20160725016849A

Accident · Substantial damage

FAA accident report · Cessna 188A · What Cheer, IA · July 25, 2016

Date
July 25, 2016 · 18:00 local
Place
What Cheer, IA
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9979G
NTSB investigation
NTSBGAA16CA393
Reported as
Cessna 188A
Reported engine
Continental O-470 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,313 total34 in this make and model58 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.

In late afternoon on the day of the crash, the pilot performed a preflight inspection, an engine run up and took off from his private farm airstrip to practice agricultural application operations. After approximately 30 minutes of flying, and during a "spray run", the engine slowly but steadily lost power resulting in a total loss of power. The pilot was able to gain enough altitude to identify a nearby soybean field as a place to land. He touched down going up hill. Cresting the hill, the aircraft turned slightly to the left at which point the right main landing gear separated from the aircraft and the aircraft came to rest upright with the right wing laying on the ground. With the exception of a small abrasion on the right arm, the pilot was uninjured.

Visible damage included the deformed right wing, right wing tip broken off, the right landing gear separated from the aircraft, dents to the front lower engine cowling and a bent prop blade.

An undetermined amount of fuel was found in the single header tank. The fuel shutoff control in the cockpit was found to be in the on position. Approximately one pint of fuel was sumped from the fuel tank. No contamination was observed.

A malfunction or defect report will be submitted if additional information becomes available at a later date.

As the FAA filed it

IN LATE AFTERNOON ON THE DAY OF THE CRASH, THE PILOT PERFORMED A PREFLIGHT INSPECTION, AN ENGINE RUN UP AND TOOK OFF FROM HIS PRIVATE FARM AIRSTRIP TO PRACTICE AGRICULTURAL APPLICATION OPERATIONS. AFTER APPROXIMATELY 30 MINUTES OF FLYING, AND DURING A "SPRAY RUN", THE ENGINE SLOWLY BUT STEADILY LOST POWER RESULTING IN A TOTAL LOSS OF POWER. THE PILOT WAS ABLE TO GAIN ENOUGH ALTITUDE TO IDENTIFY A NEARBY SOYBEAN FIELD AS A PLACE TO LAND. HE TOUCHED DOWN GOING UP HILL. CRESTING THE HILL, THE AIRCRAFT TURNED SLIGHTLY TO THE LEFT AT WHICH POINT THE RIGHT MAIN LANDING GEAR SEPARATED FROM THE AIRCRAFT AND THE AIRCRAFT CAME TO REST UPRIGHT WITH THE RIGHT WING LAYING ON THE GROUND. WITH THE EXCEPTION OF A SMALL ABRASION ON THE RIGHT ARM, THE PILOT WAS UNINJURED.

VISIBLE DAMAGE INCLUDED THE DEFORMED RIGHT WING, RIGHT WING TIP BROKEN OFF, THE RIGHT LANDING GEAR SEPARATED FROM THE AIRCRAFT, DENTS TO THE FRONT LOWER ENGINE COWLING AND A BENT PROP BLADE.

AN UNDETERMINED AMOUNT OF FUEL WAS FOUND IN THE SINGLE HEADER TANK. THE FUEL SHUTOFF CONTROL IN THE COCKPIT WAS FOUND TO BE IN THE ON POSITION. APPROXIMATELY ONE PINT OF FUEL WAS SUMPED FROM THE FUEL TANK. NO CONTAMINATION WAS OBSERVED.

A MALFUNCTION OR DEFECT REPORT WILL BE SUBMITTED IF ADDITIONAL INFORMATION BECOMES AVAILABLE AT A LATER DATE.

NTSB investigation

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