19930531019819I

Incident

FAA incident report · Cessna 310P · Kodiak, AK · May 31, 1993

Date
May 31, 1993 · 13:55 local
Place
Kodiak, AK
Airport
Kodiak Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N5847M
NTSB investigation
NTSBANC93IA076
Reported as
Cessna 310P
Reported engine
Continental IO520E
People aboard
2
Fatal injuries
0
Pilot’s flight hours
4,300 total400 in this make and model15 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.

Narrative: on retraction of the nose gear, the pilot-in-command heard a loud noise. He then noticed on a subsequent extension that the gear would not lock down. Examination of the system showed a failure on the nose gear idler bell crank. Metallurgical examination of the idler bell crank by use of the bench binocular microscope showed that the fractures revealed features typical of over stress separation. The bell crank was replaced and a gear retraction test was conducted and the system operated normally. The problem could not be duplicated. The nose wheel centering mechanism was examined and no abnormalities were noted. NTSB determined the probable cause of incident was failure of the nose gear idler bell crank due to over stress by an undetermined source.

As the FAA filed it

NARRATIVE: ON RETRACTION OF THE NOSE GEAR, THE PILOT-IN-COMMAND HEARD A LOUD NOISE. HE THEN NOTICED ON A SUBSEQUENT EXTENSION THAT THE GEAR WOULD NOT LOCK DOWN. EXAMINATION OF THE SYSTEM SHOWED A FAILURE ON THE NOSE GEAR IDLER BELL CRANK. METALLURGICAL EXAMINATION OF THE IDLER BELL CRANK BY USE OF THE BENCH BINOCULAR MICROSCOPE SHOWED THAT THE FRACTURES REVEALED FEATURES TYPICAL OF OVER STRESS SEPARATION. THE BELL CRANK WAS REPLACED AND A GEAR RETRACTION TEST WAS CONDUCTED AND THE SYSTEM OPERATED NORMALLY. THE PROBLEM COULD NOT BE DUPLICATED. THE NOSE WHEEL CENTERING MECHANISM WAS EXAMINED AND NO ABNORMALITIES WERE NOTED. NTSB DETERMINED THE PROBABLE CAUSE OF INCIDENT WAS FAILURE OF THE NOSE GEAR IDLER BELL CRANK DUE TO OVER STRESS BY AN UNDETERMINED SOURCE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.