N8501F

Service difficulty reports · 24

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 = 'N8501F' 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 REXA2013083001720Line · leakingDURING APPROACH, WHILE TRYING TO BRING GEAR DOWN, RECEIVED A MASTER WARNING GEAR DISAGREE. NOSE WHEEL DOOR WAS OPEN BUT GEAR DID NOT COME DOWN. WARNING SOUNDED WITHIN 5 SECONDS OF GEAR HANDLE DOWN. HAD AMBER DASHES FOR NOSE WHEEL, FOLLOWED QRH ON 2ND ATT. Aug 30, 2013 · N8501F · Cndair CL6002B19 · Hydraulic System, MainSDR REXA2013071601371Container · damagedCAPTAIN AND F/O LIFE VEST HAS HOLE IN BAGS. R & R CAPTAIN AND F/O LIFE VEST IAW AMM 25-61-03.Jul 16, 2013 · N8501F · Cndair CL6002B19 · Life JacketSDR REXA2013061701192Mount · crackedCRASH AXE HOLDER THAT MOUNTS TO COCKPIT PANEL 222LRW IS CRACKED. R & R WITH SERVICEABLE CRASH AXE HOLDER IAW SRM 51-41-02.Jun 17, 2013 · N8501F · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2012121001758Proximity Sensor · out of adjustGEAR DISAGREE AND NOSE DOOR WARNING ON ED1 WITH BOTH MAIN GEAR UP INDICATIONS AND NOSE WHEEL DOWN INDICATION WITH GEAR HANDLE IN UP POSITION. ADJUSTED PROXIMITY SENSOR PS14GA IAW 32-61-05 OPS CHECK OF MAIN LANDING GEAR EXTENSION AND RETRACTION IAW 32-32-00 OPDec 10, 2012 · N8501F · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2012081201257Battery · inoperativeFLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECKED GOOD.Aug 12, 2012 · N8501F · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012072001176Trim System · malfunctionedAILERON TRIM MOVES POSITION IN FLIGHT UN-COMMANDED. CANNOT DUPLICATE DISCREPANCY. PERFORMED OPS CHECK IAW AMM 27-12-00. OPS CHECKED NORMAL AT THIS TIME.Jul 20, 2012 · N8501F · Cndair CL6002B19 · Aileron Tab Control SystemSDR REXA2012071801169Unknown · unknownAILERON TRIM DOESN'T APPEAR TO BE WORKING. TRIM IS HARD TO CENTER. FULL DEFLECTION ON TRIM DOESN'T MOVE YOKES OR CONTROL SURFACES. PERFORMED OPERATIONAL TEST OF AILERON TRIM SYSTEM IAW AMM 27-11-00. ALL CHECKED GOOD.Jul 18, 2012 · N8501F · Cndair CL6002B19 · Aileron Control SystemSDR REXA2012043000590Selector Valve · faultyON CLIMBOUT GEAR SELECTED UP RECEIVED ANTI-SKID MSG, THEN RECEIVED GEAR DISAGREE MSG AND PARKING BRAKE SOV MSG. C/W PA 05-018F, REMOVED AND REPLACED MLG SELECTOR VALVE OPC GOOD CLEARS DM AND RETURN TO SVC. GEAR SWING PERFORMED, OPS CHECKS GOOD.Apr 30, 2012 · N8501F · Cndair CL6002B19 · Landing Gear SelectorSDR REXA2012032300368Vane · chafedLEFT AND RIGHT INBOARD FLAP VANE LEADING EDGES CHAFED. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2012032300367Bulkhead · crackedFS 280 BULKHEAD CRACKED AND CORRODED BETWEEN LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012032200036Floorbeam · corrodedLBL 27 FLOORBEAM CAP HAS CORROSION AROUND NUT PLATE HOLES FROM FS 574 TO FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012032100365Floorbeam · corrodedLBL 9 FLOORBEAM CAP HAS CORROSION AROUND NUT PLATE HOLES FROM FS 589 TO FS 605. REPAIRED IAW BOMBARDIER REO 601R-53-00-005.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012032100364Structure · corrodedACCESS OPENING FOR PANEL 640AT, 640BT, 640CT HAVE CORROSION. BLENDED 0.003" DEEP IAW SRM 57-21-32.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA2012032100362Bulkhead · gougedFS 621 PRESSURE BULKHEAD WEB GOUGED IN 6 AREAS ABOVE WL 73.5. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012031900259Floor Support · corrodedTHE FLOOR SUPPORT BEAM AT FS 349 TO BE CORRODED ON THE UPPER FLANGE AROUND A NUT PLATE LOCATED BETWEEN LBL 27 AND LBL 36. REPAIRED IAW EA CRJ253-00421B AND ASSOCIATED 8110-3.Mar 19, 2012 · N8501F · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201200110Strut · lowGEAR DISAGREE IN FLIGHT NOSE GEAR DOWN MAINS RETRACTED. SERVICED NLG STRUT WITH OIL AND NITROGEN IAW AMM 12-12-32 ALSO ADJUSTED NOSE LANDING GEAR CENTERED EXTENDED PROX SENSOR IAW AMM 32-61-05 ALL CHECKS GOOD. JACKED AND SWING GEAR IAW AMM 07-11-00 AND 32-30Jan 13, 2012 · N8501F · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR REXA201100788Warning System · activatedA CARGO OVERHEAT CAUTION MESSAGE WITH LIVE CARGO IN THE HOLD MESSAGE WAS DEFERRED PER MEL 21-55-05. PLACARD INSTALLED.Oct 29, 2011 · N8501F · Cndair CL6002B19 · Heating SystemSDR REXA201100690Battery · dischargedCAPT'S, F/O'S, F/A'S EMERGENCY FLASHLIGHT FAILS "RED" LED TEST. REMOVED AND REPLACED CAPT'S, F/O'S, F/A'S EMERGENCY FLASHLIGHT BATTERIES, OPS CHECK GOOD IAW AMM 25-60-00. VERIFIED PARTS EFFECTIVITY.Oct 8, 2011 · N8501F · Cndair CL6002B19 · Emergency EquipmentSDR REXA201100596Reservoir · faultyGEAR DISAGREE MASTER WARNING ON APPROACH. QRH EP12-4 COMPLETED. GEAR CAME DOWN PRIOR TO USING EMERGENCY RELEASE. REMOVED AND REPLACED NR 3 HYD SYSTEM RESERVOIR IAW AMM 29-12-30. OPS CHECK/LEAK CHECK GOOD. SEE AML 707543 ITEM 2 FOR PA 05-018B COMPLIANCE.Sep 23, 2011 · N8501F · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR REXA201100207Downlock Sensor · out of adjustAIR RETURN FOR GEAR DISAGREE. ADJUSTED NR1 AND NR 2 RT DOWNLOCK SENSORS, PERFORMED GEAR SWINGS IAW AMM 32-30-00.Mar 29, 2011 · N8501F · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201000006Seal · blownGEAR DISAGREE ON TAKEOFF. MTX C/W PA 05-018. NOSE STRUT SEALS WERE BLOWN AND GEAR WOULD NOT EXTEND FULLY. REPACKED AND SERVICED STRUT IAW AMM 32 -21-20.Jan 12, 2010 · N8501F · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR REXA200900131Angle · crackedTWO INCH CRACK FOUND WITH EDDY CURRENT AT SEMI PRESSURE BULKHEAD FRAME CAP-ANGLE BEND RADIUS AT FS 559 TO BL 18.00 DURING 16 K INSPECTION.Dec 10, 2009 · N8501F · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REX2009F00026Smoke Detector · faultyON CLIMB-OUT, RECEIVED CARGO SMOKE WARNING MESSAGE. QRH FOLLOWED WITH UNEVENTFUL LANDING, NO ACTUAL SMOKE OR FIRE. TROUBLESHOT IAW FIM AND AMM FOUND NR1 SMOKE DETECTOR BAD, REMOVED AND REPLACED DETECTOR. OPS CHECK GOOD. (K)Jan 29, 2009 · N8501F · Cndair CL6002B19 · Smoke DetectionSDR REXA200600071Flap · malfunctionedFLAPS FAIL AT SELECTED 8 DEGREES DURING TAXI. RETURNED TO GATE. PERFORMED OPERATION CHECK IAW AIRCRAFT MAINTENANCE MANUAL 27-51-00. MONITOPRING FLAPS PER AD 98-20-01 FOR 72 HRS.Jun 25, 2006 · N8501F · Cndair CL6002B19 · Trailing Edge Flap Control System
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