20190709004379A

Accident · Substantial damage

FAA accident report · Stinson 108-3 · Klamath Falls, OR · July 9, 2019

Date
July 9, 2019 · 14:00 local
Place
Klamath Falls, OR
Airport
Klamath Falls
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6642M
NTSB investigation
NTSBWPR19LA207
Reported as
Stinson 108-3
Reported engine
Franklin 6A4165 series
People aboard
2
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.

The aircraft departed lmt (Klamath Falls). PIC described a procedure he has been using to work around an issue with the carburetor, acceleration and full power. The procedure he described was to advance the throttle slowly until the last quarter then rapidly otherwise the engine would not throttle to full power.

The PIC stated that the newly manufacturer rebuilt carburetor was installed, would not accelerate propoerly or achieve full power so it was removed and sent back to the manufacturer, rebuilt (again) and reinstalled. The issue was lessened but still present.

On departure from lmt the PIC reported the procedure was used, takeoff and subsequently the engine wuit on climbout forcing a landing in a field. The field was soft and the left main landing gear collapsed upward causing damage to the left wing tip, aileron and gear attachment areas.

As the FAA filed it

THE AIRCRAFT DEPARTED LMT (KLAMATH FALLS). PIC DESCRIBED A PROCEDURE HE HAS BEEN USING TO WORK AROUND AN ISSUE WITH THE CARBURETOR, ACCELERATION AND FULL POWER. THE PROCEDURE HE DESCRIBED WAS TO ADVANCE THE THROTTLE SLOWLY UNTIL THE LAST QUARTER THEN RAPIDLY OTHERWISE THE ENGINE WOULD NOT THROTTLE TO FULL POWER.

THE PIC STATED THAT THE NEWLY MANUFACTURER REBUILT CARBURETOR WAS INSTALLED, WOULD NOT ACCELERATE PROPOERLY OR ACHIEVE FULL POWER SO IT WAS REMOVED AND SENT BACK TO THE MANUFACTURER, REBUILT (AGAIN) AND REINSTALLED. THE ISSUE WAS LESSENED BUT STILL PRESENT.

ON DEPARTURE FROM LMT THE PIC REPORTED THE PROCEDURE WAS USED, TAKEOFF AND SUBSEQUENTLY THE ENGINE WUIT ON CLIMBOUT FORCING A LANDING IN A FIELD. THE FIELD WAS SOFT AND THE LEFT MAIN LANDING GEAR COLLAPSED UPWARD CAUSING DAMAGE TO THE LEFT WING TIP, AILERON AND GEAR ATTACHMENT AREAS.

NTSB investigation

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