20010217001849A

Accident · Substantial damage

FAA accident report · Cessna 182H · Weaver, AL · February 17, 2001

Date
February 17, 2001 · 10:36 local
Place
Weaver, AL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8556S
NTSB investigation
NTSBMIA01LA081
Reported as
Cessna 182H
Reported engine
Continental O470R
People aboard
2
Fatal injuries
0
Pilot’s flight hours
2,239 total800 in this make and model13 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) Pilot stated that the engine started to backfire and run rough. He circled a large field and made an landing. On roll out after the alnding the a/c hit a ditch and the nose gear was broken off from the a/c. there was substantial damage to the fire wall and engine cowling. No injuries reported.(.19)on February 17, 2001, about 1036 central standard time, a Cessna 182H, N8556S, registered to an individual, separated the nose landing gear while making a forced landing in a field, following loss of engine power near Weaver, Alabama, while on a title 14 CFR part 91 personal flight from auburn, Alabama to anniston, Alabama. Visual meteorological conditions prevailed at the time andan instrument flight rules flight plan was filed. The airplane received substantial damage and the private-rated pilot and one passenger were not injured. The flight originated from auburn, the same day, about 1000. The pilot stated that while in cruise flight at 4,000 feet, the engine began to "pop" and lose power. He was unable to maintain altitude, and while making a forced landing in a field, the airplane collided with a ditch during landing rollout. The nose landing gear separated, and the airplane came to a stop nose down. (.4) the pilot stated that while in cruise flight, the engine began to "pop" and lose power. He was unable to maintain altitude and made a forced landing in a field. During the landing roll, the airplane collided with a ditch and the nose landing gear separated. Postcrash examination of the engine showed the no. 4 cylinder intake push rod housing was dented inward and the push rod had rubbed on the housing and failed. It was not determined when the dent was made in the push rod tube.

As the FAA filed it

(-23) PILOT STATED THAT THE ENGINE STARTED TO BACKFIRE AND RUN ROUGH. HE CIRCLED A LARGE FIELD AND MADE AN LANDING. ON ROLL OUT AFTER THE ALNDING THE A/C HIT A DITCH AND THE NOSE GEAR WAS BROKEN OFF FROM THE A/C. THERE WAS SUBSTANTIAL DAMAGE TO THE FIRE WALL AND ENGINE COWLING. NO INJURIES REPORTED.(.19)ON FEBRUARY 17, 2001, ABOUT 1036 CENTRAL STANDARD TIME, A CESSNA 182H, N8556S, REGISTERED TO AN INDIVIDUAL, SEPARATED THE NOSE LANDING GEAR WHILE MAKING A FORCED LANDING IN A FIELD, FOLLOWING LOSS OF ENGINE POWER NEAR WEAVER, ALABAMA, WHILE ON A TITLE 14 CFR PART 91 PERSONAL FLIGHT FROM AUBURN, ALABAMA TO ANNISTON, ALABAMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME ANDAN INSTRUMENT FLIGHT RULES FLIGHT PLAN WAS FILED. THE AIRPLANE RECEIVED SUBSTANTIAL DAMAGE AND THE PRIVATE-RATED PILOT AND ONE PASSENGER WERE NOT INJURED. THE FLIGHT ORIGINATED FROM AUBURN, THE SAME DAY, ABOUT 1000. THE PILOT STATED THAT WHILE IN CRUISE FLIGHT AT 4,000 FEET, THE ENGINE BEGAN TO "POP" AND LOSE POWER. HE WAS UNABLE TO MAINTAIN ALTITUDE, AND WHILE MAKING A FORCED LANDING IN A FIELD, THE AIRPLANE COLLIDED WITH A DITCH DURING LANDING ROLLOUT. THE NOSE LANDING GEAR SEPARATED, AND THE AIRPLANE CAME TO A STOP NOSE DOWN. (.4) THE PILOT STATED THAT WHILE IN CRUISE FLIGHT, THE ENGINE BEGAN TO "POP" AND LOSE POWER. HE WAS UNABLE TO MAINTAIN ALTITUDE AND MADE A FORCED LANDING IN A FIELD. DURING THE LANDING ROLL, THE AIRPLANE COLLIDED WITH A DITCH AND THE NOSE LANDING GEAR SEPARATED. POSTCRASH EXAMINATION OF THE ENGINE SHOWED THE NO. 4 CYLINDER INTAKE PUSH ROD HOUSING WAS DENTED INWARD AND THE PUSH ROD HAD RUBBED ON THE HOUSING AND FAILED. IT WAS NOT DETERMINED WHEN THE DENT WAS MADE IN THE PUSH ROD TUBE.

NTSB investigation

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