20151106022539A

Accident · Minor damage

FAA accident report · Eurocopter Deutschland EC 135 T2+ · Monongahela, PA · November 6, 2015

Date
November 6, 2015 · 06:00 local
Place
Monongahela, PA
Airport
Monongahela Valley Hospital He
Phase of flight
Takeoff: Climb Out
Operating rules
Air taxi and commuter (Part 135)
Operator
E3MA
Damage
Minor damage
Aircraft
N639ME
NTSB investigation
NTSBERA16CA060
Reported as
Eurocopter Deutschland EC 135 T2+
Reported engine
Turbomeca ARRIUS-2B2
People aboard
4
Fatal injuries
0
Other injuries
0

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.

During take-off from monongehela valley Hospital (5PA5) helipad with two medical crewmembers and a patient onboard, the helicopter rotor wash blew a vinyl cover off of the 33-gallon wheeled foam fire extinguisher. The vinyl cover impacted the aircraft and was shredded by the fenestron blades (tail rotor) severely hindering the pilot's ability to control the helicopter. The pilot immediately landed the helicopter back on the helipad and shut down the engines. An inspection of the helicopter following this incident revealed minor damage to the fenestron blades, fenestron composite housing, the tail rotor long driveshaft and the forward and aft landing gear crosstubes.

As the FAA filed it

DURING TAKE-OFF FROM MONONGEHELA VALLEY HOSPITAL (5PA5) HELIPAD WITH TWO MEDICAL CREWMEMBERS AND A PATIENT ONBOARD, THE HELICOPTER ROTOR WASH BLEW A VINYL COVER OFF OF THE 33-GALLON WHEELED FOAM FIRE EXTINGUISHER. THE VINYL COVER IMPACTED THE AIRCRAFT AND WAS SHREDDED BY THE FENESTRON BLADES (TAIL ROTOR) SEVERELY HINDERING THE PILOT'S ABILITY TO CONTROL THE HELICOPTER. THE PILOT IMMEDIATELY LANDED THE HELICOPTER BACK ON THE HELIPAD AND SHUT DOWN THE ENGINES. AN INSPECTION OF THE HELICOPTER FOLLOWING THIS INCIDENT REVEALED MINOR DAMAGE TO THE FENESTRON BLADES, FENESTRON COMPOSITE HOUSING, THE TAIL ROTOR LONG DRIVESHAFT AND THE FORWARD AND AFT LANDING GEAR CROSSTUBES.

NTSB investigation

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