20020821027939I

Incident · Minor damage

FAA incident report · Cessna 150D · Crete, NE · August 21, 2002

Date
August 21, 2002 · 19:15 local
Place
Crete, NE
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7998Z
Reported as
Cessna 150D
Reported engine
Continental O200A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
60 total50 in this make and model20 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) On August 21, 2002, approximately 1915 CDT, Cessna 150D, N7998Z, departed the Crete, Nebraska, municipal airport for a positioning flight to red oak, Iowa. During climb out the PIC was unable to maintain a positive rate of climb due to inadequate engine power. Approximately 500 feet AGL, the PIC diverted to the Crete municipal airport and was forced to lande in a field one mile east of the airport. No injury was reported. Subsequent investigation confirmed low engine power due to a combination of low cylinder compression and malfunctioning carburetor heat control system.

As the FAA filed it

(-23) ON AUGUST 21, 2002, APPROXIMATELY 1915 CDT, CESSNA 150D, N7998Z, DEPARTED THE CRETE, NEBRASKA, MUNICIPAL AIRPORT FOR A POSITIONING FLIGHT TO RED OAK, IOWA. DURING CLIMB OUT THE PIC WAS UNABLE TO MAINTAIN A POSITIVE RATE OF CLIMB DUE TO INADEQUATE ENGINE POWER. APPROXIMATELY 500 FEET AGL, THE PIC DIVERTED TO THE CRETE MUNICIPAL AIRPORT AND WAS FORCED TO LANDE IN A FIELD ONE MILE EAST OF THE AIRPORT. NO INJURY WAS REPORTED. SUBSEQUENT INVESTIGATION CONFIRMED LOW ENGINE POWER DUE TO A COMBINATION OF LOW CYLINDER COMPRESSION AND MALFUNCTIONING CARBURETOR HEAT CONTROL SYSTEM.