20010513008559A

Accident · Substantial damage

FAA accident report · Beech E33A · South Lake Taho, CA · May 13, 2001

Date
May 13, 2001 · 16:50 local
Place
South Lake Taho, CA
Airport
Lake Tahoe
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N464SR
NTSB investigation
NTSBLAX01LA177
Reported as
Beech E33A
Reported engine
Continental IO520B
People aboard
4
Fatal injuries
0
Pilot’s flight hours
283 total30 in this make and model28 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) After take-off the pilot selected gear-up about mid field. The pilot was not satisfied with the rate-of-climb and the take-off was aborted. The throttle was retarded and the gear was lowered. The aircraft contacted the runway prior to the landing gear extending to the locked position. The aircraft slid about 500' before coming to rest about 1500' short of the departure end of the runway used for take-off. The pilot stated that he attempted to add power to arrest the sink rate; however, the throttle jammed. An inspection of the throttle revealed that the throttle release button retaining screw was 8 turns loose allowing the release button to misalign. (.4) on may 13, 2001, about 1650 hours pacific daylight time, a Beech E33A, N464SR, impacted the runway during an aborted takeoff from the Lake Tahoe Airport, south Lake Tahoe, California. At the time of the mishap, the airplane's landing gear was in transit to the extended position. The airplane was substantially damaged. Neither the private pilot nor the three passengers was injured. The pilot had rented the airplane from south bay aviation, inc., torrance, California. Visual meteorological conditions prevailed, and n o flight plan was filed for the personal flight that was performed under 14 CFR part 91. The flight was originating at the time of the accident. According to the front right-seated pilot-rated passenger, during the pretakeoff check, the pilot observed a mechanical malfunction with the throttle control knob. The pilot stated to the passenger "look at this," and he showed the passenger the loose vernier control button on the throttle knob. The passenger indicated that he observed the pilot screw the vernier control back into position. Then, the pilot proceeded to takeoff. The pilot indicated to the national transportation safety board investigator that he initiated the takeoff roll from the beginning of runway 18. The airplane accelerated normally, and he felt the effect of the strong gusty wind. In an effort at increasing the airplane's rate of climb, the pilot indicated that he retracted the landing gear. Then, the airplane was pushed toward the ground by a strong downdraft. The pilot-rated passenger reported that he heard a horn going off in the cockpit. A witness reported observing the airplane with its landing gear retracted and its wings rocking up and down. At the time, the airplane was about midfield, and approximately 30 feet above the runway's surface. The pilot subsequently reported to the safety board investigator that he aborted the takeoff because he was "not satisfied with the rate of climb." The pilot indicated that he retarded the throttle and attempted to lower the landing gear. When it became evident that the airplane would touchdown before the gear was extended, he attempted to push the throttle forward but was unable. The pilot said it was stuck. The airplane impacted the runway with the landing gear partially extended. It slid about 500 feet before coming to a stop about 1,500 feet before reaching the runway's departure end. Responding rescue personnel stated that luggage was observed inside the airplane. There was no fire.

As the FAA filed it

(-23) AFTER TAKE-OFF THE PILOT SELECTED GEAR-UP ABOUT MID FIELD. THE PILOT WAS NOT SATISFIED WITH THE RATE-OF-CLIMB AND THE TAKE-OFF WAS ABORTED. THE THROTTLE WAS RETARDED AND THE GEAR WAS LOWERED. THE AIRCRAFT CONTACTED THE RUNWAY PRIOR TO THE LANDING GEAR EXTENDING TO THE LOCKED POSITION. THE AIRCRAFT SLID ABOUT 500' BEFORE COMING TO REST ABOUT 1500' SHORT OF THE DEPARTURE END OF THE RUNWAY USED FOR TAKE-OFF. THE PILOT STATED THAT HE ATTEMPTED TO ADD POWER TO ARREST THE SINK RATE; HOWEVER, THE THROTTLE JAMMED. AN INSPECTION OF THE THROTTLE REVEALED THAT THE THROTTLE RELEASE BUTTON RETAINING SCREW WAS 8 TURNS LOOSE ALLOWING THE RELEASE BUTTON TO MISALIGN. (.4) ON MAY 13, 2001, ABOUT 1650 HOURS PACIFIC DAYLIGHT TIME, A BEECH E33A, N464SR, IMPACTED THE RUNWAY DURING AN ABORTED TAKEOFF FROM THE LAKE TAHOE AIRPORT, SOUTH LAKE TAHOE, CALIFORNIA. AT THE TIME OF THE MISHAP, THE AIRPLANE'S LANDING GEAR WAS IN TRANSIT TO THE EXTENDED POSITION. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. NEITHER THE PRIVATE PILOT NOR THE THREE PASSENGERS WAS INJURED. THE PILOT HAD RENTED THE AIRPLANE FROM SOUTH BAY AVIATION, INC., TORRANCE, CALIFORNIA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND N O FLIGHT PLAN WAS FILED FOR THE PERSONAL FLIGHT THAT WAS PERFORMED UNDER 14 CFR PART 91. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. ACCORDING TO THE FRONT RIGHT-SEATED PILOT-RATED PASSENGER, DURING THE PRETAKEOFF CHECK, THE PILOT OBSERVED A MECHANICAL MALFUNCTION WITH THE THROTTLE CONTROL KNOB. THE PILOT STATED TO THE PASSENGER "LOOK AT THIS," AND HE SHOWED THE PASSENGER THE LOOSE VERNIER CONTROL BUTTON ON THE THROTTLE KNOB. THE PASSENGER INDICATED THAT HE OBSERVED THE PILOT SCREW THE VERNIER CONTROL BACK INTO POSITION. THEN, THE PILOT PROCEEDED TO TAKEOFF. THE PILOT INDICATED TO THE NATIONAL TRANSPORTATION SAFETY BOARD INVESTIGATOR THAT HE INITIATED THE TAKEOFF ROLL FROM THE BEGINNING OF RUNWAY 18. THE AIRPLANE ACCELERATED NORMALLY, AND HE FELT THE EFFECT OF THE STRONG GUSTY WIND. IN AN EFFORT AT INCREASING THE AIRPLANE'S RATE OF CLIMB, THE PILOT INDICATED THAT HE RETRACTED THE LANDING GEAR. THEN, THE AIRPLANE WAS PUSHED TOWARD THE GROUND BY A STRONG DOWNDRAFT. THE PILOT-RATED PASSENGER REPORTED THAT HE HEARD A HORN GOING OFF IN THE COCKPIT. A WITNESS REPORTED OBSERVING THE AIRPLANE WITH ITS LANDING GEAR RETRACTED AND ITS WINGS ROCKING UP AND DOWN. AT THE TIME, THE AIRPLANE WAS ABOUT MIDFIELD, AND APPROXIMATELY 30 FEET ABOVE THE RUNWAY'S SURFACE. THE PILOT SUBSEQUENTLY REPORTED TO THE SAFETY BOARD INVESTIGATOR THAT HE ABORTED THE TAKEOFF BECAUSE HE WAS "NOT SATISFIED WITH THE RATE OF CLIMB." THE PILOT INDICATED THAT HE RETARDED THE THROTTLE AND ATTEMPTED TO LOWER THE LANDING GEAR. WHEN IT BECAME EVIDENT THAT THE AIRPLANE WOULD TOUCHDOWN BEFORE THE GEAR WAS EXTENDED, HE ATTEMPTED TO PUSH THE THROTTLE FORWARD BUT WAS UNABLE. THE PILOT SAID IT WAS STUCK. THE AIRPLANE IMPACTED THE RUNWAY WITH THE LANDING GEAR PARTIALLY EXTENDED. IT SLID ABOUT 500 FEET BEFORE COMING TO A STOP ABOUT 1,500 FEET BEFORE REACHING THE RUNWAY'S DEPARTURE END. RESPONDING RESCUE PERSONNEL STATED THAT LUGGAGE WAS OBSERVED INSIDE THE AIRPLANE. THERE WAS NO FIRE.

NTSB investigation

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