N153GL

Service difficulty reports · 96

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 = 'N153GL' 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 GLBA2016060100590Downlock Switch · inoperativePILOT REPORTED THAT THEY HAD NO NLG INDICATIONS ON GEAR EXTENSION, RAN ABNORMAL CHECKLIST, DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R THE NOSE GEAR DRAG BRACE DOWN LOCK SWITCH IAW TC 1900-3220.0 REV 1 STEPS 3,4, & 21. PERFORMED GEAR SWING, OPERATIONS May 31, 2016 · N153GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2016041400580Unknown · malfunctionedPILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD NOT DUPLICATE DISCREPANCY SIGNED OFF USING REF 1900DMM 61-21-00. OPERATIONS CHECKED GOOD.Apr 14, 2016 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2015010800490Skin · damagedDURING A SCHEDULED INSPECTION FOUND A BURN HOLE IN THE RT ELEVATOR TOP OTBD SKIN TE 1.5 INCH WIDE BY .75 INCHES LONG IN AN EXISTING PATCH. HOLE IS 4.5 INCHES FROM OTBD TIP & .5 INCHES FROM THE TE. REPAIRED IAW EO 14-120-53-002.Jan 8, 2015 · N153GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA2014122400486Strut · low pressureTHE CABIN DOOR SNUBBER IS READING 200 PSI LOW & THE DOOR IS HARD TO CLOSE. SERVICED THE CABIN DOOR STRUT AS NEEDED IAW AIM 3 4 0 STEP 23. OPERATIONS CHECKED GOOD.Dec 22, 2014 · N153GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2014112400468Skin · dentedMAJOR REPAIR. DURING A SCHEDULED INSPECTION FOUND DENT IN THE RT HORIZONTAL STAB LE 3.25 INCHES BY 1.375 INCHES, DENT AT HSS 58.00, DENT LOCATED AT RIB AREA, SMALLER DENT OTBD OF DENT AT HSS 58.00, APPROX AT HSS 61.00, 2 INCHES BY 1.5 INCHES, DUE TO BIRD STRNov 23, 2014 · N153GL · Beech 1900D · Horizontal Stabilizer, Plate/SkinSDR GLBA2014021400384Frame · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK AT FS 456 LT SIDE LOWER FRAME, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-011.Feb 13, 2014 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2014021000377Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE CARGO DOOR AFT LOWER FRAME AT FS 509.50 AT THE INTERSECTION OF THE LOWER SILL, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-006.Feb 8, 2014 · N153GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2013121600360Unknown · odorPILOT REPORTED THAT THERE WAS A HOT ELEC SMELL COMING FROM THE FIRST OFFICER'S SIDE OF THE COCKPIT, POSSIBLE FROM THE CB PANEL. INSPECTED BEHIND THE CB PANEL, PULLED UP FLOORBOARDS, RAN ENG NO DISCREPANCIES OR ABNORMAL ODORS NOTED.Dec 15, 2013 · N153GL · Beech 1900D · Air Distribution SystemSDR GLBA2013100400335Structure · crackedDURING A SCHEDULED INSPECTION, FOUND CRACK IN THE HORIZONTAL STABILIZER LT LOWER TEE SECTION AT HSS 0.00, .5" IN LENGTH. REPAIRED IAW EO 13-1900-55-024.Oct 4, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2013100200332Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE IN THE BEND RADIUS AT FS 451 AND STRINGER 10R, .875 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-068. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013100200330Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK BS 107 AND STRINGER 8R FRAME, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-070. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013100200331Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME LT SIDE OF FS 107 BY STRINGER 8L, .125 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-069. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013100200333Frame · crackedDURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN FUSELAGE FRAME, STRINGER 8L BS 438.25, .999 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-067. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013100200329Skin · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN FUSELAGE SKIN, PROTRUDING OUT OF 2 RIVETS AT FS 150.6 STRINGER 1, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-071. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013100200328Frame · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ON EITHER SIDE OF STRINGER 2L AT FS 378.25, ONE INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-072. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013100200327Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB 2ND FROM TOP RIVET, .125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-023. MAJOR REPAIR.Oct 1, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2013100200326Structure · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EXIT DOOR 4C, UPPER FWD CORNER, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-002. MAJOR REPAIR.Sep 30, 2013 · N153GL · Beech 1900D · Emergency ExitsSDR GLBA2013031900214Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE HORIZONTAL STAB AFT WEB AT THE 10 & 2 O'CLOCK POSITION AROUND THE ACCESS HOLE, .15" IN LENGTH. REPAIRED IAW EO 13-1900-55-007. MAJOR REPAIR.Mar 19, 2013 · N153GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2013031800213Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STABILIZER LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT FSS 84.10, GOING THROUGH THE THIRD FASTENER FROM THE TOP (SECOND FASTENER BELOW THE HAT SECTION) IN THE AREA OF THE HORIZONTAL STAB ATTACH Mar 18, 2013 · N153GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013021500177Bulb · inoperativePILOT REPORTED THAT THE EMERGENCY LIGHTS ON THE F/O'S SIDE DO NOT ILLUMINATE AND ARE ALSO INOPERATIVE IN INDIRECT LIGHT MODE. MX REPLACED THE BULBS AND SECURED WIRING, OPS CHECKED GOOD.Feb 14, 2013 · N153GL · Beech 1900 · Emergency LightingSDR GLBA2012122600144Wire · brokenPILOT REPORTED THE THE F/O'S EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE BULB AND REPAIRED A WIRE, OPS CHECKED GOOD.Dec 25, 2012 · N153GL · Beech 1900D · Light System WiringSDR GLBA2012101800080Warning Light · illuminatedPILOT REPORTED THAT THE CARGO DOOR CAME OPEN IN FLIGHT, LANDED SAFELY. MAINTENANCE REPLACED ALL PARTS AND FRAMES REQ IAW SRM, OPS CHECKED FLIGHT SAT.Oct 18, 2012 · N153GL · Beech 1900D · Door Warning SystemSDR GLBA2012100500076Structure · damagedBIRD STRIKE ON LT OTBD WING FROM WS 192.74 TO APPROX 201.74, APPROX .5" IN DEPTH. REPAIRED IAW EO 12-1900-57-011. MAJOR REPAIROct 5, 2012 · N153GL · Beech 1900D · Wing Main, Frame StructureSDR GLBA2012091000049Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS 84.10, .75" IN LENGTH. REPAIRED IAW FR-CO002516R1, STEP 1. MAJOR REPAIR.Sep 7, 2012 · N153GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012070500010Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING AUX RIB AT WS 29.00 AND FS 288, 1.1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-006.Jul 5, 2012 · N153GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012062700007Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER 1 AND 2R, CRACK IS ALONG A ROW OF FASTENERS, 3.65" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO12-1900-53-037.Jun 27, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062600006Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SKIN CRACKED AT THE EMERGENCY EXIT DOOR 6C SKIN AT THE LWR AFT CORNER, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-52-001.Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062600005Skin · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE BELLY SKIN AT FS 303, IB 2.5" FROM SKIN EDGE, 4.25" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-036.Jun 26, 2012 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012062500002Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-033. MATERIALS UTILIZED ARE INCLUDED INJun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, StructureSDR GLBA201206250004Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FWD LWR LT PRESSURE BULKHEAD AT FS 84, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-034.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012062500003Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FWD LWR RT PRESSURE BULKHEAD AT FS 84, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-035.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012062500001Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3" IN LENGTH.Jun 25, 2012 · N153GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2012040201Engine · failedPILOT REPORTED THAT AFTER TAKEOFF AT 5000 FT, NR 1 ENGINE SHUTDOWN, RAN CHECKLIST, DECLARED EMERGENCY, RETURNED TO DEPARTURE, MANUALLY FEATHER NR 1 PROP. MX R & R LT ENGINE, PWR SEC AND GAS GENERATOR, IAW TC 1900-7100-00, OPS CHECKED GOOD.Apr 1, 2012 · N153GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20111114FPressure Switch · inoperativeRIGHT AUTOFEATHER WILL NOT TEST DURING RUN UP. MX REPLACED THE RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH.Nov 12, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20111101GPump · leakingPILOT REPORTED THAT THERE WAS A FUEL LEAK ON THE LT ENGINE. MX REPLACED THE LP FUEL PUMP.Oct 30, 2011 · N153GL · Beech 1900D · Fuel Boost PumpSDR GLBA20111017HLine · leakingPILOT REPORTED THAT FUEL WAS LEAKING FROM THE BOTTOM OF THE ENGINE. MX TIGHTED A LOOSE FUEL LINE, LEAK AND OPS CHECKED GOOD.Oct 15, 2011 · N153GL · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA20110926GPcb · inoperativePILOT REPORTED THAT DURING THE PROP OVERSPEED TEST ON THE RT SIDE THE AFX DISABLE LIGHT ILLUMINATED. MX REPLACED THE AFX PCB IAW MI 24-01 AND BMM 61-21-00, PN: 129-364091-9 SN: 742-D-96, OPS CK GOOD.Sep 23, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110919FLife Vest · tornPILOT REPORTED THAT THE CAPT'S LIFE PRESERVER POUCH IS RIPPED. MX REPLACE THE PRESERVER.Sep 16, 2011 · N153GL · Beech 1900D · Life JacketSDR GLBA20110831HFire Warning · illuminatedPILOT REPORTED THAT WHILE CLIMBING THE MASTER WARNING AND NR 2 T-HANDLE ILLUMINATED, EMERGENCY DECLARED, NR 2 ENGINE WAS SHUTDOWN, LANDED WITHOUT INCIDENT. MX REPLACED PCB E173 IAW MI 24-01 PN: 129-364037-1 SN: 657-I-86 AND FWD & AFT FIRELOOPS IAW 26-10-01 PNAug 30, 2011 · N153GL · Beech 1900D · Fire DetectionSDR GLBA20110830GExhaust Stack · cracked"SUP" - SIG EVENT - PILOT REPORTED THAT THE NR2 T-HANDLE ILLUMINATED IN FLIGHT, NO INDICATION OF A FIRE WAS VISIBLE, WITH NO ABNORMAL ENGINE INDICATIONS NOTED. MX FOUND EVIDENCE OF AN EXHAUST LEAK ON THE FIRE LOOP NEAR THE EXHAUST MOUNTING FLANGE, RR EXHAUST Aug 30, 2011 · N153GL · Beech 1900D · Engine Collector/Tailpipe/NozzleSDR GLBA20110829AConnector · looseNR 2 T-HANDLE ILLUMINATED IN FLIGHT. ENGINE SECURED, FIRE EXTINGUISHER ACTIVATED, T-HANDLE REMAINED ILLUMINATED. LIGHT EXTINGUISHED SHORTLY BEFORE TOUCHDOWN. NO OTHER INDICATION OF FIRE. PROP WAS VISUALLY VERIFED TO HAVE FEATHERED. MX INSPECTED FIRE LOOP SYAug 29, 2011 · N153GL · Beech 1900D · Fire Protection System WiringSDR GLBA20110830FGround Wire · loose"SUP" - SIG EVENT - PILOT REPORTED THAT THE NR 2 TEE HANDLE ILLUMINATED, SHUTDOWN RT ENGINE AND ACTUATED EXTINGUISHER, VISUALLY CHECKED THAT ENGINE WAS FEATHERED. MX INSPECTED FIRE LOOP SYS, FOUND LOOSE GROUND ON AFT CONNECTOR, REPAIRED GROUND REF AIM 14.3.0,Aug 29, 2011 · N153GL · Beech 1900D · Fire Protection System WiringSDR GLBA2011082911FSnubber · leakingPILOT REPORTED THAT THE CABIN DOOR SNUBBER IS AT 700LBS. MX REPLACED THE DOOR SNUBBER DUE TO LEAKING SEALS IAW BMM 52-10-01, OPS CHECKED GOOD.Aug 28, 2011 · N153GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110817FUplock Switch · inoperativePILOT REPORTED THAT WITH GEAR IN UP POSITION AND AUTO FEATHER SWITCH IN OFF POSITION. AUTO FEATHER OFF ANNUNCIATOR ILLUMINATED. MX REPLACED THE LT UPLOCK SWITCH, IAW TC 1900-3260.00, OPS CHECKED GOOD.Aug 16, 2011 · N153GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110817GSnubber · low pressurePILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER PSI WAS BELOW 1000 PSI. MX SERVICED THE SYS IAW BMM 12-10-00, SYS WITHIN LIMITS.Aug 16, 2011 · N153GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110811HBulb · inoperativePILOT REPORTED THAT THE BULB IN THE LT AUTOFEATHER ANNC IS BURNED OUT. MX REPLACED THE BULB IAW BMM 33-10-01, OPS CHECKED GOOD.Aug 10, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110721FPropeller · malfunctionedPILOT REPORTED THAT DURING APPROACH THE LT PROP WAS CYCLING IN AND OUT OF FEATHER WITH ABOUT 500LBS OF TORQUE. R & R LT & RT LOW PRESSURE AUTO FEATHER SWITCHES & RIGGED LT & RT ENG TORQUE IAW CH 7, SECTION 7.5 & BMM 61-21-01, OPS CHECKED GOOD.Jul 20, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110715HPcb · inoperativeDURING THE OVERSPEED TEST ON THE RT ENGINE THE AUTOFEATHER DISABLE ANNUNCIATOR ILLUMINATED. MX REPLACED THE AFX PCB IAW MI 24-01, OPS CHECKED GOOD.Jul 14, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110630FSwitch · inoperativePILOT REPORTED THAT WHILE REDUCING POWER FROM 1200 LBS TORQUE TO IDLE NR1 ENGINE TRIED TO AUTOFEATHER. MX R & R LT & RT LOW PRESSURE AUTOFEATHER SWITCHES & RIGGED LT & RT ENGINE TORQUE IAW AIM CH 7, SECTION 7.5 & BMM 61-21-01, OPS CK GOOD.Jun 28, 2011 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110628GConnector · loosePILOT REPORTED THAT WHEN THEY REDUCED POWER FROM 1200 TO IDLE THE LT ENGINE TRIED TO AUTOFEATHER, DISENGAGED AUTOFEATHER AND LANDED. MX RESECURED THE CONNECTOR PLUG ON THE LT LOW PRESSURE AFX SWITCH, OPS CK GOOD.Jun 27, 2011 · N153GL · Beech 1900D · Propeller/Propulsor System Wiring
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