N91SK, cancelled May 30, 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 = 'N91SK' AND deregistration_id = 'N91SK-2008-05-30'
  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 S2YA07007Angle · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE TO WING ANGLE P/N 114-43002-180 AND THE DOUBLER INSTALLED IN AUGUST OF 2000. THE ANGLE HAD BEEN PREVIOUSLY REPAIRED, RECORDED AND SUBMITTED ON A 337 DATED 08/15/00. THSep 8, 2007 · N91SK · Beech 1900D · Fuselage Miscellaneous StructureSDR S2YA07006Angle · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE LT FUSELAGE TO WING ANGLE. THE ANGLE IS LOCATED NEAR FS 288 IN THE AREA OF STRINGER 10L AND 10R. THE ANGLE WAS CRACKED IN THE RADIUS AT THE FORWARD END: THE CRACK WAS NO GREATER THEN 1.80 Sep 8, 2007 · N91SK · Beech 1900D · Fuselage Main, StructureSDR S2YA07005Seat Track · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN A SEAT TRACK EXTRUSION. THE SEAT TRACK IS LOCATED AT FS 290.85 EXTENDING APPROXIMATELY 5 INCHES. THE DAMAGE CONSISTED OF A HALF-INCH CRACK IN THE LOWER VERTICAL FLANGE WHERE THE UPPER PORTION OSep 8, 2007 · N91SK · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR S2YA05061Wire · damagedDURING APPROACH, THE CREW REPORTED THEY WERE UNABLE TO EXTEND THE GEAR AND FOUND THE CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB ONLY TO HAVE IT POP WHEN SELECTING GEAR DOWN. THE CREW MANUALLY EXTENDED THE GEAR, ACHIEVED 3 GREEN AND PROCEEDED TO LAND Sep 25, 2005 · N91SK · Beech 1900D · Landing Gear System WiringSDR S2YA05048Wire · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE FOUND A CHAFED WIRE AT THE LT SAFETY SWITCH. MAINTENANCE REPAIRED THE WIRE, OPS CHECKED THEAug 15, 2005 · N91SK · Beech 1900D · Flight Control System WiringSDR S2YA05024Relay · malfunctionedAFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR TURNBACK. MECHANIC INSPECTED THE AC AND REPLACED THE LANDING GEAR RELAY AND THE POWER PACK MOTOR. (K)Mar 14, 2005 · N91SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA05023Valve · inoperativeDURING APPROACH, THE CREW REPORT THEY WHERE UNABLE TO EXTEND THE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND MECHANIC WAS UNABLE TO DUPLICATE THE PMar 10, 2005 · N91SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA04008Indicator · erraticDURING TAKEOFF ROLL, THE CREW NOTICED THE FO`S AIRSPEED INDICATOR WENT FROM INDICATING 0 KNOTS TO 55 KNOTS WHEN THE PILOT`S GAUGE INDICATED 75 KNOTS. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE FO`S AIRSPEED INMar 22, 2004 · N91SK · Beech 1900D · Airspeed/Mach IndicatorSDR S2YA02033Warning System · inoperativeAFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT GO A RED GEAR UNSAFE LIGHT. THE CREW CONSULTED WIGH MECHANIC AND CYCLED THE GEAR BUT STILL HAD AN RED IN TRANSIT LIGHT. THE CREW DID AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MECHANIC INSPECTED THE SYSTEM ANDAug 16, 2002 · N91SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA02005Relay · failedDURING FLIGHT 1027 - MKE-ATW - THE CREW NOTED THAT THE LEFT AC BUS FAILED FOLLOWED BY A LOUD HISSING AND CRACKLING NOISE FOLLOWED BY SEEING AND SMELLING A SMALL AMOUNT OF SMOKE. MAINTENANCE INSPECTED THE A/C AND FOUND THE ANNUNCIATOR RELAY SHORTED. MAINTENANFeb 20, 2002 · N91SK · Beech 1900D · AC Indicating SystemSDR S2YA02001Adi · failedFLT 1157 - MLI-MKE - THE CREW NOTED ELECTRICAL SMOKE IN THE COCKPIT AND EVACUATED THE A/C. OUTSTATION MAINTENANCE FOUND THE LEFT EADI HAD EMITTED THE SMOKE. MAINTENANCE DISCONNECTED THE EADI AND THE A/C WAS FERRIED TO MKE. MKE MAINTENANCE REPLACED THE IH EAJan 14, 2002 · N91SK · Beech 1900D · Integrated Flight SystemSDR S2YA01006Windshield · odorFLT 1426 - MKE-CMH - DURING CRUISE, THE FLIGHT CREW NOTICED A STRANGE ODOR IN THE COCKPIT. THE CREW MADE AN AIRTURN BACK AND LANDING AT MKE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE GROUND TERMINAL ON THE RIGHT WINDSHIELD BURNED. MAMar 23, 2001 · N91SK · Beech 1900D · Flight Compartment WindowsSDR S2YA01005Switch · out of adjFLT 1111 - MKE-CHM - DURING APPROACH, THE CREW SELECTED GEAR DOWN BUT DID ACHIEVE DOWN AND LOCKED ON THE NOSE GEAR. THE CREW FLEW BY THE TOWER TO VERIFY THE NOSE GEAR WAS DOWN. THE CREW THEN EMERGENCY HAND PUMPED THE GEAR DOWN BUT DID NOT ACHIEVE THREE GREENMar 11, 2001 · N91SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA00003Altimeter · failedFLT 1071 - EN ROUTE MKE-CWA - THE CAPTAINS ALTIMETER FLAGGED AND ALERTER WENT BLANK. AFTER TALKING WITH MAINTENANCE AND OPERATIONS THE DECISION WAS MADE TO RETURN TO MKE WHERE MAINTENANCE COULD WORK THE PROBLEM. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER. Feb 28, 2000 · N91SK · Beech 1900D · Altimeter, Barometric/EncoderSDR S2YA98010Engine · malfunctionedAFTER TAKEOFF OF FLT 1235 - MKE TO MQT, THE FLT CREW NOTICED THAT THERE WERE SPARKS COMING OUT OF THE RT ENGINE EXHAUST STACK. THE FLIGHT CREW DECIDED TO RETURN TO MKE SO MAINTENANCE COULD INSPECT THE ENGINE. AFTER AN UNEVENTFUL LANDING MAINTENANCE INSPECTEDMar 30, 1998 · N91SK · Beech 1900D · Engine (Turbine/Turboprop)SDR 97ZZZX1801Pressure Switch · inoperativeDURING THE MONTH OF JANUARY, SIX FUEL PRESSURE SWITCHES, P/N 100-389018-21 WERE REPLACED. THE TBR FOR THE SWITCHES WAS: 3,933.2 HRS FROM N NR 148SK; 1,418.2 HRS FROM N NR 831SK; 1,479.7 HRS FROM N NR 87SK; 2,525.6 HRS FROM N NR 881SK; 1,715.7 HRS FROM N NR 8Mar 25, 1997 · N91SK · Beech 1900D · Fuel Pressure IndicatorSDR S2YA97013Hydraulic Line · leakingRFD/DTW - FLT 1892 - CREW DID AIR TURNBACK DUE TO LANDING GEAR BEING FOUND EXTENDED AND LOCKED WHILE CLIMBING THROUGH FL 160. THE GEAR WAS EXTENDED WITH 3 GREEN, THEY VISUALLY CHECKED GEAR WAS DOWN. CFR CALLED OUT AND EMERGENCY LANDING PERFORMED WITHOUT INCFeb 26, 1997 · N91SK · Beech 1900D · Hydraulic System, MainSDR S2YA97004Seal · out of positionMKE/DSM - FLT 1751 - FLIGHT CREW PERFORMED AN AIR TURNBACK DUE TO THE CABIN DOOR SEAL SQUEALING VERY LOUDLY. THE DOOR SEAL HAD BEEN CHANGED BY MAINTENANCE PRIOR TO DEPARTURE. WHEN THE AIRCRAFT LANDED, MAINTENANCE INSPECTED THE DOOR SEAL AND FOUND A SMALL PORFeb 16, 1997 · N91SK · Beech 1900D · Passenger/Crew DoorsSDR 97ZZZX1790Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM ACFT 118SK; 6,526.6 HRS FROM N NR 831SK; 6,Nov 1, 1996 · N91SK · Beech 1900D · Attitude and Direction Data SystemSDR S2YA950027Cam · brokeDURING A POST-FLIGHT INSPECTION, FLIGHT CREW NOTICED THE OUTBOARD GEAR DOOR ACTUATING CAM HAD THE UPPER TANG BROKEN OFF. MAINTENANCE REPLACED THE CAM ASSY AND OPERATIONAL CHECKED GOOD. THE TANG THAT BROKE HAD SIGNS OF A PREVIOUS BREAK. (X)Oct 10, 1995 · N91SK · Beech 1900D · Landing Gear Door Retract SectionSDR S2YA950006Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 69.00 TO HAVE A CRACK 1.5 INCHES LONG ON THE TOP PORTION NEXT TO THE LOWER MOUNT HOLE OF THE MANUAL HYDRAULIC RESERVOIR BLEED VALVE, PN 114-388012-1. A REPAIR WAS MADE PER THE BEECH SRM.May 15, 1995 · N91SK · Beech 1900D · Wing, Rib/BulkheadSDR S2YA950005Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 83.00 TO HAVE CRACKED ON THE BOTTOM PORTION BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS. THE CRACKS WERE APPROXIMATELY 3 INCHES AND 1 INCH LONG EXTENDING FROM THE CENTER OF THE RIB REIMay 15, 1995 · N91SK · Beech 1900D · Wing, Rib/BulkheadSDR S2YA950002Ctr Bal Arm · crackedTHE CENTERBALANCE ARM WAS FOUND BENT. HAVE REPLACED 14 OF THE DASH 17 TYPES AND, SO FAR, 2 OF THE DASH 33 NEW DESIGNS BETWEEN 13 AIRCRAFT.May 3, 1995 · N91SK · Beech 1900D · Passenger/Crew Doors
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