20180223005189I

Incident · Minor damage

FAA incident report · Neff William A VANS RV-6 · Tonopah, AZ · February 23, 2018

Date
February 23, 2018 · 18:57 local
Place
Tonopah, AZ
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N220CB
Reported as
Neff William A Vans RV-6
Reported engine
Lycoming O-360 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
16,000 total300 in this make and model150 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.

During a flight from lax to kbxx at an approximate altitude of 5000 ft in a slow decent for phoenix engine RPM indicated 3000. At which time the airspeed began to decay. The pilot indicated he brought back the manifold pressure and propeller lever as he diagnosed the problem. Approximately 45 seconds into the event the engine and propeller stopped and a small amount of smoke appeared in the cockpit. Pilot could not make nearest airport and landed on rural road with no further incident.

Upon arrival to review aircraft, noted engine and propeller were already off aircraft. Found #4 connecting rod protruding through engine case. Noted crank seal was not seated in proper location. Could not positively identify cause of failure, due to aircraft propeller and engine being removed and partially disassembled and no tear down of engine being conducted/authorized by owner.

As the FAA filed it

DURING A FLIGHT FROM LAX TO KBXX AT AN APPROXIMATE ALTITUDE OF 5000 FT IN A SLOW DECENT FOR PHOENIX ENGINE RPM INDICATED 3000. AT WHICH TIME THE AIRSPEED BEGAN TO DECAY. THE PILOT INDICATED HE BROUGHT BACK THE MANIFOLD PRESSURE AND PROPELLER LEVER AS HE DIAGNOSED THE PROBLEM. APPROXIMATELY 45 SECONDS INTO THE EVENT THE ENGINE AND PROPELLER STOPPED AND A SMALL AMOUNT OF SMOKE APPEARED IN THE COCKPIT. PILOT COULD NOT MAKE NEAREST AIRPORT AND LANDED ON RURAL ROAD WITH NO FURTHER INCIDENT.

UPON ARRIVAL TO REVIEW AIRCRAFT, NOTED ENGINE AND PROPELLER WERE ALREADY OFF AIRCRAFT. FOUND #4 CONNECTING ROD PROTRUDING THROUGH ENGINE CASE. NOTED CRANK SEAL WAS NOT SEATED IN PROPER LOCATION. COULD NOT POSITIVELY IDENTIFY CAUSE OF FAILURE, DUE TO AIRCRAFT PROPELLER AND ENGINE BEING REMOVED AND PARTIALLY DISASSEMBLED AND NO TEAR DOWN OF ENGINE BEING CONDUCTED/AUTHORIZED BY OWNER.