N195GL
Service difficulty reports · 85
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 = 'N195GL' 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 = 'N195GL' 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 GLBA2018030800702Cable · frayedMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IS FRAYED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IAW MM 52-10-02.SDR GLBA2017121500697Door Frame · crackedMAJOR REPAIR - MAINTENANCE NOTED THAT THE FUSELAGE DOOR FRAME WAS CRACKED AT STRINGER 11L AND FS 171.0. CRACK IS APPROXIMATELY 1.1 INCHES IN LENGTH. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **SDR GLBA2017081800678Hinge · looseMAINTENANCE REPORTED THAT THE AIRCRAFT SIDE OF THE AIRSTAIR DOOR HINGE HAD AFT RIVETS WHICH WERE LOOSE. REMOVED AND REPLACED LOOSE RIVETS REF SRM 51-40-03.SDR GLBA2017063000669Cable · wornMAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR CABLE IAW AMM 52-10-02.SDR GLBA2017063000668Cable · wornMAINTENANCE REPORTED THAT THE UPPER FWD AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER FWD AIRSTAIR CABLE IAW AMM 52-10-02. PN OFF/ON: 1440-42GLA, NSN.SDR GLBA2017051000654Circuit Breaker · poppedSIG EVENT, THE CREW DECLARED AN EMERGENCY ON APPROACH FOR LANDING [GEAR] FAILED TO EXTEND NORMALLY. IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE FOUND 60A(CB11) POPPED, INSPECTED WIRES FROM BUS BAR TO C/B TO GEAR MOTOR, NO FAULTS FOUND AIM 14.3. RESET C/B 11 & C/SDR GLBA2017041300648Pressure Switch · dirtyTHE CREW NOTED THAT THEY EXPERIENCED AN UNSCHEDULED AUTOFEATHER CYCLING DURING APPROACH TO LAND. THE ISSUE OCCURRED ON THE RIGHT ENGINE. MAINTENANCE REMOVED AND INSTALLED RIGHT ENGINE COWL IAW TC 1900-7100.10 STEPS 1, 2, 13, AND 14. CLEANED RIGHT LOW PRESSURESDR GLBA2017020300632Cable · brokenMAINTENANCE NOTED THAT THE LOWER FWD AIRSTAIR DOOR CABLE WAS BROKEN.SDR GLBA2017012500630Cable · brokenSIG EVENT, PILOT REPORTED THAT THE A/S DOOR CABLE BROKE. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **SDR GLBA2016071300596Snubber · disconnectedPILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER ARM CENTER PIVOT BOLT WAS DISCONNECTED. OPENSDR GLBA2015032300506Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE LT FUSELAGE SKIN UNDER THE VORTEX GEN MOUNT AREA. FWD SKIN CRACK IS .9" IN LENGTH AT FS 238.25, STRINGER 12L, & AFT SKIN CRACK IS 1.0" IN LENGTH AT FS 248.25, STRINGER 12L, CRACK 1.9" IN TOTAL LENGTH. RESDR GLBA2015032000505Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME REPAIR & FRAME AT FS 163.975, STRINGER 10R, FRAME CRACK BEYOND STOP DRILL, .65" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-004. MAJOR REPAIR.SDR GLBA2015031900503Channel · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.SDR GLBA2015031900504Frame · crackedDURING A SCHEDULED INSPECTION, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS AT THE OTBD END OF THE FRAME, 1.25" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-003. MAJOR REPAIR.SDR GLBA2015010200488Snubber · low pressureTHE AIR STAIR DOOR OPENS REALLY FAST & FOUND THAT THE DOOR SNUBBER PRESS READ 500 PSI. SERVICED THE AIR STAIR DOOR SNUBBER AS NEEDED IAW MI 52-01. OPERATIONS CHECKED GOOD AT THIS TIME.SDR GLBA2014020400375Brake Sys · malfunctionedSIG EVENT PILOT REPORTED THAT THE RT BRAKE PEDAL GOES COMPLETELY TO THE FLOOR ON THE CAPTAIN`S & FIRST OFFICER'S SIDE, RIGHT BRAKE COMPLETELY INEFFECTIVE. SUPPLEMENT INFORMATION ION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORKSDR GLBA2013110100347Skin · damagedDURING A SCHEDULED INSPECTION, FOUND A DENT FROM A BIRD STRIKE ON THE LT WING L/E BETWEEN WS 236.62 AND 223.48 AND HAS A FUEL LEAK DUE TO THE DAMAGE. REPAIRED IAW EO 13-1900-57-019. MAJOR REPAIRSDR GLBA2012121000132Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE EDGE OF A LIGHTNING HOLE, HORIZONTAL STABILIZER AFT SPAR WEB CENTERLINE AT HSS 0.00, .1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-068.SDR GLBA2012120700130Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION AT FS 228.25, ON SKIN, CORROSION FOUND JUST OTBD OF THIS REPAIR, STRINER 14R 4" OTBD. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-075. MAJOR REPAIRSDR GLBA2012120600129Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SPAR CAP ANGLE ON VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-066. MAJOR REPAIRSDR GLBA2012120600128Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SPAR CAP ANGLE ON VERT STAB AT SECOND FASTENER FROM THE TOP, 1.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-067. MAJOR REPAIRSDR GLBA2012120600127Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND BELLY CORROSION AT FS 243.25, APPROX 1" LEFT OF STRINGER 16. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-074. MAJOR REPAIRSDR GLBA20111216FFilter · leakingPILOT REPORTED THAT THERE IS A FUEL LEAK AROUND THE NR 1 ENG FUEL FILTER. MX REPLACED THE NR1 ENG FUEL FILTER.SDR GLBA20110824GSwitch · out of adjustPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. MX ADJUSTED THE DOOR LATCH SWITCH IAW MM 52-70-00, OPS CK GOOD.SDR GLBA20110817HLamp · inoperativePILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ARE INOP ON THE F/O'S SIDE. MX REPLACED THE LAMP IAW BMM 33-10-04, OPS CK GOOD.SDR GLBA20110725JSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE EMERGENCY EXIT AT SEAT 6A SKIN CRACKED IN LOWER FWD CORNER, 1.25" INCHES IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-009. MATERIALS UTILIZEDSDR GLBA20110722HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 509.50 BETWEEN STRINGERS 3L & 4L, 3.75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1SDR GLBA20110714FPropeller · malfunctionedTHE PILOT REPORTED THAT ON APPROACH, AT 500' AGL WITH BOTH TORQUES AROUND 750LBS THE RT ENGINE CYCLED INTO AND OUT OF FEATHER TWICE, ADDED POWER TO 1500LBS AND IT STOPPED. MX FOUND LT ENGINE HIGH & LOW TORQUES OUT OF RIG, RERIGGED POWER LEVERS IAW AIM 7.2.4 &SDR GLBA20101105APressure Switch · malfunctionedLT SIDE PROP AUTOFEATHER W/ 1000LBS TQ SHORT FINAL. STOPPED AUTOFEATHERING ABOVE 1000 LBS TQ. MX INSPECTED THE SYS AND ADJUSTED THE FLIGHT IDLE TORQUE IAW AIM CH 7 SEC 2.5, PARA 2 AND REPLACED THE LOW PRESS SWITCH, RAN ENGINES, OPS CHECK GOOD IAW BMM.SDR GLBA20100823GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-052. MATERISDR GLBA20100812FSkin · debondedDURING A SCHEDULED ROUNTINE INSP, FOUND THE AIRSTAIR DOOR SKIN DEBONDING ON THE LOWER AFT, APPROX 19" IN LENGTH. MX REPLACED THE AIRSTAIR DOOR BONDED SKIN IAW BMM 52-10-03 AND COMPLIED WITH SB 52-3094, OPS CHECKS GOOD.SDR GLBA20100618GSpar · damagedMAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKET IN LEFT WHEEL WELL. DAMAGE AT BL 107.0 TO 99.0 AND 104.5 TO 101.5 DELAMINATION IS APPROX 8 " LONGSDR GLBA20100615FArm · failedSIG EVENT - UPON LANDING IN "DEN" THE LEFT HAND MAIN LANDING GEAR COLLAPSED CAUSING SIGNIFICANT DAMAGE TO THE LEFT MAIN LANDING GEAR AND ASSOCIATED SPAR AREA. IT HAS BEEN ISOLATED AT THIS TIME TO A FAILURE OF THE UPPER DRAG BRACE "A" ARM ASSEMBLY LUGS WHICH BSDR GLBA201005122Switch · deterioratedPILOTS REPORTED THAT THE RIGHT AUTOFEATHER CYCLED DURING LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT PRESSURE SWITCH. THE OPERATIONAL CHECK WAS GOOD IAW BMM 61-21-01. P/N ON AND OFF 50-389121-47. S/N OFF 0112.SDR GLBA201005121Switch · malfunctionedPILOTS REPORTED THAT THE AUTOFEATHER SEQUENCE CYCLED MULTIPLE TIMES DURING LANDING FLARE. MAINTENANCE ADJUSTED THE RIGHT AUTOFEATHER ARMING SWITCH IN THE PEDESTAL IAW BMM 61-21-02. OPERATIONAL CHECK WAS GOOD.SDR GLBA20091111FSpar · damagedDURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 127.288 AND 129.588. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTSDR GLBA20091110HSpar · damagedDURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, A HOLE WAS FOUND TO BE STEPPED AND OVERSIZED AT THE LEFT HAND WING SPAR W.S. 104.0. APPROXIMATE DIAMETER OF .230". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIOSDR GLBA20091110GSpar · damagedDURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS FOUND TO BE APPROXIMATELY .230" ACROSS AT LEFT HAND WING SPAR W.S. 114.250. MAINTENANCE REPAIRED SDR GLBA20091110FSpar · damagedDURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX .150" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS SDR GLBA20091104FAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE RADIUS AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 2" LONG EXTENDING 1" FORWARD AND OF AFT OF F.S. 303.25. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RSDR GLBA200908122Latch · out of rigPILOTS REPORTED THAT THE 6C EMERGENCY EXIT HANDLE APPEARED TO BE UNLOCKED FROM THE OUTSIDE. MX RIGGED THE 6C DOOR LATCH AND OPS CHECKED GOOD.SDR GLBA200908121Handle · looseDURING ROUTINE WALK AROUND PILOTS REPORTED THAT LT OVERWING EXIT HANDLE APPEARED TO BE UNSECURED. MX ENSURED THAT LATCH WAS SECURED MM 52-20-00. SUBSEQUENT INSP BY PILOTS RESULTED IN OBSERVANCE THAT HANDLE BECAME UNSECURED SPONTANEOUSLY. MX REMOVED AND INSP SDR GLBA20090703ATach Generator · deterioratedABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED NR 1 PROPELLER TACH GENERATOR IAW 67D MM 70-00-00. OPS AND LEAK CHECKS WERE GOOD IAW MM 77-10-00.SDR GLBA200906011Indicator · malfunctionedNR 2 TORQUE GAUGE DROPPED TO 0 ON TAKEOFF ROLL. THE NR 2 TORQUE GAUGE DROPPED TO ZERO. MX REMOVED AND REPLACED THE NR 2 TORQUE GAUGE IAW MM 31-10-00. OPS CHECK WAS GOOD.SDR GLBA2009022809GKeel · crackedMAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT INBOARD KEEL. MAINTENANCE REPAIRED THE LEFT HAND INBOARD KEEL AT FS 321 IAW ENGINEERING ORDER 09-195-01.SDR GLB2008F00005Angle · crackedLT HEAVY ANGLE CRACKED APPROX 1.125 INCH IN LENGTH AT FORWARD BEND RADIUS AT FS 288.0. REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53.90. REPAIR AREA APPROX 13.125 INCH LONG. RII INSPECTION CP,[;OED WOTJ OAW TASKCARD NR 8.2.1. (K)SDR GLBA20060919Skin · misrepairedUPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 17SDR GLBA20060918Stringer · crackedUPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.SDR GLBA20060917Stringer · crackedUPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.9 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.SDR GLBA20060911Skin · crackedUPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REPAIRED BELLY SKIN AT APPROXIMATELY F.S.298.0 B.L. 27.0 PER BEECH SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1.
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