19970826023989A

Accident · Substantial damage

FAA accident report · Amtr MINI 500 · Huffman, TX · August 26, 1997

Date
August 26, 1997 · 19:45 local
Place
Huffman, TX
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N570F
NTSB investigation
NTSBFTW97LA328
Reported as
Amtr MINI500
Reported engine
ROTAX ROTAX582
People aboard
1
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
50 total28 in this make and model22 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.

Collective disconnect. Damaged on run on log. Failed preflite collective used incorrect control inputs. Unskilled. (-23) see narrative #FTW97LA320 (.19) on August 26, 1997, at 1945 central daylight time, a fingerhut revolution mini 500 homebuilt helicopter, N570F, was substantially damaged during a forced landing near Huffman, Texas. The student pilot, sole occupant of the helicopter, was not injured. The helicopter was owned and operated by the pilot under title 14 CFR part 91. Visual meteorological conditions prevailed for the local flight for which a flight plan was not filed. The instructional flight originated from a helipad at the pilot's home in Huffman, Texas at 1915. According to the pilot, he experienced an intermittent disconnect of the collective control system which resulted in the main rotor blades going to flat pitch while in cruise flight. The pilot added that he elected to execute a running landing to a cultivated field rather than try to land in a confined helipad. During the landing flare the helicopter yawed to the left as the pilot applied collective to flare prior to touching down. T he pilot added that the helicopter was not properly aligned during touch down and the helicopter rolled over on its side. The FAA inspector confirmed that the 1997 model helicopter sustained structural damage. He added that the student pilot was properly endorse for solo flight and had accumulated a total of 50 hours of flight in helicopters, of which 28 were in the same make and model.

As the FAA filed it

COLLECTIVE DISCONNECT. DAMAGED ON RUN ON LOG. FAILED PREFLITE COLLECTIVE USED INCORRECT CONTROL INPUTS. UNSKILLED. (-23) SEE NARRATIVE #FTW97LA320 (.19) ON AUGUST 26, 1997, AT 1945 CENTRAL DAYLIGHT TIME, A FINGERHUT REVOLUTION MINI 500 HOMEBUILT HELICOPTER, N570F, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING NEAR HUFFMAN, TEXAS. THE STUDENT PILOT, SOLE OCCUPANT OF THE HELICOPTER, WAS NOT INJURED. THE HELICOPTER WAS OWNED AND OPERATED BY THE PILOT UNDER TITLE 14 CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE LOCAL FLIGHT FOR WHICH A FLIGHT PLAN WAS NOT FILED. THE INSTRUCTIONAL FLIGHT ORIGINATED FROM A HELIPAD AT THE PILOT'S HOME IN HUFFMAN, TEXAS AT 1915. ACCORDING TO THE PILOT, HE EXPERIENCED AN INTERMITTENT DISCONNECT OF THE COLLECTIVE CONTROL SYSTEM WHICH RESULTED IN THE MAIN ROTOR BLADES GOING TO FLAT PITCH WHILE IN CRUISE FLIGHT. THE PILOT ADDED THAT HE ELECTED TO EXECUTE A RUNNING LANDING TO A CULTIVATED FIELD RATHER THAN TRY TO LAND IN A CONFINED HELIPAD. DURING THE LANDING FLARE THE HELICOPTER YAWED TO THE LEFT AS THE PILOT APPLIED COLLECTIVE TO FLARE PRIOR TO TOUCHING DOWN. T HE PILOT ADDED THAT THE HELICOPTER WAS NOT PROPERLY ALIGNED DURING TOUCH DOWN AND THE HELICOPTER ROLLED OVER ON ITS SIDE. THE FAA INSPECTOR CONFIRMED THAT THE 1997 MODEL HELICOPTER SUSTAINED STRUCTURAL DAMAGE. HE ADDED THAT THE STUDENT PILOT WAS PROPERLY ENDORSE FOR SOLO FLIGHT AND HAD ACCUMULATED A TOTAL OF 50 HOURS OF FLIGHT IN HELICOPTERS, OF WHICH 28 WERE IN THE SAME MAKE AND MODEL.

NTSB investigation

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