20180104006179I

Incident · Minor damage

FAA incident report · Bell Helicopter Textron Canada 407 · Norfolk, NE · January 4, 2018

Date
January 4, 2018 · 20:20 local
Place
Norfolk, NE
Phase of flight
Landing: Approach
Operating rules
Air taxi and commuter (Part 135)
Operator
QMLA
Damage
Minor damage
Aircraft
N214AM
NTSB investigation
NTSBCEN18CA072
Reported as
Bell Helicopter Textron Canada 407
Reported engine
Rolls-Royce 250-C47B
People aboard
3
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
10,030 total202 in this make and model16 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.

The pilot and two medical crewmembers were on a return flight to a hospital helipad. During the approach to the helipad, the crew heard a noise outside the helicopter. The medical crewmembers

Reported they felt a "shudder", believing it to be wind as they

Approached the helipad. The pilot heard the noise, but there was no effect on the controls or flight

Characteristics. He continued the approach and landed without incident. After engine shutdown, the

On coming pilot noticed the helicopter's tail rotor drive shaft cover missing. A search of the

Surrounding area near the helicopter's approach path, located the missing cover.

An examination of the helicopter noted damage to the tail rotor (t/r) drive shaft. The t/rs were struck during the cover departure from the aircraft, leaving dents in the t/r leading edges.

The day prior to the incident, scheduled maintenance was performed on the helicopter's tail rotor

Pitch change mechanism, which required removal of the drive shaft cover. The cover was reinstalled, and no problems were reported during a subsequent pre-flight inspection.

As the FAA filed it

THE PILOT AND TWO MEDICAL CREWMEMBERS WERE ON A RETURN FLIGHT TO A HOSPITAL HELIPAD. DURING THE APPROACH TO THE HELIPAD, THE CREW HEARD A NOISE OUTSIDE THE HELICOPTER. THE MEDICAL CREWMEMBERS

REPORTED THEY FELT A "SHUDDER", BELIEVING IT TO BE WIND AS THEY

APPROACHED THE HELIPAD. THE PILOT HEARD THE NOISE, BUT THERE WAS NO EFFECT ON THE CONTROLS OR FLIGHT

CHARACTERISTICS. HE CONTINUED THE APPROACH AND LANDED WITHOUT INCIDENT. AFTER ENGINE SHUTDOWN, THE

ON COMING PILOT NOTICED THE HELICOPTER'S TAIL ROTOR DRIVE SHAFT COVER MISSING. A SEARCH OF THE

SURROUNDING AREA NEAR THE HELICOPTER'S APPROACH PATH, LOCATED THE MISSING COVER.

AN EXAMINATION OF THE HELICOPTER NOTED DAMAGE TO THE TAIL ROTOR (T/R) DRIVE SHAFT. THE T/RS WERE STRUCK DURING THE COVER DEPARTURE FROM THE AIRCRAFT, LEAVING DENTS IN THE T/R LEADING EDGES.

THE DAY PRIOR TO THE INCIDENT, SCHEDULED MAINTENANCE WAS PERFORMED ON THE HELICOPTER'S TAIL ROTOR

PITCH CHANGE MECHANISM, WHICH REQUIRED REMOVAL OF THE DRIVE SHAFT COVER. THE COVER WAS REINSTALLED, AND NO PROBLEMS WERE REPORTED DURING A SUBSEQUENT PRE-FLIGHT INSPECTION.

NTSB investigation

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