N208GL, cancelled Aug 18, 2026

Service difficulty reports · 74

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 = 'N208GL' AND deregistration_id = 'N208GL-2026-08-18'
  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 GLBA2017110600690Cable · frayedMAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HAND RAIL CABLE WAS FRAYED. REMOVED AND REPLACED THE HAND RAIL CABLE IAW MM 52-10-02.Nov 3, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017070600672Seal · deterioratedMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR INNER HANDLE SEAL DETERIORATED. INSTALLED NEW INNER DOOR HANDLE SEAL IAW SRM 51-30-05.Jul 3, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017052200659Cam · out of rigMAINTENANCE FOUND THE PAX DOOR CAMS OUT OF ADJUSTMENT. RIGGED THE PAX DOOR CAMS IAW BMM 52-10-00-C, OPS & RIG CHECKED GOOD.May 18, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017052200658Strut · low pressureMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR STRUT REQUIRED SERVICING. SERVICED THE DOOR STRUT ASSY IAW AMM 12-10-00-11A.May 18, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017051900656Handle · unsecureMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR HANDLE FELL OFF. REINSTALLED AIRSTAIR DOOR HANDLE AND RE-RIGGED THE AIRSTAIR DOOR.May 17, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017030200637Cable · damagedDURING SCHEDULED MAINTENANCE,THE UPPER AFT HANDRAIL CABLE ON THE PASSENGER DOOR WAS DAMAGED. REMOVED AND REPLACED THE PASSENGER DOOR UPPER AFT CABLE IAW BMM 52-10-02-2 A&B.Feb 28, 2017 · N208GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016112900618Rudder Pedal · stiffPILOT REPORTED THAT DURING TAXI THE RUDDER PEDELS ARE EXTREMELY STIFF MAKING IT HARD TO TAXI. MANTENANCE RERACKED THE YAW DAMP COMPUTER, TAXI CHECKS NORMAL.Nov 26, 2016 · N208GL · Beech 1900D · Landing Gear Steering SystemSDR GLBA2016010600563Doubler · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDE WALL AT FS 163.97 & STRINGER 9 AR, REPAIR DOUBLER CRACKED. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Dec 19, 2015 · N208GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2014011300366Downlock Switch · faultyPILOT REPORTED THAT EN ROUTE TO DVL GOT A GPWS C/O & FLICKERING IN TRANSIT LIGHTS WITH 3 GREEN DOWN LOCK INDICATED. FOLLOWED CHECKLIST, HAD NO CHANGE, WAS REROUTED BACK TO MSP, DID NORM EXTENSION, CONF WITH ATC THAT GEAR WAS DOWN, STILL GOT C/O, BUT NO IN TRAJan 12, 2014 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2013082200299Door · failedMX REPORTED THAT THE 4C EMERGENCY DOOR COULDN'T BE OPENED FROM THE INSIDE. R & R EMERGENCY EXIT IAW MM 52-20-00.Aug 22, 2013 · N208GL · Beech 1900D · Emergency ExitsSDR GLBA2013082200300Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORROSION AT FS 213.25, STRINGER 15R. REPAIRED IAW EO 13-1900-53-057. MAJOR REPAIR.Aug 21, 2013 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013031200201Controller · malfunctionedCABIN OXYGEN CONTROL PULLED DUE TO CABIN ALTITUDE EXCEEDING 10000FT AND CABIN ALTITUDE INCREASING AT 4000FT IAW MIN CREW TRIED TO RESET SYS, ADJ CABIN HEAT, RAN CHECKLIST, DEPLOYED MASKS AND DESCENDED. AT 5000FT ALTITUDE, ACFT BEGAN TO PRESSURIZE. OUTFLOW VMar 10, 2013 · N208GL · Beech 1900D · Cabin Pressure ControllerSDR GLBA2013022700187Skin · crackedEMERGENCY EXIT 6A SKIN PANEL LOWER FWD CORNER CRACKED IN 2 LOCATIONS. 1 CRACK IS 1.4" IN LENGTH, THE OTHER CRACK IS 1.8" IN LENGTH. REPAIRED IAW EO 13-1900-52-001. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Emergency ExitsSDR GLBA2013002600186Skin · crackedFUSELAGE SKIN CRACKED AT FS 150.60 & STRINGER 1. CRACK ON LT SIDE OF STRINGER 1 IS .25" IN LENGTH, CRACK ON RT SIDE OF STRINGER 1 IS .65" IN LENGTH. REPAIRED IAW EO 13-1900-53-016. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013022600185Skin · corrodedBELLY SKIN CORROSION AT FS 228.25 BETWEEN STRINGERS 16 & 15R. CORROSION INDICATIONS RUN ON FRAME AREA BETWEEN STRINGERS 16 & 15R. REPAIRED IAW EO 13-1900-53-015. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013022800189Frame · crackedFUSELAGE FRAME DOUBLER AT FS 177.25 & STRINGER 13L CRACKED 1.2" IN LENGTH IN FLANGE BEND RADIUS TO SECOND FASTENER FROM THE OTBD EDGE OF DOUBLER. REPAIRED IAW EO 13-1900-53-018. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013022600184Frame · crackedRIGHT SIDEWALL AT FS 107, FRAME CRACKED AT UPPER FASTENER AREA. LONGERON AT FS 107 CRACKED. REPAIRED IAW EO 13-1900-53-014. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013022600183Rib · crackedLEFT WING INBD RIB AT 288 & BL 29.0 CRACKED. CRACK 1" IN LENGTH FROM OTBD EDGE INWARD TO BEND RADIUS AREA. REPAIRED IAW EO 13-1900-57-006. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2013022600182Rib · crackedRT INBD WING RIB AND DOUBLER AT AT 288 & BL 29.0 CRACKED & WORN. CRACK IS 1.0" IN LENGTH. REPAIRED IAW EO 13-1900-57-005. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012091000051Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT SPAR CAP ANGLE AT 20 PERCENT AT VSS 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-031. MAJOR REPAIRSep 10, 2012 · N208GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091000050Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT AT VXX 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-030. MAJOR REPAIR.Sep 10, 2012 · N208GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091000052Spar · crackedDURING A SCHEDULED ROUTINE INSP FOUND A CRACK IN THE HORIZONTAL STAB AFT SPAR WEB AT HSS 00.00 AT THE LIGHTENING HOLE, .125" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-032. MAJOR REPAIR.Sep 10, 2012 · N208GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA201205291Bulb · inoperativeLEFT INSTRUMENT/EMERGENCY LIGHT FLICKERS. MX REPLACED THE BULB, IAW BMM 33-10-04, OPS CHECKED GOOD.May 28, 2012 · N208GL · Beech 1900D · Emergency LightingSDR GLBA20111114LFrame · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 288 AND STRINGER 4R, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-064. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINov 14, 2011 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20111114KFrame · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE AT FS 150 AND STRINGER 9AL AT THE AS DOOR STRUT LWR MOUNT UPPER AFT INNER NUTPLATE AREA, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSNov 14, 2011 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20111005GSpring · damagedPILOT REPORTED THAT THE EMERGENCY EXIT AT SEAT 4C INNER PANEL LOOSE. MX REPLACED THE RETAINER SPRING ON THE DOOR PANEL.Oct 3, 2011 · N208GL · Beech 1900D · Emergency ExitsSDR GLBA20110825FGovernor · inoperativePILOT REPORTED THAT WHEN PERFORMING THE FEATHER TEST THE CB POPS. MX REPLACED THE RT OVERSPEED GOV AND PCB A123 IAW 61-20-01 , MI 24-01, AND TC 1900-7100, OPS CHECKED GOOD.Aug 24, 2011 · N208GL · Beech 1900D · Propeller GovernorSDR GLBA20110822FOxygen Mask · leakingPILOT REPORTED THAT THE FO'S OXY MASK WAS LEAKING AFTER SWITCHING TO EMERGENCY AND BACK TO OFF. MX REPLACED THE F/O'S OXY MASK IAW BMM 35-10-01, OPS CHECKED GOOD.Aug 20, 2011 · N208GL · Beech 1900D · Crew Oxygen SystemSDR GLBA20110819HPcb · unknownPILOT REPORTED THAT DURING THE AUTOFEATHER TEST ON THE RT SIDE, THE AUTOFEATHER CB POPPED AND THE RT PROP DID NOT FEATHER. MX CLEANED AND INSPECTED THE PCB, RESEATED THE PCB, RAN ACFT, ALL TESTED GOOD IAW BMM 61-21-00.Aug 18, 2011 · N208GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110811GPcb · inoperativeMX REPORTED THAT DURING ENGINE RUNS THE AUTOFEATHER CB POPPED DURING THE AFX TEST. MX REPLACED THE AUTOFEATHER RELAY PCB IAW AIM MI 24-01, OPS CK GOOD. PN: 129-364091-9 SN: 359B94.Aug 10, 2011 · N208GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20100604FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK IN THE FRAME AT FS 456 AND STRINGER 10R, FOUND IN THE STRINGER CUTOUT, .45" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-029. MATERJun 3, 2010 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100604GSkin · misrepairedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A REPAIR WAS FOUND ON THE BELLY SKIN AT F.S. 265.75 BETWEEN STRINGER 13R AND 12R, REPAIR DOES NOT CONFORM. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-190Jun 3, 2010 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100601GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND IN THE FRAME RADIUS, RT SIDE AT FS 451.0 AT STRINGER 10R, 1.0" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-026. MATERIALSJun 1, 2010 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100601HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND AT THE CUTOUT AT FS 177.35 AND STRINGER 5R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-025. MATERIALS UTILIZED ARE INCLUDED IN THJun 1, 2010 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA06012010001Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND AT THE CUTOUT AT FS 177.35 AND STRINGER 5R, .2" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK.Jun 1, 2010 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100601FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND AT A RIVET ON AN ANGLE AT F.S. 451 AND STRINGER 11L, BELOW FLOOR BOARD, LEFT SIDE OF FUSELAGE JUST FORWARD OF CARGO DOOR, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMMay 31, 2010 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2010051203Landing Gear · malfunctionedPILOTS REPORTED THAT WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION, THE NOSE WHEEL ANNUNCIATOR DID NOT ILLUMINATE & THE IN TRANSIT LIGHT ILLUMINATED. PERFORMED CHECKLIST & VERIFIED NOSE WHEEL WAS IN THE UP POSITION. MANUAL EXTENSION WAS THEN PERFORMED AND May 12, 2010 · N208GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20091002FUplock Switch · out of adjustAIR RETURN - PILOTS REPORTED THAT A GEAR UNSAFE LIGHT WAS ILLUMINATED AFTER GEAR RETRACTION AND THEY MANUALLY EXTENDED THE GEAR. MAINTENANCE ADJUSTED THE RIGHT HAND MAIN LANDING GEAR UPLOCK SWITCH FOR MORE COMPRESSION. AN OPERATIONAL CHECK WAS JPERFORMED AND WSep 29, 2009 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090929GUplock Switch · intermittentAIR RETURN - PILOTS REPORTED THE THE LANDING GEAR WOULD NOT RAISE AFTER TAKE OFF. RED UNSAFE LIGHTS WERE ON. PILOTS RECYCLED THE GEAR THEN IT WOULD NOT LWR. GEAR WAS MANUALLY PUMPED DOWN AND GOT 3 GREEN LIGHTS AND RED HANDLE LIGHTS WERE OUT. MX REMOVED AN Sep 28, 2009 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090910ATurbine Wheel · damagedPILOTS REPORTED THAT UPON TAKEOFF WITH TORQUE ONLY AT 3200 FOOT LBS. RT ITT EXCEEDED 800 C. AND THE TAKEOFF WAS THEN ABORTED. MX PERFORMED MANY CHECKS INCLUDING AN INSP OF THE BLEED AIR VALVE IAW 75-30-00. MX PERFORMED A HOT SECTION BORESCOPE AND FOUND SOME RSep 10, 2009 · N208GL · Beech 1900D · Turbine SectionSDR GLBA20090629FShaft · corrodedDURING MX IT WAS DISCOVERED THAT THE LT EXIT DOOR AT ROW 6A WOULD NOT LATCH SHUT PROPERLY. MX REMOVED AND REPLACED THE EXIT DOOR WHICH WAS REMOVED FROM ACFT IN SERVICEABLE CONDITION IAW 52-20-00. LEAK CHECK IAW 21-30-00 AND OPS CHECK WERE GOOD. THE ORIGINAL DJun 23, 2009 · N208GL · Beech 1900D · Emergency ExitsSDR GLBA20090409FCam · wornPILOTS REPORTED THAT THE ACFT YAWS VIOLENTLY TO THE LT ON FLAIR (LANDING). MX REMOVED AND REPLACED THE RT ENGINE PROPELLER CAM/LEVER IAW MM 76-10-00. GROUND RUNS WERE PERFORMED AND WERE WITHIN GIVEN PARAMETERS.Apr 6, 2009 · N208GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090224MInsulation · out of positionSMOKE SMELL - ENROUTE FROM "DEN" TO "CYS" THE PILOTS REPORTED A BURNING SMELL AFTER OPENING THE BLEEDS AFTER TAKEOFF. MX FOUND A PIECE OF SIDEWALL INSULATION AGAINST THE RECIRCULATION EJECTOR. MX RE-POSITIONED AND SECURED THE INSULATION. MX RAN THE ACFT WITH FFeb 23, 2009 · N208GL · Beech 1900D · Passenger Compartment EquipmentSDR GLBA200901091Skin · crackedMAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION THE LT BELLY SKIN WAS FOUND CRACKED APPROXIMATELY 6" IN LENGTH AT APPROXIMATELY BL 265 8.5" AFT AS WING SPAR AND 2.250" OTBD AT BELLY SKIN INBD EDGE. MAINTENANCE REPAIRED CRACK IN BELLY SKIN IAW BEECH SRM Jan 8, 2009 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20061082Skin · crackedCRACK ON BELLY SKIN AT FS 303.25 AT BL 29.06. CRACK APPROX 2.250 INCH. MAINT STOP DRILLED AND PATCHED AFFECTED AREA IAW SRM 51-70. DAMAGED AREA APPROX 6.3 BY 4.5. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1.Mar 13, 2008 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060986Spar · crackedMAJOR REPAIR - HORIZONTAL STAB SPAR WEB CRACKED AROUND DE-ICE TUBE HOLE. MAINTENANCE REPAIRED HORZONTAL STAB SPAR WEB I.A.W. BEECH 1900D SRM 55-91. REPAIR APPROXIMATELY 5 3/4 INCHE BY 4 3/4 INCH. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.Aug 15, 2007 · N208GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20060984Skin · canningEVIDENCE OF OIL CANNING PRESENT AT FS 202.25 2 INCHES FROM CENTER OF REPAIR TO STRINGER 15 R APPROXIMATELY 2 INCHES SQUARE. MAINTENANCE REPAIRED AFFECTED AREA IAW SRM 51-70. INSERTION PATCH DIMENSION APPROXIMATELY 2 INCH X 2 INCH WITH REPAIR APPROXIMATELY 4.5 Aug 14, 2007 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060985Hinge · crackedMAINTENANCE DISCOVERED BOTH CARGO DOOR HINGES CRACKED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR HINGES IAW EO 05-02 . DOOR HINGE PN 129-440049-1. FUSELAGE PN 129-440049-3.Aug 14, 2007 · N208GL · Beech 1900D · Cargo/Baggage DoorsSDR GLBA20060983Stringer · cracked(2) CRACKS FOUND ON STRINGER 10R AT F.S. 451.0. FORWARD CRACK .5625 INCH LONG AFT CRACK .2500 INCH LONG. MAINTENANCE REPAIRED CRACKS ON STRINGER 10R AT F.S. 451.0 IAW SRM 51-70. REPAIR APPROXIMATELY 9 INCHES LONG. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.Aug 14, 2007 · N208GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20060982Angle · crackedRT HEAVY ANGLE CRACKED AT RADIUS AT FS 288. CRACK IS APPROXIMATELY 2.2500 INCH LONG. MAINTENANCE REPAIRED THE RT HEAVY ANGLE IAW SRM 53-90. REPAIR APPOXIMATELY 13.5 INCHES. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.Aug 13, 2007 · N208GL · Beech 1900D · Fuselage Miscellaneous Structure
Back to N208GL, cancelled Aug 18, 2026