20131126022059A

Accident · Substantial damage

FAA accident report · Quad City Ultralight Acft CHALLENGER II · Kalispell, MT · November 26, 2013

Date
November 26, 2013 · 09:45 local
Place
Kalispell, MT
Airport
Kalispell City Airport
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N522PE
NTSB investigation
NTSBWPR14CA058
Reported as
Quad City Ultralight Acft Challenger II
Reported engine
HIRTH 2706
People aboard
1
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.

Shortly after takeoff to the south, at about 200 feet AGL, the aircraft's engine failed to little or no power due to a spark plug exiting the aft cylinder of the two cylinder engine. The pilot attempted to land on a gravel road adjacent to the airport, but contacted a fence post with the right horizontal stabilizer. The pilot stated he had significant sun glare on the plexiglass windshield during the landing attempt. The sparkplug's steel threads had pulled the cylinder head's mating aluminum threads. The aircraft sustained damage to the landing gear, fuselage longerons and tail. The aircraft kit manufacturer and owner's association have a notification system for all owner/operators that disseminates technical service information. The failure of plug threads is a well known problem with this model of hirth engine. The plug's thread barrel is narrow and has a short reach which results in less thread contact. The manufacturer no longer offers the hirth engine as part of its kit.

As the FAA filed it

SHORTLY AFTER TAKEOFF TO THE SOUTH, AT ABOUT 200 FEET AGL, THE AIRCRAFT'S ENGINE FAILED TO LITTLE OR NO POWER DUE TO A SPARK PLUG EXITING THE AFT CYLINDER OF THE TWO CYLINDER ENGINE. THE PILOT ATTEMPTED TO LAND ON A GRAVEL ROAD ADJACENT TO THE AIRPORT, BUT CONTACTED A FENCE POST WITH THE RIGHT HORIZONTAL STABILIZER. THE PILOT STATED HE HAD SIGNIFICANT SUN GLARE ON THE PLEXIGLASS WINDSHIELD DURING THE LANDING ATTEMPT. THE SPARKPLUG'S STEEL THREADS HAD PULLED THE CYLINDER HEAD'S MATING ALUMINUM THREADS. THE AIRCRAFT SUSTAINED DAMAGE TO THE LANDING GEAR, FUSELAGE LONGERONS AND TAIL. THE AIRCRAFT KIT MANUFACTURER AND OWNER'S ASSOCIATION HAVE A NOTIFICATION SYSTEM FOR ALL OWNER/OPERATORS THAT DISSEMINATES TECHNICAL SERVICE INFORMATION. THE FAILURE OF PLUG THREADS IS A WELL KNOWN PROBLEM WITH THIS MODEL OF HIRTH ENGINE. THE PLUG'S THREAD BARREL IS NARROW AND HAS A SHORT REACH WHICH RESULTS IN LESS THREAD CONTACT. THE MANUFACTURER NO LONGER OFFERS THE HIRTH ENGINE AS PART OF ITS KIT.

NTSB investigation

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