20050611009839A

Accident · Substantial damage

FAA accident report · Cessna A188B · Goodlett, TX · June 11, 2005

Date
June 11, 2005 · 17:45 local
Place
Goodlett, TX
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Agricultural (Part 137)
Operator
TTTG
Damage
Substantial damage
Aircraft
N4919R
NTSB investigation
NTSBDFW05CA155
Reported as
Cessna A188B
Reported engine
Lycoming IO540K1G5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
700 total286 in this make and model200 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) The pilot reported that the engine lost power during pull-up maneuver. The pilot made a forced landing in a nearby field. The aircraft struck a fence with the right wing and skidded through some shrubs and came to rest approximately 268 feet from initial impact with the terrain. During the investigation, it was noted that there was adequate fuel for engine operation, the spark plugs showed consistent signs of normal operation, there was gear train continuity from the crankshaft gear to the cam gear, the left magneto appeared to fire on the correct cylinder near top dead center, and there was some fuel present at the fuel line from the engine driven fuel pump to the throttle servo. The pilot described the engine stoppage as very sudden without any warning. There was some damage to the propeller consistent with blades turning at a slow RPM. The throttle was at high power setting, the mixture was at or near full rich, and the propeller control was set to low pitch.

As the FAA filed it

(-23) THE PILOT REPORTED THAT THE ENGINE LOST POWER DURING PULL-UP MANEUVER. THE PILOT MADE A FORCED LANDING IN A NEARBY FIELD. THE AIRCRAFT STRUCK A FENCE WITH THE RIGHT WING AND SKIDDED THROUGH SOME SHRUBS AND CAME TO REST APPROXIMATELY 268 FEET FROM INITIAL IMPACT WITH THE TERRAIN. DURING THE INVESTIGATION, IT WAS NOTED THAT THERE WAS ADEQUATE FUEL FOR ENGINE OPERATION, THE SPARK PLUGS SHOWED CONSISTENT SIGNS OF NORMAL OPERATION, THERE WAS GEAR TRAIN CONTINUITY FROM THE CRANKSHAFT GEAR TO THE CAM GEAR, THE LEFT MAGNETO APPEARED TO FIRE ON THE CORRECT CYLINDER NEAR TOP DEAD CENTER, AND THERE WAS SOME FUEL PRESENT AT THE FUEL LINE FROM THE ENGINE DRIVEN FUEL PUMP TO THE THROTTLE SERVO. THE PILOT DESCRIBED THE ENGINE STOPPAGE AS VERY SUDDEN WITHOUT ANY WARNING. THERE WAS SOME DAMAGE TO THE PROPELLER CONSISTENT WITH BLADES TURNING AT A SLOW RPM. THE THROTTLE WAS AT HIGH POWER SETTING, THE MIXTURE WAS AT OR NEAR FULL RICH, AND THE PROPELLER CONTROL WAS SET TO LOW PITCH.

NTSB investigation

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