20101029050679A

Accident · Substantial damage

FAA accident report · Piper PA-32R-301T · Waterloo, IA · October 29, 2010

Date
October 29, 2010 · 15:10 local
Place
Waterloo, IA
Airport
Waterloo
Phase of flight
Takeoff: Departure Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8370L
NTSB investigation
NTSBCEN11LA048
Reported as
Piper PA-32R-301T
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
9,000 total8,800 in this make and model1 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 passenger states that he is absolutely certain that the elevator control cable was intact during preflight inspection and preflight run up. The passenger states that during the take off roll, the pilot eased back on the yoke, and for a split second, the nose wheel seemed to lift normally. Then the pilot discovered that there was no lift and cycled the yoke full forward and full aft then immediately cut power and added full right rudder to avoid the approaching drainage ditch. This action changed the direction of the aircraft by about 15 or 20 degrees, which allowed the aircraft to cross the ditch at its narrowest point. Crossing the ditch caused the aircraft landing gear to shear off, slowing the aircraft to the point that it slid approximately 60 feet more and came to rest approximately 2/3 of the way up the embankment at the highway.

As the FAA filed it

THE PASSENGER STATES THAT HE IS ABSOLUTELY CERTAIN THAT THE ELEVATOR CONTROL CABLE WAS INTACT DURING PREFLIGHT INSPECTION AND PREFLIGHT RUN UP. THE PASSENGER STATES THAT DURING THE TAKE OFF ROLL, THE PILOT EASED BACK ON THE YOKE, AND FOR A SPLIT SECOND, THE NOSE WHEEL SEEMED TO LIFT NORMALLY. THEN THE PILOT DISCOVERED THAT THERE WAS NO LIFT AND CYCLED THE YOKE FULL FORWARD AND FULL AFT THEN IMMEDIATELY CUT POWER AND ADDED FULL RIGHT RUDDER TO AVOID THE APPROACHING DRAINAGE DITCH. THIS ACTION CHANGED THE DIRECTION OF THE AIRCRAFT BY ABOUT 15 OR 20 DEGREES, WHICH ALLOWED THE AIRCRAFT TO CROSS THE DITCH AT ITS NARROWEST POINT. CROSSING THE DITCH CAUSED THE AIRCRAFT LANDING GEAR TO SHEAR OFF, SLOWING THE AIRCRAFT TO THE POINT THAT IT SLID APPROXIMATELY 60 FEET MORE AND CAME TO REST APPROXIMATELY 2/3 OF THE WAY UP THE EMBANKMENT AT THE HIGHWAY.

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 N8370L · 2

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