ERA16CA060

NTSB accident investigation · Eurocopter Deutschland EC 135 · Monongahela, PA · November 6, 2015

Accident · No injuriesData collectionFinal report
Date
November 6, 2015, 06:00 local (11:00 UTC)
Place
Monongahela, PA
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N639MEEurocopter Deutschland EC 135
Defining event
Takeoff: Loss of control in flight
Weather
Visual (VMC) · Dawn
Status
Completed · report January 15, 2016
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA-Allegheny FSDO
FAA report
20151106022539A
Case key
92401

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The inadequate securing of the wheeled fire extinguisher's cover which resulted in it being blown off of the fire extinguisher and ingested into the helicopter's fenestron during takeoff, resulting in a loss of directional control.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Object/animal/substance: debris/dirt/foreign objectEnvironmental issues › Physical environment · Effect on equipmentAll aircraft: 101 casesProbable cause
Tail rotor: tail rotor bladeAircraft › Aircraft propeller/rotor · Damaged/degradedAll aircraft: 31 casesProbable cause
Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Attain/maintain not possibleAll aircraft: 3,958 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

After liftoff during a helicopter emergency medical service (HEMS) flight with a patient on board, the pilot of the HEMS helicopter brought it in to a 1 to 2 foot hover and was preparing to make a right pedal turn into the wind, when a cover from a wheeled fire extinguisher, was blown airborne by the main rotor wash and ingested into the tail rotor (fenestron) of the helicopter. The helicopter lost tail rotor authority and began to spin clockwise. The pilot lowered the collective and the helicopter rotated approximately 150 degrees, then impacted the ground and continued to rotate another 20 to 30 degrees, for a total of 170 to180 degree turn, and came to rest. Examination of the helicopter by a Federal Aviation Administration inspector revealed damage to the landing gear skid tubes, fenestron composite housing, and the forward cross tube gimbal which had pushed up into a composite non-structural area of the fuselage. It was discovered, that the wheeled fire extinguisher that the cover had blown off of, had been inspected for serviceability just four days prior to the accident.

Factual narrative

After liftoff during a helicopter emergency medical service (HEMS) flight with a patient on board, the pilot of the HEMS helicopter brought it in to a 1 to 2 foot hover and was preparing to make a right pedal turn into the wind, when a cover from a wheeled fire extinguisher, was blown airborne by the main rotor wash and ingested into the tail rotor (fenestron) of the helicopter. The helicopter lost tail rotor authority and began to spin clockwise. The pilot lowered the collective and the helicopter rotated approximately 150 degrees, then impacted the ground and continued to rotate another 20 to 30 degrees, for a total of 170 to180 degree turn, and came to rest. Examination of the helicopter by a Federal Aviation Administration inspector revealed damage to the landing gear skid tubes, fenestron composite housing, and the forward cross tube gimbal which had pushed up into a composite non-structural area of the fuselage. It was discovered, that the wheeled fire extinguisher that the cover had blown off of, had been inspected for serviceability just four days prior to the accident.

Aircraft

Registration
N639ME
Reported as
Eurocopter Deutschland EC 135 (T2)
Category
Helicopter
Serial number
0563
Built
2007
Airframe hours
5,110.2
Engines
Turbomeca ARRIUS 2B2, 634 horsepower, turbo shaftTurbomeca Arrius 2B2, 634 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 135
Operator
Center For Emergency Medicine Of Western
Registered owner
Center For Emergency Medicine Of Western
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · November 4, 2015
Departed
5PA5 · Monongahela, PA
Destination
78PA · Newtown Square, PA
Flight plan
Company VFR
Airport
5PA5 · Monongahela Valley Hospital
Equipment
Satellite tracking device, Auto-pilot, Electronic multifunction display, Onboard weather

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
55
Injuries
None
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 1, With waivers/limitations
Last flight review
May 28, 2015
Seat
Right
Restraint
4-point
Flight hours
4,413 total · 1,198 in this make and model · 2,663 as pilot in command · 82 in the last 90 days · 14 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Dawn
Wind
180° at 9 knots
Visibility
10 statute miles
Lowest ceiling
12,000 ft broken
Temperature
66 °F, dew point 52 °F
Altimeter
29.95 inHg
Observed at
KAGC, 10 nm away

Docket · 4

The files NTSB released with the investigation on January 8, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.5 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.