20100610035209A

Accident · Substantial damage

FAA accident report · Piper PA-46-310P · Ontario, CA · June 10, 2010

Date
June 10, 2010 · 16:27 local
Place
Ontario, CA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N121HJ
NTSB investigation
NTSBWPR10LA284
Reported as
Piper PA-46-310P
Reported engine
Continental IO-550 series
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
850 total1 in this make and model30 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.

The pilot and flight instructor on board both stated that at approximately 17,000 ft MSL the aircraft experienced a loud "pop" or "bang". The pilot and flight instructor stated that this "pop" or "bang" led to a loss of engine power. The pilot and flight instructor then diverted to kont in coordination with approach control (socal TRACON). The pilot and flight instructor both stated that a checklist was referred to regarding partial loss of power, but no emergency "engine out" checklists were performed. The pilot and flight instructor elected to utilize a non-emergency approach profile to the airfield. On final to runway 26R, the pilot attempted to add power on an appx. 1/2 mile final. The pilot and flight instructor stated that there was no response from the engine when the power levers were pushed forward, leading to the aircraft landing short of the runway. Before making contact with the ground, the aircraft hit a fence where a small brush fire was started. Both main gear were sheared off of the aircraft during contact with the fence and/or ground.

As the FAA filed it

THE PILOT AND FLIGHT INSTRUCTOR ON BOARD BOTH STATED THAT AT APPROXIMATELY 17,000 FT MSL THE AIRCRAFT EXPERIENCED A LOUD "POP" OR "BANG". THE PILOT AND FLIGHT INSTRUCTOR STATED THAT THIS "POP" OR "BANG" LED TO A LOSS OF ENGINE POWER. THE PILOT AND FLIGHT INSTRUCTOR THEN DIVERTED TO KONT IN COORDINATION WITH APPROACH CONTROL (SOCAL TRACON). THE PILOT AND FLIGHT INSTRUCTOR BOTH STATED THAT A CHECKLIST WAS REFERRED TO REGARDING PARTIAL LOSS OF POWER, BUT NO EMERGENCY "ENGINE OUT" CHECKLISTS WERE PERFORMED. THE PILOT AND FLIGHT INSTRUCTOR ELECTED TO UTILIZE A NON-EMERGENCY APPROACH PROFILE TO THE AIRFIELD. ON FINAL TO RUNWAY 26R, THE PILOT ATTEMPTED TO ADD POWER ON AN APPX. 1/2 MILE FINAL. THE PILOT AND FLIGHT INSTRUCTOR STATED THAT THERE WAS NO RESPONSE FROM THE ENGINE WHEN THE POWER LEVERS WERE PUSHED FORWARD, LEADING TO THE AIRCRAFT LANDING SHORT OF THE RUNWAY. BEFORE MAKING CONTACT WITH THE GROUND, THE AIRCRAFT HIT A FENCE WHERE A SMALL BRUSH FIRE WAS STARTED. BOTH MAIN GEAR WERE SHEARED OFF OF THE AIRCRAFT DURING CONTACT WITH THE FENCE AND/OR GROUND.

NTSB investigation

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