N154GL
Service difficulty reports · 58
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 = 'N154GL' 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 = 'N154GL' 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 GLBA2014091100437Skin · damagedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A LIGHTNING STRIKE ON THE OTBD RT ELEVATOR TE JUST OTBD OF THE OTBD MOST STATIC WICK CAUSING DAMAGE TO THE FIBERGLASS TIP, THE ADJACENT SHEET METAL & AN EXISTING PATCH. THERE ARE .060 INCH DIAMETER & .225 INCH DSDR GLBA2014012300373Spar · crackedDURING A SCHEDULED INSPECTION MX ACCOMPLISH PROACTIVE REPAIR TO THE RT VERTICAL SPAR CAP ANGLE IAW EO 14-1900-55-001. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.SDR GLBA2014011600371Skin · dentedDURING A SCHEDULED INSPECTION, MX FOUND THE LT AFT SKIN DENTED AT BS 446 BETWEEN STRINGERS 11-12L. REPAIREDS IAW EO 14-1900-53-005.SDR GLBA2014011300368Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK AT BS 183 & STRINGER 9R FRAME ANGLE, .375 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-003.SDR GLBA2014011300367Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR CUTOUT LOWER FRAME AT APPROXIMATELY FS 172 LOWER AFT CORNER, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-002.SDR GLBA2014011300370Skin · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS AT BS 150 & STRINGER 1 EXTERIOR FUSELAGE SKIN PROTRUDING OUT OF RIVETS ON EITHER SIDE OF STRINGER, .25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-004.SDR GLBA2014011300369Door · crackedDURING A SCHEDULED INSPECTION, FOUND THE EMERGENCY DOOR CRACKED, 4C AT THE RT FWD ASSEMBLY, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-001.SDR GLBA2013090900307Wire · damagedPILOT REPORTED THAT THE RT FIRE LOOP AND TEE HANDLE ANNUNCIATORS FLICKERED DURING CLIMB OUT. MAINTENANCE TROUBLESHOT SYSTEM, NO FAULTS FOUND MEGGED WIRE W16A22 FROM J410 T. HRU S16 SWITCH TO PIN 3 OF P157 AND FOUND SHORT TO GROUND. R & R SWITCH S16 IAW AIM 1SDR GLBA2013070500269Blower · odorPILOT REPORTED A FOUL ODOR EMINATING FROM THE ENVIROMENTAL SYS WITH A NOTIABLE VIBRATION IN THE BACK OF THE ACFT. MX CLEANED THE ENVIRO VENT BLOWER AND SECURED THE PANEL, OPS CHECKED GOOD, NO ODOR NOTED.SDR GLBA2012082300037Attach Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT THE RT ANGLE AT FS 107.00 AS IT ATTACHES TO THE LONGERON, RT ANGLE AT THE UPPER END OF THE BEND RADIUS, .5" IN LENGTH, AND AT THE UPPER FASTENER AREA, .375" IN LENGTH. REPAIRED THE AFFECTED AREA IAW ESDR GLBA2012082300038Attach Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE LT SIDEWALL AT FS 107.00, LT ANGLE UPPER INBD FLANGE PORTION IN THE BEND RADIUS AS IT ATTACHED TO THE LONGERON, .75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-047.SDR GLBA2012082300036Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT LONGERON AT JUNCTION WITH RT ANGLE AT FS 107.00 CRACKED FROM THE INBD FLANGE AT THE LONGERON TO THE BEND RADIUS, .75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-048. MAJOR REPAIRE.SDR GLBA2012082100035Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10, BEGINNING AT THE TOP EDGE AND RADIATES DOWNWARD, THE CRACK IS ON THE FWD FAIRING PORTION OF THE ANGLE, 4.25" IN LENGTH. SDR GLBA2012082100034Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND RT LWR FWD PRESSURE BULKHEAD CRACKED AROUND FASTENERS ALONG THE BULKHEADS INBD EDGE, FOUND 2 CRACKS APPROX .1 INCH IN LENGTH THAT RADIATES FROM FASTENER HOLES AT FS 84.0. REPAIRED IAW EO 12-1900-53-045.SDR GLBA2012082100033Pressure Blkhd · crackedDURING A SCHEDULED INSPECTION, FOUND LT LWR FWD PRESSURE BULKHEAD IS CRACKED ALONG THE INBD EDGE DOUBLE ROW OF FASTENER, 3 CRACKS .2 INCHES IN LENGTH RADIUS FROM FASTENER HOLES AT FS 84. REPAIRED IAW EO 12-1900-53-045.SDR GLBA2012061900001Web · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-017.SDR GLBA20111227FSwitch · dirtyCABIN DOOR ANNUNCIATOR ILLUMINATED ON DESCENT THEN EXTINGUISHED SHORTLY AFTER. MX CLEANED THE SWITCH, OPS CHECKED GOOD.SDR GLBA20111109FWire · damagedPILOT REPORTED THEAT THE CABIN DOOR ANNUNCIATOR EXTINGUISHES WHEN DOOR IS OPEN AND HANDLE IS CLOSED. MX REPAIRED SPLICE D436, OPS CHECKED GOOD.SDR GLBA20111003JCircuit Board · malfunctionedPILOT REPORTED THAT DURING RUNUP THE AFX DISABLE ANNUNCIATOR WON'T ILLUMINATE ON THE RT AUTOFEATHER TEST. MX RERACKED THE A123 PCB IAW MI 24-01, OPS CHECKED GOOD.SDR GLBA20110906FSwitch · inoperativePILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR DOES NOT EXTINGUISH. MX REPAIRED MULTIPLE WIRES TO SPLICE D436, REPLACED FWD MICROSWITCH REF 14.12.10, RIGGED SWITCH IAW BMM 52-70-01, OPS CHECK GOOD.SDR GLBA201108081Valve · failedLANDING GEAR FAILED TO EXTEND ON APPROACH. DID NOT HEAR THE PUMP TURN ON WHEN MOVING THE LANDING GEAR CONTROL HANDLE. PUMPED GEAR DOWN MANUALLY, HAD ALL 5 GREEN LIGHTS AND IN TRANSIT LIGHT WAS EXTINGUISHED. MX REPLACED THE LG SERVICE VALVE IAW BMM 32-30-16,SDR GLBA20110706HSupport · failedPILOT REPORTED THAT THE CABIN DOOR STRAP SUPPORT ON THE LT SIDE IS COMING APART. MX REINSTALLED A FASTENER ON THE LT CABIN DOOR STRAP SUPPORT IAW BMM 52-10-60, ALL CHECKS GOOD.SDR GLBA20110519FSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED AT THE LOWER BOTTOM, DEBONDED FROM FORWARD EDGE TO THE AFT EDGE, FROM LOWER EDGE TO 5" UPWARD. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RISDR GLBA20110518FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE BELLY SKIN AT FS 300 AND RT WING IB BULK HEAD, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-035. MATERIALSDR GLBA20110516LFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND CRACKS AT F.S. 456 BETWEEN STRINGERS 3L AND 4L AT THE UPPER IB NUTPLATE AREA, 1.9" IN LENGTH, 7 CRACKS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAWSDR GLBA20110516KFrame · crackedMAJOR REPAIR. DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE FRAME AT FS 456 AND S10R, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-034. MATERIALS UTILIZED ARE INCLSDR GLBA20100904ATube · leakingPILOT REPORTED THAT THEY NOTICED SMOKE/FUMES IN THE CABIN PRIOR TO TAKEOFF, SUSPECT VAPOR CYCLE SYSTEM LEAK. MAINTENANCE REPLACED THE TUBE FROM RECEIVER-DRIER TO CONDENSOR IAW BMM 21-52-00, REPLACED CONDENSER BLOWER IAW BMM 21-52-03, AND SERVICED SYSTEM IAW BMSDR GLBA20100805FAEngine · overtorquedPILOT REPORTED THAT UPON APPROACH, RT POWER LEVER STUCK WITH AN OVERTORQUE INDICATION, PERFORMED PRECAUTIONARY RT ENGINE SHUTDOWN. RT PROPELLER CONTINUED TO WINDMILL AFTER ENGINE SHUTDOWN. MX PERFORMED AN INSPECTION ON RT ENGINE POWER CONTROL LINKAGE, CABLE, CSDR GLBA2010051601Bearing · failedPILOTS REPORTED, WHILE PERFORMING A 2ND START FOR NR 2 ENG. NR 2 STARTER SEEMED TO TURN ON & OFF VERY QUICKLY WHEN IGNITION & ENG START SWITCH IN ON. DURING ENG START, N1 DOES NOT CLIMB ABOVE 6 %. ON 3RD ATTEMPT TO START, NOTICED NR 2 ENG ACCY SECTION HAD VISDR GLBA20091116FBrace · chafedMX DISCOVERED THAT THERE WAS CHAFING ON THE FWD RT SIDE OF THE RT MLG BRACE CTR TUBE APPROX 11 INCHES FROM TOP. CHAFE IS APPROX AT A 45 DEGREE ANGLE AND MEASURES .5 INCHES LONG, .310 INCHES WIDE AND .020 INCHES MAX DEPTH. CHAFE ON FWD RT SIDE OF THE MLG BRACSDR GLBA20090909HSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BELLY SKIN AT B.L. 29.0 AND F.S. 303.25. CRACK IS APPROXIMATELY 2.250" IN LENGTH. MAINTENANCE REPAIRED THE BELLY SKIN AT F.S. 303.25 AND B.L 29.0 IAW EO 09-1900-53-016. RII INSPECTIOSDR GLBA20090502ACircuit Board · looseRIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED DURING TAKEOFF WITH TAKEOFF POWER AND BLEED AIR VALVES CLOSED. MAINTENANCE RE-SEATED THE PRINTED CIRCUIT BOARD AND OPERATIONAL CHECKS WERE GOOD.SDR GLBA20090424BGenerator · failedPILOTS REPORTED THE THE LEFT DC GENERATOR FELL OFFLINE ON TAKEOFF ROLL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK PER MM 24-00-00-001. NO FAULTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR GLBA20090312ARelay · deterioratedPILOTS REPORTED THAT THE FLAPS STUCK INTERMITTENTLY AT 17 DEGREES AND EVENTUALLY CAME UP UPON LANDING. MAINTENANCE REMOVED AND REPLACED FLAP RELAY I.A.W. BMM 27-50-05 OPERATIONAL CHECKS WERE GOOD PART NUMBER ON/OFF. SM50B7 CLEARED MEL AND PLACARDS WERE REMOVESDR GLBA20090301BIndicator · wornFLIGHT 5014- NO AIRSPEED INDICATION ON CA AIRSPEED ON T/O ROLL. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIRSPEED INDICATOR IAW TASKCARD 1900.3411.00-1. OPERATIONAL CHECK WAS GOOD.SDR GLBA20061099Skin · damagedRT UPPER ICE SHIELD DIVIDED INTO (2) PIECES AT APPROXIMATE LOCATION OF STRINGER 8R FROM F.S. 183.25 TO F.S. 220.75. MAINT REPLACED THE RT UPPER ICE SHILED IAW. SRM 51-40. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.SDR GLBA20061098Frame · crackedFUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .6 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME AT FS 177.3 AT STRINGER 9R RELIEF HOL IAW. SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3 .071. RII INSPECTION COSDR GLBA20061097Frame · crackedFUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE FRAME AT FS 163.97 AT STRINGER 9R RELIEF HOLE IAW. SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024-T3 .071. RII INSPECTION COMPSDR GLBA20061096Frame · crackedFUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FUSELAGE FRAME FLANGE AT FS 451 STRINGER 10R IAW SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH. 2024-T3 .071. RII INSPECTIONS COMPLIED WITHSDR GLBA20061095Stringer · crackedSTRINGER 10R CRACKED AT F.S. 451. CRACK LENGTH APPROXIMATELY.5 INCH. MAINT REPAIRED STRINGER 10R FLANGE AT F.S. 451 I.A.W. BEECH 1900D SRM 51-70. REPAIR DIMENSION APPROX 7.5 INCH BY 1 INCH. 2024-T3 .050 INCH. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.SDR GLBA20061054Engine · deterioratedENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE ENG SECURE PROCEDURES AND SHUTDOWN THE ENG MAINT REMOVED AND REPLACED THE NR1 ENG ASSY IAW TASKCARD NR 1900-7100.00. RII INSP COMPLIED WITH.SDR GLBA20060961Torquemeter · malfunctionedABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECTLY. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE LT TORQUE GAUGE IAW MM 33-10. OPERATIONAL CHECK OF THE SYSTEM GOOD.SDR 20030785Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.SDR GLBA20030683Skin · crackedCRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN.SDR GLBA20030652Compressor · stalledNR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D.SDR GLBA20030598Wire · brokenLOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOODSDR GLBA20030594Indicator · frozenRT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CNDSDR GLBA20030527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONSDR GLBA2003527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONSDR GLBA2003153Indicator · malfunctionedLT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE.
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