20020430014899I

Incident

FAA incident report · Cessna T337G · Dallas, TX · April 30, 2002

Date
April 30, 2002
Place
Dallas, TX
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N300
Reported as
Cessna T337G
Reported engine
Continental TSIO360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,400 total650 in this make and model

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) While inflight between rbd and dal experienced catastrophic engine failure on front engine. Subsequent inspection revealed six inch hole in top of case between 1 & 2 cylinders, rods 1 and 2 separated from rod caps. Spirolletic rod nuts spun off of rod bolts and were found in sump. Crankcase sump tube contained crankshaft and counterweight bushing material from one counterweight pad, the other pad and counterweight were found in pieces in oil sump pan. Engine had 309 hours since factory rebuilt.

As the FAA filed it

(-23) WHILE INFLIGHT BETWEEN RBD AND DAL EXPERIENCED CATASTROPHIC ENGINE FAILURE ON FRONT ENGINE. SUBSEQUENT INSPECTION REVEALED SIX INCH HOLE IN TOP OF CASE BETWEEN 1 & 2 CYLINDERS, RODS 1 AND 2 SEPARATED FROM ROD CAPS. SPIROLLETIC ROD NUTS SPUN OFF OF ROD BOLTS AND WERE FOUND IN SUMP. CRANKCASE SUMP TUBE CONTAINED CRANKSHAFT AND COUNTERWEIGHT BUSHING MATERIAL FROM ONE COUNTERWEIGHT PAD, THE OTHER PAD AND COUNTERWEIGHT WERE FOUND IN PIECES IN OIL SUMP PAN. ENGINE HAD 309 HOURS SINCE FACTORY REBUILT.