20011003027359A

Accident · Substantial damage

FAA accident report · Amtr Genesis · Grants, NM · October 3, 2001

Date
October 3, 2001 · 12:20 local
Place
Grants, NM
Airport
Grants-Milan Municipal Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N715MP
NTSB investigation
NTSBFTW02LA002
Reported as
Amtr Genesis
Reported engine
ROTAX ROTAX618
Fatal injuries
0

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.

(.19) On October 3, 2001, at 1220 mountain daylight time, a hamilton Genesis, experimental homebuilt airplane, N715MP, impacted the terrain following a loss of engine power near Grants, new Mexico. The airplane was owned and operated by the pilot under code of federal regulations part 91. The private pilot, sole occupant, received minor injuries, and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the planned cross-country flight, and a flight plan was not filed. The flight departed Grants at 1815. (-23) on 10/03/01, at approximately 1220 MDT, N715MP, an experimental inovation gensis, on departure from the Grants-Milan airport, Grants, new Mexico, experienced a loss of power, thus impacting the terrain approximately 3.5 NM nw of the Grants-Milan airport. The private pilot was the sole occupant of the aircraft and received a broken tail bone as a result of the accident. The aircraft was substantially damaged. The flight was conducted under VMC conditions and a flight plan was not filed. (.4) the experimental homebuilt airplane impacted terrain following a partial loss of engine power during the climb to cruise over rough terrain. The throttle cable movement was 1/2-inch in the engine compartment when the throttle control was full forward in the cockpit. The airplane had not been flown in several months, and had not received a condition inspection in over a year. Numerous attempts to obtain a completed pilot/operator aircraft accident report (NTSB form 6120.1/2) were unsuccessful.

As the FAA filed it

(.19) ON OCTOBER 3, 2001, AT 1220 MOUNTAIN DAYLIGHT TIME, A HAMILTON GENESIS, EXPERIMENTAL HOMEBUILT AIRPLANE, N715MP, IMPACTED THE TERRAIN FOLLOWING A LOSS OF ENGINE POWER NEAR GRANTS, NEW MEXICO. THE AIRPLANE WAS OWNED AND OPERATED BY THE PILOT UNDER CODE OF FEDERAL REGULATIONS PART 91. THE PRIVATE PILOT, SOLE OCCUPANT, RECEIVED MINOR INJURIES, AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PLANNED CROSS-COUNTRY FLIGHT, AND A FLIGHT PLAN WAS NOT FILED. THE FLIGHT DEPARTED GRANTS AT 1815. (-23) ON 10/03/01, AT APPROXIMATELY 1220 MDT, N715MP, AN EXPERIMENTAL INOVATION GENSIS, ON DEPARTURE FROM THE GRANTS-MILAN AIRPORT, GRANTS, NEW MEXICO, EXPERIENCED A LOSS OF POWER, THUS IMPACTING THE TERRAIN APPROXIMATELY 3.5 NM NW OF THE GRANTS-MILAN AIRPORT. THE PRIVATE PILOT WAS THE SOLE OCCUPANT OF THE AIRCRAFT AND RECEIVED A BROKEN TAIL BONE AS A RESULT OF THE ACCIDENT. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED. THE FLIGHT WAS CONDUCTED UNDER VMC CONDITIONS AND A FLIGHT PLAN WAS NOT FILED. (.4) THE EXPERIMENTAL HOMEBUILT AIRPLANE IMPACTED TERRAIN FOLLOWING A PARTIAL LOSS OF ENGINE POWER DURING THE CLIMB TO CRUISE OVER ROUGH TERRAIN. THE THROTTLE CABLE MOVEMENT WAS 1/2-INCH IN THE ENGINE COMPARTMENT WHEN THE THROTTLE CONTROL WAS FULL FORWARD IN THE COCKPIT. THE AIRPLANE HAD NOT BEEN FLOWN IN SEVERAL MONTHS, AND HAD NOT RECEIVED A CONDITION INSPECTION IN OVER A YEAR. NUMEROUS ATTEMPTS TO OBTAIN A COMPLETED PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT (NTSB FORM 6120.1/2) WERE UNSUCCESSFUL.

NTSB investigation

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