20020725020159A

Accident · No damage

FAA accident report · Piper PA-30 · Marblehill, MO · July 25, 2002

Date
July 25, 2002 · 12:59 local
Place
Marblehill, MO
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N8563Y
NTSB investigation
NTSBCHI02FA215
Reported as
Piper PA30
People aboard
1
Fatal injuries
1

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) Approximately 8 miles north of the marble hill, MO airport the pilot reported losing power on the right engine privacy data omitted during this time, privacy data omitted as post accident investigation revealed the left engine controls were in the following positions: throttle-idle, prop-feathered, and mixture-retarded toward cutoff position. The left side fuel tanks were nearly full and the left fuel selector was in the main position. The right engine controls were forward although the mixture control was aft of the left one. The fuel selector for the right tank was in the aux tank position and that tank was completely empty while the right main was nearly full. There was no post accident fuel leakage or fire. The accident site was close to the end of the field privacy data omitted the aircraft's right wing tip made initial ground contact with the aircraft striking the ground in a nearly vertical attitude.

As the FAA filed it

(-23) APPROXIMATELY 8 MILES NORTH OF THE MARBLE HILL, MO AIRPORT THE PILOT REPORTED LOSING POWER ON THE RIGHT ENGINE ^PRIVACY DATA OMITTED^ DURING THIS TIME, ^PRIVACY DATA OMITTED^ AS POST ACCIDENT INVESTIGATION REVEALED THE LEFT ENGINE CONTROLS WERE IN THE FOLLOWING POSITIONS: THROTTLE-IDLE, PROP-FEATHERED, AND MIXTURE-RETARDED TOWARD CUTOFF POSITION. THE LEFT SIDE FUEL TANKS WERE NEARLY FULL AND THE LEFT FUEL SELECTOR WAS IN THE MAIN POSITION. THE RIGHT ENGINE CONTROLS WERE FORWARD ALTHOUGH THE MIXTURE CONTROL WAS AFT OF THE LEFT ONE. THE FUEL SELECTOR FOR THE RIGHT TANK WAS IN THE AUX TANK POSITION AND THAT TANK WAS COMPLETELY EMPTY WHILE THE RIGHT MAIN WAS NEARLY FULL. THERE WAS NO POST ACCIDENT FUEL LEAKAGE OR FIRE. THE ACCIDENT SITE WAS CLOSE TO THE END OF THE FIELD ^PRIVACY DATA OMITTED^ THE AIRCRAFT'S RIGHT WING TIP MADE INITIAL GROUND CONTACT WITH THE AIRCRAFT STRIKING THE GROUND IN A NEARLY VERTICAL ATTITUDE.

NTSB investigation

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

Other reports on N8563Y · 2

Matched to the same aircraft by N-number and date.