N201GL
Service difficulty reports · 57
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 = 'N201GL' 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 = 'N201GL' 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 2022FA0000756Rib · crackedCRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80.5. BS 30SDR GLBA2017050400651Cable · not reportedMAINTENANCE REPORTED THAT THE UPPER FORWARD [AIRSTAIR] DOOR REQUIRES REPLACEMENT. REMOVED AND REPLACED THE UPPER FORWARD DOOR CABLE IAW BEECH 1900D AMM 52-10-02.SDR GLBA2016082300605Stringer · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 4R IS CRACKED IN THE RADIUS ON THE FORWARD END. MAJOR REPAIRSDR GLBA2015033000508Acm · wornPILOT REPORTED THAT THE PRESSURIZATION OPERATIONS CHECKED GOOD DURING RUN-UP, UPON CLIMB PRESSURIZED TO APPROX DIFF OF 3.0 & FAILED TO FURTHER PRESSURIZE. CABIN ALTITUDE HIGH ANNUNCIATOR ILLUMINATED, DEPLOYED OXYGEN MASKS, DECLARED AN EMERGENCY & RETURNED. SDR GLBA2015030900501Bulkhead · buckledDURING A SCHEDULED INSPECTION, FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO 12L. REPAIRED THE BULKHEAD IAW EO 15-120-53-001. MAJOR REPAIR.SDR GLBA2015011200491Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND THE UPPER INBD RT WING SKIN TE CHAFED & CORRODED WITH SEVERAL ELONGATED HOLES AT BL 36. CHAFE 8.5 INCHES LONG, 2 INCHES WIDE AT THE WIDEST PART & .020 INCHES DEEP BEFORE CORROSION REMOVAL. FOUND TO BE A MINOR REPAIR IAW SDR GLBA2014121700480Skin · wornDURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT BS 220 & STRINGER 15L HAS A .25 INCH HOLE WORN THROUGH THE SKIN. WORN AREA IS FWD & AFT APPROX 25 INCHES IN LENGTH & WIDTH IS APPROX .065 INCHES. REPAIRED IAW EO 14-1900-53-054SDR GLBA2014121900484Skin · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE CARGO BAY LT INNER SKIN AT BS 509.5 & STRINGER 11L, .9 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-059.SDR GLBA2014121700483Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 460 & STRINGER 3L, 2.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-058.SDR GLBA2014121700481Frame · crackedDURING A SCHEDULED INSPECTION, FOUND THREE CRACKS IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.50 BETWEEN STRINGERS 4 - 5L IN THE BEND RADIUS OF THE FRAME, TWO INCHES IN TOTAL LENGTH. REPAIRED IAW EO 14-1900-53-057.SDR GLBA2014121700482Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.5 & STRINGER 11L, .75 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-057.SDR GLBA2014121500478Bulkhead · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE CANT BULKHEAD FLANGE AT FS 588.10 & BETWEEN STRINGER 8R & 7R, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-055.SDR GLBA2014121500479Frame · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE FUSELAGE FRAME IN THE FLANGE BEND RADIUS AT FS 177.35 BETWEEN STRINGERS 12L & 13L, 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-SDR GLBA2014091900439Stringer · bentMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND STRINGER 11L BENT APPROX 2 INCHES IN LENGTH BETWEEN FS 513.50 & FS 523.50. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-034. MATERIALS UTILIZED ARE INCLUDSDR GLBA201403140001Connector · looseUPON EXTENDING GEAR ON FINAL, RT GEAR R & H ANNUNCIATORS FAILED TO ILLUMINATE. UPON COMPLETION OF CHECKLIST, ALL OTHER INDICATIONS REVEALED GEAR DOWN & LOCKED. INSTRUCTED BY MX TO RECYCLE GEAR, J HOOK WOULD NOT ALLOW GEAR HANDLE TO BE MOVED UP. ATTEMPTED TO SDR GLBA2013031500211Clamp · loosePILOT REPORTED THAT AT ALTITUDE 18500, CABIN ALTITUDE HIGH ANNUCICATOR ILLUMINATED. CABIN ALTITUDE INDICATED 10000 FT AND CABIN INDICATED 800 FT IAW MIN WITH INCREASE IN TRENDS, PASS O2 MASK DEPLOYED, CLIMB DIFFERENTIAL PRESSURE AT 2.8 AT TIME OF CLIMB ALTITSDR GLBA2012100100070Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE HORIZONTAL STAB AFT SPAR WEB AT RELIEF HOLE AT HSS 00.0, .5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-045.SDR GLBA2012100100069Spar · crackedDURING A SCHEDULED ROUTINE INSP FOUND FOUR CRACKS ON THE HORIZONTAL STAB FWD SPAR WEB AT HSS 00.00, 2" IN LENGTH TOTAL. REPAIRED IAW EO 11-1900-55-046.SDR GLBA2012100100072Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT. 1.5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-043.SDR GLBA2012100100071Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT CHORD, CRACKED FROM FIRST RIVET HOLE AND SECOND CRACK IS FROM SECOND RIVET HOLE, AND THIRD CRACK AT THIRD RIVET HOLE, AND FOURTH CRASDR GLBA20111204BBulb · inoperativeEMERGENCY LIGHTS ON THE CAPTAIN'S SIDE INOP. MX RELAMPED CAPT EMERGENCY LIGHT IAW B-1900 33-60-00-801, ALL CHECKED GOOD.SDR GLBA20111019FFcu · leakingPILOT REPORTED THAT THERE IS A LEAK COMING FROM THE SMALL DRAIN ON THE LT ENGINE. MX REPLACED THE LT HP FUEL PUMP AND FCU, OPS AND LEAK CHECKED GOOD.SDR GLBA20110829GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE FUSELAGE FRAME AT FS 456 & STRINGER 10R CRACKED, .55" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-052. MATERIALS UTILIZED ARE INCLUDED IN THESDR GLBA20110829HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE CARGO BAY BULKHEAD AT FS 531, LT UPPER OTBD CORNER CRACKED .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-053. MATERIALS UTILIZED ARE INCLUDED IN THE SDR GLBA20110823GFuel Control · leakingPILOT REPORTED THAT THE RT ENGINE IS LEAKING FUEL FWD OF THE WHEEL WELL, DRIPPING STOPS ATFTER SHUTDOWN. MX REPLACED THE RT FCU IAW TC 1900-7320.00 AND REPLACED HP PUMP IAW MM 73-10-02 SEC 6, REPLACED STARTER GEN, RIG CHECKS, RUN AND LEAK CHECKED GOOD.SDR GLBA201108101Bulb · inoperativeON FINAL, DID NOT RECEIVE NOSE GEAR DOWN AND LOCKED INDICATION. MX REPLACED THE LIGHT BULBS, PN: 327 IAW BMM 33-10-05, OPS CKS AND SWING CHECKS GOOD IAW AIM MI 32-01.SDR GLBA20110810GBulb · inoperativePILOT REPORTED THAT THEY DID NOT GET A NOSE GEAR DOWN AND LOCK INDICATION WITH THE GEAR DOWN AND LOCKED. MX REPLACED THE LIGHT BULBS, OK FOR SERVICE.SDR GLBA20110719FPump · leakingPILOT REPORTED THAT FUEL WAS LEAKING FROM THE NR2 ENGINE GANG DRAIN. MX REPLACED THE NR2 ENGINE DRIVEN FUEL PUMP IAW BMM 73-10-00.SDR GLBA201105131Unknown · odorTHE PILOT REPORTED THAT DURING DESCENT THEY SMELLED FUEL. MX CLEANED THE EPA CANNISTER AND CHECKED FUEL VALUES ON BOTH ENGINES, PERFORMED FCD 1900-08-30-01 STEPS 3&4, NO FURTHER DEFECTS NOTED.SDR GLBA20100422GFloor Support · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT FS 482 APPROX 24" INBD OF DOOR THRESHOLD. CRACK APPROX 1". CRACK IS AFT OF NUTPLATE IN RADIUS OF UPPER ANGLE FOR FLOOR SUPPORT WEB. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RIISDR GLBA20100422FAngle · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT FS 456 JUST LT OF STRINGER NR 1 FWD OF THE REINFORCING ANGLE ATTACHED TO THE FUSELAGE SECTION CRACK EXTENDS FROM EDGE OF ANGLE THROUGH FASTENER HOLE APPROX .375". TOTAL LENGTH OF CRACK APPROX 1".SDR GLBA201003231Bulb · burned outTHE PILOTS DISCOVERED THAT THE CAPTAINS SIDE INTRUMENT EMERGENCY LIGHT WAS BURN OUT. MAINTENANCE REMOVED AND REPLACED THE BULB AND THE LIGHT OPERATIONALLY CHECKED GOOD I.A.W. 1900D MM 33-10-00.SDR GLBA20091202BTransmitter · malfunctionedRT ENG WENT INTO AND OUT OF FEATHER ON SHORT FINAL. MX TROUBLESHOT THE SYS AND FOUND THE TORQUE INDICATION BAD. MX REMOVED AND REPLACED THE TORQUE TRANSMITTER IAW MM 77-10-00. OPS CHECK OF THE AUTOFEATHER SYS WAS GOOD IAW MM 61-20-00.SDR GLBA20091127091Autofeather Sys · malfunctionedSUSPECTED AUTOFEATHER - UPON APPROACH, THE PILOTS REPORTED THAT THE RT PROPELLER AUTOFEATHERED WITH TORQUE AT APPROX 1000 LBS. MX PERFORMED THE AUTOFEATHER OPERATIONAL CHECK 5 TIMES AND ALL INDICATIONS WERE WELL WITHIN LIMITS. NO DEFECTS NOTINE IN DURING THE SDR GLBA200909291Bulb · inoperativePILOTS REPORTED THAT ONE EMERGENCY INSTRUMENT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED BULB 1864 BY PUSHING IN AND TURNING THE A QUARTER UNTIL IT WAS FREE, REMOVED AND REPLACED THE BLUE SLEEVE TO THE NEW BULB AND INSTALLED BY PUSHING IN AND PERFOSDR GLBA200930041Indicator · erraticIN CRUISE AT 2300 NR 1 TORQUE GAUGE WAS FLUCTUATING 200-300FT/LBS. COULD HEAR THE CHANGE IN TORQUE. OCCURRED WITH PROP SYNC ON AND OFF. WHEN TORQUE BELOW 2500FT/LBS IN DESCENT ALL PWR CHANGE DECREASES AN ADDITIONAL 300FT/LBS WITHOUT BEING COMMANDED WITH POWER SDR GLBA20090224FSkin · chafedDURING ROUTINE SCHEDULED MX A CHAFE WAS FOUND ON THE BELLYSKIN AT APPROX FS 224.0 BETWEEN STRINGER 15L & 16L. ONE OF THEM WAS 2.9 INCHES IN LENGTH AND THE OTHER WAS 2.4 INCHES IN LENGTH RUNNING PARALLEL TO EACH OTHER. MAINTENANCE REPAIRED THE BELLY SKIN AT FSSDR GLBA20090223PSkin · damagedDURING ROUTINE SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE WAS FOUND AT F.S. 405.5 LEFT OF STRINGER 14L APPROXIMATELY 1.5 INCHES. HOLE SIZE APPROXIMATELY .375 X .125. MAINTENANCE REMOVED DAMAGE, HOLE .875” CIRCLE, INSTALLED COVER PATCH. COVER PATCH ALODINEDSDR GLBA20090223NFrame · crackedDURING ROUTINE SCHEDULED MAINTENANCE FOUND A FRAME CRACKED ON THE FORWARD SIDE OF THE AIRSTAIR DOOR ENTRANCE FRAME AT THE LOWER SNUBBER MOUNT BRACKET UPPER NUTPLATE. MAINTENANCE REPAIRED THE AIRSTAIR DOOR ENTRANCE FRAME IAW EO 09-UE201-05.SDR GLBA20090220IFrame · crackedDURING ROUTINE SCHEDULED MX CRACK WAS FOUND ON FRAME AT STRINGER 9R FS 163.975 STRINGER RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.SDR GLBA20090223HStringer · crackedDURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FSS 150.60 STRINGER 9R RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.SDR GLBA20090220KAngle · crackedDURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAJOR REPAIR - MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER IAW EO 09-201-2. REPAIR APPROXIMATELY 13.5". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR GLBA20090220LAngle · crackedDURING ROUTINE SCHEDULED MX, THE RT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER I.A.W. .EO. 09-201-2. REPAIR APPROXIMATELY 13.5". PART NUMBER 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR GLBA20090223FSkin · crackedDURING ROUTINE SCHEDULED MX THE SKIN OF FUSELAGE WAS FOUND CRACKED AROUND TWO RIVETS ONE ON EACH SIDE OF STRINGER ONE AT F.S. 150.60. MAINTENANCE REMOVED CRACKS BY .750” DIAMETER CUT OUTS. FABRICATED FILLERS FOR LT AND RT SIDE. FABRICATED EXTERNAL PATCH.SDR GLBA20090223GSkin · corrodedDURING ROUTINE SCHEDULED MX THE SKIN OF THE FUSELAGE IS CORRODED UNDERNEATH FRAME AT FS 203.25 AT STRINGER 15R TOWARDS 16R. LENGTH IS APPROIMATELY 3.5" AND RUNS UNDER FRAME. MX REMOVED DAMAGED SKIN AND INSTALLED INSERTION PATCH AND DOUBLERS. SKIN PATHC 11 X 5.SDR GLBA20060966Rib · crackedLT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAINTENANCE REPAIRED THE LT WING RIB OB OF HYDRAULIC POWER PACK ONE INCH CRACK AT W.S. 79.65 IAW SRM 51-70. REPAIR DIMENSION 4 INCH BY 2.7500 ISDR GLBA20030710Skin · corrodedPAX DOOR HAS CORROSION AROUND DOOR HANDLE, REPAIRED PER EO 04-14.SDR GLBA20030589Shutoff Valve · failedRT ENVIRO FAIL ANN ILLUMINATED, R&R RT PRSOV PN 114-380059-5 MM OPS AND LEAK CK GOODSDR GLBA20030570Warning Light · illuminatedCABIN DOOR ANNUNCIATOR CAME ON,R&R AIRSTAIR DOOR FWD LATCH HANDLE SWITCH PN V3-10108 OPS CK GOODSDR GLBA20030520Brush Block · inoperativeRT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5.
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