19980519010179A

Accident · Substantial damage

FAA accident report · Cessna 182A · Independence, MO · May 19, 1998

Date
May 19, 1998 · 20:30 local
Place
Independence, MO
Airport
Independence Memorial Airport
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N507SD
NTSB investigation
NTSBCHI98LA156
Reported as
Cessna 182A
Reported engine
Continental O470L
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,457 total1,661 in this make and model58 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 pilot reported that as the airplane was descending through 4,000 feet MSL it started loosing power. She leveled off, pulled carburetor heat on, and switched fuel tanks. She reported that, 'upon restart the engine backfired and quit.' She reported that she trimmed the airplane for best glide (80 mph) and flew directly for the airport 2.5 miles away. At .5 miles from the airport she realized she would not make the runway so she decided to land short. She set 10 degrees of flaps and landed in a field. The airplane hit a wooden fence post during landing roll in the muddy field and nosed over. An examination of the engine found the induction system balance tube separated from the intake manifold tube assembly. The induction system balance tube coupling did not line up with the intake manifold. The engine was test run. During the first test run, the induction system balance tube coupling was left disconnected. The engine started but would only run when the throttle was continuously pumped. The balance tube coupling was connected and the engine restarted. The engine operated and did not require continuous pumping of the throttle. The engine was run up to 1,700 RPM. Th e engine ran smoothly at 1,700 RPM with no missing or backfiring. No other pre-impact mechanical anomalies were noted on the engine. (-23) see attached; no narrative attached.

As the FAA filed it

(.4)THE PILOT REPORTED THAT AS THE AIRPLANE WAS DESCENDING THROUGH 4,000 FEET MSL IT STARTED LOOSING POWER. SHE LEVELED OFF, PULLED CARBURETOR HEAT ON, AND SWITCHED FUEL TANKS. SHE REPORTED THAT, 'UPON RESTART THE ENGINE BACKFIRED AND QUIT.' SHE REPORTED THAT SHE TRIMMED THE AIRPLANE FOR BEST GLIDE (80 MPH) AND FLEW DIRECTLY FOR THE AIRPORT 2.5 MILES AWAY. AT .5 MILES FROM THE AIRPORT SHE REALIZED SHE WOULD NOT MAKE THE RUNWAY SO SHE DECIDED TO LAND SHORT. SHE SET 10 DEGREES OF FLAPS AND LANDED IN A FIELD. THE AIRPLANE HIT A WOODEN FENCE POST DURING LANDING ROLL IN THE MUDDY FIELD AND NOSED OVER. AN EXAMINATION OF THE ENGINE FOUND THE INDUCTION SYSTEM BALANCE TUBE SEPARATED FROM THE INTAKE MANIFOLD TUBE ASSEMBLY. THE INDUCTION SYSTEM BALANCE TUBE COUPLING DID NOT LINE UP WITH THE INTAKE MANIFOLD. THE ENGINE WAS TEST RUN. DURING THE FIRST TEST RUN, THE INDUCTION SYSTEM BALANCE TUBE COUPLING WAS LEFT DISCONNECTED. THE ENGINE STARTED BUT WOULD ONLY RUN WHEN THE THROTTLE WAS CONTINUOUSLY PUMPED. THE BALANCE TUBE COUPLING WAS CONNECTED AND THE ENGINE RESTARTED. THE ENGINE OPERATED AND DID NOT REQUIRE CONTINUOUS PUMPING OF THE THROTTLE. THE ENGINE WAS RUN UP TO 1,700 RPM. TH E ENGINE RAN SMOOTHLY AT 1,700 RPM WITH NO MISSING OR BACKFIRING. NO OTHER PRE-IMPACT MECHANICAL ANOMALIES WERE NOTED ON THE ENGINE. (-23) SEE ATTACHED; NO NARRATIVE ATTACHED.

NTSB investigation

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