20191109019239I

Incident · Minor damage

FAA incident report · Rockwell International 112A · West Greenwich, RI · November 9, 2019

Date
November 9, 2019 · 16:52 local
Place
West Greenwich, RI
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N1337J
Reported as
Rockwell International 112A
Reported engine
Lycoming I0360 series
People aboard
2
Fatal injuries
0
Other injuries
0

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.

A/c was enroute from kpvd to kfrg, established in cruise at 3,500' MSL. About 20 minutes after departure, the pilot heard a loud noise and the propeller stopped instantly. The pilot conducted a forced landing on a highway in the dark. The pilot did not lower the landing gear. There were no injuries and no damage to other vehicles or structures. The aircraft sustained minor damage to the belly as a result of the gear-up landing. Upon inspection, the engine had multiple holes and cracks in the crankcase, one of which was approx. 2 inches in diameter above the number 4 connecting rod area. The engine showed evidence of internal component failure. The engine still had 6 quarts of oil in the sump.

As the FAA filed it

A/C WAS ENROUTE FROM KPVD TO KFRG, ESTABLISHED IN CRUISE AT 3,500' MSL. ABOUT 20 MINUTES AFTER DEPARTURE, THE PILOT HEARD A LOUD NOISE AND THE PROPELLER STOPPED INSTANTLY. THE PILOT CONDUCTED A FORCED LANDING ON A HIGHWAY IN THE DARK. THE PILOT DID NOT LOWER THE LANDING GEAR. THERE WERE NO INJURIES AND NO DAMAGE TO OTHER VEHICLES OR STRUCTURES. THE AIRCRAFT SUSTAINED MINOR DAMAGE TO THE BELLY AS A RESULT OF THE GEAR-UP LANDING. UPON INSPECTION, THE ENGINE HAD MULTIPLE HOLES AND CRACKS IN THE CRANKCASE, ONE OF WHICH WAS APPROX. 2 INCHES IN DIAMETER ABOVE THE NUMBER 4 CONNECTING ROD AREA. THE ENGINE SHOWED EVIDENCE OF INTERNAL COMPONENT FAILURE. THE ENGINE STILL HAD 6 QUARTS OF OIL IN THE SUMP.

Other reports on N1337J · 1

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