20030412004569A

Accident · Substantial damage

FAA accident report · Amtr AC-5M · Richland, WA · April 12, 2003

Date
April 12, 2003 · 16:00 local
Place
Richland, WA
Airport
Richland Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N125MZ
NTSB investigation
NTSBSEA03LA061
Reported as
Amtr AC5M
People aboard
1
Fatal injuries
0
Pilot’s flight hours
38 total7 in this make and model2 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.

(-23) Aircraft departed runway 01 krld, lost thrust at about 100 feet AGL. Pilot attempted turn to land on cross runway, but lost altitude and struck right wingtip on surface during turn, then struck ground in a medium rate of descent. Aircraft is a powered (self-launching) glider, certificated as experimental/exhibition. Propeller is driven by a twin belt system, with belt tension adjusted by an eccentric mount that also anchors propeller hub. Eccentric is retained by a pinch bolt system. On accident flight, eccentric is believed to have slipped, resulting in loss of drive belt tension and loss of thrust. This deficiency is believed to be a relatively well-known problem for this model of aircraft.

As the FAA filed it

(-23) AIRCRAFT DEPARTED RUNWAY 01 KRLD, LOST THRUST AT ABOUT 100 FEET AGL. PILOT ATTEMPTED TURN TO LAND ON CROSS RUNWAY, BUT LOST ALTITUDE AND STRUCK RIGHT WINGTIP ON SURFACE DURING TURN, THEN STRUCK GROUND IN A MEDIUM RATE OF DESCENT. AIRCRAFT IS A POWERED (SELF-LAUNCHING) GLIDER, CERTIFICATED AS EXPERIMENTAL/EXHIBITION. PROPELLER IS DRIVEN BY A TWIN BELT SYSTEM, WITH BELT TENSION ADJUSTED BY AN ECCENTRIC MOUNT THAT ALSO ANCHORS PROPELLER HUB. ECCENTRIC IS RETAINED BY A PINCH BOLT SYSTEM. ON ACCIDENT FLIGHT, ECCENTRIC IS BELIEVED TO HAVE SLIPPED, RESULTING IN LOSS OF DRIVE BELT TENSION AND LOSS OF THRUST. THIS DEFICIENCY IS BELIEVED TO BE A RELATIVELY WELL-KNOWN PROBLEM FOR THIS MODEL OF AIRCRAFT.

NTSB investigation

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