20150716014379A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R44 II · Fentress, TX · July 16, 2015

Date
July 16, 2015 · 20:30 local
Place
Fentress, TX
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N804DF
NTSB investigation
NTSBGAA15CA232
Reported as
Robinson Helicopter R44 II
Reported engine
Continental IO-540 series
People aboard
3
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
6,750 total1,745 in this make and model72 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.

After conducting a downwind manuvering turn the low rotor RPM alert came on. Due to low altitude the pilot was unable to recover and made a hard landing from 20-25 feet.

The pilot exited the helicopter (with engine running) to inspect for damage. He noticed skin wrinkling above the rear struts.

The pilot then flew the aircraft (with passengers aboard) to his hangar approximately 5 miles distance. After engine shut down he noticed substantial damage to both main and tail rotor blades.

As the FAA filed it

AFTER CONDUCTING A DOWNWIND MANUVERING TURN THE LOW ROTOR RPM ALERT CAME ON. DUE TO LOW ALTITUDE THE PILOT WAS UNABLE TO RECOVER AND MADE A HARD LANDING FROM 20-25 FEET.

THE PILOT EXITED THE HELICOPTER (WITH ENGINE RUNNING) TO INSPECT FOR DAMAGE. HE NOTICED SKIN WRINKLING ABOVE THE REAR STRUTS.

THE PILOT THEN FLEW THE AIRCRAFT (WITH PASSENGERS ABOARD) TO HIS HANGAR APPROXIMATELY 5 MILES DISTANCE. AFTER ENGINE SHUT DOWN HE NOTICED SUBSTANTIAL DAMAGE TO BOTH MAIN AND TAIL ROTOR BLADES.

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 N804DF · 2

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