19960703022819A

Accident · Substantial damage

FAA accident report · Beech 95-A55 · Ardmore, OK · July 3, 1996

Date
July 3, 1996 · 17:45 local
Place
Ardmore, OK
Airport
Ardmore Downtown Executive
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2992F
NTSB investigation
NTSBFTW96LA298
Reported as
Beech 95A55
Reported engine
Continental IO470L
People aboard
2
Fatal injuries
0
Pilot’s flight hours
336 total46 in this make and model59 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.

Lost control on takeoff with safety CFI pilot. Hit fence and ditch. Indicates early gear retraction near rotation. (-23) both pilots heard a "loud bang" from the right side of the airplane and the flight instructor took command of the flight. The airplane "ballooned into the air, settled onto the left main gear, and then veered to the right." The instructor realized that the propellers had struck the runway. Subsequently, the airplane veered to the left, crossed a taxiway at approximately 85 mph, hit a drainage area, and "went back into the air" before coming to rest at the bottom of a ditch. The operator examined the gear system and determined that "the damage occurred to the activating mechanism by the gear retracting upon lift-off from the runway." He did not observe "any major component failure or lack of continuity in (the) gear retracting torque tubes or bellcrank."

As the FAA filed it

LOST CONTROL ON TAKEOFF WITH SAFETY CFI PILOT. HIT FENCE AND DITCH. INDICATES EARLY GEAR RETRACTION NEAR ROTATION. (-23) BOTH PILOTS HEARD A "LOUD BANG" FROM THE RIGHT SIDE OF THE AIRPLANE AND THE FLIGHT INSTRUCTOR TOOK COMMAND OF THE FLIGHT. THE AIRPLANE "BALLOONED INTO THE AIR, SETTLED ONTO THE LEFT MAIN GEAR, AND THEN VEERED TO THE RIGHT." THE INSTRUCTOR REALIZED THAT THE PROPELLERS HAD STRUCK THE RUNWAY. SUBSEQUENTLY, THE AIRPLANE VEERED TO THE LEFT, CROSSED A TAXIWAY AT APPROXIMATELY 85 MPH, HIT A DRAINAGE AREA, AND "WENT BACK INTO THE AIR" BEFORE COMING TO REST AT THE BOTTOM OF A DITCH. THE OPERATOR EXAMINED THE GEAR SYSTEM AND DETERMINED THAT "THE DAMAGE OCCURRED TO THE ACTIVATING MECHANISM BY THE GEAR RETRACTING UPON LIFT-OFF FROM THE RUNWAY." HE DID NOT OBSERVE "ANY MAJOR COMPONENT FAILURE OR LACK OF CONTINUITY IN (THE) GEAR RETRACTING TORQUE TUBES OR BELLCRANK."

NTSB investigation

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