20130717013789A

Accident · Destroyed

FAA accident report · Grumman Acft ENG Cor-Schweizer G-164A · Elmira, MI · July 17, 2013

Date
July 17, 2013 · 16:30 local
Place
Elmira, MI
Phase of flight
Maneuver
Operating rules
Agricultural (Part 137)
Operator
9SBG
Damage
Destroyed
Aircraft
N8719H
NTSB investigation
NTSBCEN13LA422
Reported as
Grumman Acft ENG Cor-Schweizer G-164A
Reported engine
Pratt & Whitney R1340 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,500 total1,000 in this make and model150 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.

On 7/17/2013 N8719H a gruman 164A crashed at 1630 local near Elmira, MI. The aircraft was piloted by privacy data omitted, commercial pilot certificate number privacy data omitted while conducting agricultural spraying for slf air, certificate number 9SBG. The aircraft operated from lakes of the north airport (4Y4) prior to commencing the spraying operation. The aircraft cleared approximately 700FT of wooded land prior to impacting two trees and coming to rest 110FT later. The aircraft was consumed by fire and destroyed. The pilot was able to extricate himself from the aircraft prior to emergency vehicle response. The aircraft was carrying agricultural pesticide at the time of the crash and evidence of this could be seen on a wide area of foliage near the crash site.

On scene investigation revealed that the aircraft came to rest 110FT after first impacting the trees which indicates that is descended at a steep angle. The aircraft debris path was minimal showing no indication of inflight breakup. The propeller showed some twisting and leading edge damage consistent with the engine producing some power at the time of the accident. There was no remaining fuel onboard the aircraft as fire would have consumed any that remained at the time of the accidnet.

There were no known eyewitnesses to the crash and the pilot reports only having memory of flight prior to spraying the final field and again as he was loaded into the ambulance. No abnormal flight characteristics were noted during previous flights and the pilot says that he does not remember any of the events leading up to or during the accident.

Post-accident interviews conducted with the pilot indicate the aircraft was fueled to approximate loads (1/2 to ¾ full) prior to each flight from a metal tank in the back of a pickup truck. The pilot stated that the aircraft fuel tanks were not sumped after each fueling and prior to each flight.

As the FAA filed it

ON 7/17/2013 N8719H A GRUMAN 164A CRASHED AT 1630 LOCAL NEAR ELMIRA, MI. THE AIRCRAFT WAS PILOTED BY ^PRIVACY DATA OMITTED^, COMMERCIAL PILOT CERTIFICATE NUMBER ^PRIVACY DATA OMITTED^ WHILE CONDUCTING AGRICULTURAL SPRAYING FOR SLF AIR, CERTIFICATE NUMBER 9SBG. THE AIRCRAFT OPERATED FROM LAKES OF THE NORTH AIRPORT (4Y4) PRIOR TO COMMENCING THE SPRAYING OPERATION. THE AIRCRAFT CLEARED APPROXIMATELY 700FT OF WOODED LAND PRIOR TO IMPACTING TWO TREES AND COMING TO REST 110FT LATER. THE AIRCRAFT WAS CONSUMED BY FIRE AND DESTROYED. THE PILOT WAS ABLE TO EXTRICATE HIMSELF FROM THE AIRCRAFT PRIOR TO EMERGENCY VEHICLE RESPONSE. THE AIRCRAFT WAS CARRYING AGRICULTURAL PESTICIDE AT THE TIME OF THE CRASH AND EVIDENCE OF THIS COULD BE SEEN ON A WIDE AREA OF FOLIAGE NEAR THE CRASH SITE.

ON SCENE INVESTIGATION REVEALED THAT THE AIRCRAFT CAME TO REST 110FT AFTER FIRST IMPACTING THE TREES WHICH INDICATES THAT IS DESCENDED AT A STEEP ANGLE. THE AIRCRAFT DEBRIS PATH WAS MINIMAL SHOWING NO INDICATION OF INFLIGHT BREAKUP. THE PROPELLER SHOWED SOME TWISTING AND LEADING EDGE DAMAGE CONSISTENT WITH THE ENGINE PRODUCING SOME POWER AT THE TIME OF THE ACCIDENT. THERE WAS NO REMAINING FUEL ONBOARD THE AIRCRAFT AS FIRE WOULD HAVE CONSUMED ANY THAT REMAINED AT THE TIME OF THE ACCIDNET.

THERE WERE NO KNOWN EYEWITNESSES TO THE CRASH AND THE PILOT REPORTS ONLY HAVING MEMORY OF FLIGHT PRIOR TO SPRAYING THE FINAL FIELD AND AGAIN AS HE WAS LOADED INTO THE AMBULANCE. NO ABNORMAL FLIGHT CHARACTERISTICS WERE NOTED DURING PREVIOUS FLIGHTS AND THE PILOT SAYS THAT HE DOES NOT REMEMBER ANY OF THE EVENTS LEADING UP TO OR DURING THE ACCIDENT.

POST-ACCIDENT INTERVIEWS CONDUCTED WITH THE PILOT INDICATE THE AIRCRAFT WAS FUELED TO APPROXIMATE LOADS (1/2 TO ¾ FULL) PRIOR TO EACH FLIGHT FROM A METAL TANK IN THE BACK OF A PICKUP TRUCK. THE PILOT STATED THAT THE AIRCRAFT FUEL TANKS WERE NOT SUMPED AFTER EACH FUELING AND PRIOR TO EACH FLIGHT.

NTSB investigation

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

Other reports on N8719H · 1

Matched to the same aircraft by N-number and date.