N211GL
Service difficulty reports · 50
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 = 'N211GL' 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 = 'N211GL' 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 GLBA2012090700048Web · crackedDURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.0 AND FS 630 AT THE DEICE TUBE HOLE, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-028. MAJOR REPAIRSDR GLBA2012090600047Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT WING INBD RIB AT BL 29.06 AND WING SPAR JUNCTION, RIBS DOUBLER, 1" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-57-010. MAJOR REPAIRSDR GLBA2012031601Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK EXTENDING FROM THE 2 O'CLOCK POSITION ON THE AFT HORIZONTAL STAB SPAR CENTER WEB, .281" IN LENGTH. REPAIRED IAW FR-EO-02386. MAJOR REPAIRSDR GLBA20111219FSwitch · dirtyPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MX CLEANED THE SWITCH, OPS CHECKED GOOD.SDR GLBA20111212FConnector · damagedPILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATES WITH THE SWITCH ON DURING TAKEOFF, TESTED NORMAL. MX REPAIRED PIN 22 ON THE A123 PCB IAW MI 24-01, OPS CHECKED GOOD.SDR GLBA20111007FDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK ON THE DOOR LOWER FRAME AT FS 172-174, 2.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-058. MATERIALS UTILIZED ARE INCLUDED IN THE EO.SDR GLBA20110906GBulb · inoperativePILOT REPORTED THAT THE GEAR HANDLE HAS ONE RED LIGHT THAT IS INOPERATIVE. MAINTENANCE REPLACED THE BULB IAW BMM 33-10-05, OPS CHECKED GOOD.SDR GLBA201106241Bulb · inoperativeINSTRUMENT EMERGENCY LIGHT ON F/O SIDE INOPERATIVE. MX REPLACED THE BULBS PN 1864 IAW BMM 33-10-00, OPS CHECKED GOOD.SDR GLBA201105241Line · wornAUTO FEATHER OFF ANNUNCIATION ILLUMINATED WHEN THE AUTO FEATHER WAS TURNED OFF IN THE CLIMB. THE GEAR IN TRANSIT LIGHT THEN ILLUMINATED NO GREEN GEAR LIGHTS ILLUMINATED. DID NOT EXCEED 180 KNOTS. MAINTENANCE REPLACED THE LT MLG RETRACT LINE IAW AIM 10-32-01SDR GLBA20110503FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN CARGO DOOR FUSELAGE FWD FRAME AT F.S. 456, AT THE UPPER IB NUTPLATE AREA AT THE LONG GAS STRUT MOUNT, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUISDR GLBA20110502GKeel · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH NACELLE OB KEEL CRACKED AT GRAVEL FENDER WEB AND THINNED ABOVE CRACK AT UPPER 2 RIVETS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11SDR GLBA20110502JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS, FRAME AT F.S. 273.25 AND STRINGER 10L AND IN T-FRAME AT SAME LOCATION, .7" AND .9" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS ISDR GLBA20110502FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS ON LT SIDE OF FUSELAGE UPWARD ALONG F.S. 273.25 AND STRINGER 10L, LENGTHWISE ALONG W.L. 93, 2.2" HIGH AND 4.2 WIDE IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMEDSDR GLBA201120110502HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED AT STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53SDR GLBA20100910GSkin · burnedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A BURN HOLE IN THE RIGHT ELEVATOR 4" INBOARD OF OUTBOARD EDGE, .75" WIDE BY .625" DEEP. MAINTENANCE REPLACED THE RIGHT ELEVATOR, IAW BMM TC 1900-2730-00. REMOVED IN SERVICABLE CONDITION FSDR GLBA201007201Circuit Board · burnedPILOT REPORTED THAT ON APPROACH TO PHX FO NOTICED A SYNTHETIC BURNING SMELL BRIEFLY, THEN GOT A BATT TIE ANNUNCIATOR LIGHT. MAINTENANCE INSPECTED THE ELECTRICAL SYSTEM AND FOUND CIRCUIT BOARD A130 HAD A BURNT DIODE, REPLACED BOARD IAW AIM 10-24-01, RAN AIRCRAFSDR GLBA201005151Wire · damagedUPON APPROACH TO LAND, SELECTED MLG DOWN IN WHICH THE PUMP SOUNDED, DID NOT RECEIVE INTRANSIT LIGHT & NO GREEN LIGHTS TO INDICATE SAFE MLG. PERFORMED SEVERAL TEST TO ENSURE MLG SAFETY. TASK INCLUDED TAXI LIGHT, AUTOFEATHER, FLAPS AT 35 AND THE GPWS. ALL TEST ISDR GLBA20090416AControl Handle · deterioratedPILOTS REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED, THEY OBSERVED 3 GREEN DOWN LIGHTS. PILOTS THEN RETARDED THE LOWER LEVERS BACK WITH GEAR DOWN AND GOT A GEAR HORN, THE C/B THEN POPPED AGAIN. A MANUAL EXTENSION WAS THEN PERFORMED. MX R & R THE LSDR GLBA20090925FStructure · damagedLIGHTNING STRIKE ON THE LT ELEVATOR. DISCHARGE ON TRAILING EDGE APPROXIMATELY 9" TO 10.250" FROM TAB CUTOUT ON THE TOP AND BOTTOM SIDES. TRAILING EDGE DAMAGE APPROXIMATELY 1.5" BY .750" EIGHT INCHES OUT FROM TRIM TAB. MAINTENANCE REMOVED AND REPLACED THE ELEVSDR GLBA20090425ACabin Pressure · malfunctionedPILOTS REPORTED THAT UPON CLIMBING THE AIRCRAFT FAILED TO PRESSURIZE AND THEY THEN RETURNED TO FMN. MAINTENANCE OPERATIONALLY CHECKED THE SYSTEM ON THE GROUND WHICH WAS GOOD PER MM 21-30-00. OPERATIONAL CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY.SDR GLBA200903041Pedestal · out of adjustUPON SHORT FINAL THE PILOTS REPORTED THAT THE RIGHT HAND PROPELLER BEGAN TO CYCLING IN AND OUT OF AUTOFEATHER. THE PILOT INCREASED POWER HOWEVER IT DID NOT FIX THE PROBLEM. PILOTS TURNED OF THE AFX AND IT STOPPED FEATHERING. MAINTENANCE INSPECTED THE AUTOFEATHSDR GLBA20090220JFrame · crackedDURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FS 177.35 STRINGER 9R RELIEF CUTOUT. MAJOR REPAIR, 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 GLB2008F00026Stiffener · crackedDURING STRUCTURAL CHECK MAINT DISCOVERED A CRACK ON THE RT WHEEL WELL OB KEEL TAB TO OB FENDER STIFFENER 1" AT THE BOTTOM END OF STIFFENERS TO KEEL AREA. " SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR". (K)SDR GLB2008F00025Frame · crackedDURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .5". MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 164.4 REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3SDR GLB2008F00024Frame · crackedDURING STRUCTURAL INSPECTION MAINTENANCE FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .750". MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 177.3 AT STRINGER 9AR. REPAIR APPROXIMASDR GLB2008F00020Frame · crackedDURING STRUCTURAL INSP MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .750. (K)SDR GLB2008F00019Frame · crackedDURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY .5 INCH. OPEN (K)SDR GLB2008F00021Connector · looseSUSPECTED AUTOFEATHER EVENT, UPON APPROACH, PILOTS REPORTED THAT RT AUTOFEATHER ACTUATED (AS IT NORMALLY DOES DURING TESTING) ON APPROACH AFTER A MINOR POWER INCREASE. MAINT REMOVED AND REPLACED THE OVERSPEED GOVERNOR IAW MM 61-20. OPS CHECK WAS GOOD, HOWEVERSDR GLB2008F00015Autofeather Sys · malfunctionedACFT 211GL SUSPECTED AUTOFEATHER FLT 5127 "PIR" 08/15/08 PILOTS REPORTED DURING FINAL DESCENT INTO LANDING, THAT POWER WAS REDUCED TO APPROX 500 LBS WITH PROPS FULL FORWARD. DURING POWER REDUCTION ONE OR BOTH PROPELLERS APPEARED TO FEATHER, THEN SURGE. POWERSDR GLB2008F00000Valve · wornAC 211GL, AIR RETURN FLT NR 5066 "GBD" 06/27/08. PILOTS REPORTED THAT AFTER GEAR RETRACTION, THE GEAR WOULD NOT RETRACT. APPROXIMATE SPEED AT THE TIME WAS 106 KTS. "3" GREEN LIGHTS, NO RED GEAR UNSAFE LIGHTS. MAINTENANCE REMOVED AND REPLACED SERVICE VALVE IASDR GLB2008F00007Landing Gear · malfunctionedPILOTS REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND AIR RETURNED TO DEPARTURE. MAINT PERFORMED NUMEROUS GEAR RETRACTIONS AND EXTENSIONS IAW MM 32.00. NO DEFECTS WERE NOTED. (K)SDR GLBA20061106Landing Gear · malfunctionedAIR RETURN - FLIGHT 5031 ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT WAS FOUND SAFE FOR INTENDED FERRY FLIGHT TO WHERE MAINTENANCE PERFORMED NUMEROUS EXTENSIONS AND RETRACTIONS WITH NO DEFECTS NOTED IAW. MM 32-00. SUBSEQUENT OPESDR GLBA20061079Wire · detachedSMOKE/FUMES, FLIGHT 5061 AIR RETURN, PILOTS REPORTED THAT WHILE CLIMBING THROUGH 21.5 FOR 240 THEY NOTICED AN ELECTRICAL FUME ODOR. PILOTS PERFORMED WINDSHILED FAULT EMERGENCY CHECKLIST. TURNING OFF WINSHIELD ANTI-ICE GOT RID OF THE FUMES. MAINT SECURED A LOOSSDR GLBA20061011Angle · crackedLT HEAVY ANGLE CRACKED AT FS 288. MX REPAIRED THE LT HEAVY ANGLE AT FS 288 IAW BEECH 1900D SRM 53-90. REPAIR DIMENSIONS 13.5. PN 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
SDR GLBA20060902Unknown · odorUNSCHEDULED LANDING DURING TRAINING, GLA FLIGHT 41. PILOTS REPORTED THAT THE AIRCRAFT HAD JUST BEEN FUELED AND AFTER TAKEOFF A STRONG FUEL ODOR WAS PRESENT. MAINTENANCE INSPECTED THE WINGS AND FUSELAGE FOR LEAKS, AIRED OUT CABIN AND PERFORMED ENVIRONMENTAL CHESDR 20030856Fire Loop · defectiveDURING FLIGHT, FLIGHT CREW NOTICED RT ENGINE T-HANDLE ANNUNCIATOR AND YELLOW (LOOP) ANNUCIATOR FLICKERING ON AND OFF AND WAS DETERMINED BY CREW THAT IT WAS A FALSE INDICATION. MAINTENANCE TROUBLESHOT PROBLEM TO DEFECTIVE RT AFT FIRE LOOP IN ENGINE COMPARTMENT.SDR GLBA20030646Odor · detectedSMELL OF ELECTRICAL SMOKE IN COCKPIT, INSPECTED A/C SYSTEMS, FOUND NO DEFECTS.SDR GLBA20030648Door · corrodedCABIN DOOR IS CORRODED AROUND BUTTON, REPAIRED CORROSION.SDR GLBA2003113Uplock Switch · malfunctionedGEAR INTRANSIT LIGHT DID NOT EXTINGUISH. REMOVED AND REPLACED RT MLG UPLOCK SWITCH.SDR GLBA2003089Skin · crackedCRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED SKIN IAW BEECH SRM.SDR GLBA2003044Clutch · stuckELEVATOR TRIM STUCK. REMOVED AND REPLACED ELEVATOR ELECTRIC TRIM MAGNETIC CLUTCH AND CONNECTING CABLE PULLEYS, OPS CK GOOD.SDR GLBA2003036Wire · brokenLT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUM. REPAIRED BROKEN WIRE SPLICE ON LEFT ENG FIRE BOTTLE SQUIB.SDR GLBA202182Uplock Switch · malfunctionedIN-TRANSIT LIGHT STAYS ON WITH GEAR UP, R&R LT UP-LOCK SWITCHSDR GLBA2002135Plug · missingRT BLEED FAIL ON TAKE OFF, REPLACED EVA TUBE PLUG OPS CHECK OK.SDR GLBA2002109Switch · stuck#1 COMM FAILED, REPLACED PTT SWITCH OPS CHECKED SATISFACTORYSDR GLBA2002076Cable · brokenCABIN DOOR WILL NOT OPEN. REPLACED INNER DOOR CABLES, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2002023Terminal · looseFLAPS STUCK AT 17 PERCENT, FOUND LOOSE TERMINAL ON MOTOR RELAY. SECURED, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2001234Indicator · leakingAIR SPEED INDICATOR FAILED ON T/O, REPLACED OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2001194Seal · deterioratedCABIN PRESSURIZATION INOPERATIVE. REPLACED SEAL IN RIGHT WING ROOT, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2001184Relay · failedLANDING GEAR CIRCUIT BREAKER POPPED. REPLACED K3 RELAY AND A316 PCB, OPS CHECKED SYSTEM SATISFACTORY.
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