N8525B

Service difficulty reports · 39

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 = 'N8525B' 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.

SDR REXA2014051500450Sign · unsecureAISLE EMER EXIT SIGN FELL DOWN EN ROUTE. DEFERRED AISLE EMER EXIT SIGN IAW NEF C6 IAW MOC CONT 005170 MOC INITIAL SF ENTERED IN MM02.May 15, 2014 · N8525B · Cndair CL6002B19 · Emergency LightingSDR REXA2013122102317Skin · dentedDURING ROUTINE LINE MAINTENANCE, FOUND FUSELAGE SKIN BETWEEN FS 627 AND 645 JUST BELOW S14R DENTED. THE SKIN AND UNDERLYING SKIN SPLICE WERE REPAIRED IAW EA CRJ253-02187B.Dec 21, 2013 · N8525B · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2013072701384Container · tornCO-PILOT'S LIFE VEST BAG TORN. R & R CO-PILOT LIFE VEST IAW AMM 25-61-03.Jul 27, 2013 · N8525B · Cndair CL6002B19 · Life JacketSDR REXA2013060301041Smoke Goggles · brokenCAPTAIN SMOKE GOOGLES BROKEN. R & R CAPTAIN SMOKE GOGGLES IAW AMM 25-26-00. OK FOR SERVICE.Jun 3, 2013 · N8525B · Cndair CL6002B19 · Emergency EquipmentSDR REXA2013031900577Bracket · bentON FLIGHT 3680 (MSP TO CVG) THE AIRCRAFT PERFORMED AN AIR RETURN FOR NOSE GEAR NOT RETRACTING. THE CREW FOLLOWED THE QRH PROCEDURES AND LANDED. THE NOSE LANDING GEAR PROXIMITY SENSOR BRACKET WAS FOUND BENT. THE STRUT ALSO REQUIRES SERVICING. REMOVED AND REMar 19, 2013 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2013021300292Life Vest · unserviceableOBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.Feb 13, 2013 · N8525B · Cndair CL6002B19 · Life JacketSDR REXA2013020200214Life Vest · unserviceableFLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.Feb 2, 2013 · N8525B · Cndair CL6002B19 · Life JacketSDR REXA2013020200213Life Vest · unserviceableINFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IN ACCORDANCE WITH PA 25-096A.Feb 2, 2013 · N8525B · Cndair CL6002B19 · Life JacketSDR REXA2013012300188Warning System · false activationON FLIGHT 4142 (ORF TO JRK) ON EARLY CLIMBOUT FROM ORF <1000 FT CATUION MESSAGES HYD 3(B) HYD 3 LOW PRESS FOLLOWED BY WARNING MESSAGES NOSE DOOR OPEN AND GEAR DISAGREE. THEN THEY ALL WENT AWAY IN LESS THAN A MINUTE EVERYTHING NORMAL ON LANDING. PERFORMED ISOJan 23, 2013 · N8525B · Cndair CL6002B19 · Hydraulic Indicating SystemSDR REXA2013011400146Pump · malfunctionedON FLIGHT 3583 (DTW TO LAN) AFTER TAKEOFF RETRACTED GEAR AND RECEIVED HYD 3 LO PRESS CAUTION AND GEAR DISAGREE MESSAGE. THE GEAR TOOK 45 SEC-1 MIN TO RETRACT WHICH TRIGGERED A GEAR DISAGREE WARNING HYD 3 QUANTITY AT 100%. NO EMERGENCY WAS DECLARED AND AIRCRAJan 14, 2013 · N8525B · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR REXA2012111001671Priority Valve · malfunctionedAFTER TAKEOFF ON FLIGHT 4089, FROM YOW TO DTW, WHEN GEAR LEVER MOVED TO UP POSITION WE RECEIVED FIRST A HYDRAULICS 3 LOW PRESS CAUTION. THEN RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING WITH BOTH MAIN GEAR INDICATING DISAGREE. AFTER 3-5 MINUTES ALL GENov 10, 2012 · N8525B · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2012070801049Control Unit · failedSTABILIZER STATUS MESSAGE POSTED AFTER TAKEOFF. ENGAGED AND SHORTLY AFTER STAB TRIM/MACH TRIM CAUTION MESSAGED POSTED. RESET PER QRH, 60 SECONDS LATER STAB/MACH TRIM POSTED AGAIN. ONLY STAB 2 WAS ABLE TO BE ENGAGED. REMOVED AND REPLACED HSTCU IAW AMM 27-41Jul 8, 2012 · N8525B · Cndair CL6002B19 · Stabilizer Control SystemSDR REXA2010627201027Line · damagedFLIGHT 4419. RECEIVED FUEL IMBALANCE MESSAGE AND DIVERTED. REMOVED AND REPLACED FUEL LINE. LEAK CHECKED GOOD FIM 28-40-00.Jun 27, 2012 · N8525B · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR REXA2012062601022Warning Light · illuminatedAFTER TAKEOFF HAD HYDRAULIC SYSTEM 3, LOW PRESSURE CAUTION FOLLOWED BY GEAR DISAGREE. CREW SELECTED GEAR BACK DOWN AND RECEIVED THREE GREEN AND DIVERTED.Jun 26, 2012 · N8525B · Cndair CL6002B19 · Hydraulic System, MainSDR REXA2012062500863Floorbeam · crackedFS 280 UPPER FLOORBEAM CAP ANGLE CRACKED AT LBL 9. REPAIRED IAW REO 601R-53-11-138.Jun 23, 2012 · N8525B · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012063000868Hinge · damagedHORIZONTAL STAB RT ELEVATOR HINGE CTR HINGE FITTING GOUGED 0.274 INCH BY 0.081 INCH BY 0.011 INCH DEEP. RT ELEVATOR OTBD HINGE FITTING GOUGE 0.361 INCH BY 0.060 INCH BY 0.012 INCH DEEP. LT ELEV CTR HINGE FITTING GOUGED 0.34 INCH BY 0.071 INCH BY 0.007 INCH Jun 20, 2012 · N8525B · Cndair CL6002B19 · Elevator StructureSDR REXA2012063000867Angle · crackedFS 280 INBOARD ANGLE CRACKED AT RBL9. REPLACED IAW SRM 51-42-21/51-42-06.Jun 20, 2012 · N8525B · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012070100871Stiffener · chafedFS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED 0.050 INCH DEEP BY 0.4 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523 AND 601R-53-61-4565.Jun 14, 2012 · N8525B · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012061600854Access Panel · corrodedWING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE CORROSION AT LEFT HOLE NR 14, 0.007 INCH, LEFT HOLE NR16, 0.003 INCH DEEP, RIGHT HOLE NR 16, 0.008 INCH. REPAIRED IAW REO 601R-57-21-030.Jun 13, 2012 · N8525B · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2012052300765Life Vest · damagedOBSERVERS LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.May 23, 2012 · N8525B · Cndair CL6002B19 · Life JacketSDR REXA2012021200227Flap · malfunctionedFLAPS FAILED IN-FLIGHT AT 30 DEGREES QRH COMPLETED. C/W PA AD 27-052 G FOUND CODES 1-30-BC & 1-31-BC WHICH POINTS TO FLAP CONTROL LEVEL, PERFORMED FLAP TEST OF CONTROL LEVER IAW FIM 27-50-00. ALL SYSTEMS PASSED TEST. A/C OK FOR SERVICE AT THIS TIME.Feb 12, 2012 · N8525B · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA2012020500186Coalescer Bag · dirtyAIR RETURN FOR SMOKE IN TOILET. BOTH COALESCER SOCKS SMELL OILY. REMOVED AND REPLACED LT AND RT COALESCER SOCKS IAW AMM 21-51-13.Feb 5, 2012 · N8525B · Cndair CL6002B19 · Humidity Control SystemSDR REXA201200174Warning System · activatedPERFORM GEAR DISAGREE EVENT PROCEDURES PER PA 05-018B. COMPLIED WITH PA05-018B GEAR DISAGREE EVENT PROCEDURES. OPS CHECK GOOD.Jan 31, 2012 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201200128Pitot Tube · obstructedHIGH SPEED ABORT DUE TO EFIS/COMPMON/ AIRSPEED AT 120KTS ALSO DURING ABORT A CINFIG SPOILERS WARN. C/W PITOT/ STATIC TEST IAW CRJ200 AMM 34-11-00. OPS CKD GOOD. A/C SAFE FOR FLIGHT. FOUND BUG IN PITOT TUBE.Jan 17, 2012 · N8525B · Cndair CL6002B19 · Pitot/Static SystemSDR REXA201100897Hydraulic Line · chafedLOST HYDRAULIC PSI IN SYSTEM NR 3 AND DIVERTED TO TYS. EMERGENCY WAS DECLARED. FOUND HYD SYSTEM 3B PRESSURE LINE CHAFED THROUGH FAIRLEAD IN MLG BY AREA. REPAIRED LINE IAW AMM 20-22-00. LEAK CHECK GOOD. VERIFIED PART EFFECTIVITY. REMOVED AND REPLACED 3A &Dec 1, 2011 · N8525B · Cndair CL6002B19 · Hydraulic System, MainSDR REXA201100761Ecu · defectiveON LANDING ON BLEED TRANSFER TO APU, APU OVERTEMP WARNING. TROUBLESHOT PER FIM 49-10-00 FOUND ECU BAD. REMOVED AND REPLACED ECU IAW AMM 49-61-01, OP/C GOOD. VERIFIED PART EFFECTIVITY.Oct 20, 2011 · N8525B · Cndair CL6002B19 · APU ControlsSDR REXA201100567Sensing Element · groundedL 14TH DUCT FOUND HEAT SENSING ELEMENT AT CONNECTOR A47WK TO BE GROUNDING ON AIRFRAME. REROUTED, RESECURED ELEMENT AND OPS CHECKED IAW AMM 36-21-00. NO DEFECTS NOTED. OK FOR SERVICE. EMERGENCY WAS DECLARED.Sep 18, 2011 · N8525B · Cndair CL6002B19 · Pneumatic Indicating SystemSDR REXA201100477Windshield · crackedF/O'S WINDSHIELD SHATTERED INFLIGHT. REMOVED AND REPLACED F/O'S WINDSHIELD.Jul 26, 2011 · N8525B · Cndair CL6002B19 · Flight Compartment WindowsSDR REXA201100237Warning System · activatedCREW DECLARED AN EMERGENCY INTO YUL DUE TO ANTI-SKID OUTBOARD CAUTION DEFERRED IAW MEL 32-44-01 AUTH 42551.Apr 21, 2011 · N8525B · Cndair CL6002B19 · Brake Anti-Skid SectionSDR REXA201100057Bulkhead · crackedCRACK FOUND IN FS 559.00 PRESSURE BULKHEAD WEB. REPAIRED FS 559.00 BULKHEAD WEB LAW BOMBARDIER REO 601 R-53-41-260 REV E AND BOMBARDIER REO 601 R-53-41-609 REV B, DEVIATION "E".Jan 19, 2011 · N8525B · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100056Plate · corrodedPASSENGER DOOR COUNTERBALANCE FORWARD AND AFT FITTING PLATES, P/N 600-38061-6 AND 600-38061-11, CORRODED. REMOVED AND REPLACED WITH SERVICEABLE PLATES P/N 600-38061-6 AND 600-38061-11 ON PAX DOOR FITTINGS IAW CRJ 200 AMM 20-21-00-910-801.Jan 19, 2011 · N8525B · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201000126Skin · puncturedUPON FUELING CENTER TANK, LEAK WAS FOUND FROM PUNCTURE IN LOWER WING SKIN BETWEEN FS 409+112 AND FS 409+128, WING STRINGER 25L AND 26L, LBL 7.2. PUNCTURE MEASURED 1.809 X 0.25 INCH. REPAIRED IAW REO 601R-57-11-047.Sep 2, 2010 · N8525B · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201000003Proximity Switch · out of adjustAFTER TAKEOFF FROM DTW THE NOSE GEAR WOULD NOT RETRACT. PILOTS COORDINATED A LOW PASS "TOWER FLY BY" FOR ADDITIONAL VISUAL VERIFICATION OF THE LANDING GEAR. AN UNEVENTFUL LANDING BACK IN DTW AFTER 1 HOUR OF BURNING FUEL. LANDING BACK IN DTW WAS UNEVENTFUL, Jan 7, 2010 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA200900141Strut · lowGEAR DISAGREE ON T/O MAINS UP NOSE DOWN WOW INPUT CAUTION WOW OUT PUT STATUS MSG. MTX SERVICED THE NOSE STRUT WITH OIL AND NITROGEN IAW AMM 12-12-32 AND PERFORMED GEARS WING IAW AMM 32-30-00 AND C/W PA 05-01 8A, ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURDec 24, 2009 · N8525B · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR REX2008F00057Rvdt · malfunctionedON CLIMB OUT GOING THROUGH FL270 RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MASTER CAUTION. QRH FOLLOWED WITH NO FIX. WAS SCHEDULED FOR MEM ASKED FOR LONGEST RUNWAY. LANDING WAS UNEVENTFUL. TOWED TO GATE. R&R THE NOSE WHEEL STEERING RT STEERING RVOct 28, 2008 · N8525B · Cndair CL6002B19 · Landing Gear Steering SystemSDR REXA200600054Seal · deterioratedON FINAL APPROACH INTO DTW THE ORAL WARNING -ENGINE OIL- WENT OFF FOLLOWED BY THE ILLUMINATION OF THE -R ENGINE OIL PRESSURE- MESSAGE. WHEN THE FLIGHT CREW REDUCED THE RIGHT HAND THRUST LEVER TO IDLE, THE ENGINE FLAMED OUT. THE CAPTAIN DECLARED AN EMERGENCY Apr 25, 2006 · N8525B · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REX2005F00000Proximity Switch · loose(REF NR: 05-092) GEAR DISAGREE WARNING AFTER TAKEOFF, DURING GEAR RETRACTION. RT MAIN SHOWS IN TRANSIT. FOLLOWED QRH WITH UNEVENTFUL LANDING. INTERROGATED PSEU, FOUND TARGET FOR RT MLG UPLOCK PROXIMITY SWITCH LOOSE. TIGHTENED TARGET IAW AMM AND PERFORMED Jul 27, 2005 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00014Warning Light · illuminated(REF NR: 05-088) GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF, DURING GEAR RETRACTION, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/ RETRACTION. OPS CHECK GOOD, OK FOR SERVICE. (K)Jul 16, 2005 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA04002Odor · detectedAPU AUTO SHUTDOWN DURING CLIMB-OUT. PILOT ATTEMPTED TO RESTART APU. THIS START ATTEMPT RESULTED IN A STRONG FUEL SMELL IN THE CABIN AND COCKPIT. CREW REQUESTED AND WAS GRANTED PERMISSION TO RETURN TO DAYTON. AN OTHERWISE UNEVENTFUL LANDING WAS PERFRMED AT Jan 19, 2004 · N8525B · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
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