N126YV, cancelled Jun 30, 2010

Service difficulty reports · 37

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

Query with SQL
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 n_number = 'N126YV' AND deregistration_id = 'N126YV-2010-06-30'
  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 AMWA89204Pcb · inoperativeLANDING GEAR GAVE NO REACTION WHEN GEAR HANDLE EXTENDED. MOVED FLAPS TO FULL DOWN, LANDING GEAR WARNING HORN SOUNDED. FOLLOWED EMERGENCY CHECKLIST AND MANUALLY EXTENDED THE GEAR AND GOT 3 GEAR SAFE INDICATION LIGHTS AND LANDED SAFELY. MAINTENANCE REPLACED A316Dec 20, 2007 · N126YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR AMWA28032Spar · shearedSHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R.Jul 5, 2007 · N126YV · Beech 1900D · Wing SparSDR AMWA7026DRib · corrodedBIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/BulkheadSDR AMWA7026CSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR AMWA7026BSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR AMWA7026ARib · corrodedBIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702-4 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/BulkheadSDR AMWA7020ESkin · crackedFUSELAGE SKIN CRACKED, LENGTH APPROX 1.5 INCHES. REPAIRED IAW REPORT #6702-3 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA7020DSkin · crackedRT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 6702-2 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Plate/SkinSDR AMWA7020BFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR AMWA7020AFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR AMWA7020CFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW ACFT REPORT NR 6702-1 REV 1RJun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR AMW082671Actuator · false indicationON APPROACH TO LANDING THE NOSE GEAR INDICATOR D/N SHOW GEAR DOWN AND LOCKED. CREW PERFORMED EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. A FLY-BY OF THE TOWER CONFIRMED GEAR WAS DOWN. THE INTRANSIT LIGHT IN THE GEAR HANDLE WAS ALSO OUT. SO CREW LANDED SFeb 15, 2007 · N126YV · Beech 1900D · Landing Gear ActuatorSDR AMWA82479BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR THE DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Feb 5, 2007 · N126YV · Beech 1900D · Battery/Charger SystemSDR AMWA81896Bulb · inoperativeWHEN GEAR WS EXTENDED FOR LANDING, THERE WAS NO DOWN AND LOCKED INDICATION ON ANNUNCIATOR. CREW DECLAIRED EMERGENCY, AND FOLLOWED PROCEDURES. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED ANNUNCIATOR BULBS. PENDING ADL RETURN.Jan 7, 2007 · N126YV · Beech 1900D · Landing Gear Position and WarningSDR AMW1061011025Spar Cap · corrodedFOUND CHAFING AREA, LT WING LOWER MAIN SPAR CAR, FORWARD SURFACE AT APPROX. WS 72.0. REPAIRED IAW MFG FR-CO-01437 REV. 1.Oct 13, 2006 · N126YV · Beech 1900D · Wing SparSDR AMWA078634Cable · brokenON PREFLIGHT, THE CREW COULD NOT OPEN THE CABIN DOOR. MAINTENANCE WAS CALLED AND FOUND THE INNER FORWARD DOOR CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BROKEN CABLE AND CABLE GUIDE ASSY.Jul 27, 2006 · N126YV · Beech 1900D · Passenger/Crew DoorsSDR 1051213026AAngle · crackedDURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED.Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous StructureSDR 1051213026Angle · crackedDURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED.Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous StructureSDR 71138Diode · faultyEMERGENCY COCKPIT LIGHTING ON, OFF HOT BATTERY BUSS, MAIN BATTERY SWITCH OFF AND SWITCH FOR FLIGHT INSTRUMENT INDIRECT LIGHTS ON. ELECTRICAL ODOR IN COCKPIT AREA. MAINTENANCE REMOVED AND REPLACED DIODE.Jun 2, 2005 · N126YV · Beech 1900D · Emergency LightingSDR 71124Rheostat · burnedCREW CALLED IN AND REPORTED THAT WITH COCKPIT EMERGENCY LIGHTS ON, BATTERY OFF, INDIRECT LIGHTING ON, THERE WAS AN ELECTRICAL BURNING ODOR. MAINTENANCE REMOVED AND REPLACED INDIRECT LIGHT RHEOSTAT SWITCH.Jun 1, 2005 · N126YV · Beech 1900D · Passenger Compartment LightingSDR 68027Wheel · damagedUPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STOPPED THE AIRCRAFT ON THE APRON WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY, NOSE GEAR ASSY, DRAG LEG ASSY. VISUALLY INSDec 29, 2004 · N126YV · Beech 1900D · Nose/Tail Landing GearSDR 66764Light · looseDURING TAXI, CREW NOTED TAXI LIGHT JUMPING BACK AND FORTH. RETURNED TO GATE AND NOTED TAXI LIGHT HAD COME LOOSE AT MOUNTING POINT. NO FURTHER INCIDENT. REMOVED AND REPLACED LIGHT ASSY BULB AND HARDWARE, P/N A715-1, 130909B124, 130909B45, 130909N32.Nov 14, 2004 · N126YV · Beech 1900D · Exterior LightingSDR 66269Yaw Damper · malfunctionedYAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETURNED TO GATE AND THE SYSTEM WAS DEFERRED WITH NO FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND YAW DAMPER OPS CK NORMAL.Oct 29, 2004 · N126YV · Beech 1900D · Autopilot SystemSDR 63720Wire · brokenAIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE BOTTLE, OPS CK NORMAL.Aug 7, 2004 · N126YV · Beech 1900D · Fire Protection System WiringSDR 61901Downlock Switch · malfunctionedWITH MAIN LANDING GEAR SELECTED DOWN THE LEFT MAIN LANDING GEAR WON'T INDICATE DOWN AND LOCKED. AIRCRAFT DIVERTED TO DUJ. EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LT MLG ACTUATOR/DOWNLOCK SWITCH CK GOOD. P/N 114-38May 31, 2004 · N126YV · Beech 1900D · Landing Gear Position and WarningSDR 61743Control Unit · malfunctionedON APPROACH FOR LANDING IN PFN, THE LT MAIN GEAR WON'T INDICATE DOWN AND LOCK. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED A125 PCB, OPS CHECK NORMAL. P/N 101-364578-9, S/N 671396.May 25, 2004 · N126YV · Beech 1900D · Landing Gear Position and WarningSDR 61073Connector · burnedCREW REPORTED ON APPROACH ANNUNICATOR C.B. TRIPPED. IT WAS RESET AND POPPED AGAIN. THERE WAS A FAINT BURNED ODOR IN THE CABIN. LANDED WITH NO FURTHER INCIDENT. R&R FEED THRU CONNECTOR.May 3, 2004 · N126YV · Beech 1900D · Electrical ConnectorsSDR 56696Latch · brokenUPON ARRIVAL CREW HAD DOOR WARNING ANNUNCIATOR. IT WOULD NOT EXTUNGUISH. MAINT WAS CALLED AND FOUND LATCH CABLE BROKEN. CABIN DOOR INOPERATIVE CAMS ON AFT SIDE WILL NOT CLOSE. REMOVED AND REPLACED AFT DOOR LATCH CABLE. P/N 129-514059-25Dec 2, 2003 · N126YV · Beech 1900D · Passenger/Crew DoorsSDR 54992Indicator · failedRIGHT TORQUE GAUGE FAILED ON TAKE OFF DURING INITIAL POWER UP. RETURNED TO GATE AND CALLED MX. REPLACED GAUGE OPS CK GOOD P/N 114-3800-653 SN 390MU.Oct 6, 2003 · N126YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR 52034Uplock Switch · faultyDURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3GREEN) INICATIONS. LANDING NORMAL WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED ON TJun 28, 2003 · N126YV · Beech 1900D · Landing Gear Position and WarningSDR 52034AMWA2Valve · failedDURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3 GREEN) INDICATIONS. LANDED NORMALLY WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED OJun 28, 2003 · N126YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 049124Circuit Breaker · failedAFTER TAKE OFF FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 706,WHEN THE LANDING GEAR WAS SELECTED UP, SMOKE WAS DETECTED FROM THE RIGHT HAND CIRCUIT BREAKER PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. THE CREW RETURNED TO FAMar 24, 2003 · N126YV · Beech 1900D · Electrical Power System WiringSDR 57708Actuator · malfunctionedAPPROACH, L/G HANDLE MOVED TO LWR GEAR, RED INTRANSIT LAMPS FLICKERED, 5-AMP L/G IND ON RT C/B PANEL POPPED. L/G EXTENDED, 3 GEAR DOWN LIGHTS FAILED TO ILLUM, WOULD NOT RESET. TOWER VERIFIED NOSE L/G EXTENDED. MALFUNCTION NOT DUPLICATED ON GROUND. L/G IND Jan 7, 2003 · N126YV · Beech 1900D · Landing Gear ActuatorSDR 044989Fire Loop · brokenDURING CREW CHANGEOVER IN ALBUQUERQUE, THE PILOTS DISCOVERED THAT THE LT FIRE HANDLE ILLUMINATED DURING PREFLIGHT CHECKS. THE LIGHT WOULD NOT EXTINGUISH. THE CORRECTIVE ACTION WAS THAT MAINTENANCE FOUND THE FORWARD LOOP BROKE. THEY INSTALLED A NEW LOOP. NO TEANov 12, 2002 · N126YV · Beech 1900D · Fire DetectionSDR MASA98175Switch · out of adjustFLT 5331 - RDG-PHL - THE LEFT AUTOFEATHER WOULD NOT ARM ON TAKEOFF, AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 12, 1998 · N126YV · Beech 1900D · Propeller Feathering/ReversingSDR 97ZZZX3290Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N126YV · Beech 1900D · Trailing Edge FlapsSDR 95ZZZW464De-Ice Boot · separatedTWO PROP DE-ICE BOOTS SEPARATING FROM LEADING EDGE EROSION SHIELD. PAINT ON SHIELD SEPARATED FROM SHIELD. SUBMITTER SUGGEST IMPROVING PAINTING PROCEDURES ON PROP BLADES OR LEAVING PAINT OFF OR EROSION SHIELD.Mar 11, 1995 · N126YV · Beech 1900D · Propeller Deice Boot Section
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