20110829020209A

Accident · Substantial damage

FAA accident report · Enstrom F-28F · Menominee, MI · August 29, 2011

Date
August 29, 2011 · 13:15 local
Place
Menominee, MI
Airport
Menominee-Marinette Twin Count
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N228F
NTSB investigation
NTSBCEN11CA638
Reported as
Enstrom F-28F
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
2,200 total152 in this make and model31 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.

According to the pilot, the purpose of the company test flight was to measure collective stick forces with the collective bias disabled. The pilot, who was the helicopter's only occupant, lifted the helicopter into a hover and then hovered clear of any obstacles. He reported the collective controls were heavy as expected, but the helicopter was very controllable. During his attempt to position a force gauge between his hand and the collective grip, the pilot lost control of the helicopter and it landed hard onto the ramp. The helicopter's tail rotor blades impacted the ramp and the helicopter came to rest upright. Post-accident examination of the helicopter showed the tail rotor blades were bent and the tail rotor drive shaft was sheared. The pilot reported he should have taken an observer or other personnel on the flight to assist while he concentrated on flying the helicopter.

As the FAA filed it

ACCORDING TO THE PILOT, THE PURPOSE OF THE COMPANY TEST FLIGHT WAS TO MEASURE COLLECTIVE STICK FORCES WITH THE COLLECTIVE BIAS DISABLED. THE PILOT, WHO WAS THE HELICOPTER'S ONLY OCCUPANT, LIFTED THE HELICOPTER INTO A HOVER AND THEN HOVERED CLEAR OF ANY OBSTACLES. HE REPORTED THE COLLECTIVE CONTROLS WERE HEAVY AS EXPECTED, BUT THE HELICOPTER WAS VERY CONTROLLABLE. DURING HIS ATTEMPT TO POSITION A FORCE GAUGE BETWEEN HIS HAND AND THE COLLECTIVE GRIP, THE PILOT LOST CONTROL OF THE HELICOPTER AND IT LANDED HARD ONTO THE RAMP. THE HELICOPTER'S TAIL ROTOR BLADES IMPACTED THE RAMP AND THE HELICOPTER CAME TO REST UPRIGHT. POST-ACCIDENT EXAMINATION OF THE HELICOPTER SHOWED THE TAIL ROTOR BLADES WERE BENT AND THE TAIL ROTOR DRIVE SHAFT WAS SHEARED. THE PILOT REPORTED HE SHOULD HAVE TAKEN AN OBSERVER OR OTHER PERSONNEL ON THE FLIGHT TO ASSIST WHILE HE CONCENTRATED ON FLYING THE HELICOPTER.

NTSB investigation

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