20031105028699I

Incident · Minor damage

FAA incident report · Cessna 650 · Naples, FL · November 5, 2003

Date: November 5, 2003 · 21:00 local
Place: Naples, FL
Airport: Naples Municipal
Phase of flight: Roll-Out (Fixed Wing)
Operating rules: General operating rules (Part 91)
Operator: FKEA
Damage: Minor damage
Aircraft: N24237
Reported as: Cessna 650
People aboard: 2
Fatal injuries: 0
Pilot’s flight hours: 11,000 total355 in this make and model100 in the last 90 days

N24237Registration cancelled Feb 23, 2011 · Cessna 650S/N 650-0102 · Built 1986 Airframe modelCessna 650 Engine modelGarrett TFE731 seriesTurbo-fan

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) Upon landing on runway 5 at Naples airport, Naples Florida, the aircraft experienced a brake failure, which resulted in the aircraft overrunning the departure end of runway 5. An examination of the aircraft performed by maintenance personnel revealed a chaffed hydraulic line, which operates the aircraft heat exchanger hydraulic fan. As a result of the failed line, the aircraft lost hydraulic fluid resulting in a loss of hydraulic pressure and subsequent brake failure. A malfunction or defect report, m or d, FAA form 8010-4, filed by operator.

As the FAA filed it

(-23) UPON LANDING ON RUNWAY 5 AT NAPLES AIRPORT, NAPLES FLORIDA, THE AIRCRAFT EXPERIENCED A BRAKE FAILURE, WHICH RESULTED IN THE AIRCRAFT OVERRUNNING THE DEPARTURE END OF RUNWAY 5. AN EXAMINATION OF THE AIRCRAFT PERFORMED BY MAINTENANCE PERSONNEL REVEALED A CHAFFED HYDRAULIC LINE, WHICH OPERATES THE AIRCRAFT HEAT EXCHANGER HYDRAULIC FAN. AS A RESULT OF THE FAILED LINE, THE AIRCRAFT LOST HYDRAULIC FLUID RESULTING IN A LOSS OF HYDRAULIC PRESSURE AND SUBSEQUENT BRAKE FAILURE. A MALFUNCTION OR DEFECT REPORT, M OR D, FAA FORM 8010-4, FILED BY OPERATOR.