Beech 1900C

Service difficulty reports · 1,840

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '1900C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA121023007Relay · failed(CAN) ON APPROACH, THE LANDING GEAR WOULD NOT DEPLOY, AFTER SEVERAL ATTEMPTS THE GEAR EXTENDED ON ITS OWN. THE AIRCAFT LANDED UNEVETFULLY. UPON INSPECTION THE LANDING GEAR RELAY WAS FOUND TO BE FULL OF WATER, FREEZING AT ALTITUDE CAUSING THE RELAY TO FAIL UNTOct 22, 2012 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA121022023Line · cracked(CAN) DURING CRUISE, THE CREW SHUTDOWN THE ENGINE IN FLIGHT AFTER GETTING THE LOW OIL PRESSURE WARNING IN THE COCKPIT. THE ACFT RETURNED SAFELY TO BASE. UPON INSPECTION OF THE ENGINE, THE OIL LINE RUNNING FROM THE TORQUE MANIFOLD TO THE ENGINE REDUCTION GEAOct 19, 2012 · Beech 1900C · Turbine Engine Oil SystemSDR CA121022007Oil System · low pressure(CAN) IT WAS REPORTED THAT JUST AFTER TAKEOFF THE PILOT NOTICED A LOSS OF OIL PRESSURE, AUTOFEATHER AND SHUTDOWN. GROUND INSPECTION REVEALED NO METAL CHIP AND OIL IN THE EXHAUST. TROUBLESHOOTING IN PROGRESS, WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPOct 10, 2012 · Beech 1900C · Engine Oil Indicating SystemSDR JIKA2012101001Sense Line · crackedAT APPROX 900 FT DURING CLIMBOUT FROM KSAT, RT ENGINE FAILED AND AUTOFEATHERED. ENGINE TORQUE, RPM AND PROP RPM ALL DROPPED. SECURED ENGINE PER THE CHECKLIST, DECLARED AN EMERGENCY AND RETURNED TO KSAT. MX DISCOVERED OIL RESIDUE IN THE EXHAUST AND ON THE 2NOct 10, 2012 · N3229A · Beech 1900C · Fuel Controlling SystemSDR YADA2012F00188Indicator · false indicationON DEPARTURE, PILOT EXPERIENCED A FUEL IMBALANCE THAT REQUIRED FULL AILERON TRIM TO CORRECT. ACFT RETURNED TO BASE, MX DETERMINED 1 FUEL QUANTITY INDICATOR WAS INDICATING INCORRECT FUEL QUANTITY. THE FUEL TANKS WERE SUMPED AND THE FAULTY GUAGE THEN INDICATEDOct 10, 2012 · N116AX · Beech 1900C · Fuel Quantity IndicatorSDR ERAA20120077Powerpack · defectiveNR 1 TRANSIT LIGHT FAILS TO GO OUT. RESET 60 AMP CURCUIT BREAKER IN LEFT NACELLE FOR MLG POWER PACK, OPS CHECKED GEAR 5 CYCLES, NO FAULTS FOUND. NR 2 GEAR FAILS TO EXTEND, REQUIRING MANUAL EXTENSION. REMOVED AND REPLACED POWER PACK ASSY IAW BEECH1900C MAINTOct 6, 2012 · N575A · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR TIMA20121003010Door Frame · crackedA CRACK WAS DISCOVERED IN THE AIRSTAIR DOOR FRAME DURING A FUSELAGE "C" STRUCTURAL INSPECTION. THE CRACK WAS LOCATED IN THE LOWER AFT SECTION OF DOOR FRAME AT FS 168. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH BEECH 1900C STRUCTURAL REPAIR MANUAL 53-90-08 & Oct 3, 2012 · N219VP · Beech 1900C · Fuselage Main, StructureSDR ERAA201209190063Warning System · false activationGEAR FAIL TO RETRACT-RED HANDLE UNSAFE LIGHTS REMAIN ON AFTER RETRACTION. PERFORMED GEAR SWINGS, LANDING GEAR INDICATION LIGHTS OPS CHECK NORMAL PER BEECH 1900C MM 32-30-00, OK FOR SERVICE.Sep 17, 2012 · N575A · Beech 1900C · Landing Gear Position and WarningSDR ERAA20120054Pipe · crackedDEPART ANC, PAX INDICATED SMOKE IN CABIN, LEVEL OUT, TURN BLEED AIR OFF, DUMP CABIN, DECLARED EMERGENCY, ROW 2 LEFT SIDE ROW 5 BOTH SIDES INDICATE BY 3 PAX. PERFORMED HP ENGINE RUNS WITH BLEEDS ON IN HOT AND COLD MODES, COULD NOT DUPLICATE VAPOR/SMOKE SMELL DAug 3, 2012 · N575Q · Beech 1900C · Humidity Control SystemSDR YADA2012F00156Windshield · crackedON CLIMBOUT, PASSING THROUGH 500 FT, THE OUTER PLY OF THE PILOT'S WINDSHIELD CRACKED FROM TOP TO BOTTOM. LANDED WITHOUT INCIDENT. THE WINDSHIELD WAS REPLACED BY MX.Jul 30, 2012 · N116AX · Beech 1900C · Flight Compartment WindowsSDR ERAA20120051Switch · out of adjustANC - FLAPS STUCK AT TAKEOFF. ANC- INFLIGHT GEAR HANDLE LIGHT DOES NOT COME ON. WARNING HORN SOUNDS. ADJUSTED RIGHT FLAP SWITCH IAW B-1900 MM 27-50-06. OPS CHECKED GOOD. OPS CHECKED GEAR WARNING SYSTEM AFTER ADJUSTING SPLIT FLAP SWITCH IAW B-1900MM 32-60-Jul 13, 2012 · N575Q · Beech 1900C · Trailing Flap Position Indicating SystemSDR CA120802011Compressor · fluctuates(CAN) DURING A TRAINING FLIGHT, THE CREW WAS CONDUCTING A SIMULATED ILS APPROACH AT THE AIRPORT. DURING THE INTERMEDIATE APPROACH, 5 NM FINAL. THE NR 2 ENGINE BEGAN TO SURGE WITH FLUCTUATING TORQUE AND COMPRESSOR SPEEDS. A PRECAUTIONARY SHUTDOWN WAS COMPLETJul 12, 2012 · Beech 1900C · Turbine Engine Compressor SectionSDR ERAA20120050Blower Motor · malfunctionedSMOKE IN CABIN REPORTED BY PASSENGERS. PASSENGERS BELIEVE THE SOURCE MAY HAVE BEEN THE FLOOR VENTS. PILOTS COULD NOT CONFIRM SMOKE, BUT RETURNED TO FAIRBANKS IMMEDIATELY AFTER DEPARTURE. CONFIRMED AFT VENT MOTOR AS CAUSE OF SMOKE. REMOVED BAD MOTOR INSTALLJun 28, 2012 · N575Q · Beech 1900C · Air Distribution FanSDR CA120420002Door Frame · cracked(CAN) CRACK FOUND ON CABIN DOOR FRAME CENTER LOCATION. THIS AREA IS NOT SPECIFIED TO INSPECT IN THE MFG INSPECTION PROGRAM. THIS LOCATION CAN BE SEEN WITH THE USE OF A BORESCOPE.Apr 20, 2012 · Beech 1900C · Fuselage Main, StructureSDR CA120502012Mount · delaminated(CAN) DURING SCHEDULED INSPECTION OF ENGINE MOUNT RUBBERS IT WAS DISCOVERED THAT THE RUBBERS WERE SEPARATING FROM THE METAL THAT THEY ARE ATTACHED TO AND ON SOME OF THEM ALMOST THE WHOLE LENGTH OF THE MOUNT. THE MOUNTS HAD ONLY BEEN INSTALLLED FOR 4 MONTHS AApr 19, 2012 · Beech 1900C · Engine Mount SectionSDR CA120413005Bracket · bent(CAN) WHILE COMPLETING THE LT ENGINE REMOVAL, MAINTENANCE PERSONNEL NOTED A FUEL DRIP COMING OUT OF THE LT WING ROOT. FURTHER INVESTIGATION FOUND THAT THE BLEED AIR LINE CLAMP HAD CHAFED THROUGH THE FUEL CROSSFEED TUBE IN 2 PLACES. THE BRACKET THAT HOLDS THEApr 12, 2012 · Beech 1900C · Wing, Attach FittingsSDR CA120412005Landing Gear · unknown(CAN) LANDING GEAR FAILED TO RETRACT FULLY AFTER TAKEOFF. GEAR MANUALLY EXTENDED SUCCESSFULLY LANDED WITHOUT FURTHER INCIDENT.Apr 12, 2012 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA120411014Starter Gen · seized(CAN) DURING TAXI, WE HAD A STARTER GENERATOR WARNING LIGHT ILLUMINATE ON THE NR 1 ENGINE. THE PILOTS SHUTDOWN THE ENGINE AT THE APRON AND CALLED MAINTENANCE. MAINTENANCE DISCOVERED THE STARTER/GEN FAN SHROUD HAD COME LOOSE DUE TO, 2 OUT OF THE 4 SCREWS FALLApr 9, 2012 · Beech 1900C · Starter-GeneratorSDR TIMA20120403006Skin · crackedA 1.75 INCH CRACK WAS DISCOVERED IN THE LOWER FUSELAGE SECTION AFT OF THE MAIN SPAR ON THE LEFT SIDE (FS 292) DURING A ROUTINE INSPECTION. THE CRACK WAS STOP DRILLED AND A DOUBLER INSTALLED IAW BEECH SRM CHAP 53-90-18.Apr 3, 2012 · N154GA · Beech 1900C · Fuselage Main, Plate/SkinSDR TIMA20120331005Cap · crackedAIRCRAFT WAS ON JACKS. WHILE CYCLING GEAR A LOUD POP WAS HEARD FROM THE NOSE LANDING GEAR ACTUATOR. EXAMINATION SHOWED A CRACK IN THE ACTUATOR END CAP AND HYDRAULIC FLUID LEAKAGE.Mar 30, 2012 · N114AX · Beech 1900C · Landing Gear ActuatorSDR TIMA20120329004Control Horn · wornRUDDER CONTROL HORN FOUND TO BE WORN DURING A DETAILED INSPECTION. INSTALLED A NEW RUDDER CONTROL HORN ASSEMBLY.Mar 29, 2012 · N125BA · Beech 1900C · Rudder Control SystemSDR TIMA20120329003Torque Tube · wornRUDDER TORQUE TUBE FOUND TO BE WORN DURING A DETAILED INSPECTION. INSTALLED NEW RUDDER TORQUE TUBE.Mar 29, 2012 · N125BA · Beech 1900C · Rudder Control SystemSDR JIKA2012032900001Wire · chafedON APPROACH, WHEN THE GEAR WAS SELECTED DOWN, CIRCUIT BREAKER TRIPPED. USED THE EMERGENCY LANDING GEAR EXTENSION. NO EMERGENCY WAS DECLARED. A SAFE LANDING WAS MADE. MAINTENANCE INVESTIGATION REVEALED DAMAGED AND CHAFED WIRING AT THE RIGHT GEAR SQUAT SWITMar 29, 2012 · N31705 · Beech 1900C · Landing Gear System WiringSDR CA120418007Oil System · low pressure(CAN) AFTER AROUND 40 MINUTES IN CRUISE ABOVE FL220, RT ENGINE OIL PRESSURE DROPS FROM 130 PSI DOWN TO 110 PSI AND FLUCTUATES ACCOMPANIED BY OIL LOSS. AS SOON AS THE ALTITUDE GOES DOWN BELOW FL220, OIL PRESSURE GOES BACK TO NORMAL. AFTER PERFORMING ALL TROUBLMar 23, 2012 · Beech 1900C · Engine Oil Indicating SystemSDR CA120323005Starter Gen · failed(CAN) IN FLIGHT FAILURE OF LY STARTER GENERATOR. THE PILOTS FOLLOWED SOP`S FOR A FAILED GENERATOR AND CONTINUED TO DESTINATION. MAINTENANCE PERFORMED MFG INSPECTIONS FOLLOWING A STARTER GENERATOR FAILURE. STARTER GENERATOR REPLACED WITH SERVICEABLE UNIT.Mar 20, 2012 · Beech 1900C · Starter-GeneratorSDR CA120321001Gear · failed(CAN) WHILE CARRYING OUT A 200 HR DETAILED INSPECTION, THE LT CHIP DETECTOR WAS REMOVED AND A SMALL BALL BEARING WAS FOUND ATTACHED TO 1 OF THE PROBES. IT WAS TOO SMALL TO BRIDGE THE GAP TO SHORT OUT THE CHIP DETECTOR. 2 BEARING RETAINERS WERE FOUND IN THE REMar 19, 2012 · Beech 1900C · Turbine Engine Reduction GearSDR EPUA20120307002Brake Sys · malfunctionedLT & RT BRAKE PEDALS HARD WHEN DEPRESSED BUT NO BRAKES WHEN PEDALS PUSHED VERY HARD MINIMAL BREAKING FELT. FEELS LIKE ANTI-SKID IS ACTIVATED BUT SWITCH IS IN OFF POSITION. CLEANED BREAKS, CHECKED RESERVOIR FLUID, OPS CHECKED GOOD ON GROUND.Mar 7, 2012 · N575Z · Beech 1900C · Landing Gear Brake SystemSDR JIKA12022301Valve · leakingAPPROXIMATELY 15 MINUTES AFTER DEPARTURE, THE PILOT REPORTED SMOKE IN THE COCKPIT COMING FROM THE CONDITIONED AIR VENTS. THE PILOT SHUTOFF THE LEFT AND RIGHT ENGINE ENVIRONMENTAL BLEED AIR AND DUMPED THE CABIN PRESSURIZATION, SMOKE DISSIPATED. PILOT RETURNEDFeb 23, 2012 · N31702 · Beech 1900C · Engine Fuel and ControlSDR CA120221002Compressor · cracked(CAN) FOLLOWING REMOVAL OF ACM DUE TO INABILITY OF RETAINING OIL, THE COMPRESSOR HOUSING INLET TUBE WAS FOUND CRACKED AROUD THE WELDED BASE ON APPROXIMATELY 200 DEGREES OF CIRCUMFERENCE. WAITING REPLACEMENT ACM FOR INSTALLATION.Feb 21, 2012 · Beech 1900C · Cabin Cooling SystemSDR YADA2012F00054Reduction Gb · making metalDURING FLIGHT 765, ENROUTE, THE PILOT OBSERVED TORQUE SURGES OF 400 FT LBS. TO 1,000 FT LBS. ON THE NR 1 ENGINE. THE ENGINE WAS SHUTDOWN AND THE FLIGHT CONTINUED ON TO ANC. ON LANDING, MX FOUND THE OIL FILTER CONTAMINATED WITH METAL DEBRIS AND CHUNKS OF WHATFeb 16, 2012 · N119AX · Beech 1900C · Turbine Engine Reduction GearSDR HSYA201202121Engine · failedDURING CLIMB OUT FOR A STAGING FLIGHT, CREW PULLED THROTTLE BACK AT APPROX 4000 FT, NR 1 ENGINE MADE A POPPING NOISE, FOLLOWED BY TORQUE DECREASING TO 2100 FT LBS, FOLLOWED BY AN ADDITIONAL POPPING NOISE FROM THE NR 1 ENGINE. THE CREW PULLED THE POWER ON THEFeb 12, 2012 · N319BH · Beech 1900C · Engine (Turbine/Turboprop)SDR CA120222008Oil Cooler · failed(CAN) OIL COOLER HAD ONLY BEEN INSTALLED THE MONTH BEFORE AND FAILED IN THE SAME AREA AS THE PREVIOUS COOLER LEADING TO AN INFLIGHT SHUTDOWN OF THE ENGINE. THE PROPELLERS WERE BALANCED, ENGINE ATTACH STRUCTURE INSPECTED, OIL COOLER MOUNTING INSPECTED ETC. BUTFeb 10, 2012 · Beech 1900C · Engine Oil CoolerSDR ERAA201200008Altimeter · inoperativeNR 1 ALTIMETER INOP. REPLACED ALTIMETER AND DID 2 YEAR CERTIFICATION IAW FAR 91.411, IAW FAR 43 APPENDIX E.Jan 28, 2012 · N575Q · Beech 1900C · Altimeter, Barometric/EncoderSDR ERAA201200007Switch · out of adjustCABIN WARNING DOOR LIGHT CAME ON. ADJUSTED CABIN DOOR SILL SWITCH, REFERENCE BEECH 1900C MAINTENANCE MANUAL 52-70-00. OPS CHECK GOOD.Jan 22, 2012 · N575U · Beech 1900C · Door Warning SystemSDR EPUA20120120003Indicator · malfunctionedFLAPS INDICATED STUCK DOWN.Jan 19, 2012 · N1553C · Beech 1900C · Trailing Flap Position Indicating SystemSDR YADA201201170001Wire Harness · corrodedON CLIMB OUT, THE PILOT RETRACTED THE LANDING GEAR BUT THE RED "GEAR INTRANSIT LIGHT" IN THE LANDING GEAR SELECTOR HANDLE NEVER EXTINGUISHED. THE GEAR WAS EXTENDED AND THE ACFT WAS LANDED AND RETURNED TO BASE. MX PERSONNEL FOUND THE A CONNECTOR PLUG AND WIRIJan 17, 2012 · N115AX · Beech 1900C · Landing Gear System WiringSDR CA120125006Oil Cooler · leaking(CAN) PILOTS NOTICED OIL PRESSURE DECREASING DURING CRUISE AND SHUTDOWN ENGINE AND LANDED AT NEAREST AIRPORT. MAINTENANCE DISCOVERED OIL UNDERNEATH THE PLANE IN THE GEAR WELL AREA AND THE OIL LEVEL WAS LOW AS WELL. GROUND RUNS INDICATED THAT THE OIL COOLER WASJan 12, 2012 · Beech 1900C · Engine Oil CoolerSDR ERAA201200002Relay · failedINTERMITTENT AND COMPLETE FAILURE OF EHSI, COMM NR 1 AND GPS SIMULTANEOUSLY WHILE IN CRUISE FLIGHT. HAPPENED TWICE FOR APPROX 1 TO 2 MINUTES. CHECKED ALL CONNECTIONS EHSI, COMM NR 1 COMM, GPS RESEATED ALL CONNECTIONS OPS CHECK SAT. ON GROUND. AFTER START TJan 6, 2012 · N575Q · Beech 1900C · Navigation SystemSDR CA120103021Relay · damaged(CAN) ON APPROACH, THE CREW SELECTED GEAR DOWN. THE LANDING GEAR FAILED TO EXTEND, AFTER SOME TIME, ABOUT 5 MINUTES, THE GEAR EXTENDED ON IT`S OWN. THE ACFT LANDED SAFELY, NO EMERGENCY WAS DECLARED. UPON INSPECTION, TECH DISCOVERED THE MLG RELAY WAS FILLED WDec 30, 2011 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 2011FA0000813Socket · unsecureON APPROACH WITH THE LANDING GEAR SELECTED DOWN, THE RT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. THE PILOT CYCLED THE GEAR AGAIN AND STILL DID NOT GET A RT MAIN GEAR DOWN AND LOCKED INDICATION. THE LANDING WAS ABORTED. THE PILOT TAPPED ON THE LIGHT AND Dec 30, 2011 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR JIKA11122301O-Ring · wornON CLIMBOUT THE PILOT REPORTED THAT VISIBLE SMOKE AND A SLIGHT OIL SMELL WAS PRESENT WHEN HE TURNED THE BLEED AIR ENVIRONMENTAL SYSTEM ON. THE PILOT SHUT OFF THE ENVIRONMENTAL BLEED AIR SYSTEM AND RETURNED TO KPHX AND LANDED WITHOUT INCIDENT. MAINTENANCE PERDec 23, 2011 · N718AF · Beech 1900C · Turbine Engine Oil SystemSDR EPUA20120112001Bulb · burned outLANDING LIGHT INDICATOR NO GREEN RT MAIN, MX DETERMINED THAT BULBS WERE BLOWN, INSTALLED NEW INDICATOR BULBS FOR THE GEAR INDICATION PANEL, OPS CHECK OK.Dec 19, 2011 · N15503 · Beech 1900C · Landing Gear Position and WarningSDR HSYA2011FA0000764Wire · brokenDURING CLIMB OUT OF A FERRY FLIGHT, CREW ATTEMPTED TO RETRACT THE LANDING GEAR. GEAR LIGHTS REMAINED IN THE DOWN AND 3 GREEN POSITION. ELECTED TO RETURN TO DEPARTURE. CREW PERFORMED A FLY BY OF THE TOWER, WHO ADVISED IT APPEARED THE RT GEAR WAS NOT FULLY EXTNov 29, 2011 · N205CA · Beech 1900C · Landing Gear System WiringSDR TIMA20110005Actuator · bypassingWHEN LANDING GEAR WERE LOWERED FOR LANDING, THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. CB WAS RESET AND LANDING GEAR EXTENDED FULLY WITH 3 GREEN LIGHTS. POST FLIGHT INSPECTION REVEALED THAT THE RIGHT MAIN LANDING GEAR ACTUATOR WAS BYPASSING FLUID.Nov 13, 2011 · N192GA · Beech 1900C · Landing Gear ActuatorSDR CA111114012Bracket · misaligned(CAN) CRITICAL FAILURE, BOB WEIGHT STOP BRACKET WAS MISALIGNED FROM THE FACTORY, ALLOWING THE BOB WEIGHT ASSEMBLY PN 114-524061-17 TO PERIODICALLY SLIP PAST THE STOP. THE BOB WEIGHT SLIPPED PAST IT`S STOP, ALLOWING THE LINK ASSEMBLY PN 101-524112-1 TO GO OVERNov 11, 2011 · Beech 1900C · Control Column SectionSDR YADA2011110700001Wire · looseON TAKEOFF ROLL, THE LANDING GEAR "IN TRANSIT" LIGHT ILLUMINATED. THE CREW ABORTED THE TAKEOFF AND TAXIED BACK TO THE HANGAR. THE LIGHT REMAINED ILLUMINATED UNTIL THE LT ENGINE WAS SHUTDOWN. MX DISCOVERED THAT A WIRE HAD COME LOOSE FROM A LANDING GEAR WARNINNov 7, 2011 · N116AX · Beech 1900C · Landing Gear System WiringSDR CA111108008Bearing · failed(CAN) STARTER GENERATOR DRIVE END BEARING SUFFERED CATASTROPHIC FAILURE. BEARING IS INSTALLED IN A STARTER GEN WITH A 1500HR TBO, BEARING FAILED AFTER 370HRS SINCE NEW.Nov 4, 2011 · Beech 1900C · Starter-GeneratorSDR YADA2011F00212Line · rupturedON A PREFLIGHT WALK AROUND INSPECTION OF THE ACFT, THE FLIGHT CREW NOTICED A PUDDLE OF HYD FLUID ON THE GROUND AROUND THE RT MLG. HYD FLUID WAS ALSO NOTED ON THE GEAR AND IN THE WHEEL WELL. ARRANGEMENTS WERE MADE AND A FERRY PERMIT ISSUED FOR A FERRY FLIGHT Oct 13, 2011 · N113AX · Beech 1900C · Hydraulic System, MainSDR CA110916005Wire Harness · damaged(CAN) THE WIPER CIRCUIT BREAKER WAS TRIPPING. WE FOUND THE DAMAGED WIRING IN THE OVERHEAD PANEL LOCATED IN THE COCKPIT BETWEEN THE PILOT AND CO-PILOT SEAT.Sep 15, 2011 · Beech 1900C · Ice/Rain Protection System WiringSDR JIKA20110826001Control Cable · brokenON PREFLIGHT INSPECTION, THE PILOT NOTICED THERE WAS NO RESISTANCE IN THE RUDDER PEDALS WHEN MOVED FROM LT TO RT, THIS WAS CONFIRMED WHEN THE PILOT MOVED THE RUDDER PEDALS AND ANOTHER PILOT CONFIRMED THERE WAS NO RUDDER MOVEMENT. MX INSPECTED THE RUDDER CONTRAug 26, 2011 · N31701 · Beech 1900C · Rudder Control System
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