20070901021709A

Accident · Substantial damage

FAA accident report · Amtr VORTEX · Mesa, AZ · September 1, 2007

Date
September 1, 2007 · 15:46 local
Place
Mesa, AZ
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N546SW
NTSB investigation
NTSBLAX07CA262
Reported as
Amtr Vortex
People aboard
1
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.

(-23) While operating in the Mesa, AZ area on a pleasure flight, the aircraft made a loud noise and began vibrating violently, at the same time losing thrust. The pilot reduced power, set up for best glide @ 50 mph, and executed an emergency landing in a dry river bed off airport. The rotor and landing gear contacted high sage brush, causing the aircraft to roll over. The pilot (the sole occupant) exited the aircraft safely without injury. The aircraft sustained substantial damage when it rolled over. Investigation revealed that an engine exhaust clamp, located directly in front of the propeller, had failed and gone through the composite propeller. As a consequence, one blade of the three-bladed propeller broke off, causing the vibration and loss of thrust.

As the FAA filed it

(-23) WHILE OPERATING IN THE MESA, AZ AREA ON A PLEASURE FLIGHT, THE AIRCRAFT MADE A LOUD NOISE AND BEGAN VIBRATING VIOLENTLY, AT THE SAME TIME LOSING THRUST. THE PILOT REDUCED POWER, SET UP FOR BEST GLIDE @ 50 MPH, AND EXECUTED AN EMERGENCY LANDING IN A DRY RIVER BED OFF AIRPORT. THE ROTOR AND LANDING GEAR CONTACTED HIGH SAGE BRUSH, CAUSING THE AIRCRAFT TO ROLL OVER. THE PILOT (THE SOLE OCCUPANT) EXITED THE AIRCRAFT SAFELY WITHOUT INJURY. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE WHEN IT ROLLED OVER. INVESTIGATION REVEALED THAT AN ENGINE EXHAUST CLAMP, LOCATED DIRECTLY IN FRONT OF THE PROPELLER, HAD FAILED AND GONE THROUGH THE COMPOSITE PROPELLER. AS A CONSEQUENCE, ONE BLADE OF THE THREE-BLADED PROPELLER BROKE OFF, CAUSING THE VIBRATION AND LOSS OF THRUST.

NTSB investigation

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