N251GL

Service difficulty reports not matched to an aircraft · 86

They name N251GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N251GL' AND registry_match IS NULL
  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 GLBA2018032100704Cable · brokenMAINTENANCE REPORTED THAT THE FORWARD LOWER PASSENGER DOOR CABLE WAS BROKEN. MAINTENANCE REPLACED THE CABLE IAW MM 52-10-02 3A & B.Mar 20, 2018 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017060200664Post · crackedMAINTENANCE REPORTED THAT THE BRACKET ASSEMBLY ON THE AFT HANDRAIL POST IS CRACKED. REMOVED & REPLACED THE AFT HANDRAIL POST ASSEMBLY IAW AMM 52-10-02. PMay 30, 2017 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017042800650Cable · looseMAINTENANCE REPORTED THAT THE UPPER FORWARD AIRSTAIR DOOR HANDRAIL CABLE WAS LOOSE. SECURED THE UPPER FORWARD ASD CABLE WITH PROPER TENSION IAW BMM 52-10-02.Apr 26, 2017 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016120800622Unknown · malfunctionedSIG EVENT, PILOT REPORTED THAT THEY HAD A BLEED AIR FAIL AND DESCENDED TO FL110 AND DROPPED THE MASKS, NO EMER DECLARED. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **Dec 8, 2016 · N251GL · Beech 1900D · Passenger Oxygen SystemSDR GLBA2016080200601Motor · failedPILOT REPORTED THAT THEY HAD A GEAR ISSUE, LOW HYD LIGHT ILLUMINATED, MANUALLY EXTENDED THE GEAR, DECLARED AN EMERGENCY, HAD 3 GREENS ILLUMINATED, LANDED SAFELY. CIRCUIT BREAKER POPPED, RESET, POPPED WITHIN 4 SEC. HYD FLOW LOW ANNUNCIATOR ILLUM IN FLT. HYD Aug 1, 2016 · N251GL · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR GLBA2016051900588Stringer · corrodedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND CORROSION ON STRINGER 14 AT FS 213.25, APPROX 1.5" BY 2" AREA. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 19, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016051700587Angle · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND THE LT HEAVY ANGLE CRACKED ON THE FWD SIDE, .5" IN LENGTH. FOUND TO NOT BE A MAJOR REPAIR, THE PART WILL BE REPLACED VERSES REPAIRED.May 16, 2016 · N251GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2016051200586Skin · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 213.35 & STRINGER 14L, JUST AFT OF ADF ANTENNA. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 11, 2016 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016050200585Stringer · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND STRINGER 9F CRACKED, AT JUNCTION WITH CANT BULKHEAD AT FS 588.10, .7" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 2, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016050200584Stringer · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND STRINGER 9L CRACKED AT JUNCTION WITH CANT BULKHEAD AT FS 588.10, .2" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 2, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2015091800538Pin · out of positionSIGNIFICANT EVENT, PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER PIN CAME OUT. INSTALLED SAME AIR STAIR DOOR SNUBBER & COUNTER BALANCED ASSEMBLY. REPLACED STUD, PN 129-514123-1, NO FURTHER DEFECTS NOTED AT THIS TIME.Sep 17, 2015 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2013072000278Unknown · odorPILOT REPORTED THAT THERE WAS AN ODOR COMING FROM THE ENVIRO SYSTEM. MX INSPECTED BOTH ENGS, NO OIL OR FUEL LEAKS INSPECTED, ENVIROMENTAL SYS, NO DEFECTS NOTED.Jul 20, 2013 · N251GL · Beech 1900D · Air Distribution SystemSDR GLBA2013071900277Unknown · odorPILOT REPORTED THAT THERE WAS AN IRRITATING ODOR COMING FROM THE ENVIROMENTAL SYSTEM WITH THE BLOWERS ON. MX STARTED LT AND RT ENGINES AND RAN WITH BLOWERS AND VCM ON, ODOR DISAPATED AFTER 20 MIN, NO FURTHER DISCREPANCY NOTED.Jul 19, 2013 · N251GL · Beech 1900D · Air Distribution SystemSDR GLBA2013072200276Unknown · odorPILOT REPORTED AN IRRIATING ODOR COMING FROM THE ENVIROMENTAL SYS WITH THE BLOWERS OFF. MX R & R THE EPA CAN CHECK VALVE AND LOWER FUEL TUBE, LEAK AND OPS CHECKED GOOD.Jul 19, 2013 · N251GL · Beech 1900D · Air Distribution SystemSDR GLBA2013071800275Unknown · odorPILOT REPORTED THAT WHILE RUNNING ACFT, AN ODOR WAS COMING FROM THE BLOWERS. MX INSPECTED, THE VENT BLOWERS AND ASSOCIATED SYSTEMS, NO DEFECTS, ALL CHECKED GOOD.Jul 17, 2013 · N251GL · Beech 1900D · Air Distribution SystemSDR GLBA2013062100263Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FUSELAGE FRAME FLANGE AT FS 183.25 AND STRINGER 2R, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-047.Jun 21, 2013 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013061800262Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ANGLE AT FS 150.00 & STRINGER 6L AT THE UPPER & LOWER A/S DOOR GAS STRUT MOUNT NUTPLATE AREA, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-046.Jun 18, 2013 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013061400259Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE HORIZONTAL STAB AFT SPAR WEB, .25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-017. MAJOR REPAIR.Jun 14, 2013 · N251GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2013061400260Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE CARGO DOOR FRAME IN THE BEND RADIUS AT FS 456.00 AND STRINGER 3L, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-045. MAJOR REPAIR.Jun 14, 2013 · N251GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2013061300258Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-016. MAJOR REPAIR.Jun 13, 2013 · N251GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013061300613Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. OPENJun 13, 2013 · N251GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012110800104Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE LT VERTICAL STAB FWD SPAR CAP ANGLE AT 84.10 AND 20 PERCENT CHORD RADIATING UPWARD FROM THE TOP FASTENER HOLE AND THE OTHER CRACK RADIATING AROUND THE SECOND FASTENER HOLE FROM THE TOP, .875" IN TNov 8, 2012 · N251GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012110100100Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION AT STRINGER 15R BETWEEN 228.25 AND 243.25. REPAIRED IAW EO 11-1900-53-064. MAJOR REPAIR.Nov 1, 2012 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2012103100099Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE BELLY AT FS 228 BETWEEN STRINGERS 16 AND 15L, .75" BY .75, AND A CRACK IN THE AREA, .5" IN LENGTH. REPAIRED IAW EO 11-1900-53-065. MAJOR REPAIR.Oct 31, 2012 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012103100098Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE STRINGER BETWEEN FS 228.25 AND 243.25. REPAIRED IAW EO 11-1900-53-062. MAJOR REPAIR.Oct 31, 2012 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA201206081Cam · obstructedTOP LEFT LOCKING CAM IS CONTACTING THE STUD AND MOVING INWARD ON MAIN CABIN DOOR. MX R & R AIRSTAIR DOOR (DOOR SIDE) HINGE HALF IAW SRM AND RE-RIGGED THE FORWARD AND AFT UPPER LATCH POSTS IAW MM.Jun 6, 2012 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2012060101Turnbuckle · brokenPILOT REPORTED THAT THE INSIDE CABIN DOOR HANDLE IS BROKEN, COULDN'T OPEN DOOR FROM THE INSIDE. MX REPLACED THE HANDLE TURNBUCKLE BOLT IAW MM 52-10-05, OPS CHECKED GOOD.May 31, 2012 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2012022901Trim Panel · dislodgedPILOT REPORTED THAT THE MAIN DOOR GETS STUCK CLOSED DUE TO A LOOSE PIECE OF PLASTIC TRIM. MX RESECURED MAIN DOOR TRIM PANEL, TRIM PIECE TIGHTENED, OPS CK GOOD.Feb 28, 2012 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20120210GFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE STRINGER CUTOUT OF FRAME AT STRINGER 9AR AND FS 150.6, .2" IN LENGTH. REPAIRED IAW EO 12-1900-53-009. MAJOR REPAIR.Feb 9, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120210FAngle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS, EACH .4 INCHES IN LENGTH IN THE VERTICAL ANGLE FS 107 JUST BELOW AND FWD OF THE RT OPENABLE WINDOW. REPAIRED IAW EO 12-1900-53-008. MAJOR REPAIR.Feb 9, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120207FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME AT FS 509.5 BETWEEN STRINGER 4L AND 5L AT THE AFT LONG SNUBBER MOUNT.1.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-006. MATERIAFeb 7, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120207GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE FUSELAGE FRAME AT FS 456 BETWEEN STRINGER 4L AND STRINGER 5L AT THE FORWARD LONG SNUBBER MOUNT, .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12Feb 7, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120206GKeelbeam · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT OTBD KEEL UPPER FENDER MOUNT FLANGE HAS OVERSIZED HOLES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-54-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 6, 2012 · N251GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20120206FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON FRAME AT FS 163 AND STRINGER 9AR, .9 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-53-005. MAJOR REPAIR.Feb 6, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120203GDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND THE AIR STAIR DOOR FRAME AFT CORNER AT FS 177.35 CRACKED, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-003. MATERIALS UTILIZED ARE INCLUDED IN THE Feb 3, 2012 · N251GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20120203FAngle · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND THE RT HEAVY CLOSING ANGLE CRACKED AT FS 288, 1.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-004. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 3, 2012 · N251GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20111207JCable · brokenPILOT REPORTED THAT THE DOOR SNUBBER CABLE IS BROKEN. MX REPLACED THE DOOR CABLE IAW 52-10-00, OPS CHECKED GOOD.Dec 6, 2011 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20111115GSkin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE BELLY SKIN, FWD OF THE FWD DME ANTENNA AT FS 228.25, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-065. MATERIALS UTILIZED ARE INCLUDED IN Nov 15, 2011 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20111114HSelector Valve · inoperativeAFTER SWINGING GEAR 11 TIMES, THE INTRANSIT LIGHT DID NOT ILLUMINATE, DID NOT HEAR HYD PUMP. MX REPLACED THE SELECTOR VALVE IAW AMM 32-30-03, OPS CHECKED GOOD.Nov 13, 2011 · N251GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20111111GPcb · inoperativePILOT REPORTED THAT UPON RAISING THE GEAR HANDLE THE GEAR REMAINED DOWN WITH 3 GREEN AND RED INTRANSIT LIGHTS EXTINGUISHED. MX REPLACED THE TIME DELAY PCB PN: 68-10GLA SN: 506I96, IAW MI 28-01, OPS CHECKED GOOD.Nov 10, 2011 · N251GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20110804KSwitch · out of rigPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR STAYS ON WHEN THE DOOR IS CLOSED. MX RIGGED FWD CAM SWITCH R & R LATCH HANDLE SWITCH PN V3-101-08 IAW BMM 52-70-00 & AIM 12-10-0. OPS & RIG CHECKED NORMAL.Aug 3, 2011 · N251GL · Beech 1900D · Door Warning SystemSDR GLBA20110804JSwitch · out of positionPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR STAYS ON WHEN THE DOOR IS CLOSED. MX REPOSITIONED THE DOOR SWITCH IAW BMM 52-70-00, OPS CK GOOD.Aug 3, 2011 · N251GL · Beech 1900D · Door Warning SystemSDR GLBA20110720FIndication Sys · malfunctionedPILOT REPORTED THAT ON APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR DIDN'T SHOW DOWN, AFTER CYCLING, THE NOSE DID ILLUMINATE AND LANDED. MX INSP WIRING AND CONNECTORS ON NOSE DOWNLOCK SWITCH, MEGGED WIRING TO PC BOARD AND ANNUNCIATOR FROM DJul 19, 2011 · N251GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110711PCover · tornPILOT REPORTED THAT THE AIR STAIR DOOR RUBBER CASING WAS TORN, UPPER AFT CABLE. MX R & R THE UPPER AFT AIRSTAIR CABLE IAW AMM 52-10-02, PN 1440-40GLA.Jul 8, 2011 · N251GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110705HHandle · out of rigPILOT REPORTED THAT THE 6C EMERGENCY DOOR HANDLE WAS POPPED OUT. MX RIGGED THE DOOR HANDLE IAW BMM 52-20-00, OPS CK GOOD.Jul 4, 2011 · N251GL · Beech 1900D · Emergency ExitsSDR GLBA20110131FSkin · crackedDURING A SCHEDULED ROUTINE INSP, MX FOUND A RIVET SHEARED AT APPROX AT FS 163.9 & WL 98, AND A CRACK ON THE RT SIDE .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-004. MATERIALS UTILIZED AJan 30, 2011 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110131GSkin · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A GAUGE & SMALL HOLE IN SKIN AT FS 508 & W.L. 90. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-005. MATERIALS UTILIZED ARE INCLUDED IJan 30, 2011 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100818GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION FOUND EMERGENCY EXIT DOOR 4C INNER LOWER AFT CORNER SKIN CRACKED , 1.7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-004. MATERIALS UTILIAug 18, 2010 · N251GL · Beech 1900D · Emergency ExitsSDR GLBA20100818FFrame · crackedDURING A SCHEDULED ROUNTINE INSP, A CRACK IN THE FRAME AT FS 456 WAS FOUND AT STRINGER CUTOUT 10R, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-050. MATERIALS UTILIZED ARE INCLUDED IN TAug 17, 2010 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA201007261Gas Generator · seizedPILOT REPORTED THAT RIGHT ENGINE SECURED IN FLIGHT, ITT WAS STEADILY RISING ABOVE LIMITS TO AROUND 940C AND TORQUE WAS STEADILY DECREASING UNTIL ENGINE WAS SECURED. AFTER LANDING OIL FOUND LEAKING FROM ENGINE AND PROP WAS SEIZED. MAINTENANCE PULLED THE COCKPITJul 26, 2010 · N251GL · Beech 1900D · Turbine Section
Back to N251GL