19980511026889A

Accident · Substantial damage

FAA accident report · Cessna 172N · Hannibal, MO · May 11, 1998

Date
May 11, 1998 · 16:30 local
Place
Hannibal, MO
Airport
Hannibal Municipal Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N733HY
NTSB investigation
NTSBCHI98LA147
Reported as
Cessna 172N
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
42 total40 in this make and model18 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.

(.4)The student pilot reported that during takeoff, at an altitude of 200-300 feet AGL, the engine lost power. He applied carburetor heat and that 'seemed to help a little for 30-45 seconds.' He then turned off the carburetor heat at which time, according to the pilot, the engine RPM didn't change much. Shortly thereafter the engine lost all power and the propeller stopped. A forced landing was made in a plowed field during which time the airplane was substantially damaged. Post accident inspection failed to determine the cause of the power loss. (-23) the narrative is from a written statement provided by the PIC, a student pilot. Following before take-off checks; began take-off run, power 2400 RPM, rotated at 60-65 KIAS, at the runway end, 200-300 ft AGL, engine lost RPM, engine lost power and propeller stopped completely. PIC stated that fuel tanks were filled to the top before the flight, sumps were checked several minutes after fueling.

As the FAA filed it

(.4)THE STUDENT PILOT REPORTED THAT DURING TAKEOFF, AT AN ALTITUDE OF 200-300 FEET AGL, THE ENGINE LOST POWER. HE APPLIED CARBURETOR HEAT AND THAT 'SEEMED TO HELP A LITTLE FOR 30-45 SECONDS.' HE THEN TURNED OFF THE CARBURETOR HEAT AT WHICH TIME, ACCORDING TO THE PILOT, THE ENGINE RPM DIDN'T CHANGE MUCH. SHORTLY THEREAFTER THE ENGINE LOST ALL POWER AND THE PROPELLER STOPPED. A FORCED LANDING WAS MADE IN A PLOWED FIELD DURING WHICH TIME THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. POST ACCIDENT INSPECTION FAILED TO DETERMINE THE CAUSE OF THE POWER LOSS. (-23) THE NARRATIVE IS FROM A WRITTEN STATEMENT PROVIDED BY THE PIC, A STUDENT PILOT. FOLLOWING BEFORE TAKE-OFF CHECKS; BEGAN TAKE-OFF RUN, POWER 2400 RPM, ROTATED AT 60-65 KIAS, AT THE RUNWAY END, 200-300 FT AGL, ENGINE LOST RPM, ENGINE LOST POWER AND PROPELLER STOPPED COMPLETELY. PIC STATED THAT FUEL TANKS WERE FILLED TO THE TOP BEFORE THE FLIGHT, SUMPS WERE CHECKED SEVERAL MINUTES AFTER FUELING.

NTSB investigation

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