N210GL, cancelled Jun 29, 2026

Service difficulty reports · 62

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 = 'N210GL' AND deregistration_id = 'N210GL-2026-06-29'
  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 TIMA20250215002Unknown · odorWHILE IN CRUISE FLIGHT AT 10,000FT PILOT BEGAN TO SMELL SOMETHING SUSPICIOUS. MOMENTS LATER THE PILOT EXPERIENCED A LEFT AC BUS FAILURE AND BEGAN TO SEE SMOKE COMING FROM UNDERNEATH THE CO-PILOTS SIDE OF THE AVIONICS PANEL. IMMEDIATELY PROCEEDED WITH THE MEMOFeb 15, 2025 · N210GL · Beech 1900D · Air Distribution SystemSDR GLBA2015042700515Check Valve · leakingSIG EVENT, PILOT REPORTED THAT THERE WAS A STRONG SMELL OF FUEL IN CABIN. REMOVED FLOORBOARDS & INSPECTED FUEL TRANSFER LINES, PRESSURIZED & LEAK CHECKED FUEL LINES, NO DISCREPANCIES NOTED. INOPERATIVE LT & RT ENG ACCESSORIES FOR FUEL LEAKS, NO LEAKS NOTED AApr 25, 2015 · N210GL · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA2014022800389Motor · faultyPILOT REPORTED THAT THERE WAS A STRONG BURNING SMELL COMING FROM THE CABIN & IS IRRITATING TO TO EYES. TROUBLESHOT BURNING SMELL COMING FROM FLAP GEAR BOX MOTOR ASSEMBLY. R & R FLAP GEAR BOX MOTOR ASSEMBLY PN 100-524073-1 SN OFF 5693, IAW BMM 27-50-03 OPERATFeb 26, 2014 · N210GL · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2014021300383Motor · faultyPILOT REPORTED THAT WHEN THEY WENT TO EXTEND THE FLAPS HAD A STRONG ELECTRICAL SMELL & THE FLAPS DID NOT EXTEND. MAINTENANCE R&R FLAP GEAR BOX MOTOR P/N 100-524073-1 S/N OFF 6137 S/N ON. 5693 OPS CHECK GOOD AT THIS TIME REF 1900DMM 27-50-03.Feb 12, 2014 · N210GL · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2013091300310Skin · crackedDURING A SCHEDULED INSPECTION, FOUND THE LT LOWER BELLY SKIN AT FS 288 CRACKED, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-059. MAJOR REPAIR.Sep 12, 2013 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013090900306Fire Loop · chafedSIG EVENT - PILOT REPORTED THAT THE RT FIREWALL FUEL VALVE T-HANDLE FLICKERED ON AND OFF IN FLIGHT. MX TESTED FIRE LOOP ON RT SIDE, TESTED NORMAL. INSPECTED FWD AND AFT LOOP FOUND CHAFE ON TOP SIDE OF FWD LOOP. R & R LOOP IAW BMM 26-10-01. OPS CHECK GOOD ATSep 6, 2013 · N210GL · Beech 1900D · Fire DetectionSDR GLBA2013052900255Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FWD PRESSURE BULKHEAD, RT WEB AT FS 84.00, CRACKS AT THE INBD EDGE OF WEB ATTACHING FASTENERS, 2" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.May 29, 2013 · N210GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2013052900254Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 7 CRACKS IN THE FWD PRESSURE BULKHEAD, LT WEB AT FS 84.00, CRACKS AT INBD EDGE OF WEB ATTACHING FASTENERS, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.May 29, 2013 · N210GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2013052800253Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013052800252Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS AT THE CARGO DOOR FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L, LOCATED IN THE BEND RADIUS OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-042. MAJOR REPAIR.May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013040100222Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE TEE SECTION OF THE LT HORIZONTAL STAB LOWER AT HSS 5.000 AND 10.5 PERCENT AT A SCREW HOLE, .5" IN LENGTH. REPAIRED IAW EO 13-1900-55-011. MAJOR REPAIR.Apr 1, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2013032900219Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK EXTENDING FROM A SCREW HOLE ON THE TOP SIDE OF THE LT HORIZONTAL STAB AT HSS 5.000 AND 10.5 PERCENT CHORD, ON THE FLANGE FOR PANEL 332 BTC ON THE FORWARD LT CORNER, .25" IN LENGTH. REPAIRED IAW EO 13-1900-55Mar 28, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer, Plate/SkinSDR GLBA2013032900218Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT HORIZONTAL STAB LOWER TEE SECTION AT HSS 5.000 AND 10.5 PERCENT CHORD, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-010. MAJOR REPAIR.Mar 28, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012120400126Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIRDec 4, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012083100043Skin · burned.5 X .5 INCH BURN HOLE IN TOP AND BOTTOM SKIN, 3.8750" CENTER FROM OTBD TIP OF LT ELEVATOR T/E. REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-002.Aug 31, 2012 · N210GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA2012040203Skin · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT FUSELAGE FS 288 HAS ELONGATED HOLES FROM ATTACHING FAIRING PANEL TO FS 327. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN TApr 2, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012040202Fairing · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R, .687 BY .25. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-01Apr 2, 2012 · N210GL · Beech 1900D · Aerodynamic FairingsSDR GLBA2012032101Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0, .73" IN LENGTH. ED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-008. MATERIALS UTILMar 20, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA201203191205Skin · chafedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 RIVET HEADS CHAFING ON A PREVIOUS REPAIR OF THE LOWER RT WING WHERE THE FUSELAGE MEETS THE WING. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR.Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012031904Attach Fitting · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE NUTPLATE, FWD CARGO DOOR SNUBBER FUSELAGE ATTACH POINT, UPPER IB NUTPLATE FS 456, .35" IN LENGTH. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Cargo/Baggage DoorsSDR GLBA2012031903Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE SKIN, LT BELLY AT FS 303.25 WHERE THE FUSELAGE MEETS THE WING, 5" IN LENGTH. REPAIRED IAW EO 12-1900-53-015. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012031902Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R, .9" IN LENGTH. REPAIRED IAW EO 12-1900-53-016. MAJOR REPAIRMar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2012031901Doubler · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT DOUBLER, FWD END, FS 288, 1.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-017.Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2012022101Warning Light · false activationPILOT REPORTED THAT THE GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT, RAN CHECKLIST, GEAR OPERATED NORMALLY TO THE EXTENDED POSITION, EMERGENCY DECLARED, LANDED SAFELY. MX COULD NOT DUPLICATE, REPLACED THE NLG UPLOCK SWITCH IAW TC 1900-3260.00, OPS CHECKED GOODFeb 18, 2012 · N210GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20120209FCircuit Board · damagedPILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND WHEN SELECTED AND RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR, NO IN-TRANSIT LIGHTS, LANDED SAFELY. MX REPLACED THE PCB A116 AND THE LANDING GEAR RELAY, OPS CK GOOD.Feb 8, 2012 · N210GL · Beech 1900D · Landing Gear System WiringSDR GLBA20111208FActuator · inoperativePILOT REPORTED THAT THE LEFT GEAR INDICATION DID NOT SHOW DOWN AND LOCKED UNTIL APPROX 25 SECONDS AFTER THE HANGLE WAS PLACED IN THE DOWN POSITION. MX REPLACED THE LT MLG ACTUATOR IAW TC 1900-3230.10, PN: 114-300041-15, SN: 0561A, OPS CK GOOD.Dec 7, 2011 · N210GL · Beech 1900D · Landing Gear ActuatorSDR GLBA20111128FSolenoid · dirtyPILOT REPORTED THAT THE ACFT YAWED TO THE LT IN THE LANDING FLARE. MX CLEANED THE LOW PITCH SOLENOID, OPS CHECKED GOOD.Nov 27, 2011 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110809FWire · chafedPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS EXTINGUISHED WHEN THE DOOR IS OPENED UP UNTIL ABOUT A FOOT OPEN. MX INSPECTED WIRE AT AIRSTAIR DOOR FOUND 4 CHAFED WIRES, REPAIRED WIRE. PERFORMED CABIN DOOR AM LIGHTING SYS CK, OPS CK GOOD REF CHAP 14, Aug 8, 2011 · N210GL · Beech 1900D · Door System WiringSDR GLBA20110803GSwitch · inoperativePILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR GOES OUT WITHOUT LOCKING THE DOOR. MX CLEANED THE MICRO SWITCHES, OPS CK GOOD.Aug 2, 2011 · N210GL · Beech 1900D · Door Warning SystemSDR GLBA20110802GSwitch · inoperativePILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WENT OUT BEFORE THE DOOR WAS LOCKED. MX CLEANED THE CABIN DOOR MICRO SWITCH REF AIM 14.3.0, OK FOR SERVICE.Aug 1, 2011 · N210GL · Beech 1900D · Door Warning SystemSDR GLBA20110801HActuator · inoperativePILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. MX REPLACED THE LT MLG ACTUATOR, OPS AND RIG CKS IAW TC. 1900-3230.10.Jul 29, 2011 · N210GL · Beech 1900D · Landing Gear ActuatorSDR GLBA20110706PSwitch · out of rigPILOT REPORTED THAT UPON RAISING THE LANDING GEAR WHILE FLAPS AT 17 DEGREES. TAKEOFF GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED. IN TRANSIT LIGHT REMAINED ILLUMINATED UNTIL FLAPS 0 DEGREES WAS OBTAINED. MX RIGGED LANDING GEAR WARNING HORN FLAP POSITJul 4, 2011 · N210GL · Beech 1900D · Trailing Flap Position Indicating SystemSDR GLBA20110606GSwitch · stuckPILOT REPORTED THAT WITH THE CABIN DOOR OPEN THE CABIN ANNC DID NOT ILLUMINATE. MX CLEANED THE MICRO SWITCH, SYS OPS CK GOOD.Jun 4, 2011 · N210GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110603FKeelbeam · gougedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE RT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-006. MATERIAJun 1, 2011 · N210GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20110602FKeelbeam · gougedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE LT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-005. MATERIALJun 1, 2011 · N210GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20101206ABleed Air Sys · inoperativeCLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE FDec 6, 2010 · N210GL · Beech 1900D · Engine Bleed Air SystemSDR GLBA20100819FFastener · looseSIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWARD SPAR, REPLACED FASTENERS AND SEALED AREA, REFUELED, NO LEAKS OR ODOR PRESENT IAW SRM 51-10-00, CAug 18, 2010 · N210GL · Beech 1900D · Wing Main, Frame StructureSDR GLBA20100818BFuel Sys · leakingOVERWHELMING ODORS OF JET FUEL PRESENT IN CABIN COCKPIT EXTREMELY BAD TO A POINT OF BEING NAUSEATING AND AFFECTING SAFETY SLOW DRIP UNDER RT NACELLE DIFFERENT AREA THAN REPAIR.Aug 18, 2010 · N210GL · Beech 1900D · Fuel StorageSDR GLBA20100802JBulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND AT THE AFT CARGO BAY FLOORBOARD FORWARD SUPPORT BULKHEAD AT F.S. 531.0 LH SIDE WHERE IT ATTACHES TO THE FRAME, 13/16" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPEAug 2, 2010 · N210GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA20100802KBulkhead · buckledMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A BULKHEAD AT FS 531 AFT CARGO FLOORBOARD FORWARD SUPPORT BUCKLED ABOUT 11/32" AT TOP, TOTAL DAMAGE AREA ABOUT 26" IN LENGTH, AND A .5" CRACK IN THE RADIUS 12" FROM RT SIDE. MAINTENANCE REPAIRED THE AFFECTEAug 2, 2010 · N210GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA20100730FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK IN THE SKIN WAS FOUND ON THE EMERGENCY EXIT DOOR 6A, LOWER FORWARD CORNER, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-003. MJul 30, 2010 · N210GL · Beech 1900D · Emergency ExitsSDR GLBA20100728FFrame · crackedDURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 303, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-045. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDEJul 27, 2010 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100729GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A2 CRACKS WAS FOUND IN THE FRAME AT FS 456 AND STRINGER 10R CUTOUT, .45" AND .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-046. MATERIALS UTIJul 27, 2010 · N210GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100409FSkin · puncturedCOMPONENT MAJOR REPAIR - UPON RECEIVING A SERVICEABLE AIRSTAIR DOOR THAT WAS PURCHASED, IT WAS DETERMINED THAT IT REQUIRED A MAJOR REPAIR ON THE EXTERIOR DOOR SKIN DUE TO 3 SCRATCHES AND 1 PUNCTURE THROUGH THE SKIN. MX REPAIRED THE AFFECTED AREA AND PERFORMED Apr 9, 2010 · N210GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20090807FUnknown · odorPILOTS REPORTED THAT A STRONG FUEL ODOR FROM THE VENTS IN THE FLIGHT DECK AND CABIN WAS PRESENT. MAINTENANCE INSPECTED THE NR 1 AND 2 ENGINES FOR LEAKS OF WHICH NONE WERE FOUND AND SUBSEQUENTLY PERFORMED INDIVIDUAL ENGINE RUNS WITH NO FUEL ODORS NOTED. REFERENAug 6, 2009 · N210GL · Beech 1900D · Air Distribution SystemSDR GLBA20090504FStructure · corrodedMAJOR REPAIR - AIRSTAIR DOOR WAS FOUND CORRODED ON LOWER END CLOSURE AREA. MAINTENANCE REMOVED A SECTION OF THE LOWER INNER DOOR PAN, CLEANED CORROSIONFROM INNER MATERIAL, INTALLED NEW LOWERE DOOR PAN AND INSTALLED THE HINGE ASSEMBLY IAW EO 09-1900-52-001.Apr 28, 2009 · N210GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA200904225Pressure Switch · wornON APPROACH AT 500 LBS TORQUE, WHILE LEVELING ALTITUDE AND ADVANCING POWER THE R/H ENGINE ATTEMPTED FEATHER CAUSING CYCLES SIMILAR TO AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AUTOFEATHER LOW PRESSURE SWITCH AND COMPLIED WITH FCD 1900-0Apr 22, 2009 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090205ACircuit Board · shortedSUSPECTED AUTO FEATHER - PILOTS REPORTED THAT ON SHORT FINAL THE RT ENGINE CYCLED IN AND OUT OF FEATHER. MX R&R THE A123 PRINTED CIRCUIT BOARD AND OPS CHECKED THE SYSTEM IAW MM 61-21-00.Feb 5, 2009 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA200901093Switch · dirtySIGNIFICANT EVENT - PILOTS REPORTED THAT THE RT ENG AUTOFEATHERED IN FLIGHT AND CAUSED SURGES AND EXTREME YAWING MOTION. MX CLEANED AFX SWITCHES IAW BMM 61-21-01-201. OPS CHECKS WERE OK.Jan 7, 2009 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20061041Bulb · burned outSMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GOJan 1, 2008 · N210GL · Beech 1900D · Emergency Lighting
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