20010416006459A

Accident · No damage

FAA accident report · Mooney M20K · Bountiful, UT · April 16, 2001

Date
April 16, 2001 · 17:45 local
Place
Bountiful, UT
Airport
Salt Lake Skypark Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N921Z
NTSB investigation
NTSBDEN01LA087
Reported as
Mooney M20K

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/c lost all electrical power approx. 10 minutes after departure frombtf airport. Pilot made an emergency return to airport. Initial investigation indicated that the pilot was applying right brake pressure during landing resulting in major cross-control input causing in the left main wheel to seperate when brake pressure was released. However, subsequent investigation shows that the pilot flew a very shallow approach and touched down short of the runway where both main tires came in contact with a tubular runway barrier (approx. 18" high). The left main wheel separated from the aircraft when the aircraft contacted the barrier. Subsequently, the aircraft exited on the right side of the runway and damage was sustained to the right leading edge of the wing fuselage left aileron, and left main gear strut. No injuries were sustained by the pilot or passengers.

As the FAA filed it

(-23) A/C LOST ALL ELECTRICAL POWER APPROX. 10 MINUTES AFTER DEPARTURE FROMBTF AIRPORT. PILOT MADE AN EMERGENCY RETURN TO AIRPORT. INITIAL INVESTIGATION INDICATED THAT THE PILOT WAS APPLYING RIGHT BRAKE PRESSURE DURING LANDING RESULTING IN MAJOR CROSS-CONTROL INPUT CAUSING IN THE LEFT MAIN WHEEL TO SEPERATE WHEN BRAKE PRESSURE WAS RELEASED. HOWEVER, SUBSEQUENT INVESTIGATION SHOWS THAT THE PILOT FLEW A VERY SHALLOW APPROACH AND TOUCHED DOWN SHORT OF THE RUNWAY WHERE BOTH MAIN TIRES CAME IN CONTACT WITH A TUBULAR RUNWAY BARRIER (APPROX. 18" HIGH). THE LEFT MAIN WHEEL SEPARATED FROM THE AIRCRAFT WHEN THE AIRCRAFT CONTACTED THE BARRIER. SUBSEQUENTLY, THE AIRCRAFT EXITED ON THE RIGHT SIDE OF THE RUNWAY AND DAMAGE WAS SUSTAINED TO THE RIGHT LEADING EDGE OF THE WING FUSELAGE LEFT AILERON, AND LEFT MAIN GEAR STRUT. NO INJURIES WERE SUSTAINED BY THE PILOT OR PASSENGERS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N921Z · 1

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