO360A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
940 total5 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.

Narrative: on the day of this incident, 10/23/96, the FBO towed the airplane from the hangar. The pilot conducted a preflight inspection and everything appeared normal. The airplane was taxied to the runup area. After completing the engine runup, an ATC clearance was received for take off. As the airplane taxied toward the runway the mechanical gear lever "popped out" of the down and locked position and the airplane settled to the ground as all three wheels retracted. The pilot/owner said there had never been any problem with the landing gear and he has owned this airplane since 1983. The previous flight was completed on 10/06/96 without incident. The last annual inspection was completed in October 1995 by spencer aircraft, butler, Missouri. The airplane received minor damage. Both of the propeller blade tips struck the taxiway and the engine sustained sudden stoppage damage. There was minor damage to the nose wheel doors. Pitot tube and one antenna was broken off. A landing gear retraction test was conducted. Right main gear sustained bell crank damage when the gear folded and was locked in the down position during the inspection. The left gear and nose gear functioned properly. The landing gear handle was checked for proper operation and no malfunction was noted; however, it did take about 5 lbs. Of up pressure to get the handle into the up and locked position. This incident (CE97IGA0007) is closed.

As the FAA filed it

NARRATIVE: ON THE DAY OF THIS INCIDENT, 10/23/96, THE FBO TOWED THE AIRPLANE FROM THE HANGAR. THE PILOT CONDUCTED A PREFLIGHT INSPECTION AND EVERYTHING APPEARED NORMAL. THE AIRPLANE WAS TAXIED TO THE RUNUP AREA. AFTER COMPLETING THE ENGINE RUNUP, AN ATC CLEARANCE WAS RECEIVED FOR TAKE OFF. AS THE AIRPLANE TAXIED TOWARD THE RUNWAY THE MECHANICAL GEAR LEVER "POPPED OUT" OF THE DOWN AND LOCKED POSITION AND THE AIRPLANE SETTLED TO THE GROUND AS ALL THREE WHEELS RETRACTED. THE PILOT/OWNER SAID THERE HAD NEVER BEEN ANY PROBLEM WITH THE LANDING GEAR AND HE HAS OWNED THIS AIRPLANE SINCE 1983. THE PREVIOUS FLIGHT WAS COMPLETED ON 10/06/96 WITHOUT INCIDENT. THE LAST ANNUAL INSPECTION WAS COMPLETED IN OCTOBER 1995 BY SPENCER AIRCRAFT, BUTLER, MISSOURI. THE AIRPLANE RECEIVED MINOR DAMAGE. BOTH OF THE PROPELLER BLADE TIPS STRUCK THE TAXIWAY AND THE ENGINE SUSTAINED SUDDEN STOPPAGE DAMAGE. THERE WAS MINOR DAMAGE TO THE NOSE WHEEL DOORS. PITOT TUBE AND ONE ANTENNA WAS BROKEN OFF. A LANDING GEAR RETRACTION TEST WAS CONDUCTED. RIGHT MAIN GEAR SUSTAINED BELL CRANK DAMAGE WHEN THE GEAR FOLDED AND WAS LOCKED IN THE DOWN POSITION DURING THE INSPECTION. THE LEFT GEAR AND NOSE GEAR FUNCTIONED PROPERLY. THE LANDING GEAR HANDLE WAS CHECKED FOR PROPER OPERATION AND NO MALFUNCTION WAS NOTED; HOWEVER, IT DID TAKE ABOUT 5 LBS. OF UP PRESSURE TO GET THE HANDLE INTO THE UP AND LOCKED POSITION. THIS INCIDENT (CE97IGA0007) IS CLOSED.

Other reports on N5578Q · 1

Matched to the same aircraft by N-number and date.