20180717011409A

Accident · Destroyed

FAA accident report · Ryan NAVION B · Truckee, CA · July 17, 2018

Date
July 17, 2018 · 07:33 local
Place
Truckee, CA
Airport
Truckee-Tahoe
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5329K
NTSB investigation
NTSBWPR18FA198
Reported as
Ryan Navion B
Reported engine
Lycoming GO-480 series
People aboard
3
Fatal injuries
2
Other injuries
1
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.

After departure from tke runway 11, at 0732, the pilot reported to the tower he had an engine failure and was returning to the airport. Approximately 1 mile south of the airport the aircraft impacted the ground. Examination of the accident scene revealed the aircraft landed upright into rising terrain and had made a 50 foot ground scar. The right wing was bent aft with leading edge damage. The 3 bladed propeller showed no rotational damage. The lower blade had separated from the hub and was located approximately 20 feet aft of the engine. The separated blade showed no rotational damage only reward bending due to contact with the ground.

As the FAA filed it

AFTER DEPARTURE FROM TKE RUNWAY 11, AT 0732, THE PILOT REPORTED TO THE TOWER HE HAD AN ENGINE FAILURE AND WAS RETURNING TO THE AIRPORT. APPROXIMATELY 1 MILE SOUTH OF THE AIRPORT THE AIRCRAFT IMPACTED THE GROUND. EXAMINATION OF THE ACCIDENT SCENE REVEALED THE AIRCRAFT LANDED UPRIGHT INTO RISING TERRAIN AND HAD MADE A 50 FOOT GROUND SCAR. THE RIGHT WING WAS BENT AFT WITH LEADING EDGE DAMAGE. THE 3 BLADED PROPELLER SHOWED NO ROTATIONAL DAMAGE. THE LOWER BLADE HAD SEPARATED FROM THE HUB AND WAS LOCATED APPROXIMATELY 20 FEET AFT OF THE ENGINE. THE SEPARATED BLADE SHOWED NO ROTATIONAL DAMAGE ONLY REWARD BENDING DUE TO CONTACT WITH THE GROUND.

NTSB investigation

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