20000627034619I

Incident · Minor damage

FAA incident report · Bell 214ST · June 27, 2000

Date
June 27, 2000 · 10:10 local
Phase of flight
To Vertical (Helicopter Only)
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Damage
Minor damage
Aircraft
N59805
Reported as
Bell 214ST
People aboard
17
Fatal 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.

(-23)The flight crew felt a shutter and vibration from the aircraft shortly after takeoff from an offshore platform. The flight crew returned to the platform and landed without incident. Subsequent inspection of the aircraft revealed that one set of tail rotor counter weights were missing and one tail rotor blade had significant leading edge damage. Further evaluation that the counter weight bellcrank mounting stud on the tail rotor crosshead failed at the cotter pin hole. The failed crosshead was sent to the manufacture for engineering evaluation was corrdinated with the FAA rotorcraft certification office (ASW-170).

As the FAA filed it

(-23)THE FLIGHT CREW FELT A SHUTTER AND VIBRATION FROM THE AIRCRAFT SHORTLY AFTER TAKEOFF FROM AN OFFSHORE PLATFORM. THE FLIGHT CREW RETURNED TO THE PLATFORM AND LANDED WITHOUT INCIDENT. SUBSEQUENT INSPECTION OF THE AIRCRAFT REVEALED THAT ONE SET OF TAIL ROTOR COUNTER WEIGHTS WERE MISSING AND ONE TAIL ROTOR BLADE HAD SIGNIFICANT LEADING EDGE DAMAGE. FURTHER EVALUATION THAT THE COUNTER WEIGHT BELLCRANK MOUNTING STUD ON THE TAIL ROTOR CROSSHEAD FAILED AT THE COTTER PIN HOLE. THE FAILED CROSSHEAD WAS SENT TO THE MANUFACTURE FOR ENGINEERING EVALUATION WAS CORRDINATED WITH THE FAA ROTORCRAFT CERTIFICATION OFFICE (ASW-170).