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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA20110606JCable · tornPILOT REPORTED THAT THE UPPER AFT AIRSTAIR DOOR CABLE COVER IS TORN. MX REPLACED THE UPPER AFT AIRSTAIR DOOR CABLE IAW BMM.SDR GLBA20110603ASwitch · inoperativePILOT REPORTED THAT THE AUTOFEATHER CYCLED ABOUT 5 TIMES ON FINAL APPROACH INTO DEN, RPM DROPPED FROM 1700 TO 1400 ON NR 1 ENGINE AND RETURNED TO 1700 AFTER ADDING POWER. MAINTENANCE REPLACED THE LT AFX LOW PRESSURE SITCH AND RIGGED THE RH ENGINE , FCU DEAD BASDR GLBA201106031Valve · malfunctionedLT ENG AUTO FEATHERED ON FINAL, EACH ENGINE SET TO 300 LBS, ADVANCED TO 1000 LBS, LT ENG AUTO FX UNTIL POWER ADVANCED ABOVE 1200 LBS. MAINTENANCE ADJUSTED RT ENGINE BETA VALVE AND LOW PITCH SOLONOID REF AIM72-50 AND T.C. 1900-ENGINERUN SHEET.SDR GLBA20110603GAutofeather Sys · malfunctionedPILOT REPORTED THAT THE LT ENGINE AUTOFEATHERED ON FINAL, EACH ENGINE SET TO 300LBS, ADVACED TO 1000 LBS LT ENGINE AUTOFEATHERED UNTIL POWER WAS ADVANCED. MX RIGGED BOTH ENGINES IAW WITH THE MM, OPS CK GOOD.SDR GLBA20110410FSkin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT AT FS 316 AND WL 159, APPROX 2.25" * 2.25", JUST LESS THAN .25" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-021. MATESDR GLBA20101122FTerminal · loosePILOTS REPORTED THAT THEY NOTICED A SMOKE IN THE COCKPIT AFTER AN ODOR AND VISUAL LEAK OF SMOKE WAS NOTICED COMING FROM THE CAPTIANS WINDOW AT THE LOWER FWD CORNER. ENG ANTI-ICE AND ENGINE AUTO IGNITION WERE ON FOR TAKEOFF AND SHORTLY AFTER ALL ICE PROTECTIONSDR GLBA20101001FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A .5" CRACK IN THE SKIN 5" LEFT OF BOTTOM CENTERLINE OF FUSELAGE AT F.S. 228.25. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-057. MATERIALSSDR GLBA20100920FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE FRAME AT THE STRINGER CUTOUT 4R AT FS 288, .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-056. MATERIALS UTILIZED ARE INCLUDED INSDR GLBA20100916GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT STRINGER CUTOUT 10R AND FS 456, .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-054. MATERIALS UTILIZED ARE INCLUDED INSDR GLBA20100916FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME ANGLE AT STRINGER 13L AND FS 177.35, UNDER THE AIRSTAIR ENTRANCE FLOOR, 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-53-055SDR GLBA20100915FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND CRACK IN FRAME AT FS 327.63, 1" BELOW FLOORBOARD ON RT SIDE, 2.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO10-1900-53-060. MATERIALS UTILIZED ARE INCLUDED IN SDR GLBA20100914FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE 6A EMERGENCY EXIT DOOR SKIN, LOWER FWD RADIUS, 1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-52-006. MATERIALS UTILIZED ARE INCLUDED IN TSDR GLBA20100910FSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" BY .375" BURN HOLE IN THE T/E OF THE ELEVATOR 9" INBD OF THE OTBD EDGE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO10-1900-27-004. MATERIALS UTILIZED ARE INCLUDSDR GLBA20100323FCable · out of rigSUSPECTED AUTOFEATHER - PILOTS REPORTED THAT UPON SHORT FINAL WITH TORQUE BETWEEN 800-1000, PROPELLER WENT IN AND OUT OF FEATHER. TORQUE SEARCHED TO BETWEEN 1600-1800 LBS. THE RT SIDE WAS THE ONE THAT SURGED. MX ADJUSTED POWER LEVER CABLES AT THE GREEN ARM ANDSDR GLBA20090605FSkin · dentedMAJOR REPAIR, DURING NORMAL LINE OPERATIONS A DENT WAS FOUND JUST FWD AND UNDER THE CARGO DOOR AT FS 446.5 1 INCH ABOVE WATERLINE MEASURING APPROX 1.2 INCH LONG, .250 INCH WIDE AND .063” DEEP. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-006. RII INSP COMPLSDR GLBA20090504GFcu · malfunctionedPILOTS REPORTED THAT THE RT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A 3 NAUTICAL MILE FINAL. THE AFX DISABLE ANNUNCIATOR ILLUMINATED WHEN THIS OCCURRED AND THE AUTOFEATHER SWITCH WAS IN THE ARMED POSITION. RT SIDE FLUCTUATED BETWEEN 400 AND 1700 LBS. LT TORQUSDR GLBA20090429AEngine · malfunctionedRT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A CLOSE FINAL THE AFX DISABLE ANNUNCIATOR ILLUMINATED WHEN THIS OCCURED AND THE AUTOFEATHERS SWITCH WAS IN THE ARMED POSITION. TORQUE GAUGE ON RT SIDE FLUCTUATED BETWEEM 400 AND 1700 LBS. LT TORQUE WAS STABLE AT APPRSDR GLBA200904281Relay · odorBURNING PLASTIC ODOR WHEN MODE CONTROLLER & BLOWERS ON. MAINTENANCE REMOVED FLOORBOARDS OVER THE FORWARD AND AFT VENT BLOWERES. FOUND BLOWERS TO OPERATE. RE-INSTALLED FLOORBOARDS. REMOVED FLOORBOARD COVERING FLAP MOTOR, GEARBOX, AND FLAP RELAY. NOTICED AN SDR GLBA200924042Circuit Board · malfunctionedPILOTS REPORTED THAT UPON TAKEOFF POWER UP ABOVE 2500 LBS. FOR TAKEOFF THE AFX DISABLE LIGHT ILLUMINATED AND THE NR 2 ENGINE STARTED TO TRANSITION IN AND OUT OF FEATHER. MAINTENANCE REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD PER GMM 9.2.0 & OPERATIONASDR GLBA200904215Fcu · out of adjustON SHORT FINAL WITH PROPELLERS AT 1700 , THE NR 2 PROPELLER SEEMED LIKE IT TRIED TO FEATHER MOMENTARILY TWO OR THREE TIMES. THE RPM DROPPED TO APPROXIMATELY 1400 TO 1500 RPM EACH TIME. MAINTENANCE ADJUSTED THE RT FCU PICKUP ROD, INPUT ARM AND LOW IDLE ADJUSTSDR GLBA200904191Gasket · damagedAFTER TAKEOFF, PROP GAUGE FOR NR 1 ENGINE DROPPED TO 0 RPM AND REMAINED THERE FOR THE REMAINDER OF THE FLIGHT AND TAXI. MAINTENANCE R & R NR 1 ENGINE TACH GENERATOR. MAINTENANCE THEN INSTALLED A GASKET, TACH GEN, AND GROUND RAN NR 1 ENGINE WHICH OPERATIONALLSDR GLBA20090320BSolenoid · out of rigPILOTS REPORTED THAT WHILE ADDING TAKEOFF POWER THE RIGHT ENGINE WENT INTO FEATHER THROUGH APPROXIMATELY 1500 LB OF. TORQUE. MAINTENANCE RIGGED THE RIGHT HAND PROP BETA VALVE AND RIGHT HAND LOW PITCH SOLENOID. REFERENCE MM 76-10-00. OPERATIONAL CHECK WAS GOOD.SDR GLBA20090302FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT FUSELAGE SKIN AT FS 273.25 AT STRINGER 10L. CRACK APPROXIMATELY 3.6 INCH IN LENGTH RUNNING PARALLEL TO STRINGER 10L. ABOVE CRACK AT STRINGER 10L AT NEXT RIVET LOCATION. MAINTESDR GLBA20090205DGovernor · malfunctionedSUSPECTED AUTO FEATHER - PILOTS REPORTED THAT THE RT PROPELLER AUTO FEATHERED IN FLIGHT WITH CORRESPONDING ENGINE ISSUE. AUTOFEATHER INOPERATIVE. MX R&R THE RT OVERSPEED GOVERNOR IAW MM 61-20. RIGGED BOTH LOW IDLES AND CORRECTED POWER SPLIT. OPS CHECKS WERSDR GLBA2009020409BAutofeather Sys · unknownRT ENG AUTO FEATHERED ON APPROACH.SDR GLBA200902041Pressure Switch · wornSUP - SIGNIFICANT EVENT - SUSPECTED AUTOFEATHER - UPON APPROACH WITH AUTOFEATHER ARMED BOTH TOQUE GAUGES AT 1000 THE RIGHT HAND SURGES BETWEEN 500 & 1500 LBS. OF TORQUE. FEELS LIKE AN AUTOFEATHER TEST. THIS CONTINUED UNTIL POWER WAS REMOVED, APPROXIMATELY 500 SDR GLBA200901131Skin · crackedDURING ROUTINE MX, A CRACK WAS FOUND ON THE UPPER FUSELAGE AT FS 151.00 NEAR CENTER LINE APPROX 1.6 INCHES LONG AND ONE RIVET HEAD MISSING NEAR CRACK. MX REPAIRED THE AFFECTED AREA IAW EO-09-UE153-01. RII INSP COMPLIED WITH AND FOUND TO BE SATISFACTORY. ALODISDR GLBA20061081Spar · corrodedDURING STRUCTURAL INSP MAINT FOUND CORROSION ON THE RT WING SPAR AT APPROX WS 126.5. MAINTENANCE REMOVED CORROSION AND INSTALLED REINFORCEMENT STRAP PER E.O. 08-UE153-02. REAPAIR APPROXIMATELY 14" . .190 7075-T73. RII INSPECTION COMPLIED WITH PER TASKCARD 8.SDR 20030831B-Nut · leakingAFTER DEPARTURE, ON CLIMB-OUT FLT CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATIONS, FOLLOWED BY LOW LEFT OIL PRESSURE GAUGE INDICATION. SHORTLY AFTER LEFT OIL PRESSURE LOW ANNUNCIATION. FLT CREW DECLARED EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. MASDR 20030809Skin · corrodedDURING ROUTINE INSPECTION, UNDER FUSELAGE SKIN CORROSION WAS FOUND WHERE SKIN BONDS TO AIRCRAFT STRUCTURE FS 243-249 AT STRINGER 16, WL75. ALL AFFECTED SKIN AND CORROSION WAS REMOVED AND REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE.SDR 20030801Door · corrodedON ROUTINE STRUCTURAL INSPECTION, THE AIRSTAIR DOOR HAS CORROSION ON INNER SKIN NEAR HANDLE. AFFECTED AREA IS APPROX 5.75" TO 7.5" IN DIA. DOOR REPAIRED, AIRCRAFT RETURNED TO SERVICE.SDR 20030787Switch · inoperativeUPON APPROACH, LANDING GEAR WAS SELECTED DOWN AND CREW NOTED THAT NOSE GEAR SHOWED NO INTRANSIT OR GREEN DOWN AND LOCKED INDICATION. CREW PERFORMED CHECKLIST AND HAD GEAR VERIFIED BY TOWER GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED SDR GLBA20030595Trim Stick · malfunctionedNR 1 ENG WON'T MAKE TAKEOFF POWER, R & R TRIM STICK PN 3053995CL10.SDR GLBA20030546Windshield · crackedFO'S WINDSHIELD CRACKED, R & R WINDSHIELD RT PN 129-5025-2SDR GLBA2003104Indicator · failedNR 1 TORQUE INDICATOR FAILED. REMOVED AND REPLACED NR 1 TORQUE IND.SDR GLBA2003019Switch · out of adjustRIGHT ANTI-ICE ANNUNCIATOR ILLUMINATED. ADJUSTED RT ICE VANE SENSE SWITCHES, OPS CK GOOD.SDR GLBA2002145Engine · malfunctionedLT ENGINE LOW OIL PRESSURE ANNUNCIATOR WITH MASTER WARNING, REMOVED AND REPLACED LT ENGINE.SDR GLBA2002082Controller · out of adjustNR 1 ITT INDICATES HOT ENG ON CLIMB. ADJUSTED TRIM STICK.SDR GLBA2002075Lever · out of adjustBOTH PROPS WOULD NOT REACH 1700 RPM. ADJUSTED PROP RPM LEVER, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2002072Cable · brokenPAX DOOR WOULD NOT OPEN. INSPECTED FOUND INNER DOOR CABLE BROKEN. REPLACED INNER DOOR CABLES.SDR GLBA2002060Tube · damagedLEFT BLEED-AIR FAILURE. REPAIRED DAMAGED ENA TUBING AT WING, OPS GOOD.SDR GLBA2001061Bleed Valve · malfunctionedRIGHT ENGINE COMPRESSOR STALLING. RECLASSED BLEED VALVE TEST FLIGHT SATISFACTORY.SDR GLBA2001015Connector · looseRETURN TO BLOCK, WILL NOT PRESSURIZE. INSPECTED FOUND LOOSE CONNECTION ON SQUAT SWITCH. TIGHTENED, OPS CHECKED SYSTEM GOOD.SDR 20000620SH012Gyro · precessesGYRO REMOVED FOR PRECESSING, NO FURTHER INFORMATION IS AVAILABLE. (X)SDR 20000505AP029Seal · leakingNR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE AND OIL PRESSURE ILLUMINATING. THE ENGINE WAS REPLACED AFTER IT WAS FOUND THAT THE ENGINE HAD EXCEEDED THE RUN TIME AT LOW OIL PRESSURE. ENGINE HAD HIGH OIL CONSUMPTION AT HIGH ALTITUDES. LABRYNTH SEAL WAS FOSDR 99ZZZX3703Altimeter · malfunctionedPILOT REPORTED THE PILOT'S ALTIMETER TO BE READING 150 FEET HIGH. REMOVED AND REPLACED PILOT'S ALTIMETER. SUBSEQUENT BENCH CHECK VERIFIED ALTIMETER TO BE INDICATING 150 FEET HIGH. THE BAROMETRIC WINDOWS DISPLAYED 1,017 MILLIBARS AT 29.92 IHG.
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