20141130023039A

Accident · Destroyed

FAA accident report · Bellanca 17-30A · Boonville, MO · November 30, 2014

Date
November 30, 2014 · 09:00 local
Place
Boonville, MO
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N6629V
NTSB investigation
NTSBCEN15FA060
Reported as
Bellanca 17-30A
Reported engine
Continental IO-520 series
People aboard
4
Fatal injuries
1
Other injuries
3
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
3,100 total

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.

At approximately 0740 CST, N6629V departed ksus VFR for a flight to kmkc. The weather was clear; however, by the time the airplane was passing by columbia, MO, the cloud ceilings were lowering due to an approaching cold front. A passenger commented after the accident that the PIC continued to fly at a lower altitude to stay below "scud" clouds that were beginning to form beneath the ceiling.

Approximately 15 miles west of Boonville, MO, the PIC decided to reverse course and land at kver. Weather at the airport was reporting an overcast ceiling of 2,400', 10 miles visibility, and wind from 300 degrees at 9 KTS gusting to 14 KTS. Temperature was 13 c and dew point 11 c.

On base to final with 1/2 flaps and landing gear down, the engine began to "sputter" followed by stoppage. The PIC attempted to restart the engine without success. The airplane impacted slightly down-sloping terrain (a barren soy bean field) approximately 1/2 mile south of and on the extended centerline of runway 36. Duration of flight was approximately 1 hour, 20 minutes.

The aiplane came to rest and remained upright at the end of ground marks made by the landing gear that measured 25 feet. The engine remained partially attached to the firewall, and the propeller was detached from the shaft. The airframe remained largely intact with deformation throughout. Occupant injuries were consistent with high vertical loads. There was no post-crash fire, nor evidence of fuel spillage from the four fuel tanks. The fuel selector was determined to be in the "aux" position for the right aux tank.

Post-accident investigation revealed the fuel quantity in the four tanks as follows: lt main - 5 gal

Rt main - 3.5 pints

Lt aux - 17 gal (full)

Rt aux - 11 gal

As the FAA filed it

AT APPROXIMATELY 0740 CST, N6629V DEPARTED KSUS VFR FOR A FLIGHT TO KMKC. THE WEATHER WAS CLEAR; HOWEVER, BY THE TIME THE AIRPLANE WAS PASSING BY COLUMBIA, MO, THE CLOUD CEILINGS WERE LOWERING DUE TO AN APPROACHING COLD FRONT. A PASSENGER COMMENTED AFTER THE ACCIDENT THAT THE PIC CONTINUED TO FLY AT A LOWER ALTITUDE TO STAY BELOW "SCUD" CLOUDS THAT WERE BEGINNING TO FORM BENEATH THE CEILING.

APPROXIMATELY 15 MILES WEST OF BOONVILLE, MO, THE PIC DECIDED TO REVERSE COURSE AND LAND AT KVER. WEATHER AT THE AIRPORT WAS REPORTING AN OVERCAST CEILING OF 2,400', 10 MILES VISIBILITY, AND WIND FROM 300 DEGREES AT 9 KTS GUSTING TO 14 KTS. TEMPERATURE WAS 13 C AND DEW POINT 11 C.

ON BASE TO FINAL WITH 1/2 FLAPS AND LANDING GEAR DOWN, THE ENGINE BEGAN TO "SPUTTER" FOLLOWED BY STOPPAGE. THE PIC ATTEMPTED TO RESTART THE ENGINE WITHOUT SUCCESS. THE AIRPLANE IMPACTED SLIGHTLY DOWN-SLOPING TERRAIN (A BARREN SOY BEAN FIELD) APPROXIMATELY 1/2 MILE SOUTH OF AND ON THE EXTENDED CENTERLINE OF RUNWAY 36. DURATION OF FLIGHT WAS APPROXIMATELY 1 HOUR, 20 MINUTES.

THE AIPLANE CAME TO REST AND REMAINED UPRIGHT AT THE END OF GROUND MARKS MADE BY THE LANDING GEAR THAT MEASURED 25 FEET. THE ENGINE REMAINED PARTIALLY ATTACHED TO THE FIREWALL, AND THE PROPELLER WAS DETACHED FROM THE SHAFT. THE AIRFRAME REMAINED LARGELY INTACT WITH DEFORMATION THROUGHOUT. OCCUPANT INJURIES WERE CONSISTENT WITH HIGH VERTICAL LOADS. THERE WAS NO POST-CRASH FIRE, NOR EVIDENCE OF FUEL SPILLAGE FROM THE FOUR FUEL TANKS. THE FUEL SELECTOR WAS DETERMINED TO BE IN THE "AUX" POSITION FOR THE RIGHT AUX TANK.

POST-ACCIDENT INVESTIGATION REVEALED THE FUEL QUANTITY IN THE FOUR TANKS AS FOLLOWS: LT MAIN - 5 GAL

RT MAIN - 3.5 PINTS

LT AUX - 17 GAL (FULL)

RT AUX - 11 GAL

NTSB investigation

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