20060106002029I

Incident

FAA incident report · Piper PA-32R-300 · Raleigh, NC · January 6, 2006

Date
January 6, 2006 · 14:00 local
Place
Raleigh, NC
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Operator
FFKA
Aircraft
N333TG
Reported as
Piper PA32R300
Reported engine
Lycoming IO540K1A5D
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,071 total8 in this make and model128 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) Takeoff from rdu was unsuccessful and a cruise altitude of 3,000 feet was established. After a clearance of 4,000 was received a cruise climb was established. Passing through 3,200 feet a "pop" was heard and instruments were scanned. Manifold pressure was approximately 30 inches of mercury, 2500 RPM, oil temp and pressure were in the green. Noting a loss of altitude a stabilized descent rate was established at an airspeed of 92 KIAS and an emergency landing field was selected. While descending to the landing site the emergency flow was followed with no success of an engine restart. Once the field was assured flaps and gear were deployed and the emergency landing completed. When the airplane came to a complete stop the engine and propeller stopped wind milling. The pilot safely egressed the aircraft with no injuries. Upon post-flight inspection a steady flow of oil was observed streaming from under the left side of the cowling.

As the FAA filed it

(-23) TAKEOFF FROM RDU WAS UNSUCCESSFUL AND A CRUISE ALTITUDE OF 3,000 FEET WAS ESTABLISHED. AFTER A CLEARANCE OF 4,000 WAS RECEIVED A CRUISE CLIMB WAS ESTABLISHED. PASSING THROUGH 3,200 FEET A "POP" WAS HEARD AND INSTRUMENTS WERE SCANNED. MANIFOLD PRESSURE WAS APPROXIMATELY 30 INCHES OF MERCURY, 2500 RPM, OIL TEMP AND PRESSURE WERE IN THE GREEN. NOTING A LOSS OF ALTITUDE A STABILIZED DESCENT RATE WAS ESTABLISHED AT AN AIRSPEED OF 92 KIAS AND AN EMERGENCY LANDING FIELD WAS SELECTED. WHILE DESCENDING TO THE LANDING SITE THE EMERGENCY FLOW WAS FOLLOWED WITH NO SUCCESS OF AN ENGINE RESTART. ONCE THE FIELD WAS ASSURED FLAPS AND GEAR WERE DEPLOYED AND THE EMERGENCY LANDING COMPLETED. WHEN THE AIRPLANE CAME TO A COMPLETE STOP THE ENGINE AND PROPELLER STOPPED WIND MILLING. THE PILOT SAFELY EGRESSED THE AIRCRAFT WITH NO INJURIES. UPON POST-FLIGHT INSPECTION A STEADY FLOW OF OIL WAS OBSERVED STREAMING FROM UNDER THE LEFT SIDE OF THE COWLING.

Other reports on N333TG · 3

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