19950718019641A

Accident · Destroyed

FAA accident report · Amtr CORBEN JR. ACE E · Ames, IA · July 18, 1995

Date
July 18, 1995 · 13:40 local
Place
Ames, IA
Airport
Ames Municipal Airport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Collision
Midair collision, first aircraft
Damage
Destroyed
Aircraft
N964
NTSB investigation
NTSBCHI95LA228
Reported as
Amtr Corbenjracee
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.

Towing glider, collided with ground after tow aircraft lost power on takeoff. (.4)the glider pilot stated that after he completed his preflight in preparation for launch, he secured himself in the glider as the tow rope was connected. However, he could not recall any of the events that followed, concerning the takeoff roll or accident. The tow pilot reported that after the glider was hooked up to the tow plane, a signal was provided to begin the takeoff roll. Witnesses stated that as the tow airplane began the takeoff roll, the glider was having directional control problems. The tow airplane lifted off and climbed about 50 to 60 feet above the ground. The tow pilot said that at about that time, he noted excessive drag and the tow airplane's tail was pulled down despite his use of full forward elevator. Subsequently, the glider cartwheeled and flipped over, the tow rope failed, and the tow airplane stalled and impacted the ground. Postaccident examination revealed the glider's right ruddervator was loose and was not properly connected to the push-pull tube. The glider pilot stated that he did not recall, but he probably did not do a positive control check of the ruddervators before the launch. A witness said he observed the glider pilot climb into the glider's cockpit and work the control stick to verify aileron and ruddervator control, but he did not do a positive contorl check during his preflight.

As the FAA filed it

TOWING GLIDER, COLLIDED WITH GROUND AFTER TOW AIRCRAFT LOST POWER ON TAKEOFF. (.4)THE GLIDER PILOT STATED THAT AFTER HE COMPLETED HIS PREFLIGHT IN PREPARATION FOR LAUNCH, HE SECURED HIMSELF IN THE GLIDER AS THE TOW ROPE WAS CONNECTED. HOWEVER, HE COULD NOT RECALL ANY OF THE EVENTS THAT FOLLOWED, CONCERNING THE TAKEOFF ROLL OR ACCIDENT. THE TOW PILOT REPORTED THAT AFTER THE GLIDER WAS HOOKED UP TO THE TOW PLANE, A SIGNAL WAS PROVIDED TO BEGIN THE TAKEOFF ROLL. WITNESSES STATED THAT AS THE TOW AIRPLANE BEGAN THE TAKEOFF ROLL, THE GLIDER WAS HAVING DIRECTIONAL CONTROL PROBLEMS. THE TOW AIRPLANE LIFTED OFF AND CLIMBED ABOUT 50 TO 60 FEET ABOVE THE GROUND. THE TOW PILOT SAID THAT AT ABOUT THAT TIME, HE NOTED EXCESSIVE DRAG AND THE TOW AIRPLANE'S TAIL WAS PULLED DOWN DESPITE HIS USE OF FULL FORWARD ELEVATOR. SUBSEQUENTLY, THE GLIDER CARTWHEELED AND FLIPPED OVER, THE TOW ROPE FAILED, AND THE TOW AIRPLANE STALLED AND IMPACTED THE GROUND. POSTACCIDENT EXAMINATION REVEALED THE GLIDER'S RIGHT RUDDERVATOR WAS LOOSE AND WAS NOT PROPERLY CONNECTED TO THE PUSH-PULL TUBE. THE GLIDER PILOT STATED THAT HE DID NOT RECALL, BUT HE PROBABLY DID NOT DO A POSITIVE CONTROL CHECK OF THE RUDDERVATORS BEFORE THE LAUNCH. A WITNESS SAID HE OBSERVED THE GLIDER PILOT CLIMB INTO THE GLIDER'S COCKPIT AND WORK THE CONTROL STICK TO VERIFY AILERON AND RUDDERVATOR CONTROL, BUT HE DID NOT DO A POSITIVE CONTORL CHECK DURING HIS PREFLIGHT.

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 aircraft in the event · 1

Each aircraft in a collision has its own report.