19971125043989A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Middlefield, OH · November 25, 1997

Date
November 25, 1997 · 10:50 local
Place
Middlefield, OH
Airport
Geauga County Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1816J
NTSB investigation
NTSBNYC98LA032
Reported as
Piper PA28140
Reported engine
Lycoming O320E2A
Fatal injuries
0
Pilot’s flight hours
1,575 total1,300 in this make and model11 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.

Power loss on takeoff. Collided with trees and power lines. Conditions exsisted for carb. Ice. (.4)during the initial climb after a normal takeoff, the airplane experienced a gradual loss of engine power. While turning to avoid some houses, the airplane struck power lines and impacted terrain. Examination of the log books revealed this was the airplane's first flight since an annual inspection had been completed. At that time, the airplane's carburetor was removed, disassembled and it's two piece venturi was replaced with a one piece venturi, per precision airmotive service bulletin # MSA-2. Also, the airplane had not been flown for over a month prior to the accident. On-scene examination of the airplane did not reveal any evidence of a preimpact failure of the airframe or engine. An engine run-up and a carburetor tear-down and flow check did not disclose any evidence of malfunction. Automotive gasoline was being used as fuel per a supplemental type certificate. At an airport about 21 miles southeast of the accident site, the wind was reported to be from 200 degrees at 11 gusting 17 knots. The temperature and dew point were rep orted to be 34 and 23 degrees, respectively. According to icing probability charts, conditions were conductive to possible carburetor icing; however, carburetor icing was not verified. The pilot had checked the carburetor heat before takeoff, but did not report engaging it after the engine started losing power. (-23) pilot back taxied on runway for departure off runway 28 at 7G8, Geauga County Airport, Middlefield, Ohio. After getting airborne, the aircraft struck powerlines and trees approx. 3/10 miles wsw of the airport. A witness said the engine was running rough on take-off. 2 witnesses immediately adjacent the scene noted no engine noise was heard as they viewed the aircraft impact the power lines. The aircraft impacted the ground at an approximate 45 degree nose down attitude. The cause of engine power loss is under investigation

As the FAA filed it

POWER LOSS ON TAKEOFF. COLLIDED WITH TREES AND POWER LINES. CONDITIONS EXSISTED FOR CARB. ICE. (.4)DURING THE INITIAL CLIMB AFTER A NORMAL TAKEOFF, THE AIRPLANE EXPERIENCED A GRADUAL LOSS OF ENGINE POWER. WHILE TURNING TO AVOID SOME HOUSES, THE AIRPLANE STRUCK POWER LINES AND IMPACTED TERRAIN. EXAMINATION OF THE LOG BOOKS REVEALED THIS WAS THE AIRPLANE'S FIRST FLIGHT SINCE AN ANNUAL INSPECTION HAD BEEN COMPLETED. AT THAT TIME, THE AIRPLANE'S CARBURETOR WAS REMOVED, DISASSEMBLED AND IT'S TWO PIECE VENTURI WAS REPLACED WITH A ONE PIECE VENTURI, PER PRECISION AIRMOTIVE SERVICE BULLETIN # MSA-2. ALSO, THE AIRPLANE HAD NOT BEEN FLOWN FOR OVER A MONTH PRIOR TO THE ACCIDENT. ON-SCENE EXAMINATION OF THE AIRPLANE DID NOT REVEAL ANY EVIDENCE OF A PREIMPACT FAILURE OF THE AIRFRAME OR ENGINE. AN ENGINE RUN-UP AND A CARBURETOR TEAR-DOWN AND FLOW CHECK DID NOT DISCLOSE ANY EVIDENCE OF MALFUNCTION. AUTOMOTIVE GASOLINE WAS BEING USED AS FUEL PER A SUPPLEMENTAL TYPE CERTIFICATE. AT AN AIRPORT ABOUT 21 MILES SOUTHEAST OF THE ACCIDENT SITE, THE WIND WAS REPORTED TO BE FROM 200 DEGREES AT 11 GUSTING 17 KNOTS. THE TEMPERATURE AND DEW POINT WERE REP ORTED TO BE 34 AND 23 DEGREES, RESPECTIVELY. ACCORDING TO ICING PROBABILITY CHARTS, CONDITIONS WERE CONDUCTIVE TO POSSIBLE CARBURETOR ICING; HOWEVER, CARBURETOR ICING WAS NOT VERIFIED. THE PILOT HAD CHECKED THE CARBURETOR HEAT BEFORE TAKEOFF, BUT DID NOT REPORT ENGAGING IT AFTER THE ENGINE STARTED LOSING POWER. (-23) PILOT BACK TAXIED ON RUNWAY FOR DEPARTURE OFF RUNWAY 28 AT 7G8, GEAUGA COUNTY AIRPORT, MIDDLEFIELD, OHIO. AFTER GETTING AIRBORNE, THE AIRCRAFT STRUCK POWERLINES AND TREES APPROX. 3/10 MILES WSW OF THE AIRPORT. A WITNESS SAID THE ENGINE WAS RUNNING ROUGH ON TAKE-OFF. 2 WITNESSES IMMEDIATELY ADJACENT THE SCENE NOTED NO ENGINE NOISE WAS HEARD AS THEY VIEWED THE AIRCRAFT IMPACT THE POWER LINES. THE AIRCRAFT IMPACTED THE GROUND AT AN APPROXIMATE 45 DEGREE NOSE DOWN ATTITUDE. THE CAUSE OF ENGINE POWER LOSS IS UNDER INVESTIGATION

NTSB investigation

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