20051130030549I

Incident · Minor damage

FAA incident report · Mooney M20C · Goodyear, AZ · November 30, 2005

Date
November 30, 2005 · 16:15 local
Place
Goodyear, AZ
Airport
Phoenix-Goodyear Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6524U
Reported as
Mooney M20C
Reported engine
Lycoming O360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,000 total10 in this make and model12 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) A follow-up investigation was performed to evaluate the physical facts relative to the pilot operator statement. The pilot stated that after his landing and roll out the landing gear suddenly collapsed, causing a prop strike and the aircraft slide. The pilot was interviewed and provided a signed statement. Inspection of the aircraft indicated propeller damage, belly scraping, and scraping on the nose gear door. No transitional (landing gear) damage was detected and all damage gave an indication that the landing gear was retracted at the time of contact. Examination of the runway (21) surface, indicated a total of 13 prop blade strikes and then metal to cement slide marks over a 700' space. No evidence of rubber marks from any of the three tires was found. Tower personnel stated that another aircraft was delayed exiting the runway in front of the landing incident aircraft. The runway signatures, aircraft slide distance and aircraft damage demonstrate what appears to be a gear up landing, not a collapsed landing gear during roll out. This physical evidence contradicts the statement provided by the pilot. Possible distraction of the pilot by the landing aircraft in front of him may have been a contributing factor.

As the FAA filed it

(-23) A FOLLOW-UP INVESTIGATION WAS PERFORMED TO EVALUATE THE PHYSICAL FACTS RELATIVE TO THE PILOT OPERATOR STATEMENT. THE PILOT STATED THAT AFTER HIS LANDING AND ROLL OUT THE LANDING GEAR SUDDENLY COLLAPSED, CAUSING A PROP STRIKE AND THE AIRCRAFT SLIDE. THE PILOT WAS INTERVIEWED AND PROVIDED A SIGNED STATEMENT. INSPECTION OF THE AIRCRAFT INDICATED PROPELLER DAMAGE, BELLY SCRAPING, AND SCRAPING ON THE NOSE GEAR DOOR. NO TRANSITIONAL (LANDING GEAR) DAMAGE WAS DETECTED AND ALL DAMAGE GAVE AN INDICATION THAT THE LANDING GEAR WAS RETRACTED AT THE TIME OF CONTACT. EXAMINATION OF THE RUNWAY (21) SURFACE, INDICATED A TOTAL OF 13 PROP BLADE STRIKES AND THEN METAL TO CEMENT SLIDE MARKS OVER A 700' SPACE. NO EVIDENCE OF RUBBER MARKS FROM ANY OF THE THREE TIRES WAS FOUND. TOWER PERSONNEL STATED THAT ANOTHER AIRCRAFT WAS DELAYED EXITING THE RUNWAY IN FRONT OF THE LANDING INCIDENT AIRCRAFT. THE RUNWAY SIGNATURES, AIRCRAFT SLIDE DISTANCE AND AIRCRAFT DAMAGE DEMONSTRATE WHAT APPEARS TO BE A GEAR UP LANDING, NOT A COLLAPSED LANDING GEAR DURING ROLL OUT. THIS PHYSICAL EVIDENCE CONTRADICTS THE STATEMENT PROVIDED BY THE PILOT. POSSIBLE DISTRACTION OF THE PILOT BY THE LANDING AIRCRAFT IN FRONT OF HIM MAY HAVE BEEN A CONTRIBUTING FACTOR.

Other reports on N6524U · 1

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