19980830032099A

Accident · Substantial damage

FAA accident report · Amtr MINI500 · Hattiesburg, MS · August 30, 1998

Date
August 30, 1998 · 16:30 local
Place
Hattiesburg, MS
Airport
Bobby L Chain Municipal
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9GH
NTSB investigation
NTSBMIA98LA236
Reported as
Amtr MINI500
Reported engine
ROTAX ROTAX582
People aboard
1
Fatal injuries
0
Pilot’s flight hours
6,400 total1 in this make and model100 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.

On August 30, 1998, about 1500 central daylight time a hall revolution mini 500 homebuilt helicopter, N9GH, registered to an individual, landed hard at Hattiesburg, Mississippi, while on a title 14 CFR part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airline transpor-rated pilot was not injured and the helicopter received substantial damage. The flight was originating at the time of the accident. The pilot stated that as he hovered forward at a brick walk, he heard the low rotor RPM horn and reduced the collective control. The helicopter descended rapidly and touched down on the "toes" of the skids. The helicopter bounced back into the air and the cyclic control grip separated from the cyclic control stick. The cyclic control stick moved to the full aft position and the main rotor blades contacted the tail boom. (.4) the pilot stated that as he hovered forward at a brisk walk, he heard the low rotor RPM horn. He lowered the collective and the helicopter descended rapidly and touched down on the `toes' of the skids. The helicopter bounced back into the air and the cyclic control grip separated from the cyclic control stick. The cyclic control moved to the full aft position and the main rotor blades contacted the tail boom. (-23) pilot flew an unairworthy aircraft, did not have a registration certificate or airworthiness cert. On board aircraft. Builder removed identification plate and information on helicopter, operating limitations, maintenance log books, registration and airworthiness certificate.

As the FAA filed it

ON AUGUST 30, 1998, ABOUT 1500 CENTRAL DAYLIGHT TIME A HALL REVOLUTION MINI 500 HOMEBUILT HELICOPTER, N9GH, REGISTERED TO AN INDIVIDUAL, LANDED HARD AT HATTIESBURG, MISSISSIPPI, WHILE ON A TITLE 14 CFR PART 91 PERSONAL FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED. THE AIRLINE TRANSPOR-RATED PILOT WAS NOT INJURED AND THE HELICOPTER RECEIVED SUBSTANTIAL DAMAGE. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. THE PILOT STATED THAT AS HE HOVERED FORWARD AT A BRICK WALK, HE HEARD THE LOW ROTOR RPM HORN AND REDUCED THE COLLECTIVE CONTROL. THE HELICOPTER DESCENDED RAPIDLY AND TOUCHED DOWN ON THE "TOES" OF THE SKIDS. THE HELICOPTER BOUNCED BACK INTO THE AIR AND THE CYCLIC CONTROL GRIP SEPARATED FROM THE CYCLIC CONTROL STICK. THE CYCLIC CONTROL STICK MOVED TO THE FULL AFT POSITION AND THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM. (.4) THE PILOT STATED THAT AS HE HOVERED FORWARD AT A BRISK WALK, HE HEARD THE LOW ROTOR RPM HORN. HE LOWERED THE COLLECTIVE AND THE HELICOPTER DESCENDED RAPIDLY AND TOUCHED DOWN ON THE `TOES' OF THE SKIDS. THE HELICOPTER BOUNCED BACK INTO THE AIR AND THE CYCLIC CONTROL GRIP SEPARATED FROM THE CYCLIC CONTROL STICK. THE CYCLIC CONTROL MOVED TO THE FULL AFT POSITION AND THE MAIN ROTOR BLADES CONTACTED THE TAIL BOOM. (-23) PILOT FLEW AN UNAIRWORTHY AIRCRAFT, DID NOT HAVE A REGISTRATION CERTIFICATE OR AIRWORTHINESS CERT. ON BOARD AIRCRAFT. BUILDER REMOVED IDENTIFICATION PLATE AND INFORMATION ON HELICOPTER, OPERATING LIMITATIONS, MAINTENANCE LOG BOOKS, REGISTRATION AND AIRWORTHINESS CERTIFICATE.

NTSB investigation

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