20160828015409I

Incident · Minor damage

FAA incident report · Hart Larry T RANS 6ES COYOTE II · Newton, KS · August 28, 2016

Date
August 28, 2016 · 08:00 local
Place
Newton, KS
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N614JS
Reported as
Hart Larry T Rans 6ES Coyote II
Reported engine
ROTAX 912
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
128 total24 in this make and model14 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.

The pilotprivacy data omittedwas landing on his private grass runway. During the ground roll out, before the tailwheel had touched down, the aircraft nosed over striking and breaking both blades of the wooden propeller and bending the left lower cowling inward. The aircraft then came down on the tailwheel and stopped. The engine mount and firewall were undamaged and showed no evidence of impact. The pilot stated that the aircraft suddenly slowed prior to the propeller strike.

The pilot privacy data omitted stated that during the post incident recovery of the aircraft the left landing gear leg tube was loose where it connected to the fuselage. Upon inspection the leg was broken inside the fuselage gear mount.

As the FAA filed it

THE PILOT^PRIVACY DATA OMITTED^WAS LANDING ON HIS PRIVATE GRASS RUNWAY. DURING THE GROUND ROLL OUT, BEFORE THE TAILWHEEL HAD TOUCHED DOWN, THE AIRCRAFT NOSED OVER STRIKING AND BREAKING BOTH BLADES OF THE WOODEN PROPELLER AND BENDING THE LEFT LOWER COWLING INWARD. THE AIRCRAFT THEN CAME DOWN ON THE TAILWHEEL AND STOPPED. THE ENGINE MOUNT AND FIREWALL WERE UNDAMAGED AND SHOWED NO EVIDENCE OF IMPACT. THE PILOT STATED THAT THE AIRCRAFT SUDDENLY SLOWED PRIOR TO THE PROPELLER STRIKE.

THE PILOT ^PRIVACY DATA OMITTED^ STATED THAT DURING THE POST INCIDENT RECOVERY OF THE AIRCRAFT THE LEFT LANDING GEAR LEG TUBE WAS LOOSE WHERE IT CONNECTED TO THE FUSELAGE. UPON INSPECTION THE LEG WAS BROKEN INSIDE THE FUSELAGE GEAR MOUNT.

Other reports on N614JS · 1

Matched to the same aircraft by N-number and date.