N26549
Service difficulty reports · 54
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 = 'N26549' 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 = 'N26549' 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 ASOA2018101654055Floor Support · not reportedIAH- MAINTENANCE REMOVED AND REPLACED A REPAIR DOUBLER ON THE CENTER OMEGA BEAM BETWEEN FR 60-61 IAW TECHNICAL DISPOSITION ETD2018-145-107152. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2018101654054Doubler · dentedIAH- MAINTENANCE REMOVED AND REPLACED A REPAIR DOUBLER BETWEEN FR2-4 STRINGERS 9R-13R IAW SRM 53-10-01. AIRCRAFT RETURNED TO SERVICE.SDR ASOA201803267041Proximity Switch · brokenAFTER TAKEOFF, THE LANDING GEAR WOULDN'T RETRACT. RETURNED TO DEPARTURE. FOUND A BAD PROXIMITY SWITCH. REPLACED THE PROXIMITY SWITCH IAW WITH WO:542630. PERFORMED GEAR RETRACTIONS AND WAS RELEASED BACK TO SERVICE.SDR ASOA20180317012Display · faultyTHE CREW REPORTED STRONG ODOR IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE ODOR TO BE COMING FROM THE CAPTAIN`S MFD. THE MFD WAS REPALCED AND OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR ASOA201702123007Control Unit · malfunctionedTHE CREW REPORTED A RUDDER OVERBOOST MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RUDDER POWER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.SDR ASOA201610293063Battery · inoperativeEMERGENCY LIGHTS IN GALLEY INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.SDR ASOA20160602032Floor Support · corrodedDURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 60-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140822095Valve · stuckACFT WAS BEING VECTORED WHEN THE PRESSURIZATION BECAME ERRATIC, COULDN'T GET IT UNDER CONTROL MANUALLY AND FINALLY PRESSURIZATION DEPRESSURIZED AT 5000 FEET. ACFT LANDED AND MAINTENANCE, R THE ELECTROMAGNETIC OUTFLOW VALVE IAW AMM 21-31-03; IPC 21-30-00, FIGURSDR ASOA20140706079Fan · failedPILOT REPORTED AFTER TAKE OFF AND GEAR RETRACTION, A STRANGE ODOR PERCEIVED IN THE FLIGHT DECK. MX PERFORMED AN OPS CHECK OF APU BLEED SYS AND PERFORMED A GVI OF FWD AVIONICS BAY FOR ODOR AND ABNORMALITIES. NO DEFECTS NOTED. AN ASSOCIATED ELECTRONIC BAY EXASDR ASOA20140704050Fuse · blownDURING ROUTINE MAINTENANCE, THE LT FORWARD EXTERNAL EMERGENCY AISLE LIGHT, AND COCKPIT FLOODLIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKED GOOD.SDR ASOA20140517075Flange · crackedDURING C-CHECK, THE RUDDER II UPPER ATTACHMENT POINT NUTPLATE FLANGE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FLANGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130326045HBattery Pack · inoperativeDURING MX INSPECTION THE FORWARD LT EXTERNAL EMERGENCY LIGHT AND FWD CABIN CEILING LIGHT WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY, OP TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA201111211002Detection Sys · malfunctionedDURING CLIMB THE EICAS DISPLAY INDICATED A SYS NR 1 BLEED AIR LEAK. THE ACFT RETURNED AND LANDED AT WITHOUT INCIDENT WHERE MX PERFORMED TROUBLESHOOTING, PERFORMING SYS OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED, NOR DID THE WARNING INDICATION ILSDR C2XA11RI152Control Unit · faultyAFTER TAKEOFF, DURING CLIMB THE CREW REPORTED MAIN PITCH INOP WARNING ON EICAS. CREW PERFORMED AIR RETURN BACK TO IAD. IAD MX REMOVED AND REPLACED HORIZONTAL STABLIZER CONTROL UNIT IAW EMB145 AMM 27-40-01 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT SDR C2XA11CL150Fire Loop · chafedORF FLT 5867 THE CREW REPORTED A ENGINE FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11RI014O-Ring · wornFLIGHT 4936 - JAX - FLIGHT CREW REPORTED NR 1 BLEED LEAK ON CLIMB. CREW PERFORMED AIR RETURN AND LANDED SAFELY. MX REMOVED AND REPLACED SEVERAL O-RINGS FWD OF LAV NR 1 BLEED SIDE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SSDR C2XA10TY123Engine · malfunctionedTYS - IN BNA THE CREW EXPERIENCED A FUNNY SMELL AND VIBES AT 5000 FEET ON DESCENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE AND WILL BE RELEASED AT THE END OF THE CHANGE AND OPS CHECKS.SDR C2XA10IA234Smoke Detector · malfunctionedIAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SSDR C2XA10IA233Smoke Detector · false activationIAH - FLIGHT 2493, DURING CLIMB THE CREW REPORTED THAT THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SSDR C2XA10SH260Frame · crackedSHV - DURING C-CHECK THE RT FRAME 10 SEGMENT AT STRINGER 10R WAS FOUND TO BE CRACKED DIRECTLY BELOW THE F/O DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH259Frame · crackedSHV - DURING C-CHECK LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L DIRECTLY BELOW THE PILOT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH258Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA210Windshield · crackedIAH - FLIGHT 2550, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD SHATTERED ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NSDR C2XA09TY120Fastener · looseNR 2 ENGINE FWD MOUNT YOKE O/B PLATE HAS SEVERAL LOOSE FASTENERS. REMOVED AND REPLACED 13 LOOSE JO-BOLTS IAW EMB 145 SRM 51-40-02. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA09RI006Inverter · inoperativeFLIGHT CREW REPORTED EMERGENCY LIGHT STRIP ROW 8 TO 12 INOPERATIVE. MX REMOVED AND REPLACED AC INVERTER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08IA255Light · malfunctionedIAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT STRIPS BETWEEN ROWS 8 & 9 WERE FOUND TO BE INOPERATIVE. MX INSPECTED THE LIGHTING SYSTEM, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA08TY116Stringer · tornA/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 21L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 21L AT FRM 64-68 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. THE NEW SECTION OF STR 21L AND STR SPLICE AT FRAMES 61-62 WERE SDR C2XA08TY114Stringer · tornA/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 19L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 19L FRM 67 TO FRM 61 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. FWD SECTION OF STR 19L AND STR SPLICE AT FRM`S 66-67 WERE ISDR C2XA08ON173Handle · out of adjustFLT 0053 RNO FLIGHT CREW REPORTED AFTER LANDING IN RNO PAX DOOR DIFFICULT TO OPEN FROM INSIDE. REPO ACFT 188 ONT RNO TO COVER FLIGHT 53 AND ROUTE MECHANICS AND PARTS TO REPAIR 549. MX PERSONNEL ADJUSTED PAX DOOR INTERNAL HANDLE. OPS CHECK SATISFACTORY AND ASDR C2XA08TY066Light · inoperativeEMERGENCY LIGHT FLOOR STRIP WILL NOT ILLUMINATE BETWEEN ROWS 8A AND 10A. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. (S)SDR C2XA08TY047Light · inoperativeSERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ON SERVICE DOOR IAW EMB 145AMM 33-50-10, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA08SH005Floor Support · corrodedSHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08SH004Skin · corrodedSHV - DURING C-CHECK RIGHT HORIZONTAL STAB L/E HAS PITTING CORROSION. MX REPAIRED RIGHT HORIZONTAL L/E IAW EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08SH003Attach Bracket · damagedSHV - DURING C-CHECK LEFT WING AILERON HAS EXCESSIVE PLAY AT PCA RODS AND MIGRATED HAT BUSHING AT ATTACHMENT LUG. MX REMOVED AND REPLACED LEFT AILERON PCA BRACKET IAW EMB 145 SRM 51-40-02 & EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08SH002Door Frame · corrodedSHV - DURING C-CHECK MAIN DOOR LOWER FRAME HAVE CORROSION AROUND NUT PLATE HOLES. MX REPAIRED MAIN DOOR LOWER FRAME IAW EMB 145 EC 5210-01154. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA07CL007Static Port · inoperativeCLE FLIGHT 2061 THE CREW REPORTED A PITOT NR 2 INOPERATIVE MESSAGE ON THE ECIAS WITH A BURNING SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 STATIC PORT ASSEMBLY. OPERATIONAL CHESDR C2XA06IA108Heater · odorIAH - FLIGHT 2392, THE CREW REPORTED AN ACRID ODOR IN THE COCKPIT DURING APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE PACKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FORSDR C2XA06SH006Beam · corrodedSHV-DURING C CHECK THE BAGGAGE DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05CL048Engine · failedCLE FLIGHT 2668 THE CREW REPORTED A LOUD BANG FOLLOWED BY NR 1 ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.SDR C2XA04IA055Fuel Nozzle · faultyCREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THESDR C2XA04SH145Rib · gougedSHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RSDR C2XA04SH142Floorbeam · corrodedSHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH141Sill · corrodedSHV - DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH143Firewall · crackedSHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 6, FIGURE 205. THE AIRCRAFT WAS APPROVED FOSDR C2XA04SH140Buttstrap · corrodedSHV - DURING C-CHECK, THE L-BRACKET AFT OF THE CENTER BUTTSTRAP AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH138Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH137Stiffener · chafedSHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH135Firewall · crackedSHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH134Doubler · corrodedSHV- DURING C-CHECK THE RIGHT HAND FORWARD OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH133Crossbeam · corrodedSHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
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