N891SK, cancelled Jan 15, 2008

Service difficulty reports · 23

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 = 'N891SK' AND deregistration_id = 'N891SK-2008-01-15'
  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 S2Y2005F00000Pcb · shortedDURING APPROACH, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT DETECT PCBJul 22, 2005 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA05046Pcb · shortedDURING APPROACH OF FLIGHT, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT Jul 22, 2005 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA05044Pressure System · fluctuatesSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE OIL PRESSURE DROPPED TO ABOUT 40 PSI ACCOMPANIED BY A TEMPERATURE INCREASE TO 800 DEGREES AND TORQUE FLUCTUATIONS. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE AC AND REPLACED THE RT ENGINE. WITHJul 20, 2005 · N891SK · Beech 1900D · Engine Oil PressureSDR S2YA05036Uplock Switch · out of adjustON CLIMBOUT OF FLIGHT, THE CREW REPORT THE LANDING GEAR HANDLE LIGHT WAS FLICKERING WITH THE HANDLE IN THE UP POSITION. THE CREW PERFORMED AN AIR-TURN-BACK TO DEPARTURE AIRPORT. MECHANIC ADJUSTED THE LT MAIN UPLOCK SWITCH AND RETURNED THE AC TO SERVICE. (K)Jun 1, 2005 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR 2006FA0000149Structure · corrodedAIR STAIR DOOR LOWER CLOSURE, MFG FROM 4130 STEEL, WAS CORRODED THRU UNDER FOLDING STEP. THIS CLOSURE HAD BEEN PREVIOUSLY REPAIRED BY REMOVING CORROSION, TREATING AND A DOUBLER INSTALLED. REMOVED CLOSURE DUE TO CORROSION AND DISBOND FROM DOOR CORE MATERIAL.Feb 7, 2005 · N891SK · Beech 1900D · Fuselage Main, StructureSDR S2YA03002Valve · inoperativeSHORTLY AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR DID NOT RETRACT. THE CREW DID AN AIR-TURN-BACK AND HAD AN UNEVENTFUL LANDING. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE HYDRAULIC SERVICE VALVE. MECHANIC OPS CHECKED THE SYSTEM WITH NO FURTHJan 20, 2003 · N891SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA03001Compressor · stalledDURING FLIGHT 1044 MKE-GRB THE CREW REDUCED ENGINE TORQUE TO 2200 LBS. THE FIRST OFFICER OBSERVED FLAME COMING OUT OF FROM THE RIGHT ENGINE. THERE NO INSTRUMENT INDICATION OF ANY ENGINE PROBLEMS. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION, DECLAREDJan 12, 2003 · N891SK · Beech 1900D · Turbine Engine Compressor SectionSDR S2YA02016Switch · sticksFLT 1454 - DAY-MKE - DURING TAKEOFF, THE RIGHT AUTO FEATHER DISABLE ANNUNCIATOR ILLUMINATED. THE CREW ABORTED THE TAKEOFF. THE A/C WAS FERRIED BACK TO MKE. MAINTENANCE REPLACED THE AUTO FEATHER SWITCHES IN THE POWER LEVER, OPS CHECK GOOD. (M)Apr 29, 2002 · N891SK · Beech 1900D · Propeller Feathering/ReversingSDR S2YA00005Switch · out of rigFLT 1630 - MKE-CMH - SHORTLY AFTER TAKEOFF, THE CABIN DOOR ANNUNCIATE ILLUMINATED AND THE CREW MADE AN AIRTURN BACK TO MKE. AFTER AN UNEVENTFUL LANDING THE CREW CONSULTED WITH MX AND PUT THE ANNUNCIATOR ON MEL. MAINTENANCE CLEARED THE MEL 3/21/00 BY CLEANINGMar 18, 2000 · N891SK · Beech 1900D · Door Warning SystemSDR S2YA98019Cam · malfunctionedCMH/MKE - FLT 1829 - DURING TAKEOFF ROLL, CREW DETECTED SMELL OF SMOKE AND SAW SMOKE IN CABIN. ABORTED T/O, RETURNED TO GATE. MAINT INSPECTED ACFT, FOUND THE FLAP MOTOR DAMAGED FROM OVERHEATING. FLAP SYSTEM WAS PLACED ON MEL AND ACFT RETURNED TO SERVICE. MJul 5, 1998 · N891SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA98002Windshield · crackedMKE/CMH - WHILE CLIMBING THROUGH FL 120, THE CAPTAIN'S WINDSHIELD CRACKED. THE CREW NOTIFIED ATC, DECLARED AN EMERGENCY AND RETURNED TO MKE. AFTER MAKING A SAFE LANDING, MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED AIRCRAFT TO SERVICE. THE CRACK WAS FOJan 12, 1998 · N891SK · Beech 1900D · Flight Compartment WindowsSDR S2YA970031Rt Unit · failedFLT 1234 - MQT-MKE - DURING THE CLIMB-OUT, THE CREW TURNED ON THE RADAR AND FOUND IT TO BE INOPERATIVE. DECIDED TO RETURN TO MQT DUE TO BAD WEATHER EN ROUTE TO MKE. MADE AN UNEVENTFUL LANDING. ONCE ON THE GROUND, MAINTENANCE TROUBLESHOT THE SYSTEM. REPLACEOct 6, 1997 · N891SK · Beech 1900D · Weather Radar SystemSDR S2YA970026Fire Loop · failedMKE/FNT - FLT 1881 - ON TAKEOFF ROLL, FLIGHT CREW NOTICED LT ENGINE FIRE ANNUNCIATOR (T-HANDLE) ILLUMINATED. THE TAKEOFF ROLL WAS ABORTED AT 25 KNOTS, AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. WHEN THE AIRCRAFT WAS INSPECTED BY MAINTENANCE, THEJul 18, 1997 · N891SK · Beech 1900D · Fire DetectionSDR 97ZZZX1795Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N891SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR S2YA960028Switch · out of adjustFLT 1265 - AFTER TAKEOFF, THE CREW NOTICED THE GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED AND THE WARNING HORN SOUNDED CONTINUOUSLY WHEN LANDING GEAR HANDLE WAS RAISED TO THE RETRACT POSITION. MAINTENANCE ADJUSTED FLAP LIMIT SWITCH S4 AND ADJUSTED FLAP SYOct 21, 1996 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA960027Flap Motor · overheatedDURING RUNUP BEFORE FIRST FLIGHT OF THE DAY, THE CREW NOTICED SMOKE IN THE CABIN, MAINTENANCE FOUND THE FLAP MOTOR WINDINGS HAD OVERHEATED INTERNALLY. IT WAS REPLACED BUT THE FLAP SYSTEM WAS DEFERRED DUE TO RIGGING REQUIRED. (M)Oct 16, 1996 · N891SK · Beech 1900D · Trailing Edge Flap ActuatorSDR S2YA960016Ehsi · failedFLT NR 1203 - AFTER TAKEOFF, IT WAS NOTICED THAT THE RIGHT EHSI FAILED IN FLT AND THE CREW DECIDED TO TURN BACK TO MKE. MAINTENANCE REPAIRED WIRE NR J095002-J598013 AND OPERATIONAL CHECKED GOOD. (M)Jul 12, 1996 · N891SK · Beech 1900D · Integrated Flight SystemSDR S2YA960011Mic-Switch · stuckTHE CREW OF FLT 1906 MKE-SDF, FOUND THEY HAD A STUCK CAPTAINS MIC-SWITCH IN THE 'ON' POSITION. THEY DECIDED TO TURNBACK TO MKE AND HAVE MX LOOK AT IT. THEY DEFERRED THE SWITCH BY DISABLING IT PER MEL GUIDELINES. THE SWITCH WAS LATER REPLACED. (M)Jun 9, 1996 · N891SK · Beech 1900D · Audio Integrating SystemSDR S2YA960005Instr Air Valve · inoperativeMKE - FLT 1906 - AFTER FLIGHT CREW DEPARTED, THEY NOTICED THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED AND STAYED ON. THE RIGHT BLEED AIR FAIL ANNUNCIATOR WAS ALREADY DEFERRED SO THEY TURNED BACK TO MKE. MAINTENANCE COULD NOT DUPLICATE THE LEFT BLEED FAILMay 13, 1996 · N891SK · Beech 1900D · Pneumatic Distribution SystemSDR S2YA960004Duct · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND BLEED AIR DUCT, P/N 129-550051-1, CRACKED ALL AROUND THE BASE OF THE ACM OVERTEMPERATURE SENSOR WELD FITTING. THE PART WAS REPLACED. SUBMITTER STATES,WE HAVE NOW HAD THREE OCCURENCES ON DIFFERENT AIRCRAFT, SAMMar 29, 1996 · N891SK · Beech 1900D · Air Distribution SystemSDR S2YA950001Angle · crackedDURING AN INSPECTION, MAINTENANCE FOUND A 1.50 INCH CRACK ON THE ATTACH ANGLES OF BOTH THE LT AND RT VENTRAL FINS. THE LOCATION IS BELOW THE AFT PRESSURE BULKHEAD, FS 557.50 AND IS CAUSED BY THE LACK OF SHIMMING AT THE SKIN OVERLAP. THE CRACKS WERE REPAIRED.Apr 28, 1995 · N891SK · Beech 1900D · Ventral StructureSDR 95ZZZX2481Torque Tube · loose rivetsDISCOVERED LOOSE RIVETS ON LEFT ELEVATOR TORQUE TUBE DURING UNSCHEDULED MAINTENANCE ON TAIL. MAINTENANCE REMOVED AND REPLACED THE TORQUE TUBE ASSEMBLY.Apr 7, 1995 · N891SK · Beech 1900D · Elevator Control SystemSDR 95ZZZX2482Torque Tube · loose rivetsRIGHT ELEVATOR TORQUE TUBE ASSEMBLY FOUND TO HAVE LOOSE RIVETS AT THE ELEVATOR ATTACH BRACKET. THE PROBLEM WAS FOUND AT A DETAIL NR 6 AND THE RIVETS WERE REMOVED AND REPLACED.Feb 6, 1995 · N891SK · Beech 1900D · Elevator Control System
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