N255GL

Service difficulty reports · 77

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 = 'N255GL' AND registry_match = 'registration'
  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 GLBA2016111400615Cable · brokenPILOT REPORTED THAT THE CABLE BROKE BETWEEN THE CABIN DOOR AND THE SNUBBER. MAINTENANCE REPLACED THE AIRSTAIR DOOR CABLE FROM THE SNUBBER TO THE DOOR.Nov 12, 2016 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2015050800519Fastener · looseSIG EVENT, MX REPORTED THAT THE CABIN DOOR WILL NOT CLOSE FROM THE OUTSIDE OF ACFT. FOUND LOOSE HARDWARE AT THE INTERNAL HANDLE BELL CRANK. SECURED HARDWARE IAW AIM 12.15.0. OPERATIONS CHECKED GOOD.May 8, 2015 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2014091900443Skin · corrodedDURING A SCHEDULED INSPECTION FOUND SKIN CORROSION & BULGING, 6 INCH AREA, RUNNING LATERALLY ALONG FORMER RING UNDER CARGO BAY AREA AT APPROX FS 497.00 & APPROX WL 76.00 RUNNING APPROX RBL 9.00 TO RBL 15.00. THE CORROSION & BULGING SKIN HAS CAUSED A .5 INCH Sep 18, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014050600412Skin · crackedDURING A SCHEDULED INSPECTION, MX FOUND A CRACK AT THE EMERGENCY EXIT, RT FWD, BONDED SKIN AT THE LWR AFT CORNER, 1.3" IN LENGTH. REPAIRED IAW EO 14-1900-52-004.May 5, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014042800411Rib · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT WING INBD RIB FLANGE & DOUBLER FLANGE AT FS 288 & BL 29.06, FROM OTBD EDGES INWARD TO BEND RADIUS OF THE RIB FLANGE & DOUBLER FLANGE, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIApr 28, 2014 · N255GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014042400410Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.25 BETWEEN STRINGER 2R & 3R AT THE INBD LOWER CORNER AT AIR DUCT CUTOUT FROM A FASTENER TO THE BEND RADIUS, .2 INCHES IN LENGTH. MAJOR REPAIR, REPAIRED THE AFFECTED AREA AND PERFORApr 24, 2014 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2014041500408Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 3 CRACKS AT FS 163.97 & STRINGER 1, AT FASTENERS ON LT & RT SIDE OF STRINGER 1, .35 INCHES IN TOTAL LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-024.Apr 15, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014031700404Tire · blownPILOT NOTED THAT BOTH LT MAIN TIRES BLEW ON LANDING. R & R NR 1 & NR 2 MAIN WHEEL ASSEMBLIES IAW TASK CARD 1900-3240-01. PN 5006028-5, NR 1 SN ON 56/917, SN OFF 1601, NR 2 SN ON 561 431, SN OFF 284 1930. PERFORMED VISUAL INSPECTION OF LT MLG HUBS, BRAKES & Mar 16, 2014 · N255GL · Beech 1900D · TireSDR GLBA2014030300398Channel · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT HAT SECTION OF THE UPPER FLANGE FROM FWD FASTENER TO FLANGE LE, VSS 84.10 & 206 CHORD, .35 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-002.Mar 3, 2014 · N255GL · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA2013030700199B-Nut · loosePILOT REPORTED THAT WHILE EXTENDING THE GEAR, MAINS SHOWED DOWN AND LOCKED, NOSE DID NOT SHOW GREEN INDICATION, GEAR HANDLE IN TRANSIT, REMAINED ILLUMINATED, RAN CHECKLIST, MANUALLY PUMPED GEAR DOWN, HAD 3 GREEN INTRANSIT LIGHT EXT, LANDED WITH NO FURTHER INCIMar 6, 2013 · N255GL · Beech 1900D · Hydraulic System, MainSDR GLBA2012121100133Stabilon · damagedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT STABILON AFT OTBD CORNER HAS FIBERGLASS DAMAGE MEASURING APPROX 4" X 3". REPAIRED IAW EO 13-1900-55-001. MAJOR REPAIRDec 11, 2012 · N255GL · Beech 1900D · Horizontal Stabilizer Miscellaneous StructureSDR GLBA2012102400087Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE FROM UPPER FASTENER HOLE TO UPPER EDGE OF ANGLE, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-050. MAJOR REPAIR.Oct 24, 2012 · N255GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012102200086Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON FRAME AT FS 183.25 AND STRINGER 1, DOWNWARD TO THE EDGE OF THE FRAME, 2.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-057. MAJOR REPAIR.Oct 22, 2012 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2012102200083Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB AT THE 2 O'CLOCK POSITION, .125" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-049. MAJOR REPAIR.Oct 20, 2012 · N255GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012101900081Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT, STARTING AT TOP FASTENER AT FSS 84.18 MOVING DOWN TO THIRD FASTENER AT FSS 84.16, 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-048.Oct 19, 2012 · N255GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012092400068Cam · out of adjustPILOT REPORTED THAT THE AIRSTAIR DOOR IS DIFFICULT TO OPEN. MX ADJUSTED 2 AFT LOWER CAM'S IAW BMM 52-10-00, OPS CK GOOD.Sep 24, 2012 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20111130KWheel · out of balancePILOT REPORTED THAT WHEN THE GEAR WAS RETRACTED, A STRONG VIBRATION WAS FELT FOR ABOUT 10 SECONDS. MX PERFORMED GEAR SWINGS IAW AIM CHAP 10 32-01, NO DEFECTS NOTED, REPLACED NOSE WHEEL PN: 114-8001-35, SN: 2345 IAW TC. 1900-3240.00 R2, OPS CK GOOD.Nov 29, 2011 · N255GL · Beech 1900D · Wheel/Ski/FloatSDR GLBA20110913FLanyard · brokenPILOT REPORTED THAT THE AIR STAIR DOOR LANDYARD BROKE. MX REPLACED THE DOOR SNUBBER CABLE, PN: 129-514119-1GLA, IAW BMM 52-12-01, OPS CHECKED GOOD.Sep 12, 2011 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110818GCover · tornMX FOUND THE AIRSTAIR DOOR UPPER FWD CABLE COVER TORN. MX REPLACED THE CABLE IAW MM 52-10-02, PN: 1440-40GLA.Aug 18, 2011 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110818FCover · tornMX FOUND THE AIRSTAIR DOOR LOWER FWD CABLE COVER TORN. MX REPLACED THE CABLE IAW MM 52-10-02, PN: 1440-43GLA.Aug 18, 2011 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110817JPropeller · malfunctionedPILOT REPORTED THAT THE RT PROP GOES INTO FEATHER BEFORE TAKING BEYOND FEATHER GATE, GOES INTO FEATHER IN THE TAXI POSITION. MX RAN ENGINES, PROP DIDN'T GO INTO FEATHER UNTIL THE LEVER REACHED THE FEATHER STRIP ON THE QUADRANT, SYS OK FOR SERVICE.Aug 16, 2011 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110518GTire · failedPILOT REPORTED THAT DURING SIGNIFICANT LEFT QUARTERING CROSSWIND LANDING BOTH RT MAIN TIRES BLEW AND BECAME FLAT. MAINTENANCE R&R NR 3 AND NR 4 MAIN TIRES IAW TC 1900-3210.01,May 18, 2011 · N255GL · Beech 1900D · TireSDR GLBA20110405GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FWD FUSELAGE FRAME AT F.S. 456 CRACKED AT THE GAS STRUT MOUNT UPPER IB NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSApr 5, 2011 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110405JSkin · chafed"SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND RH OB FWD CORNER OF FUSELAGE BELLY SKIN AT F.S. 258.25 CHAFFED THROUGH, AREA OF CHAFE 2.2" BY .6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSApr 5, 2011 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110404FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CUTOUT IS CRACKED AT THE IB LWR CORNER OF THE COUTOUT, CRACK IS .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUApr 4, 2011 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100628GCircuit Board · dirtySUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE LT AUTO FEATHER SYS DISENGAGED REPEATEDLY IN ALL POWER SETTINGS. MX REMOVED THE A123 PRINTED CIRCUIT BOARD, CLEANED CONTACTS, RE-INSTALLED THE A123 PRINTED CIRCUIT BOARD IAW MX INSTRUCTION 24-01. MX RAN THE ENGIJun 27, 2010 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20100611GSkin · damagedMAJOR REPAIR - REF GLBA20100611F, FOUND UNDERLYING DAMAGE DURING REPAIR OF LEFT WING LEADING EDGE STRINGER AT LEFT WS 201 HAS REPAIR DAMAGE WITH MISSING MATERIAL. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900Jun 10, 2010 · N255GL · Beech 1900D · Wing, Plate/SkinSDR GLBA20100611FStructure · crackedPILOT REPORTED A CRACK ON THE LEFT WING UPPER FORWARD SIDE AT APPROXIMATELY WS 194, FURTHER EVALUATION DISCOVERED THE CRACK TO BE AERODYNAMIC FILLER ONLY, BUT DID FIND AN UNDERLYING REPAIR THAT REQUIRES REWORK. MAJOR REPAIR - MAINTENANCE REPAIRED THE AFFECTEDJun 10, 2010 · N255GL · Beech 1900D · Wing, Plate/SkinSDR GLBA201005162Unknown · smokeHAD SMOKEY LOOK IN ROW 2 FROM PAX MODE CONTROL IN MANUAL, SHUT SYS DOWN, MX RAN NR 1 ENG AND WITH BLEED AIR ON, OPERATED THE ENVIRONMENTAL SYS IN MANUAL AND MANUAL COOL MODES. OPERATED THE BLOWERS IN HIGH AND AUTO. COULD NOT DUPLICATE SMOKE. NO UNUSUAL ODORS DMay 16, 2010 · N255GL · Beech 1900D · Air Distribution SystemSDR GLBA200910251Bulb · inoperativeFO'S EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OF THE LIGHT WAS GOOD.Oct 25, 2009 · N255GL · Beech 1900D · Emergency LightingSDR GLBA20091026FBulb · inoperativeEES - PILOTS REPORTED THAT THE FIRST OFFICERS EMERGENCY INSTRUMENT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OFOct 20, 2009 · N255GL · Beech 1900D · Emergency LightingSDR GLBA20090918FFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK IN THE AIRSTAIR DOOR LOWER FUSELAGE FRAME AT F.S. 173.41 AND STRINGER 11L. CRACK LENGTH APPROXIMATELY .750" IN LENGTH. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER FUSELAGE FRAME IAW E.OSep 16, 2009 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20090606AValve · inoperativePILOTS REPORTED THAT THE RT ENVIRO FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. MX REMOVED AND REPLACED THE RT PRE-COOLER VALVE IAW MM 21-11-00. THE OPS CHECK WAS GOOD.Jun 6, 2009 · N255GL · Beech 1900D · Air Distribution SystemSDR GLBA20090405BConnector · loosePILOTS REPORTED THAT EXPERIENCED A DROP IN THE RIGHT HAND PROPELLER RPM AND THAT IT HAD DROOPED TO 1620 RPM ON TAKEOFF. MAINTENANCE CLEANED THE CONNECTOR ON THE RIGHT HAND PROPELLER TACH GENERATOR AND RE-INSTALLED. REFERENCE BEECH 1900 MM 77-10-00.Apr 5, 2009 · N255GL · Beech 1900D · Propeller/Propulsor System WiringSDR GLBA20090304HSwitch · out of adjustFLT 5106 - ON APPROACH THE PILOTS REPORTED THAT THE NR 2 ENGINE CYCLES IN AND OUT OF FEATHER AT APPROXIAMTELY 1000 LBS. OF TORQUE AS THEY INCREASED POWER ON FINAL. THEY WERE NOT SURE OF THE N1 AT THE TIME. MAINTENANCE REMOVED AND REPLACED THE PROP OVERSPEED GMar 3, 2009 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090228AEngine · out of rigPOWER LEVERS SEEM OUT OF ADJUSTMENT. THERE IS A LARGE SPLIT BETWEEN LEVERS IN FLIGHT, THE LANDING GEAR WARNING HORN GOES ON AT ABOUT 2100 LBS OF TORQUE, AND THE ENGINES IDLE AT ABOUT 74% N1 WITH THE POWER LEVERS AT IDLE. MAINTENENANCE RIGGED THE NR 1 & 2 ENGFeb 28, 2009 · N255GL · Beech 1900D · Power LeverSDR GLBA20090220BPressure Switch · inoperativeON SHORT FINAL, RT ENGINE HAD ABOUT 5 TO 6 POWER SURGES. DURING THE SURGES, RT TORQUE FLUCTUATED BETWEEN APPROX 500LB-1200LB. FIRST POWER SURGES OCCURED AT APPROX 500LB OF TORQUE AS THE F/O ADVANCED POWER ON BOTH POWER LEVERS FROM 500LB TO 700LB OF TORQUE. Feb 20, 2009 · N255GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA200902040Pressure Switch · wornPILOTS REPORTED THAT UPON FINAL APPROACH WITH PROPELLERS FULL FORWARD IDLE POWER, THE LT ENGINE CYCLED IN AND OUT OF AUTO FEATHER WITH 500 LBS. OF TORQUE CHANGE. THE ISSUE CEASED TO OCCUR AFTER POWER WAS INCREASED. MX R&R THE LT LOW PRESSURE SWITCH IAW 61-21Jan 25, 2009 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLB2008F00012Wire · chafedACFT 255GL - AIR RETURN - FLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE OF TIMES AND IT WOULDN’T COME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CIRCUIT BREAKER POPPEDJul 24, 2008 · N255GL · Beech 1900D · Landing Gear System WiringSDR GLB2008F00011Landing Gear · malfunctionedFLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE OF TIMES AND IT WOULDN’T COME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CIRCUIT BREAKER POPPED. PUSHED IN, GEAR CAME UPJul 24, 2008 · N255GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLB2008F00010Control Handle · malfunctionedLANDING GEAR EXTENSION-AIRCRAFT N255GL FLIGHT 5212 "STL" - PILOTS REPORTED THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED WHEN GEAR HANDLE WAS PUT TO THE DOWN POSITION. RE-SET, BROUGHT GEAR UP, THE PUMP KICKED IN AND BROUGHT THE GEAR UP. WHEN PUT HANDLE BACK Jul 24, 2008 · N255GL · Beech 1900D · Landing Gear SelectorSDR GLBA20061092Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED AT FS 84.0 AT RT AVIONICS BAY AT INTERSECTION A OF ANGLE AT WL 92.0 AND STIFFNER AT RBL 15.75. MAINTENANCE REPAIRED CRACK IN FORWARD PRESSURE BULKHEAD IAW SERVICE BULLETIN STEPS 3 THROUGH 8 & STEPS 1- THROUGH 22 AT F.S. 84.0. REPAApr 25, 2008 · N255GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA20061090Angle · crackedRT WING TO FUSELAGE HEAVY ANGLE CRACKED ATH FWD BEND RADIUS APPROX 1.125 INCH IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. SRM 53-90-23. REPAIR ANGLE 13.5 ". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.Apr 22, 2008 · N255GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20061089Skin · corrodedBELLY SKIN CORRODED AT FS 228.25 STRINGERS 15L AND 16L. MAINTENANCE REPAIRED BELLY SKIN AT F.S. 228.25 I.A.W. BEECH 1900D SRM 51-70. REPAIR APPROXIMATELY 7.5" BY 9.5. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.Apr 22, 2008 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060866Spar · crackedHORIZONTAL STABLIZER, MAIN SPAR WEB CRACKED.Nov 1, 2006 · N255GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20060864Stringer · crackedSTRINGER 10R CRACKED AT FS 451.00 APPROXIMATELY .5 INCH.Oct 31, 2006 · N255GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20060863Frame · crackedFRAME CRACKED AT STRINGER 10R FS 451.00, APPROXIMATELY .7500 INCH.Oct 31, 2006 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20060865Skin · corrodedBELLY SKIN CORROSION ON STRINGERS 15L AND 14L FROM APPROXIMATELY FS 243.25 TO 250.75.Oct 30, 2006 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20030717Engine · failedRT ENGINE FAILED ON POWER UP FOR TAKEOFF, R&R ENGINE.Sep 10, 2004 · N255GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20030528Connector · dirty104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.Jan 8, 2004 · N255GL · Beech 1900D · Engine RPM Indicating System
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