20041109035729I

Incident

FAA incident report · Cessna 310R · Payson, AZ · November 9, 2004

Date
November 9, 2004 · 07:30 local
Place
Payson, AZ
Airport
Payson Airport
Phase of flight
Descent
Operating rules
Air taxi and commuter (Part 135)
Operator
N3BA
Aircraft
N310FH
Reported as
Cessna 310R
Reported engine
Continental IO470*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,600 total300 in this make and model300 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) Pilot was making routine cargo run from phx to pan when he reached his cruise altitude (9000 ft/msl) he leaned the engines. Pilot stated, "as I made my descent the left engine died." Aircraft landed uneventfully at pan. Aero charter maintenance grounded the a/c and performed all required engine runs to check rigging and fuel flows, no defects were found with the l/h engine. Engine instruments (non-flt instrm'ts) were checked with master gauges inst'ld. All x-checks revealed all engine instruments were within limits. The problem could not be duplicated. The a/c was inspected, satisfactorily test flown, and returned to service. Possible engine failure due to over lean condition during descent but no conclusive evidence.

As the FAA filed it

(-23) PILOT WAS MAKING ROUTINE CARGO RUN FROM PHX TO PAN WHEN HE REACHED HIS CRUISE ALTITUDE (9000 FT/MSL) HE LEANED THE ENGINES. PILOT STATED, "AS I MADE MY DESCENT THE LEFT ENGINE DIED." AIRCRAFT LANDED UNEVENTFULLY AT PAN. AERO CHARTER MAINTENANCE GROUNDED THE A/C AND PERFORMED ALL REQUIRED ENGINE RUNS TO CHECK RIGGING AND FUEL FLOWS, NO DEFECTS WERE FOUND WITH THE L/H ENGINE. ENGINE INSTRUMENTS (NON-FLT INSTRM'TS) WERE CHECKED WITH MASTER GAUGES INST'LD. ALL X-CHECKS REVEALED ALL ENGINE INSTRUMENTS WERE WITHIN LIMITS. THE PROBLEM COULD NOT BE DUPLICATED. THE A/C WAS INSPECTED, SATISFACTORILY TEST FLOWN, AND RETURNED TO SERVICE. POSSIBLE ENGINE FAILURE DUE TO OVER LEAN CONDITION DURING DESCENT BUT NO CONCLUSIVE EVIDENCE.

Other reports on N310FH · 1

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