20000121035339A

Accident · Substantial damage

FAA accident report · Mooney M20M · Barre Montpelie, VT · January 21, 2000

Date
January 21, 2000 · 12:35 local
Place
Barre Montpelie, VT
Airport
Edward F Knapp State
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N223KT
NTSB investigation
NTSBNYC00LA069
Reported as
Mooney M20M
Reported engine
Lycoming TIO540AF1B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,173 total107 in this make and model83 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)A few minutes after takeoff, the pilot realized the engine was not developing full manifold pressure; shortly thereafter, the engine lost all oil pressure. When the engine began to vibrate, the pilot shut down the engine and performed a forced landing to a field. Examination of the airplane revealed the engine's cowling was covered with oil, and the engine's crankshaft seal had been 'blown outward.' Ice was observed in the engine crankcase breather line. Additionally, a 'bend' was found in the breather line near a clamp that was installed over the breather line vent hole. There were no other discrepancies found with airplane. The outside air temperature reported at the airport about the time of the accident was 0 degrees f. the airplane was last flown 1 week prior to the accident. The airplane was kept in an unheated hanger; however, the engine was preheated using a built-in engine heater to an oil temperature of 40 degrees f, just prior to engine start. (-23)NYC00LA069

As the FAA filed it

(.4)A FEW MINUTES AFTER TAKEOFF, THE PILOT REALIZED THE ENGINE WAS NOT DEVELOPING FULL MANIFOLD PRESSURE; SHORTLY THEREAFTER, THE ENGINE LOST ALL OIL PRESSURE. WHEN THE ENGINE BEGAN TO VIBRATE, THE PILOT SHUT DOWN THE ENGINE AND PERFORMED A FORCED LANDING TO A FIELD. EXAMINATION OF THE AIRPLANE REVEALED THE ENGINE'S COWLING WAS COVERED WITH OIL, AND THE ENGINE'S CRANKSHAFT SEAL HAD BEEN 'BLOWN OUTWARD.' ICE WAS OBSERVED IN THE ENGINE CRANKCASE BREATHER LINE. ADDITIONALLY, A 'BEND' WAS FOUND IN THE BREATHER LINE NEAR A CLAMP THAT WAS INSTALLED OVER THE BREATHER LINE VENT HOLE. THERE WERE NO OTHER DISCREPANCIES FOUND WITH AIRPLANE. THE OUTSIDE AIR TEMPERATURE REPORTED AT THE AIRPORT ABOUT THE TIME OF THE ACCIDENT WAS 0 DEGREES F. THE AIRPLANE WAS LAST FLOWN 1 WEEK PRIOR TO THE ACCIDENT. THE AIRPLANE WAS KEPT IN AN UNHEATED HANGER; HOWEVER, THE ENGINE WAS PREHEATED USING A BUILT-IN ENGINE HEATER TO AN OIL TEMPERATURE OF 40 DEGREES F, JUST PRIOR TO ENGINE START. (-23)NYC00LA069

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 N223KT · 1

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