N881SK, cancelled Jul 1, 2010

Service difficulty reports · 17

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 = 'N881SK' AND deregistration_id = 'N881SK-2010-07-01'
  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 GLBA2008120501Handle · detachedSIG EVENT - UPON ARRIVAL IN DEN IT WAS REPORTED THAT THE EXTERIOR AIRSTAIR DOOR HANDLE DETACHED FROM THE DOOR. ACFT HAD FERRIED TO CYS FOR REPAIRS AND WAS SUBSEQUENTLY GROUNDED TO LEASING AGREEMENT ISSUES. MX RE-INSTALLED THE AIRSTAIR DOOR EXTERIOR HANDLE IADec 2, 2008 · N881SK · Beech 1900D · Passenger/Crew DoorsSDR GLB2008F00018Switch · out of adjustSUSPECTED AUTOFEATHER EVENT. DURING CRUISE, THE PILOTS REPORTED THAT THE LT AUTOFEATHER DISARMED IN FLIGHT AND NEVER REARMED AT ANY POWER SETTING. MAIT ADJUSTED THE LT POWER LEVER SWITCH. OPS CHECK OF THE AUTOFEATHER SYS GOOD IAW MM 61-20-00. (K)Aug 28, 2008 · N881SK · Beech 1900D · Propeller Feathering/ReversingSDR S2YA06006Blower · smokeDURING FLIGHT 1454, THE CREW SMELLED SMOKE IN THE COCKPIT. THE CREW CONTACTED ATC FOR A PRIORITY DECENT BUT DID NOT DECLARED AN EMERGENCY. THE CREW FLEW THE AC BACK WITH NO FURTHER INCIDENT. MX FOUND THE FORWARD CABIN BLOWER HAD A TERMINAL END BROKEN OFF.Sep 5, 2006 · N881SK · Beech 1900D · Air Distribution FanSDR S2YA05067Pressure Switch · inoperativeDURING FLIGHT, THE CREW REPORTED THE RT AUX PUMP AUTO FUNCTION DID NOT STOP THE PUMP, RT NO AUX TRANSFER ILLUMINATED WHEN PUMP WAS IN AUTO FUNCTION. BETWEEN MX AND OPS, IT WAS DECIDED AN AIR-TURN-BACK WAS THE BEST OPTION. MX INSPECTED THE SYSTEM BUT COULD NOOct 19, 2005 · N881SK · Beech 1900D · Fuel Indicating SystemSDR S2YA05042Circuit Breaker · intermittentDURING APPROACH OF FLIGHT, THE CREW REPORTED THE GEAR WAS NOT EXTENDING NORMALLY BUT IS THEY JIGGLED THE HANDLE IT WOULD OPERATE. THE CREW PUMPED THE GEAR DOWN AND ACHIEVED THREE GREEN. MAINTENANCE FOUND INTERMITTENT HIGH OHMS READING THROUGH LANDING GEAR CIJul 14, 2005 · N881SK · Beech 1900D · Landing Gear System WiringSDR S2YA04009Elbow · crackedDURING FLIGHT, MASTER WARNING ILLUMINATED FOR THE RT ENGINE OIL PRESSURE INDICATION. THE RT ENGINE AUTO-FEATHERED AND THE CREW IAW QRH SHUTDOWN THE ENGINE IN FLIGHT. THE AC THEN MADE AN AIR-TURN-BACK AND DECLARED AN EMERGENCY. THE CREW MADE AN UNEVENTFUL LAMar 26, 2004 · N881SK · Beech 1900D · Turbine Engine Oil SystemSDR S2YA03015Switch · inoperativeDURING TAKEOFF OF FLIGHT 1076, THE CREW HEARD A LOAD POP FROM WHAT THEY REPORTED WAS THE LEFT ENGINE. THEY NOTED STRONG FUMES IN THE COCKPIT AND DONNED THEIR OXYGEN MASKS. THE CREW TURNED OFF THE ENVIRONMENTAL AIR, IAW THE QRH AND MADE AN AIR-TURN-BACK. MECApr 16, 2003 · N881SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA02015Engine · making metalFLT 1270 - MKE-CMH - THE LEFT OIL PRESSURE ILLUMINATED IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING. OUT STATION MAINTENANCE SERVICED THE LEFT ENGINE WITH OIL AND THE CREW DID A GROUND RUN. AFTER SHUTDOWN OF THE GROUND RUN, THERE WAS FLAMES COMING OUT OF Apr 17, 2002 · N881SK · Beech 1900D · Engine (Turbine/Turboprop)SDR S2YA98006Wire · chafedMKE - FLT 6350 - DURING APPROACH, MKE TO MKE TRAINING FLIGHT, CREW SELECTED LG DOWN, DID NOT EXTEND. WHEN CREW SELECTED LANDING GEAR DOWN, LG RELAY CB OPENED. CREW DECLARED EMERG, MANUALLY EXTENDED MLG, AND AFTER RECEIVING A 3-DOWN LOCKED IND, MADE SAFE LANDFeb 14, 1998 · N881SK · Beech 1900D · Landing Gear System WiringSDR S2YA98005Retract Mech · malfunctionedMSN/MKE - FLT 1158 - DURING APPROACH, CREW SELECTED LANDING GEAR DOWN WHICH FAILED TO EXTEND. CREW DECLARED AN EMERGENCY AND MANUALLY EXTENDED LANDING GEAR. AFTER RECEIVING ALL 3 GEAR DOWN AND LOCKED INDICATIONS, MADE UNEVENTFUL LANDING. MAINTENANCE INSPECTFeb 10, 1998 · N881SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA970033Panel · debondedFLT 1163 - DAY-SBN - THE OVAL INSPECTION PANEL ON THE AFT OF THE RT NACELLE, DEPARTED, AND HIT THE A/C. THE FLT CREW LANDED IN SBN WITHOUT INCIDENT. UPON INSPECTION THE PANEL WAS FOUND TO HAVE DELAMINATED FROM THE BONDED DOUBLER RING. THE DOUBLER RING WAS SOct 26, 1997 · N881SK · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR 97ZZZX1800Pressure 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 · N881SK · Beech 1900D · Fuel Pressure IndicatorSDR 97ZZZX1799Pressure 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 · N881SK · Beech 1900D · Fuel Pressure IndicatorSDR S2YA97005Engine · contaminatedKE/SBN - FLT 1162 - THE FLIGHT CREW SMELLED AN UNUSUAL ODOR WHEN THE BLEED AIR VALVES WERE TURNED ON AFTER TAKEOFF. THE CREW PERFORMED AN AIR TURNBACK TO MKE AND LANDED WITHOUT ANY OTHER PROBLEMS. ONCE ON THE GROUND, MAINTENANCE INSPECTED THE A/C, THEY NOTEDFeb 19, 1997 · N881SK · Beech 1900D · Engine (Turbine/Turboprop)SDR 97ZZZX1794Vertical 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 · N881SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR S2YA960031Pressure Switch · failedTHE CREW OF FLT 1052, MKE TO IND, CYCLED THE SURFACE DEICE SYSTEM BEFORE ENTERING ICING CONDITIONS USING AUTOMODE. THE TAIL DEICE ANNUNCIATOR FAILED TO ILLUMINATE. THE CREW TURNED BACK FOR MKE DUE TO HEAVY ICING CONDITONS IN IND. MAINTENANCE FOUND WATER IN Nov 8, 1996 · N881SK · Beech 1900D · Airfoil Anti/De-ice SystemSDR 97ZZZX1810Nav Contl Head · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,794.4 HRS FROM N NR 7Nov 1, 1996 · N881SK · Beech 1900D · Visual Omnirange (VOR) System
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