19980702026859A

Accident · Substantial damage

FAA accident report · Amtr AVID MARK IV · Couer Dalene, ID · July 2, 1998

Date
July 2, 1998 · 12:45 local
Place
Couer Dalene, ID
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4353D
NTSB investigation
NTSBSEA98LA115
Reported as
Amtr Avidmarkiv
Reported engine
ROTAX ROTAX582
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,500 total20 in this make and model25 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.

(.4)The pilot reported that after the airplane lifted off from the water, he initiated a left turn at approximately 300 to 500 feet above water level. The pilot stated that he barely applied pressure to the stick for the left turn when the next thing he remembered was the aircraft going into the water at a 45 degree angle. The pilot stated that he felt that he had adequate airspeed and altitude when he entered the turn, but could not say if it was a control problem or a stall. Inspection of the flight controls, after the accident, did not reveal evidence of a control malfunction. (-23) during climbout from lake coeur d'lane, Idaho, pilot lost control of the aircraft as he started to execute a left turn. Aircraft impacted the water nose first and was substantially damaged. Pilot stated that the aircraft and engine were performing normally before the accident. Pilot escaped with minor injuries. The last recorded condition inspection was 12/12/97 at 122.8 hours total time. The aircraft wreckage is presently being inspected for possible flight control, (flaperon), failure. It has been reported by other owners of this type of aircraft that actuation of the flaperons will CA use a nose down attitude. Followup: post accident investigation of the aricraft wreckage did not reveal evidence of flight control malfunction.

As the FAA filed it

(.4)THE PILOT REPORTED THAT AFTER THE AIRPLANE LIFTED OFF FROM THE WATER, HE INITIATED A LEFT TURN AT APPROXIMATELY 300 TO 500 FEET ABOVE WATER LEVEL. THE PILOT STATED THAT HE BARELY APPLIED PRESSURE TO THE STICK FOR THE LEFT TURN WHEN THE NEXT THING HE REMEMBERED WAS THE AIRCRAFT GOING INTO THE WATER AT A 45 DEGREE ANGLE. THE PILOT STATED THAT HE FELT THAT HE HAD ADEQUATE AIRSPEED AND ALTITUDE WHEN HE ENTERED THE TURN, BUT COULD NOT SAY IF IT WAS A CONTROL PROBLEM OR A STALL. INSPECTION OF THE FLIGHT CONTROLS, AFTER THE ACCIDENT, DID NOT REVEAL EVIDENCE OF A CONTROL MALFUNCTION. (-23) DURING CLIMBOUT FROM LAKE COEUR D'LANE, IDAHO, PILOT LOST CONTROL OF THE AIRCRAFT AS HE STARTED TO EXECUTE A LEFT TURN. AIRCRAFT IMPACTED THE WATER NOSE FIRST AND WAS SUBSTANTIALLY DAMAGED. PILOT STATED THAT THE AIRCRAFT AND ENGINE WERE PERFORMING NORMALLY BEFORE THE ACCIDENT. PILOT ESCAPED WITH MINOR INJURIES. THE LAST RECORDED CONDITION INSPECTION WAS 12/12/97 AT 122.8 HOURS TOTAL TIME. THE AIRCRAFT WRECKAGE IS PRESENTLY BEING INSPECTED FOR POSSIBLE FLIGHT CONTROL, (FLAPERON), FAILURE. IT HAS BEEN REPORTED BY OTHER OWNERS OF THIS TYPE OF AIRCRAFT THAT ACTUATION OF THE FLAPERONS WILL CA USE A NOSE DOWN ATTITUDE. FOLLOWUP: POST ACCIDENT INVESTIGATION OF THE ARICRAFT WRECKAGE DID NOT REVEAL EVIDENCE OF FLIGHT CONTROL MALFUNCTION.

NTSB investigation

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

Other reports on N4353D · 1

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