19980514009209A

Accident · Substantial damage

FAA accident report · Piper PA-22-160 · Clarksburg, CA · May 14, 1998

Date
May 14, 1998 · 18:00 local
Place
Clarksburg, CA
Airport
Borges-Clarksburg Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N198TP
NTSB investigation
NTSBLAX98LA157
Reported as
Piper PA22160
Reported engine
Lycoming O320B2B
Fatal injuries
0
Pilot’s flight hours
3,300 total150 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.

Acft exper engine failure and made an emergency landing in a plowed field off the end of rwy, Clarksburg, CA. (.4) on may 14, 1998, at 1800 hours pacific daylight time, a Piper PA-22-160, N198TP, registered to the aircraft owner's and pilot's association (aopa), experienced a total loss of engine power in the traffic pattern at the uncontrolled Clarksburg airport, Clarksburg, California. Unable to glide to the runway, the commercial pilot made a forced landing in a soft field and the airplane nosed over. The airplane was substantially damaged, and the pilot received minor injuries. Visual meteorological conditions prevailed at the time of the personal flight, and no flight plan was filed. The flight originated from sacramento, California, at 1750. The pilot reported that prior to taking off for the planned 10-minute long flight both fuel tanks contained over 5 gallons of fuel, and all airplane systems were functioning normally. The pilot arrived at Clarksburg and entered the traffic pattern. Carburetor heat was applied, the throttle was retarded, and the airplane descended. The pilot further stated that after turning onto the base leg he moved the throttle forward to increase engine power, and the engine "blubbered and totally lost power." The federal aviation administration (FAA) coordinator responded to the accident site and examined the wreckage. The FAA reported it examined the powerplant, induction system, engine controls, and magnetos. The ignition switch and the carburetor were functionally examined. No evidence was found of any mechanical malfunctions.

As the FAA filed it

ACFT EXPER ENGINE FAILURE AND MADE AN EMERGENCY LANDING IN A PLOWED FIELD OFF THE END OF RWY, CLARKSBURG, CA. (.4) ON MAY 14, 1998, AT 1800 HOURS PACIFIC DAYLIGHT TIME, A PIPER PA-22-160, N198TP, REGISTERED TO THE AIRCRAFT OWNER'S AND PILOT'S ASSOCIATION (AOPA), EXPERIENCED A TOTAL LOSS OF ENGINE POWER IN THE TRAFFIC PATTERN AT THE UNCONTROLLED CLARKSBURG AIRPORT, CLARKSBURG, CALIFORNIA. UNABLE TO GLIDE TO THE RUNWAY, THE COMMERCIAL PILOT MADE A FORCED LANDING IN A SOFT FIELD AND THE AIRPLANE NOSED OVER. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED, AND THE PILOT RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE PERSONAL FLIGHT, AND NO FLIGHT PLAN WAS FILED. THE FLIGHT ORIGINATED FROM SACRAMENTO, CALIFORNIA, AT 1750. THE PILOT REPORTED THAT PRIOR TO TAKING OFF FOR THE PLANNED 10-MINUTE LONG FLIGHT BOTH FUEL TANKS CONTAINED OVER 5 GALLONS OF FUEL, AND ALL AIRPLANE SYSTEMS WERE FUNCTIONING NORMALLY. THE PILOT ARRIVED AT CLARKSBURG AND ENTERED THE TRAFFIC PATTERN. CARBURETOR HEAT WAS APPLIED, THE THROTTLE WAS RETARDED, AND THE AIRPLANE DESCENDED. THE PILOT FURTHER STATED THAT AFTER TURNING ONTO THE BASE LEG HE MOVED THE THROTTLE FORWARD TO INCREASE ENGINE POWER, AND THE ENGINE "BLUBBERED AND TOTALLY LOST POWER." THE FEDERAL AVIATION ADMINISTRATION (FAA) COORDINATOR RESPONDED TO THE ACCIDENT SITE AND EXAMINED THE WRECKAGE. THE FAA REPORTED IT EXAMINED THE POWERPLANT, INDUCTION SYSTEM, ENGINE CONTROLS, AND MAGNETOS. THE IGNITION SWITCH AND THE CARBURETOR WERE FUNCTIONALLY EXAMINED. NO EVIDENCE WAS FOUND OF ANY MECHANICAL MALFUNCTIONS.

NTSB investigation

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