19990829042389A

Accident · Substantial damage

FAA accident report · Conaer LA4200 · Winter Haven, FL · August 29, 1999

Date
August 29, 1999 · 10:00 local
Place
Winter Haven, FL
Airport
Winter Haven'S Gilbert Airport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8002H
NTSB investigation
NTSBMIA99LA241
Reported as
Conaer LA4200
Reported engine
Lycoming IO360A1B
People aboard
2
Fatal injuries
2
Pilot’s flight hours
13,000 total160 in this make and model200 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) While performing step taxi, the left hand sponsor dug into the water causing the a/c to spin 180 degrees at a high rate of speed. Both sponsors broke off, there was no damage to the right flap, aileron and wing spar. The fuselage wrinkled due to hydraulic action. There were no injuries. (-4)the flight had landed on the lake after the pilots had been practicing landings and takeoffs. While attempting a water take off in a left step turn the bow was allowed to get too low causing the right front portion of the hull to dig in and spin the aircraft about 180 degrees. The flight instructor stated, '...I took control of the aircraft when the student did not correct the pitch attitude, but a split second too late.' The pilot receiving instruction stated, '...while completing a step turn taxi maneuver to the left apparently I allowed the bow to become too low swinging the aircraft 180 degrees to the right causing damage....'

As the FAA filed it

(-23) WHILE PERFORMING STEP TAXI, THE LEFT HAND SPONSOR DUG INTO THE WATER CAUSING THE A/C TO SPIN 180 DEGREES AT A HIGH RATE OF SPEED. BOTH SPONSORS BROKE OFF, THERE WAS NO DAMAGE TO THE RIGHT FLAP, AILERON AND WING SPAR. THE FUSELAGE WRINKLED DUE TO HYDRAULIC ACTION. THERE WERE NO INJURIES. (-4)THE FLIGHT HAD LANDED ON THE LAKE AFTER THE PILOTS HAD BEEN PRACTICING LANDINGS AND TAKEOFFS. WHILE ATTEMPTING A WATER TAKE OFF IN A LEFT STEP TURN THE BOW WAS ALLOWED TO GET TOO LOW CAUSING THE RIGHT FRONT PORTION OF THE HULL TO DIG IN AND SPIN THE AIRCRAFT ABOUT 180 DEGREES. THE FLIGHT INSTRUCTOR STATED, '...I TOOK CONTROL OF THE AIRCRAFT WHEN THE STUDENT DID NOT CORRECT THE PITCH ATTITUDE, BUT A SPLIT SECOND TOO LATE.' THE PILOT RECEIVING INSTRUCTION STATED, '...WHILE COMPLETING A STEP TURN TAXI MANEUVER TO THE LEFT APPARENTLY I ALLOWED THE BOW TO BECOME TOO LOW SWINGING THE AIRCRAFT 180 DEGREES TO THE RIGHT CAUSING DAMAGE....'

NTSB investigation

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