What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On 07-23-2004 this aircraft experienced a gear up landing. Examination of the aircraft on 07-26-2004 revealed damage to both propellers and abrasive damage to the underside of the aircraft causing structural damage to the skin and bulkheads. Examination of the interior of the aircraft revealed fire damage to the instrument panel and pilot's floor area. On 07-28-2004 the aircraft was placed on jacks and the landing gear was tested. The landing gear was completely cycled 3 times with positive indications of the gear being up and again in the down position. This was noted by the gear up and down indicator lights and also the gear mechanicl indicator. Examination of the fire area revealed the fire had not penetrated below the pilot's floor. The starter vibrator was discolored and charred indicating a possible over heated condition. Application of electrical power to the aircraft showed that the starter vibrator immediately started to spark. After removal of electrical power from the starter vibrator the rest of the aircraft systems that were tested operated normally.
As the FAA filed it
(-23) ON 07-23-2004 THIS AIRCRAFT EXPERIENCED A GEAR UP LANDING. EXAMINATION OF THE AIRCRAFT ON 07-26-2004 REVEALED DAMAGE TO BOTH PROPELLERS AND ABRASIVE DAMAGE TO THE UNDERSIDE OF THE AIRCRAFT CAUSING STRUCTURAL DAMAGE TO THE SKIN AND BULKHEADS. EXAMINATION OF THE INTERIOR OF THE AIRCRAFT REVEALED FIRE DAMAGE TO THE INSTRUMENT PANEL AND PILOT'S FLOOR AREA. ON 07-28-2004 THE AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR WAS TESTED. THE LANDING GEAR WAS COMPLETELY CYCLED 3 TIMES WITH POSITIVE INDICATIONS OF THE GEAR BEING UP AND AGAIN IN THE DOWN POSITION. THIS WAS NOTED BY THE GEAR UP AND DOWN INDICATOR LIGHTS AND ALSO THE GEAR MECHANICL INDICATOR. EXAMINATION OF THE FIRE AREA REVEALED THE FIRE HAD NOT PENETRATED BELOW THE PILOT'S FLOOR. THE STARTER VIBRATOR WAS DISCOLORED AND CHARRED INDICATING A POSSIBLE OVER HEATED CONDITION. APPLICATION OF ELECTRICAL POWER TO THE AIRCRAFT SHOWED THAT THE STARTER VIBRATOR IMMEDIATELY STARTED TO SPARK. AFTER REMOVAL OF ELECTRICAL POWER FROM THE STARTER VIBRATOR THE REST OF THE AIRCRAFT SYSTEMS THAT WERE TESTED OPERATED NORMALLY.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N88CS · 1
Matched to the same aircraft by N-number and date.