# Accident 20010426008839A: Cessna 210N, Gainesville, FL, April 26, 2001 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: April 26, 2001, 13:15 local time - Place: Gainesville, FL - Airport: Gainesville Regional Airport - Damage: Substantial damage - Phase of flight: Roll-Out (Fixed Wing) - Operating rules: Air taxi and commuter (Part 135) - Operator: DKBA - Location: 29.6900° N, 82.2717° W: From the FAA - Nearby events: https://openairdocs.org/map.md?lat=29.6900&lon=-82.2717&mi=10 - Aircraft: N6585A, a cancelled registration (https://openairdocs.org/deregistered/N6585A-2013-03-25) (OpenAirDocs) - Registry model: Cessna 210N (registry code 2073453, https://openairdocs.org/model/cessna-210n) (OpenAirDocs) - Registry engine: Continental IO-520 series (registry code 17032, https://openairdocs.org/engine/continental-io-520-series) (OpenAirDocs) - Reported make and model: CESSNA 210N - Reported engine: CONT IO520L - People aboard: 1 - Fatal injuries: 0 - Pilot flight hours: 1,040 total - NTSB investigation: [NTSB MIA01LA130](https://openairdocs.org/ntsb/MIA01LA130) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/20010426008839A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (-23)ENROUTE FROM BROOOKSVILLE (BVK) TO GAINSVILLE (GNV) ON IFR FLIGHT PLAN, ACTUAL WEATHER VMC, RADIOS STARTED TO SLOWLY FADE. AT POINT BEYOND MIDWAY OF FLIGHT PILOT LAST RADIO COMMUNICATION. PILOT CONTINUED WITH FLIGHT AS FILED USING HAND HELD GPS FOR NAVIGATION. PILOT NOTICED AMMETER SHOWED DISCHARGED AND REDUCED ELECTRICAL LOAD. PILOT RESET THRANSPONDER TO 7600 AND CONTINUED FLIGHT. UPON ARRIVING AT GNV PILOT TOWER LOOKING FOR LIGHT SIGNALS. PILOT RECEIVED CLEAR TO LAND FROM TOWER AND ENTERED PATTERN. PILOT SELECTED GEAR DOWN. PILOT OBSERVED GEAR IN DOWN POSITION, HOWEVER THE GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. PILOT ASSUMED THIS WAS DUE TO ALCK OF ELECTRICAL POWER AND CONTINUED WITH LANDING. UPON TOUCHDOWN THE MAIN GEAR COLLAPSED. DAMAGE TO THE AIRCRAFT WAS LIMITED TO THE LEFT HORIZONTAL STABILIZER, LEFT ELEVATOR, LEFT WING TIP FAIRING AND ONE ANTENNA ON LOWER FUSELAGE. (.4) ON APRIL 26, 2001, ABOUT 1315 EASTERN DAYLIGHT TIME, A CESSNA 210N, N6585A, REGISTERED TO AND OPERATED BY AIR CARRIERS, INC., AS FAST CHECK FLIGHT 269, EXPERIENCED COLLAPSE OF THE MAIN LANDING GEAR DURING THE LANDING ROL L AT THE GAINESVILLE REGIONAL AIRPORT, GAINESVILLE, FLORIDA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND AN INSTRUMENT FLIGHT RULES (IFR) FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 135 NON-SCHEDULED DOMESTIC CARGO FLIGHT. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED AND THE COMMERCIAL-RATED PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. THE FLIGHT ORIGINATED AT 1155 FROM THE HERNANDO COUNTY AIRPORT, BROOKSVILLE, FLORIDA. THE PILOT STATED THAT THE FIRST TWO LEGS IN THE ACCIDENT AIRPLANE WERE UNEVENTFUL. THE FLIGHT DEPARTED ON THE THIRD LEG AND APPROXIMATELY 15 MINUTES INTO THE FLIGHT, HE NOTED A PROBLEM WITH THE AIRPLANE'S RADIOS. HE ATTEMPTED TO TROUBLESHOOT THE RADIO PROBLEM AND CHECKED THE AMMETER WHICH INDICATED A SLIGHT DISCHARGE. HE TURNED ON ALL THE AIRCRAFT'S LIGHT TO SEE IF THE AMMETER WOULD CHANGE; IT DID NOT. HE THEN SECURED ALL ELECTRICAL EQUIPMENT WITH THE EXCEPTION OF THE NO. 1 COMMUNICATION TRANSCEIVER AND TRANSPONDER. HE CHECKED THE CIRCUIT BREAKERS AND RESET THE ALTERNATOR SWITCH; WITH NEGATIVE RESULTS. ON APPROACH TO THE DESTINATION AIRPORT HE REMAINED HIGH AND BEGAN TO CIRCLE AWAITING LIGHT GUN SIGNALS FROM THE TOWER. HE RECEIVED A SIGNAL THAT THE FLIGHT WAS CLEARED TO LAND AND LOWERED THE LANDING GEAR ELECTRICALLY. HE REPORTED HEARING THE LANDING GEAR MOTOR OPERATE, FELT A SENSATION THAT HE EQUATED TO WAS THE LANDING GEAR LOCKING INTO POSITION, AND LOOKED OUT AND THOUGHT THAT THE MAIN LANDING GEAR WERE LOCKED INTO POSITION; HE COULD NOT SEE THE GEAR DOWN AND LOCKED LIGHT DUE TO SUNLIGHT. AFTER TOUCHDOWN, THE MAIN LANDING GEAR COLLAPSED; THE NOSE LANDING GEAR DID NOT COLLAPSE. EXAMINATION OF THE AIRPLANE BY AN FEDERAL AVIATION ADMINISTRATION (FAA) AIRWORTHINESS INSPECTOR REVEALED THAT THE "A+" ELECTRICAL CABLE WHICH IS CONNECTED TO THE ALTERNATOR AND TO A TERMINAL BOARD AT THE FIREWALL, SEPARATED FROM THE WIRE CONNECTOR AT THE TERMINAL BOARD AT THE FIREWALL. FURTHER EXAMINATION DETERMINED THAT THE CABLE WAS LOCALLY MANUFACTURED AND APPEARED TO BE TOO SHORT WHICH DID NOT ALLOW FOR VIBRATION. A COPY OF THE FAA INSPECTOR STATEMENT IS AN ATTACHMENT TO THIS REPORT. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB MIA01LA130](https://openairdocs.org/ntsb/MIA01LA130), Apr 26, 2001: Cessna 210N (N6585A), Gainesville, FL, substantial damage. Probable cause: The pilot's delay in securing all non-essential electrical equipment in-flight resulting in battery depletion before complete gear extension was accomplished using the normal system and subsequent… From the FAA Accident/Incident Data System. Reports are matched to registry aircraft 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. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.