20150811016529A

Accident · Substantial damage

FAA accident report · Bell 47D1 · Clanton, AL · August 11, 2015

Date
August 11, 2015 · 14:45 local
Place
Clanton, AL
Airport
Chilton County Airport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N74823
NTSB investigation
NTSBGAA15CA221
Reported as
Bell 47D1
Reported engine
Franklin 6V4 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
6,328 total498 in this make and model24 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.

08/11/2015 1500 Local time winds were observed as 340 at 10 KTS. Student pilot was manipulating the controls of N74823 a Bell 47D1 on final terminating with a 3 foot hover when the aircraft began to settle rapidly with aft movement. CFI kenneth lee gilliland initiated control input override. The aircraft landing gear contacted runway 26 approximately 220 ft beyond the threshold on the centerline. The red main rotor blade flexed making contact with the tail boom causing the wood blade to separate and depart the spar. The CFI immediately initiated engine shut down. The rotating imbalance caused the transmission to break mounts and engine began to break apart. Both crew exited the aircraft uninjured.

Couselling was completed on 8/18/2015.

As the FAA filed it

08/11/2015 1500 LOCAL TIME WINDS WERE OBSERVED AS 340 AT 10 KTS. STUDENT PILOT WAS MANIPULATING THE CONTROLS OF N74823 A BELL 47D1 ON FINAL TERMINATING WITH A 3 FOOT HOVER WHEN THE AIRCRAFT BEGAN TO SETTLE RAPIDLY WITH AFT MOVEMENT. CFI KENNETH LEE GILLILAND INITIATED CONTROL INPUT OVERRIDE. THE AIRCRAFT LANDING GEAR CONTACTED RUNWAY 26 APPROXIMATELY 220 FT BEYOND THE THRESHOLD ON THE CENTERLINE. THE RED MAIN ROTOR BLADE FLEXED MAKING CONTACT WITH THE TAIL BOOM CAUSING THE WOOD BLADE TO SEPARATE AND DEPART THE SPAR. THE CFI IMMEDIATELY INITIATED ENGINE SHUT DOWN. THE ROTATING IMBALANCE CAUSED THE TRANSMISSION TO BREAK MOUNTS AND ENGINE BEGAN TO BREAK APART. BOTH CREW EXITED THE AIRCRAFT UNINJURED.

COUSELLING WAS COMPLETED ON 8/18/2015.

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 N74823 · 1

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