20070525009559A

Accident · Destroyed

FAA accident report · Amtr SKYGEAR · Chino, CA · May 25, 2007

Date
May 25, 2007 · 13:27 local
Place
Chino, CA
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N51291
NTSB investigation
NTSBLAX07LA175
Reported as
Amtr Skygear
People aboard
1
Fatal injuries
1
Pilot’s flight hours
12,000 total8 in this make and model4 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) Shortly after take off, the aircraft crashed on airport property. The aircraft took off from cno rwy 26R for right closed traffic. At @ 30 seconds into the flight, the aircraft gained an altitude of 500 ft (based on the aircraft's performance charts). Weather was clear with winds out of 270 at 7 knots with gusts to 16. As the pilot made a right turn over the airfield, the aircraft experienced empennage flutter, which led to a loss in directional control, then a drastic shift in center of gravity (CG). The aircraft rolled 180 degrees and impacted a lawn 10 feet north of bldg. A-503 (near intersection of merrill and bow ave). At impact, a tool box and a bench vise ejected from the aircraft. Investigation of the aircraft revealed that the support struts for the horizontal to vertical stabilizer were missing. The son of the pilot stated that his father removed the struts the day before the crash. The aircraft was the first of a new model for Skygear, inc. (si) the aircraft was manufactured in china and imported into the united states by the pilot, who was the owner of si.

As the FAA filed it

(-23) SHORTLY AFTER TAKE OFF, THE AIRCRAFT CRASHED ON AIRPORT PROPERTY. THE AIRCRAFT TOOK OFF FROM CNO RWY 26R FOR RIGHT CLOSED TRAFFIC. AT @ 30 SECONDS INTO THE FLIGHT, THE AIRCRAFT GAINED AN ALTITUDE OF 500 FT (BASED ON THE AIRCRAFT'S PERFORMANCE CHARTS). WEATHER WAS CLEAR WITH WINDS OUT OF 270 AT 7 KNOTS WITH GUSTS TO 16. AS THE PILOT MADE A RIGHT TURN OVER THE AIRFIELD, THE AIRCRAFT EXPERIENCED EMPENNAGE FLUTTER, WHICH LED TO A LOSS IN DIRECTIONAL CONTROL, THEN A DRASTIC SHIFT IN CENTER OF GRAVITY (CG). THE AIRCRAFT ROLLED 180 DEGREES AND IMPACTED A LAWN 10 FEET NORTH OF BLDG. A-503 (NEAR INTERSECTION OF MERRILL AND BOW AVE). AT IMPACT, A TOOL BOX AND A BENCH VISE EJECTED FROM THE AIRCRAFT. INVESTIGATION OF THE AIRCRAFT REVEALED THAT THE SUPPORT STRUTS FOR THE HORIZONTAL TO VERTICAL STABILIZER WERE MISSING. THE SON OF THE PILOT STATED THAT HIS FATHER REMOVED THE STRUTS THE DAY BEFORE THE CRASH. THE AIRCRAFT WAS THE FIRST OF A NEW MODEL FOR SKYGEAR, INC. (SI) THE AIRCRAFT WAS MANUFACTURED IN CHINA AND IMPORTED INTO THE UNITED STATES BY THE PILOT, WHO WAS THE OWNER OF SI.

NTSB investigation

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