19971002038119A

Accident · Substantial damage

FAA accident report · Beech E18S · St Paul, MN · October 2, 1997

Date
October 2, 1997 · 06:05 local
Place
St Paul, MN
Airport
Lake Elmo Airport
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N916TM
NTSB investigation
NTSBCHI98LA003
Reported as
Beech E18S
People aboard
2
Fatal injuries
0
Pilot’s flight hours
4,500 total356 in this make and model75 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.

Damaged due wake turbulence on take off for repositioning flight. (-23) after lift off, pilot gleason stated the aircraft felt to be wallowing and did not respond to control inputs and power applications. Due to minimal wind conditions and another aircraft having departed in opposite direction, approximately one minute before there is a distinct possibility of wake turbulence being a factor. This was a repositioning flight. (.19) on October 2, 1997, at 0605 central daylight time, a Beech E18S, N916TM, operated by may air express, collided with the terrain during an aborted takeoff on runway 31 (2,850' x 75') at the Lake Elmo Airport, lake Elmo, Minnesota, while on a 14 CFR part 91 positioning flight. The airplane was substantially damaged. Neither of the pilots on board were injured. Visual meteorological conditions prevailed. The airplane was being flown to minneapolis, Minnesota, to pick up a cargo load when the accident occurred. (.4) the airplane lifted off at 70 knots. He reported he allowed the airplane to accelerate in ground effect for several seconds after which time the airplane became "...unstable in the roll axis." He reported he added power as there was not enough runway left to land on. The airplane was 3/4 the way down the runway when the left wing tip touched the runway. He reported that at this point he added more power at which point the left wing tip contacted the terrain off the left side of the departure end of the runway causing the nose to pitch up. He then reduced the power to idle and the aircraft touched down in the grass collapsing the landing gear. The pilot stated that the airplane normally lifts off between 70 and 75 knots when it is light. In addition, he stated that the engines sounded normal during the accident sequence. An inspector from the minneapolis, Minnesota, FAA flight standards district office reported that another Beech 18 had taken off on the same runway, but in the opposite direction of N916TM less than one minute prior to the accident.

As the FAA filed it

DAMAGED DUE WAKE TURBULENCE ON TAKE OFF FOR REPOSITIONING FLIGHT. (-23) AFTER LIFT OFF, PILOT GLEASON STATED THE AIRCRAFT FELT TO BE WALLOWING AND DID NOT RESPOND TO CONTROL INPUTS AND POWER APPLICATIONS. DUE TO MINIMAL WIND CONDITIONS AND ANOTHER AIRCRAFT HAVING DEPARTED IN OPPOSITE DIRECTION, APPROXIMATELY ONE MINUTE BEFORE THERE IS A DISTINCT POSSIBILITY OF WAKE TURBULENCE BEING A FACTOR. THIS WAS A REPOSITIONING FLIGHT. (.19) ON OCTOBER 2, 1997, AT 0605 CENTRAL DAYLIGHT TIME, A BEECH E18S, N916TM, OPERATED BY MAY AIR EXPRESS, COLLIDED WITH THE TERRAIN DURING AN ABORTED TAKEOFF ON RUNWAY 31 (2,850' X 75') AT THE LAKE ELMO AIRPORT, LAKE ELMO, MINNESOTA, WHILE ON A 14 CFR PART 91 POSITIONING FLIGHT. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. NEITHER OF THE PILOTS ON BOARD WERE INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. THE AIRPLANE WAS BEING FLOWN TO MINNEAPOLIS, MINNESOTA, TO PICK UP A CARGO LOAD WHEN THE ACCIDENT OCCURRED. (.4) THE AIRPLANE LIFTED OFF AT 70 KNOTS. HE REPORTED HE ALLOWED THE AIRPLANE TO ACCELERATE IN GROUND EFFECT FOR SEVERAL SECONDS AFTER WHICH TIME THE AIRPLANE BECAME "...UNSTABLE IN THE ROLL AXIS." HE REPORTED HE ADDED POWER AS THERE WAS NOT ENOUGH RUNWAY LEFT TO LAND ON. THE AIRPLANE WAS 3/4 THE WAY DOWN THE RUNWAY WHEN THE LEFT WING TIP TOUCHED THE RUNWAY. HE REPORTED THAT AT THIS POINT HE ADDED MORE POWER AT WHICH POINT THE LEFT WING TIP CONTACTED THE TERRAIN OFF THE LEFT SIDE OF THE DEPARTURE END OF THE RUNWAY CAUSING THE NOSE TO PITCH UP. HE THEN REDUCED THE POWER TO IDLE AND THE AIRCRAFT TOUCHED DOWN IN THE GRASS COLLAPSING THE LANDING GEAR. THE PILOT STATED THAT THE AIRPLANE NORMALLY LIFTS OFF BETWEEN 70 AND 75 KNOTS WHEN IT IS LIGHT. IN ADDITION, HE STATED THAT THE ENGINES SOUNDED NORMAL DURING THE ACCIDENT SEQUENCE. AN INSPECTOR FROM THE MINNEAPOLIS, MINNESOTA, FAA FLIGHT STANDARDS DISTRICT OFFICE REPORTED THAT ANOTHER BEECH 18 HAD TAKEN OFF ON THE SAME RUNWAY, BUT IN THE OPPOSITE DIRECTION OF N916TM LESS THAN ONE MINUTE PRIOR TO THE ACCIDENT.

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 N916TM · 1

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