N8577D
Service difficulty reports · 36
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 = 'N8577D' 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 = 'N8577D' 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 REXA2014012300130Smoke Goggles · crackedFIRST OFFICER`S SMOKE GOGGLES GLASS CRACKED. R & R SMOKE GOGGLES IAW AMM 35-11-12.SDR REXA2014011400118Life Vest · tornONE INFANT LIFE VEST BAG IS TORN. R & R ONE INFANT LIFE VEST IAW PA 25-096A.SDR REXA2013112602279Torque Link · damagedRECEIVED NOSE WHEEL DOOR & GEAR DISAGREE MESSAGES AFTER TAKEOFF. PERFORMED QRH, RETURNED TO ROC. ACFT SHOOK VIOLENTLY ON LANDING ROLLOUT. BOTH WHEELS SHOW SIGNS OF SKID DAMAGE, TORQUE LINK IS DAMAGED. ACFT HAD TO BE TOWED TO THE GATE, ALSO HAD WOW INPUT OUSDR REXA2013091601737Seal · tornFWD PBE SMOKE HOOD SEAL TORN. REPLACED FWD SMOKE HOOD (PBE) IAW AMM 25-60-00.SDR REXA2013061301181Control Unit · failedFLAPS FAILED. IAW MOTR, PERFORMED TROUBLESHOOTING IAW FIM REV. 44 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), R & R FECU IAW AMM 27-51-05. OP CHECKED GOOD, OK FOR SERVICE.SDR REXA2013053101053Connector · looseLEFT JET OVERHEAT FAIL CAUTION MSG INTERMITTENT IN FLIGHT. UNABLE TO DUPLICATE ON GROUND. INSPECTED WIRING ON LT ENG. RESECURED LOOSE CONNECTION AT SENSING ELEMENT TERMINALS (LOOP B). OPS CHECK GOOD IAW MM 26-11-00. QRH COMPLETE.SDR REXA2013042900646Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE 550EB AT WS 253.022 CORRODED. REPAIRED IAW BOMBARDIER REO 601R-57-21-1913 AND 601R-57-21-030.SDR REXA2013042900645Floorbeam · corrodedFLOORBEAM CORRODED AT LBL 27 FROM FS 621 TO FS 574. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.SDR REXA2013042900643Skin · corrodedLEFT LOWER WING PLANK ACCESS HOLES FOR 550CB AND 550FB CORRODED AT WS 209.04 AND WS 274.319. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR REXA2013042500642Intercostal · corrodedFS 348 FRAME INTERCOSTAL UPPER FLANGE CORRODED. MATERIAL LOSS AFTER BLENDOUT IS .034". REPAIRED IAW EA CRJ253-01529 AND ASSOCIATED 8110-3.SDR REXA2013042200640Fitting · crackedCLIPS AT FS 484 RBL 27 AND RBL 36 ARE CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.SDR REXA2013042100639Structure · corrodedFS 280 FWD AND AFT FLANGES CORRODED AND CRACKED AT LBL 9 AND RBL 9 INBOARD AND OUTBOARD CLIPS. REPAIRED IAW BOMBARDIER REO 601R-53-11-926.SDR REXA2013030400434Smoke Detector · false activationON FLIGHT 4329 (PLN TO DTW) RECEIVED SMOKE TOILET CAUTION ON FINAL. NO SMOKE OR FUMES WERE REPORTED BY THE CREW. THE INDICATION POSTED FOR APPROX 30 SECONDS BEFORE INDICATIONS WENT BACK TO NORMAL. PERFORMEND QRH. FLIGHT ATTENDANT DID NOT SEE OR SMELL ANY SSDR REXA2013030200433Coalescer Bag · dirtyON FLIGHT 3778 (DSM TO DTW) RECEIVED SMOKE TOILET CAUTION MESSAGE INFLIGHT. COMPLIED WITH WORKSCOPE FOR SMOKE TOLIET. FOUND WATER SEPARATORS COALESCER SOCKS WITH SMELL OF OIL. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR COALESCER SOCKS IAW CMM 21-51SDR REXA2013020400273Switch · stuckON FLIGHT 3718 (RIC TO DTW) CREW RECEIVED TOILET SMOKE MESSAGE ON FINAL WITH NO SMOKE OR FUMES OBSERVED. FOUND SWITCH FOR TEST STUCK IN, UNSTUCK SWITCH. OPS CHECKS GOOD. REPEATED OPS CHECK (10 CYCLES) COULD NOT DUPLICATE DISCREPANCY NOR GENERATE ANY OTHER. SDR REXA2012080501225Unknown · vaporFOG COMING OUT OF COCKPIT VENTS. PERFORMED OPS CHECK OF PACK IN ALL RANGES. NO DEFECTS OR FOG NOTED AT THIS TIME PER AMM 21-51-00.SDR REXA2012062501016Power Lever · dirtyRIGHT THRUST LEVEL HAS SIGNIFICANT RESISTANCE WHEN APPLYING POWER OR REDUCING IT. CLEANED DUST FROM THROTTLE QUADRANT AND OPS CHECKED GOOD IAW AMM 76-10-00. AIRCRAFT OK FOR SERVICE.SDR REXA2012062600864Skin · puncturedMAINTENANCE FOUND THE FUSELAGE SKIN BETWEEN FS 654.5 AND 672.2 AND BETWEEN STRINGERS 26 AND 27 RT TO BE PUNCTURED, MEASURING 1.4 INCH BY 0.95 INCH. REPAIRED IAW PINNACLE EA CRJ253-00618 AND ASSOCIATED 8110-3.SDR REXA2012051300706Cover · damagedSERVICE DOOR EMERGENCY EXIT SIGN COVER DAMAGED AT SCREW HOLE. R&R SERVICE DOOR EMERGENCY EXIT LIGHT SIGN IAW AMM 33-51-10 OPS CHECK SATISFACTORY THIS CLEARS DM X63544.SDR REXA2012031000349Selector Valve · malfunctionedAIR RETURN FOR NOSE DOOR OPEN WARNING MSG AT 400 FT ON TAKEOFF. REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM 32-33-10, LEAK CHECK GOOD.SDR REXA2012030200322Coalescer Bag · dirtyHIGH ENERGY ABORT AT ABOUT 110 KIAS DUE TO BLUE SMOKE IN COCKPIT, SMELLED LIKE BURNT PLASTIC OR RUBBER, AT TIME OF THE SMOKE APU WAS ON AND 10TH STAGE BLEEDS ON APU. C/W WORKSCOPE FOR SMOKE/FUMES IN CABIN/FLIGHT DECK. REMOVED AND REPLACED LT & RT COALESCER SSDR REXA2012022800282Adg · deployedABORTED T/O FOR ADG DEPLOYED ON TAKEOFF. INSPECTED ADG IAW CRJ200 AMM 05-51-19 AND SB ERPS10AG-24-3 REV 2, NO DEFECTS NOTED.SDR REXA201100954Warning System · false activationLT ENG OIL PRESSURE MASTER WARNING. PERFORMED OP/C OF LT ENG OIL PRESSURE IAW AMM 79-31-05-210-002. OP/C GOOD. NO DEFECTS NOTED.SDR REXA201100953Fastener · shearedWITH ONLY HYD NR 3 SYS ON ELEVATORS ARE SPLIT AND CONTROLS ARE HARD TO MOVE FORE AND AFT. LT ELEVATOR SYMBOL DOESN’T MOVE. REMOVED AND REPLACED LT NR 3 ELEVATOR PCU IAW CRJ AMM 27-33-01. OPS CHECKED BAD. FOUND LT NR 3 SYS JAM TOLERANT MECHANISM NOT TO BE BOSDR REXA201100546Post · damagedFS 409+128 VERT POST RBL 18 FAILS NDT WITH AN INDICATION IN I/B RADIUS (AFT) GREATER THEN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW BOMBARDIER REO 601R-53-41-889 AND SRM 51-42-06.SDR REXA201100545Post · damagedFS 409+128 VERT POST LBL 18 FAILS NDT WITH ON INDICATION IN BOTH I/B + O/B AFT RADIUS BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW BOMBARDIER REO 601R-53-41-889 AND SRM 51-42-06.SDR REXA201100525Panel · damagedLT KIDNEY PANEL HAS 1 DAMAGED SCREW HOLE. REPAIRED IAW BOMBARDIER REO 601R-53-11-162.SDR REXA201100297Warning System · false activationCREW REPORTED CARGO SMOKE MSG. MSG CLEARED, OP CHECKED IAW AMM 26-15-00, OK FOR SERVICE.SDR REXA201100256Smoke Detector · malfunctionedRBM FOR LAV SMOKE CAUTION. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-16-01 & COMPLETED WORKSCOPE PACKAGE.SDR REXA201100143Apu · shutdownAPU FAULT/AUTO SHUT DOWN ABORTED TAKEOFF ECU SHOWED AUTO SHUTDOWN "DOOR POS" TRANSFERRED TO DMI LOG IAW MEL 49-10-11. PLACARD INSTALLED.SDR REXA201000196Smoke Warning · false activationSMOKE TOILET -DELLARD EMERGENCY LANDED DTW. OPC LAV SMOKE DETECTION SYSTEM IAW AMM 26-16-00. OPC GOOD.SDR REXA200900103Reservoir · bypassingDEPARTED CAE EN ROUTE TO DTW. CLEARED TO FL 300, PASSING FL 240 EICAS CAUTION MESSAGE HYD 2 HI TEMP CHECKED SYSTEMS PAGE AND CONFIRMED HYD 2 HI TEMP IN EXCESS OF 135C. CONDITION CONFIRMED, QRH INITIATED. CONTACTED ATC, ADVISED OF SYSTEM PROBLEM AND COORDINASDR REX200900047Bulkhead Web · crackedFS 280.0, LBL 9.0, FLOOR SUPPORT STRUCTURE AND FS 280.0 BULKHEAD WEB CRACKED APPROX 3.50 INCHES LONG. PERFORMED A MAJOR REPAIR TO THE BULKHEAD WEB FS 280, LBL 20.75, RBL 20.75, REO 601R-53-11-926, REV B. (K)SDR REXA200900047Bulkhead · crackedFS 280.0 LBL 9.0 FLOOR SUPPORT STRUCTURE AND FS 280.0 BULKHEAD WEB CRACKED APPROXIMATELY 3.50 INCH LONG. PERFORMED A MAJOR REPAIR TO THE BULKHEAD WEB IAW REO 601R-53-11-926 REV B.SDR REXA200600017Flap · malfunctionedFLAPS FAIL DURING DESCENT, PERFORMED QRH DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.SDR REX2004F00002Engine · malfunctionedAT LEVEL CRUISE AT FL310 AND MACH .74, THE FIRST OFFICER NOTICED A FLUXUATION IN THE RT ENGINE OIL PRESSURE. WITHIN FIVE MINUTES THE FLUXUATION BEGAN TO INCREASE. THE CAPTAIN ALSO NOTICED AN ASSOCIATED INCREASE IN OIL TEMPERATURE. THE FLIGHT CREW PERFORMED
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