N8960A

Service difficulty reports · 71

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 = 'N8960A' 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 REXA2012031100359Engine · malfunctionedSMOKE TOILET CAUTION MSG AFTER TAKEOFF AIR RETURNED, NO SMOKE IN CABIN OR LAV ALL INDICATIONS NORMAL. CHANGED THE ENGINE.Mar 11, 2012 · N8960A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA2012022700289A/C Pack · inoperativeSMOKE TOILET CAUTION ON CLIMB, BURNT RAG SMELL IN COCKPIT, NEGATIVE DE ICE PRIOR TO T/O, TOILET ALARM GOING OFF AS WELL, PAX REPORTED BURNT CHEMICAL SMELL. C/W SMOKE/FUMES IN CABIN WORKSCOPE. FOUND RT PACK INOP AND DEFERRED. DEFERRED IAW MEL 21-51-01.Feb 27, 2012 · N8960A · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA2012022700253Structure · dentedDENT REPORTED BETWEEN FS 682 AND FS 700 AND S-21L AND S-22L MEASURING 4.625 X 2.125 X 0.105 DEEP. REPAIRED IAW EA CRJ253-00390A AND CORRESPONDING 8110-3.Feb 27, 2012 · N8960A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2012021200232Connector · damagedUNSCHEDULED LANDING FOR IDG NR 2 CAUTION IN-FLIGHT. REPINNED RT IDG OIL TEMP BULB CONNECTOR AND RECONNECTED IDG. OPS CHECKED IAW AMM 24-13-05. NO DEFECTS NOTED. REPINNED TEMP BULB CONNECTOR IAW ESPM 20. READY FOR SERVICE.Feb 12, 2012 · N8960A · Cndair CL6002B19 · Electrical Power System WiringSDR REXA201200148Coalescer Bag · dirtyAIR RETURN FOR SMOKE IN TOILET. REPLACED COALESCER BAGS IAW TCM 21-310-003 AND PERFORMED ENGINE RUNS IAW AMM 71-00-00. OP/C CHECK GOOD. NO SMOKE OR SMELL NOTED.Jan 25, 2012 · N8960A · Cndair CL6002B19 · Humidity Control SystemSDR REXA201200092Cable · defectiveMAIN CABIN DOOR VERY DIFFICULT TO CLOSE. REMOVED AND REPLACED PAX DOOR ICE BREAKER CABLE IAW AMM 52-11-15. PAX DOOR OPS CHECKS NORMAL.Jan 3, 2012 · N8960A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201200027Coalescer Bag · dirtyAIR RETURN. EMERGENCY DECLARED. ON DEPARTURE EN COUNTERED STRONG SMELL LIKE SMOKE, SHORTLY THEREAFTER THE SMOKE TOTLET MASTER CAUTION APPEARED. THE MESSAGE DISSAPPEARED ON FINAL WHEN THE THRUST WAS BROUGHT BELOW APPROXIMATELY 60%. COMPLIED WITH MINIMUM WORJan 1, 2012 · N8960A · Cndair CL6002B19 · Humidity Control SystemSDR REXA2012000156Skin · chafedRIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 60.005, WS 98.509, AND WS 137.012. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2012000155Skin · chafedRIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT CHAFED AT WS 47.61 - WS 66.2. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201200154Skin · chafedRIGHT WING LOWER PLANK FUEL ACCESS DOOR CUTOUT CHAFED AT WS 294.5 - WS 314.5. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2012000153Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 56.30, WS 104.099, AND WS 139.924. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2011123001033Skin · chafedRIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT WS 60.005, 98.509, 137.012. REPAIRED IAW REO 601R-57-52-004.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201101032Skin · chafedRIGHT WING LOWER PLANK FUEL TANK ACCESS PANEL DOOR CUTOUT CHAFED AT WS 294.5 TO WS 314.5. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 30, 2011 · N8960A · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100800Wire · shortedANTI ICE DUCT WARNING IN FLIGHT LEFT WING CAME ON WITH NO WING ICE ON. T/S SYSTEM FOUND WIRE STUD AT 1GSWK SHORTED. REPAIRED WIRE, SYSTEM OPC GOOD IAW CRJ 200 AMM 36-21-00.Nov 2, 2011 · N8960A · Cndair CL6002B19 · Pneumatic System WiringSDR REXA201100700Fuel Control · misriggedLT ENG SHUT DOWN / FLAME OUT ONCE THE TRUST REVERSER WAS STOWED AFTER LANDING. CREW DID NOT DELCARE AN EMERGENCY. RIGGED LT MFC IAW CRJ AMM 73-21-01, PERFORMED ENGINE POWER RUNS OF LT ENG AT RUN PAD IAW AMM 71-00-00. OP CHECK NORMAL. OK FOR SERVICE.Oct 10, 2011 · N8960A · Cndair CL6002B19 · Fuel Controlling SystemSDR REXA201100639Warning System · activatedAIRCRAFT DIVERTED INTO TYS FOR APU OIL TEMP CAUTION AIRCRAFT DIVERTED INTO TYS AND MAINT IS IN THE PROCESS OF T/SHOOTING TO REPAIR AS REQUIRED.Sep 28, 2011 · N8960A · Cndair CL6002B19 · APU Indicating SystemSDR REXA201100187Warning System · activatedGEAR DISAGREE DURING EXTENSION WHILE INBOUND TO JFK. FLIGHT LANDED WITHOUT INCIDENT.Mar 14, 2011 · N8960A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201100139Safety Switch · out of rigAIR RETURN FOR NOSE GEAR DISAGREE ON A/C 8960 SWAPPED INTO 8797 SWUNG NOSE GEAR AND WERE ABLE TO DUPLICATE DISCREPANCY. WHILE JACKED, CHECKED THE RIG ON THE NR 1 NLG WOW SWITCH AND FOUND IT TO BE .094 INCH. PROPER RIG IS .045 - .055 INCH. SYSTEM OP'S CHECKEFeb 22, 2011 · N8960A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201000031Landing Gear · malfunctionedON TAKEOFF FROM 36L FROM MEM THE RIGHT MAIN GEAR WOULD NOT RETRACT CAUSING A GEAR DISAGREE WARNING MESSAGE. THE QRH WAS COMPLETED AND ATTEMPTED TO CONTACT DISPATCH ON 131.22, WITH NO SUCCESS. THE ACRS WAS DEFERRED. AFTER SEVERAL ATTEMPTS CONTACTED OPERATIONMar 5, 2010 · N8960A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA200600090Smoke Detector · malfunctionedRECEIVED A FALSE LAVATORY SMOKE WARNING AFTER TAKEOFF. REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR IAW BOMBARDIER AMM.Oct 6, 2006 · N8960A · Cndair CL6002B19 · Smoke DetectionSDR REXA200600063Flap · malfunctionedFLAPS FAILED AT 20 ON TAXI OUT, QRH FOLLOWED RETURN TO BLOCKS. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.Jun 10, 2006 · N8960A · Cndair CL6002B19 · Trailing Edge Flap Control System
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