N240GL
Service difficulty reports · 71
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 = 'N240GL' 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 = 'N240GL' 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 GLBA2015012800494Strut · malfunctionedPILOT REPORTED THAT THE CABIN DOOR SNUBBER WAS INOPERATIVE. SERVICED THE PAX DOOR STRUT IAW MM 12-10-00. OPERATIONS CHECKED GOOD.SDR GLBA2014090200436Skin · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION IN AN AREA OF 4.5 INCHES BY 3.5 INCHES CAUSING A CRACK & BUILDING SKIN & A SHEARED RIVET BEHIND THE LT VORTEX GENERATOR & IN FRONT OF THE FORMER RING CENTERED AT FS 243.25 & WL 85.40. REPAIRED IAW EO 1SDR GLBA2014081200427Turnbuckle · out of adjustRIGHT FWD EMER EXIT HANDLE STICKING OUT. ADJUSTED THE DOOR LATCH TURNBUCKLE IAW MM 52-20-00. OPERATIONS CHECKED GOOD.SDR GLBA2014031700403Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND LOWER AIRSTAIR DOOR FRAME AFT CRACKED APPROXIMATELY 1/2 INCH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-022.SDR GLBA2014031700402Door Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND FWD FRAME AIRSTAIR DOOR CUTOUT AT FS 150.6 BETWEEN STRINGER 10L & 11L CRACKED, CRACK IS APPROXIMATELY 1/2 INCHES. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-023.SDR GLBA2013101400340Circuit Breaker · failedPILOT REPORTED THAT THE LT AUTOFEATHER SYS WILL NOT ENGAGE, THE AUTOFEATHER LIGHT IS NOT ILLUMINATED, BUT DOES PRESS TO TEST. MAINTENANCE REPLACED PCB A129, PERFORMED RUN, OPS CK GOOD.SDR GLBA2013081300293Spar Cap · chafedDURING A SCHEDULED INSP, FOUND CHAFING ON THE AFT SPAR LOWER CAP AT WS 85.50, APPROX .002 DEEP WITH A SMALL NICK IN THE CENTER OF THE CHAFE, NO OTHER DAMAGE IS NOTED, WIDTH OF THE DAMAGE IS 1.125". REPAIRED IAW EO 13-1900-57-015.SDR GLBA2013031300202Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 107, LT SIDEWALL LONGERON AT FINGER DOUBLER AREA "M" JUNCTION WITH SIDEWALL FRAME, RADIATES UPWARD FROM A FASTENER HOLE AND TERMINATES BELOW LONGERON BEND RADIUS, .4" IN LENGTH. REPAIRED IAW EO 13-1SDR GLBA2013031300206Doubler · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SIDEWALL FINGER DOUBLER AT FS 107, .25" IN LENGTH. REPAIRED IAW EO 13-1900-53-026. MAJOR REPAIR.SDR GLBA2013031300205Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 177.35 BETWEEN STR 13 - 14L AFT SIDE, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-023. MAJOR REPAIR.SDR GLBA2013031300204Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SIDEWALL AT FS 107 AT THE UPPER END OF THE FRAME AT THE LAST ATTACHING FASTENER AREA, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-024. MAJOR REPAIR.SDR GLBA2013031300203Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SIDEWALL FRAME AT FS 107 IN THE BEND RADIUS (UPPER END OF FRAME) AND AT UPPER FASTENER AREA, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-025. MAJOR REPAIR.SDR GLBA2013010400170Spar Cap · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN RT FORWARD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 2.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-005. MAJOR REPAIR.SDR GLBA2013010400169Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-55-004. MAJOR REPAIR.SDR GLBA2013010400168Skin · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE RT ELEVATOR ON THE T/E RIGHT ABOVE THE OTBD STATIC WICK, APPROX 0.3125 INCHES DEEP BY .25 INCHES WIDE. REPAIRED IAW EO 13-1900-27-002. MAJOR REPAIR.SDR GLBA2012122400139Bulb · inoperativePILOT REPORTED THAT THE CAPT'S INSTRUMENT EMERGENCY LIGHTS WILL NOT TURN ON. MX REPLACED THE BULB, OPS CHECKED GOOD.SDR GLBA2012102200085Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION ON THE BELLY SKIN AT FS 243 BETWEEN STRINGERS 16 & 15R, VISIBLE CORROSION IS APPROX 1 BY 1 INCH. REPAIRED IAW EO 11-1900-53-055. MAJOR REPAIR.SDR GLBA2012102200084Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE BELLY SKIN AT FS 213, LOWER FUSELAGE. REPAIRED IAW EO 11-1900-53-056. MAJOR REPAIR.SDR GLBA2012082800040Bulb · inoperativePILOT REPORTED THAT THEY HAD A GEAR INDICATION PROBLEM, SWAPPED ANNC'S AND IT WORKED, ATC DECLARED EMERGENCY, MX REPLACED THE BULB, OPS CK GOOD.SDR GLBA2012072300017Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AROUND THE HORZ STAB AFT SPAR WEB AT HSS 0.00, 1.625" IN LENGTH. REPAIRED IAW EO 12-1900-55-019. MAJOR REPAIRSDR GLBA2012052901Spar · chafedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT WING MAIN SPAR CHAFED AT INBD EDGE OF LOWER ACM PANEL. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-003.SDR GLBA20111116FPlacard · missingTHE SEAT BACK UPRIGHT FOR TAKEOFF AND LANDING, & THE EMERGENCY EVACUATION PLACARD IS MISSING FROM SEAT 5A. MX REPLACED THE PLACARD IAW AIM 5-16-0.SDR GLBA20111104GFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE CARGO DOOR AFT FUSELAGE FRAME OF FS 509 AT THE GAS STRUT MOUNT BETWEEN STRINGERS 4L & 5L, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-SDR GLBA20111104FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS IN CARGO BAY FRAME FS 456 AT GAS STRUT MOUNT, 1" AND 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-062. MATERIALS UTILIZED ARE INCLUDED IN THE SDR GLBA20110920FB-Nut · loose"SUP" - SIG EVENT - PILOT REPORTED THAT THERE IS A FUEL LEAK FROM THE BOTTOM OF THE LT ENGINE COWLING. MX TIGHTENED A B-NUT ON THE FUEL PUMP IAW BMM 73-12-00, OPS CK GOOD.SDR GLBA201109071Bulb · inoperativeINSTRUMENT EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE BULB BURNED OUT, IAW BMM 33-10-04, OPS CHECKED GOOD.SDR GLBA20110818JHandle · unsecurePILOT REPORTED THAT THE RT FWD EMERGENCY DOOR HANDLE APPEARS TO BE HALF WAY OPEN. MX RESECURED THE EXIT DOOR IAW BMM 52-20-00, SEC 1 A-B, OK FOR SERVICE.SDR GLBA20110818HHandle · unsecurePILOT REPORTED THAT THE RT FWD EMERGENCY DOOR HANDLE APPEARS TO BE HALF WAY OPEN. MX RESECURED THE EXIT DOOR IAW BMM 52-20-00, SEC 1 A-B, OK FOR SERVICE.SDR GLBA20110721GCable · brokenPILOT REPORTED THAT THE CABIN DOOR SNUBBER CABLE BROKE. MX REPLACED THE SNUBBER CABLE IAW BMM 52-10-01, OPS CHECKED GOOD.SDR GLBA20110711LConnector · loosePILOT REPORTED THAT THE FIRE EXTINGUISHER TEST A WAS INOP, DISC ANNUNCIATOR ON BOTH SIDES DID NOT ILLUMINATE WHEN TESTED. MX FOUND A LOOSE CONNECTION ON THE A 257A, SECURED CONNECTOR REF AIM 10-74-1, PERFORMED TEST A, ALL LIGHTS ILLUMINATE, OPS CK GOOD.SDR GLBA201106291Latch · unsecureDURING AN INSP THE PILOT FOUND EMERGENCY EXIT 4C LATCH NOT SECURE. MX INSPECTED EMERGENCY DOOR 4C FOUND LATCH ON OUTSIDE DOOR. NOT SECURE REINSTALLED SECURE EMERGENCY DOOR 4C DOOR. SECURED REF MM 52-20-00 1(B).SDR GLBA20110630MCover · torn"SUP" - SIG EVENT - DURING ROUTINE MX INSP, FOUND THE UPPER AFT AS DOOR CABLE COVER CUT. MX R & R UPPER AFT AS DOOR CABLE IN REF WITH MM 52-10-02.SDR GLBA201103171Wire · chafedPILOT REPORTED THAT THE #1 FIRE BOTTLE "DISCH" ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND A CHAFFED WIRE GOING TO THE LH FIRE BOTTLE, REPAIRED WIRE AND SPLICED IAW AIM 12.8.0, OPS CK GOOD.SDR GLBA20100927GSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE .7" BY 1" DEEP IN THE T/E OF THE LT ELEVATOR, JUST INBD OF CAP AT OUTER STATIC WICK, AT OUTER STATIC WICK, AND A DAMAGED RIVET ON TOP OF THE CAP. MAINTENANCE REPLACED THE RT ELEVASDR GLBA20100926FSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE .5" BY .5" DEEP IN THE T/E OF THE RT ELEVATOR, JUST INBD OF THE CAP AT THE OUTER STATIC WICK. OPENSDR GLBA20100716ADownlock Switch · failedPILOT REPORTED THAT NOSE GEAR ANNUNCIATOR FAILED TO ILLUMINATE ON GEAR EXTENSION, PILOTS CONFIRMED THERE WAS A POSITIVE PRESSURE USING THE MANUAL EXTENSION PUMP IN CASE IT WOULD BE REQUIRED, GEAR WAS DOWN AND LOCKED, MANUAL EXTENSION WAS NOT PERFORMED. MAINTENSDR GLBA20100622FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 150 AT THE ATTACH POINT FOR THE LOWER PAX DOOR STRUT MOUNTS UPPER AFT NUTPLATE AREA. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS SDR GLBA20100622HSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION CRACKS WERE FOUND IN THE UPPER SKIN AT FS 273.25 BETWEEN STRINGER 1 AND STRINGER 3R, CRACKS RANGE FROM .5" TO .7", APPROXIMATELY 7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRSDR GLBA20100622GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT, .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-035. MATERIALS UTILISDR GLBA20100622JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A .75" CRACK WAS FOUND ON THE FRAME FLANGE AT F.S. 273.25 AND STRINGER 2R CUTOUT OUTBOARD OF STRINGER 2R, AND CRACKED .7" ON THE FRAME FLANGE INBOARD OF STRINGER 2R, AND A CRACK .7" I/B OF STRINGER 10R. MAISDR GLBA201005311Bearing · deterioratedUPON PRE-FLIGHT INSPECTIONS THE PILOTS REPORTED THAT THE NR 4 MAIN LANDING GEAR WHEEL ASSEMBLY WAS MISSING. (NOTE: THE LANDING GEAR WAS ALSO REMOVED AND REPLACED DUE TO DAMAGE TO THE AXLE ASSEMBLY AND THE BRAKES PRECAUTIONARY). MAINTENANCE REPLACED THE NR 3 MLSDR GLBA20090508BWindow · cracked(SUP) - DIVERSION - AIRCRAFT N240GL - FLIGHT 10 - THE PILOTS REPORTED THAT ENROUTE FROM "LWT" - "DEN" THE CAPTAINS WINDSHIELD SHATTERED/BROKEN. THE AIRCRAFT DIVERTED TO "CYS" FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW BMM 52-10SDR GLBA20090418ACircuit Board · malfunctionedHAD MASTER WARNING AND MASTER CAUTION ANNC FLASHERS ON TAKEOFF, ABORTED. MASTER WARNING FLASHERS SEEMS TO COME ON ANYTIME MASTER CAUTION FLASHERS COMES ON. MAINTENANCE R & R PRINTED CIRCUIT BOARD. OPERATIONAL CHECKS WERE GOOD IAW MM 31-61-10.SDR GLB2008F00016Regulator · malfunctionedACFT 240GL AIR RETURN FLT 5087 "DEN" 08/17/08 PILOTS REPORTED THE PNEUMATIC PRESSURE WAS EXCEEDING REDLINE DURING CLIMBOUT AT FULL POWER SETTINGS. MAINTENANCE ADJUSTED PNEUMATIC REGULATOR AS REQUIRED IAW 1900D MM 36-00-01. OPERATIONAL CHECK WAS GOOD.
SDR GLBA20060906Skin · crackedUPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED A 3.25 INCH LONG CRACK 27.5 INCHES LT OF BELLY CENTERLINE AT APPROXIMATELY STA. F.S. 352. MAINTENANCE REPAIRED THE CRACK IN THE FUSELAGE IAW SRM 51-70 FROM F.S. 351 TO F.S. 354.25. REPAIR DIMENSIONS 7.25 INCHES BSDR GLBA20060809Pressure Switch · intermittentPROPELLER SYSTEM FLUCTUATED IN AND OUT OF FEATHER ON APPROACH WITH INTERMITTENT AFX DISABLE LIGHT. REPLACED LOW PRESSURE SWITCH (PN 50-389121-47, SN 0245). (TOTAL TIME UNKNOWN)SDR GLBA20060796Motor · shortedIRRITATING SMELL / SMOKE IN COCKPIT/CABIN AFTER FLAP EXTENSION. SHUT ENGINES DOWN ON TAXIWAY, INSPECTED AIRCRAFT AND FOUND FLAP MOTOR SHORTED. REPLACED FLAP MOTOR, OPS CHECK SATISFACTORY.SDR GLBA20060700Stringer · corrodedINSPECTION OF FS258.25 TO 273.25, STRINGER 14R HAD LEVEL (2) CORROSION. REPAIRED IAW MANUFACTURES INSTRUCTIONS (FR-CO-01321) DATED 3-20-06SDR GLBA20050507Autofeather Sys · malfunctionedLEFT ENGINE SOUNDED LIKE IT CYCLED THROUGH AN AUTOFEATHER, INCREASED POWER AND CONDITION CEASED, LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN-UP, COULD NOT DUPLICATE, RETURNED TO SERVICE.SDR 20030830Wire · chafedDURING CLIMB, FLT CREW REPORTED AFX DISABLE AND LEFT AND RIGHT AUTOFEATHER ANNUNCIATORS ILLUMINATED. FLT CREW RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRES AT LT MLG UPLOCK SWITCH. OP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Back to N240GL