20001219042929A

Accident · Substantial damage

FAA accident report · Cessna 172M · Sturgis, SD · December 19, 2000

Date
December 19, 2000 · 13:20 local
Place
Sturgis, SD
Airport
Sturgis Municipal Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N13584
NTSB investigation
NTSBCHI01LA051
Reported as
Cessna 172M
Reported engine
Lycoming O360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
176 total9 in this make and model3 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 setting the airplane's elevator trim control wheel to the take-off setting, in the before take-off checklist, the pilot initiated a normal take-off on runway 29 at Sturgis muni airport. The airplane accelerated beyond the left nose wheel at 60 mph speed to 75-80 mph. Pilot reduced power to abort the takeoff and continued applying aft elevator control to become airborne. He then reapplied power and through mis-managing the flight controls, erratic flight occurred. He then reduced power again to land off the runway in a nose-low attitude resulting in the nose gear being torn off the airplane and the propeller striking the ground. The accident investigation revealed that the trim control system was faulty. When the trim control indicator was set to the takeoff position, the elevator trim was set to the full nose down position. The private pilot did not recognize the effect of the trim nor attempt to reset the trim during the takeoff.

As the FAA filed it

(-23) AFTER SETTING THE AIRPLANE'S ELEVATOR TRIM CONTROL WHEEL TO THE TAKE-OFF SETTING, IN THE BEFORE TAKE-OFF CHECKLIST, THE PILOT INITIATED A NORMAL TAKE-OFF ON RUNWAY 29 AT STURGIS MUNI AIRPORT. THE AIRPLANE ACCELERATED BEYOND THE LEFT NOSE WHEEL AT 60 MPH SPEED TO 75-80 MPH. PILOT REDUCED POWER TO ABORT THE TAKEOFF AND CONTINUED APPLYING AFT ELEVATOR CONTROL TO BECOME AIRBORNE. HE THEN REAPPLIED POWER AND THROUGH MIS-MANAGING THE FLIGHT CONTROLS, ERRATIC FLIGHT OCCURRED. HE THEN REDUCED POWER AGAIN TO LAND OFF THE RUNWAY IN A NOSE-LOW ATTITUDE RESULTING IN THE NOSE GEAR BEING TORN OFF THE AIRPLANE AND THE PROPELLER STRIKING THE GROUND. THE ACCIDENT INVESTIGATION REVEALED THAT THE TRIM CONTROL SYSTEM WAS FAULTY. WHEN THE TRIM CONTROL INDICATOR WAS SET TO THE TAKEOFF POSITION, THE ELEVATOR TRIM WAS SET TO THE FULL NOSE DOWN POSITION. THE PRIVATE PILOT DID NOT RECOGNIZE THE EFFECT OF THE TRIM NOR ATTEMPT TO RESET THE TRIM DURING THE TAKEOFF.

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 N13584 · 1

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