20110727014929A

Accident · Substantial damage

FAA accident report · Eurocopter AS 350 B3 · Troutdale, OR · July 27, 2011

Date
July 27, 2011 · 15:52 local
Place
Troutdale, OR
Airport
Troutdale
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Operator
QMLA
Damage
Substantial damage
Aircraft
N808LF
NTSB investigation
NTSBWPR11LA352
Reported as
Eurocopter AS 350 B3
Reported engine
Turbomeca ARRIEL-2B1
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
3,000 total600 in this make and model45 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.

Aircraft departed aurora in route to the dalles approx. 15 minutes into flight the pilot heard a thump and aircraft started vibrating. The pilot decided a precautionary landing at Troutdale. Upon inspection the center tail drive shaft covr was missing, one of the main rotor blades had significant damage at the tip. There were also scrapes and scrathes on the tail rotor. Aircraft had just had a 100 hour inspection completed at aurora prior to this flight. Interview with each mechanic and the pilot indicated that all had seen the panel installed and secured. The right hand side still has the fasteners installed the left side fasteners are missing.

As the FAA filed it

AIRCRAFT DEPARTED AURORA IN ROUTE TO THE DALLES APPROX. 15 MINUTES INTO FLIGHT THE PILOT HEARD A THUMP AND AIRCRAFT STARTED VIBRATING. THE PILOT DECIDED A PRECAUTIONARY LANDING AT TROUTDALE. UPON INSPECTION THE CENTER TAIL DRIVE SHAFT COVR WAS MISSING, ONE OF THE MAIN ROTOR BLADES HAD SIGNIFICANT DAMAGE AT THE TIP. THERE WERE ALSO SCRAPES AND SCRATHES ON THE TAIL ROTOR.AIRCRAFT HAD JUST HAD A 100 HOUR INSPECTION COMPLETED AT AURORA PRIOR TO THIS FLIGHT.INTERVIEW WITH EACH MECHANIC AND THE PILOT INDICATED THAT ALL HAD SEEN THE PANEL INSTALLED AND SECURED. THE RIGHT HAND SIDE STILL HAS THE FASTENERS INSTALLED THE LEFT SIDE FASTENERS ARE MISSING.

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 N808LF · 2

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