20240814010749I

Incident · Substantial damage

FAA incident report · Hood Tech Corp Mechanical HTMC-40-PLUS · Pendleton, OR · August 14, 2024

Date
August 14, 2024 · 14:35 local
Place
Pendleton, OR
Airport
Eastern Oregon Regional Airpor
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N60MC
Reported as
Hood Tech Corp Mechanical HTMC-40-PLUS
People aboard
2
Fatal injuries
0
Other 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.

A GPS failure during a maritime flares UAS training event triggered land mode, which resulted in steady descent and downwind drift of the multi-copter. The aircraft was tethered to an articulating and translating flatbed trailer (ship deck simulator). The operator is aft-facing from the back door of the tow vehicle.

The student operator’s initial joystick response to the GPS failure was correct. Then the aircraft veered off-course and out of sight. It impacted the surface, climbed above 100 feet AGL overturned and impacted a second time. Substantial damage resulted. No personnel injuries or fire was observed.

Root cause: a fatigued wire crimp failed, which cut power to the GPS receiver. Subsequent operator input caused loss of control and ground impact.

As the FAA filed it

A GPS FAILURE DURING A MARITIME FLARES UAS TRAINING EVENT TRIGGERED LAND MODE, WHICH RESULTED IN STEADY DESCENT AND DOWNWIND DRIFT OF THE MULTI-COPTER. THE AIRCRAFT WAS TETHERED TO AN ARTICULATING AND TRANSLATING FLATBED TRAILER (SHIP DECK SIMULATOR). THE OPERATOR IS AFT-FACING FROM THE BACK DOOR OF THE TOW VEHICLE.

THE STUDENT OPERATOR’S INITIAL JOYSTICK RESPONSE TO THE GPS FAILURE WAS CORRECT. THEN THE AIRCRAFT VEERED OFF-COURSE AND OUT OF SIGHT. IT IMPACTED THE SURFACE, CLIMBED ABOVE 100 FEET AGL OVERTURNED AND IMPACTED A SECOND TIME. SUBSTANTIAL DAMAGE RESULTED. NO PERSONNEL INJURIES OR FIRE WAS OBSERVED.

ROOT CAUSE: A FATIGUED WIRE CRIMP FAILED, WHICH CUT POWER TO THE GPS RECEIVER. SUBSEQUENT OPERATOR INPUT CAUSED LOSS OF CONTROL AND GROUND IMPACT.