20110325004879A

Accident · Substantial damage

FAA accident report · Hiller UH-12E · Culpepper, VA · March 25, 2011

Date
March 25, 2011 · 12:00 local
Place
Culpepper, VA
Phase of flight
Landing: Approach
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N4033P
NTSB investigation
NTSBERA11LA216
Reported as
Hiller UH-12E
Reported engine
Lycoming VO-540 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
12,382 total1,500 in this make and model7 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.

Upon arriving at the job site to begin aerial application the pilot noted an uncommanded increase in engine RPM accompanied by a loss of lift. He reduced collective in an attempt to preserve rotor RPM and initiated auto rotation. There was insufficient rotor energy and altitude (approximately 150 to 200 feet AGL) to cushion the landing. The helicopter struck the ground and suffered substantial damage. One main rotor blade severed the tail boom and the other rotor blade struck the ground causing substantial damage to both main rotor blades. The pilot shut the engine down after impacting the ground. The pilot was not injured and there was no other property damage. The NTSB, insurance company, and Hiller aircraft corporation have declined to teardown the engine and transmission assembly to determine the cause.

As the FAA filed it

UPON ARRIVING AT THE JOB SITE TO BEGIN AERIAL APPLICATION THE PILOT NOTED AN UNCOMMANDED INCREASE IN ENGINE RPM ACCOMPANIED BY A LOSS OF LIFT. HE REDUCED COLLECTIVE IN AN ATTEMPT TO PRESERVE ROTOR RPM AND INITIATED AUTO ROTATION. THERE WAS INSUFFICIENT ROTOR ENERGY AND ALTITUDE (APPROXIMATELY 150 TO 200 FEET AGL) TO CUSHION THE LANDING. THE HELICOPTER STRUCK THE GROUND AND SUFFERED SUBSTANTIAL DAMAGE. ONE MAIN ROTOR BLADE SEVERED THE TAIL BOOM AND THE OTHER ROTOR BLADE STRUCK THE GROUND CAUSING SUBSTANTIAL DAMAGE TO BOTH MAIN ROTOR BLADES. THE PILOT SHUT THE ENGINE DOWN AFTER IMPACTING THE GROUND. THE PILOT WAS NOT INJURED AND THERE WAS NO OTHER PROPERTY DAMAGE. THE NTSB, INSURANCE COMPANY, AND HILLER AIRCRAFT CORPORATION HAVE DECLINED TO TEARDOWN THE ENGINE AND TRANSMISSION ASSEMBLY TO DETERMINE THE CAUSE.

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 N4033P · 2

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