N709TA

Cancelled 2013

Deregistered aircraft · 1998 Beech 400A · Pratt & Whitney Canada JT15D 5 series

Cancelled
September 26, 2013
Exported to
Czech Republic
Status when cancelled
Valid registration
Serial number
RK-180
Year built
1998
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 11, 1998
Certificate issued
September 24, 2008
Last registry action
April 25, 2012
Mode S code
A977A7
Owner when cancelled
Flight Options LLC
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 4

FAA accident and incident reports matched to this aircraft by N709TA and the event date: up to this one’s cancellation.

Service difficulty reports · 15

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DJFA2009001Control Unit · failedAFTER LANDING, CREW REPORTED ANTI-SKID FAIL 5 SECONDS AFTER APPLICATION OF BRAKES RESULTING IN TOTAL LOSS OF BRAKING ACTION. BRAKES RETURNED WHEN ANTI-SKID WAS TURNED OFF. MX FOUND THE ANTI-SKID CONTROL UNIT FAILED AND IT WAS SUBSEQUENTLY REPLACED.Jan 6, 2009 · N709TA · Beech 400A · Brake Anti-Skid SectionSDR DJFA2008001Uplock Switch · erraticDURING CLIMB-OUT CREW REPORTED RED LIGHTS IN GEAR SELECT HANDLE ILLUMINATED FOLLOWED BY SLIGHT DECELERATION AND A THUMP. CREW SUSPECTS THE GEAR EXTENDED AND RETRACTED UNCOMMANDED. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH ERRATIC IN COLD TEMPERATURES. THE Jan 2, 2008 · N709TA · Beech 400A · Landing Gear Position and WarningSDR DJFA2007139Unknown · odorON APPROACH CREW REPORTED BURNING SMELL FROM THE RT REAR FLOOR AREA. MAINTENANCE RAN THE AIRCRAFT BUT WAS UNABLE TO DETECT ANY SMELL IN ALL CABIN TEMPERATURE MODES (AUTO/MANUAL, HOT AND COLD). AIRCRAFT WAS RELEASED.Dec 5, 2007 · N709TA · Beech 400A · Air Distribution SystemSDR DJFA2007136Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUNov 19, 2007 · N709TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006289Bulb · blownKMRY - KOAK. AFTER THE LANDING GEAR WERE EXTENDED FOR LANDING THE RIGHT MAIN GEAR DOWN INDICATION DID NOT ILLUMINATE. THE CREW PERFORMED A GO-AROUND SO THEY COULD VERIFY GEAR POSITION BEFORE LANDING. NO GEAR WARNING HORN, AND NO RED GEAR HANDLE LIGHT WERE RJul 20, 2006 · N709TA · Beech 400A · Landing Gear Position and WarningSDR DJFA2006278Anti-Skid Sys · inoperativeWHILE SLOWING THROUGH APPROX 10 -15 KTS ON ROLLOUT, LOST BRAKING ACTION. ANTI-SKID SYS WAS SELECTED OFF, BRAKES RETURNED IMMEDIATELY. ONCE AC WAS SLOWED TO TAXI SPEED ANTI-SKID (ABS) SYS WAS SELECTED BACK ON AND BRAKES WERE AVAILABLE. MAINT ISSUED MEL 32-1 Jun 30, 2006 · N709TA · Beech 400A · Brake Anti-Skid SectionSDR DJFA2006237Brake Assy · leakingTRIP ID NR 1013020, THE CREW REPORTED THAT THE BRAKES FAILED ON LANDING WHILE SLOWING THROUGH APPROXIMATELY 20 KNOTS. AFTER A FEW SECONDS POWER BRAKING OPERATED NORMALLY. NO DISCREPANCIES WERE NOTED WHEN MAINTENANCE PERFORMED ANTI-SKID RESPONSE SYSTEM CHECApr 30, 2006 · N709TA · Beech 400A · BrakeSDR DJFA2005181Odor · detectedDURING T/O A HEAVY ODOR SIMILAR TO MELTING PLASTIC COMING FROM PAX COMPT AT TIME OF DISCOVERY, TEMP CONTROL WAS SET ON AUTO, TEMP KNOB IN HOT POSITION. CREW DONNED THEIR OXYGEN MASKS & TURNED OFF ALL CABIN HEAT. APPROX 10 MINS ODOR DISSIPATED. A NORMAL LANDDec 26, 2005 · N709TA · Beech 400A · Air Distribution SystemSDR DJFA2005161Warning Light · illuminatedKRFD - KSDF DURING CRUISE FLIGHT, WHILE ENRANGE TO KLEX, THE CREW NOTED THAT THE HYDRAULIC FLUID PRESSURE WAS INDICATING 2,000 PSI. DUE TO A LONGER RUNWAY LENGTH THE AIRCRAFT WAS DIVERTED TO KSDF AND AN EMERGENCY WAS DECLARED. A MANUAL GEAR EXTENSION WAS PERNov 16, 2005 · N709TA · Beech 400A · Hydraulic System, MainSDR DJFA2005141Connector · defectiveCREW REPORTED DURING CRUISE FLT, HYDRAULIC PRESSURE INDICATED 2,000 PSI AND ON RED LINE. WHEN PRESSURE RELIEF SWITCH MOVED, HYDRAULIC PRESSURE INDICATED 100 PSI. DUE TO A LONGER RUNWAY LENGTH AIRCRAFT DIVERTED TO KLGB AND AN EMERGENCY DECLARED. A MANUAL GEASep 22, 2005 · N709TA · Beech 400A · Hydraulic Power System WiringSDR DJFA2005135Pump · wornTHE CREW REPORTED THAT THE HYDRAULIC PRESSURE WAS READING HIGH IN FLIGHT. WHEN THE HYDRAULIC PRESSURE DROPPED TO ZERO THE CREW CLOSED THE EMERGENCY DUMP VALVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KSAN DUE TO THE HIGHER RUNWAY LENGTH INAug 24, 2005 · N709TA · Beech 400A · Hydraulic Pump (Electric/Engine), MainSDR DJFA2005055Brake Assy · wornCREW REPORTED, AFTER LANDING THE BRAKES FAILED AFTER 50 KTS. EMERGENCY BRAKING SYSTEM WAS USED TO STOP THE AIRCRAFT. MAINTENANCE FOUND THE LEFT AND RIGHT BRAKE ASSEMBLIES TO BE WORN. THE LEFT AND RIGHT BRAKE ASSEMBLIES WERE REPLACED. MANUAL AND POWER BRAKEFeb 3, 2005 · N709TA · Beech 400A · BrakeSDR DJFA2004034Pump · out of limitsCREW REPORTED, IN CLIMB, NOTICED HYD PRESS FLUCTUATING ABOVE NORM. AFTER FL390, PRESS STABLE FOR 5 TO 10 MINS THEN INCREASED TO 2000 PSI AND HELD. EMERG DECLARED. A/C LANDED USING ALT GEAR EXTENSION, WITH A NO FLAPS APPROACH. PWR BRAKE FAILURE CHECKLIST USEDNov 19, 2004 · N709TA · Beech 400A · Hydraulic System, MainSDR RASFTYRK180Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.Nov 13, 2001 · N709TA · Beech 400A · Engine Mount SectionSDR RK180Bleed Valve · failedWHILE IN CRUISE FLIGHT FROM KBCT TO KBVT AT FL410 THE FLIGHT HEARD A LOUD BANG FOLLOWED BY OSCILLATIONS ON THE ROLL AXIS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED AT KLACY WITH NO FURTHER PROBLEMS. REPLACED RT ENGINE BLEED ACTUATOR VALVE PER PWCJan 25, 2001 · N709TA · Beech 400A · Compressor Bleed Valve

Other aircraft with N709TA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N709TA is registered now to the first aircraft listed.