20200430005419A

Accident · Substantial damage

FAA accident report · Engineering & Research ERCOUPE 415-C · Hallettsville, TX · April 30, 2020

Date
April 30, 2020 · 14:30 local
Place
Hallettsville, TX
Airport
Hallettsville
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2275H
NTSB investigation
NTSBCEN20LA170
Reported as
Engineering & Research Ercoupe 415-C
Reported engine
Continental A&C75 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot

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.

02 May 2020, after refueling the listed aircraft and performing a preflight, the aircraft owner operator departed uvalde, Texas (kuva), at approximately 13:30L, enroute to eagle lake, Texas (kela), at an approximate altitude of 3500 ft MSL.

At approximately 7 miles northwest of the halletsville airport (34R), near worthing, Texas the aircraft engine began to vibrate and loose power. The PIC reduced the power setting and began looking for an alternate landing area when it was apparent the flight could not reach the nearby airport. The PIC, after avoiding power-lines and making turns, realized the sink rate was higher than predicted. A cattle field was targeted as an acceptable landing area. The landing was accomplished successfully with the aircraft experiencing damage to the nose landing gear, propeller, engine, firewall and engine mount.

06/08/2020 The houston FSDO iic performed a second inspection of the aircraft powerplant and associated equipment after the vehicle had been moved to it's eagle lake regional airport (kela) hanger. The stromberg NA-S3A1 carburetor and gascolator / sediment bowl assembly was removed after disconnect of the associated tubes, lines, cables, etc. Also removed was the lower number 1 and 4 spark plugs. Visual inspection of the items revealed murky fuel in the bowl, a small amount of sediment in the bowl, plugs that were lightly fouled and carbon bridged, the carburetor was soiled / dirty beyond the accident damage.

Based on weather conditions at the time of the accident and the NTSB carburetor icing probability chart, plus the statement given by the PIC, the aircraft loss of power appears to have been brought about due to carburetor icing, poor condition of the fuel and fuel system.

As the FAA filed it

02 MAY 2020, AFTER REFUELING THE LISTED AIRCRAFT AND PERFORMING A PREFLIGHT, THE AIRCRAFT OWNER OPERATOR DEPARTED UVALDE, TEXAS (KUVA), AT APPROXIMATELY 13:30L, ENROUTE TO EAGLE LAKE, TEXAS (KELA), AT AN APPROXIMATE ALTITUDE OF 3500 FT MSL.

AT APPROXIMATELY 7 MILES NORTHWEST OF THE HALLETSVILLE AIRPORT (34R), NEAR WORTHING, TEXAS THE AIRCRAFT ENGINE BEGAN TO VIBRATE AND LOOSE POWER. THE PIC REDUCED THE POWER SETTING AND BEGAN LOOKING FOR AN ALTERNATE LANDING AREA WHEN IT WAS APPARENT THE FLIGHT COULD NOT REACH THE NEARBY AIRPORT. THE PIC, AFTER AVOIDING POWER-LINES AND MAKING TURNS, REALIZED THE SINK RATE WAS HIGHER THAN PREDICTED. A CATTLE FIELD WAS TARGETED AS AN ACCEPTABLE LANDING AREA. THE LANDING WAS ACCOMPLISHED SUCCESSFULLY WITH THE AIRCRAFT EXPERIENCING DAMAGE TO THE NOSE LANDING GEAR, PROPELLER, ENGINE, FIREWALL AND ENGINE MOUNT.

06/08/2020 THE HOUSTON FSDO IIC PERFORMED A SECOND INSPECTION OF THE AIRCRAFT POWERPLANT AND ASSOCIATED EQUIPMENT AFTER THE VEHICLE HAD BEEN MOVED TO IT'S EAGLE LAKE REGIONAL AIRPORT (KELA) HANGER. THE STROMBERG NA-S3A1 CARBURETOR AND GASCOLATOR / SEDIMENT BOWL ASSEMBLY WAS REMOVED AFTER DISCONNECT OF THE ASSOCIATED TUBES, LINES, CABLES, ETC. ALSO REMOVED WAS THE LOWER NUMBER 1 AND 4 SPARK PLUGS. VISUAL INSPECTION OF THE ITEMS REVEALED MURKY FUEL IN THE BOWL, A SMALL AMOUNT OF SEDIMENT IN THE BOWL, PLUGS THAT WERE LIGHTLY FOULED AND CARBON BRIDGED, THE CARBURETOR WAS SOILED / DIRTY BEYOND THE ACCIDENT DAMAGE.

BASED ON WEATHER CONDITIONS AT THE TIME OF THE ACCIDENT AND THE NTSB CARBURETOR ICING PROBABILITY CHART, PLUS THE STATEMENT GIVEN BY THE PIC, THE AIRCRAFT LOSS OF POWER APPEARS TO HAVE BEEN BROUGHT ABOUT DUE TO CARBURETOR ICING, POOR CONDITION OF THE FUEL AND FUEL SYSTEM.

NTSB investigation

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