# Service difficulty reports: N92SK, cancelled Jul 1, 2010 A list on [N92SK, cancelled Jul 1, 2010](https://openairdocs.org/deregistered/N92SK-2010-07-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR GLBA200812224](https://openairdocs.org/sdr/GLBA200812224.md): Control Handle · defective · Dec 20, 2008 · N92SK · Beech 1900D · Landing Gear Selector > SMELL/SMOKE/FUMES/SPARKS - PILOTS REPORTED THAT DURING PRE-FLIGHT CHECKS THEY NOTICED SPARKS BETWEEN THE GEAR HANDLE AND THE DOWN LOCK ARM. MX REMOVED AND REPLACED THE GEAR HANDLE ASSY PN 101-384137-7. PERFORMED GEAR SWINGS AND OPS CHECKS WERE GOOD IAW MM 32-6 - [SDR S2YA06010](https://openairdocs.org/sdr/S2YA06010.md): Drag Angle · broken · Nov 25, 2006 · N92SK · Beech 1900D · Main Landing Gear > DURING INSPECTION OF THE LANDING GEAR, MAINTENANCE DISCOVERED THE RIGHT MAIN LANDING GEAR DRAG BRACE ARM WAS BROKEN. THIS PART IS A TRIANGLE SHAPED PART THAT CONNECTS THE DRAG BRACE TO THE ACTUATOR. THE ARM HAD ONE OF THE TWO LUGS THAT CONNECT IT TO THE LAND - [SDR S2YA05047](https://openairdocs.org/sdr/S2YA05047.md): Boot · shorted · Aug 3, 2005 · N92SK · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice System > DURING FLIGHT, THE CREW REPORTED A GLOW COMING FROM THE RT PROPELLER. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE RT PROP AND FOUND THE DEICE BOOT HAD SHORTED AND BURNED. MAINTENANCE REPLACE - [SDR S2YA05015](https://openairdocs.org/sdr/S2YA05015.md): Wire · corroded · Feb 11, 2005 · N92SK · Beech 1900D · Landing Gear System Wiring > FLT 1851 - GRR-MKE - AFTER TAKEOFF, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AND THE INSTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW CONTINUED TO MKE WITH THE GEAR DOWN. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A CORRODED JUMPER WIRE AT A325P1 - [SDR S2YA05004](https://openairdocs.org/sdr/S2YA05004.md): Bleed Air Sys · malfunctioned · Jan 6, 2005 · N92SK · Beech 1900D · Pneumatic Distribution System > BEFORE FLIGHT, THE CREW REPORTED A RT BLEED AIR PROBLEM, THEY CONSULTED WITH MECHANIC WHO INSTRUCTED THE CREW TO RUN THE ENGINES TO LET THE SYSTEM WARM UP. AFTER RUNNING THE ENGINES THE PROBLEM COULD NOT BE DUPLICATED. WITH NO FURTHER DISCREPANCIES NOTED THE - [SDR S2YA04033](https://openairdocs.org/sdr/S2YA04033.md): Switch · inoperative · Sep 14, 2004 · N92SK · Beech 1900D · Landing Gear Retraction/Extension System > DURING APPROACH OF FLIGHT, THE CREW WAS 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 FERRIED BACK. MX REPLACED THE GEAR HANDLE - [SDR S2YA04018](https://openairdocs.org/sdr/S2YA04018.md): Inverter · erratic · Jun 1, 2004 · N92SK · Beech 1900D · AC Inverter > BEFORE FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED PROBLEMS, INCLUDING LT AC ANNUNCIATOR ILLUMINATED AND THE VOLT METER BEING ERRATIC. THE CREW RETURNED TO THE GATE AND AFTER CONSULTING WITH MX, MEL`D THE SYSTEM. MX INSPECTED THE SYSTEM INCLUDING SWA - [SDR S2YA03020](https://openairdocs.org/sdr/S2YA03020.md): Relay · failed · Jun 2, 2003 · N92SK · Beech 1900D · Rudder Control System > BEFORE TAKEOFF OF FLIGHT 1226, THE RUDDER BOOST ACTIVATED. THE CREW ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE FLIGHT CONTINUED. ON 6/16 THE MECHANIC CLEARED THE MEL BY REPLACING A RELAY AND REPAIRING SOME CHAFED WIRES TO THAT RELAY. THE AIRCRA - [SDR S2YA03005](https://openairdocs.org/sdr/S2YA03005.md): Garlock Seal · leaking · Feb 7, 2003 · N92SK · Beech 1900D · Turbine Engine Oil System > AFTER TAKEOFF ON FLIGHT 1167, A LEFT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 70 AND 90. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT, SERVICED THE LEFT ENGINE WITH 4 QUARTS OF OIL AND RETURNED THE AIRCRAFT TO SERVICE. MECHANIC INSPECTED TH - [SDR S2Y2002F00000](https://openairdocs.org/sdr/S2Y2002F00000.md): Tire · failed · Sep 4, 2002 · N92SK · Beech 1900D · Tire > DURING TAKEOFF THE CREW NOTED AN EXTRA JUMP OFF THE RUNWAY. THE CREW DID AN AIR TURN BACK BUT UPON LANDING THE AIRCRAFT BLEW ALL FOUR TIRES. MECHANIC INSPECTED THE BRAKE SYSTEM AND FOUND NO DEFECTS. MECHANIC REPLACED ALL THE TIRE AND RETURNED THE AIRCRAFT T - [SDR S2YA00012](https://openairdocs.org/sdr/S2YA00012.md): Computer · inoperative · Jun 1, 2000 · N92SK · Beech 1900D · Ground Proximity System > FLT 1090 - LSE-MKE - SHORTLY AFTER TAKEOFF, THE GPWS COMMANDED PULL UP, PULL UP. THE CREW CONTINUED TO CLIMB BUT THE GPWS WOULD NOT STOP, SO THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAINTENANCE WAS CONSULTED AND THE GPWS WAS PUT ON MEL. MAI - [SDR S2YA00002](https://openairdocs.org/sdr/S2YA00002.md): Actuator · inoperative · Feb 22, 2000 · N92SK · Beech 1900D · Landing Gear Actuator > FLT 1123 - YYZ-GRR - CREW SELECTED GEAR DOWN BUT DID NOT GET THE NOSE DOWN AND LOCK INDICATION. THE CREW MADE SEVERAL ATTEMPTS TO GET THE NOSE DOWN AND LOCKED INDICATION. THE CREW NOT GET THREE GREEN SO EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. OU - [SDR S2YA99030](https://openairdocs.org/sdr/S2YA99030.md): Actuator · malfunctioned · Dec 20, 1999 · N92SK · Beech 1900D · Landing Gear Actuator > DURING APPROACH OF FLIGHT 1024, MKE-ATW, LT MAIN GEAR SAFE LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THEN MADE AN UNEVENTFUL LANDING. OUTSTATION MX INSPECTED AND PINNED THE GEAR. THE AIRCRAFT WAS FERRIED TO MKE AND INSPECTED BY - [SDR S2YA98022](https://openairdocs.org/sdr/S2YA98022.md): Indicator · failed · Aug 11, 1998 · N92SK · Beech 1900D · Visual Omnirange (VOR) System > DURING PRE-FLIGHT RUN UP, CREW NOTICED SMOKE IN THE COCKPIT COMING FROM THE LT SUB-PANEL AND THE RMI FLAGGED INOPERABLE. AFTER FINISHING THE RUN-UP, THEY RETURNED TO THE GATE AND NOTIFIED MAINTENANCE. AFTER ACFT FERRIED TO MKE WITHOUT INCIDENT, MAINT INSPECT - [SDR S2YA98011](https://openairdocs.org/sdr/S2YA98011.md): Tire · out of round · Apr 15, 1998 · N92SK · Beech 1900D · Tire > FLT 1124 - GRR-YYZ, AFTER TAKEOFF, THE FLIGHT CREW FELT A STRONG VIBRATION FROM THE FRONT OF THE A/C. NOTIFIED ATC AND RETURNED TO GRR. AFTER MAKING A SAFE LANDING IN GRR, MAINTENANCE INSPECTED THE A/C AND FOUND THE NOSE TIRE OUT OF ROUND. THE A/C WAS FERRI - [SDR S2YA98009](https://openairdocs.org/sdr/S2YA98009.md): Brush Block · worn · Mar 18, 1998 · N92SK · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice System > MKE/MQT - FLT 1233 - WHILE IN CRUISE FLIGHT, CREW NOTICED THE RT PROP HEAT INDICATING ONLY 8 AMPS IN AUTO OR MANUAL MODES. THE WEATHER IN THE MQT AREA INDICATED ICING CONDITIONS, SO THE CREW ELECTED TO RETURN TO MKE AFTER CONSULATION WITH MAINTENANCE. AFTER - [SDR S2YA970034](https://openairdocs.org/sdr/S2YA970034.md): Connector · dirty · Nov 20, 1997 · N92SK · Beech 1900D · Ignition System > FLT 1120 - GRR-YYZ - DURING CLIMB-OUT, THE CREW NOTICED THE RT AUTO-IGNITION WOULD NOT TURN OFF. THE CREW WAS ASKED TO RETURN TO GRR FOR EASE OF LOCATING OUTSTATION MAINTENANCE. ONCE ON THE GROUND, MAINTENANCE CLEANED THE CONNECTOR AT THE PRESSURE SWITCH, CH - [SDR S2YA970024](https://openairdocs.org/sdr/S2YA970024.md): Wire · out of position · Jul 4, 1997 · N92SK · Beech 1900D · Flight Control System Wiring > BNA/MKE - FLT 1266 - BEFORE TAKEOFF, THE FLIGHT CREW WAS PERFORMING THE BEFORE TAKEOFF CHECK LIST, AND FOUND THE AILERONS BINDING/JAMMING. THEY RETURNED TO THE GATE, DEPLANED THE PASSENGERS, AND NOTIFIED MAINTENANCE. MAINTENANCE INSPECTED SYSTEM AND FOUND A - [SDR S2YA960014](https://openairdocs.org/sdr/S2YA960014.md): Skin · cracked · Jul 5, 1996 · N92SK · Beech 1900D · Rudder, Plate/Skin > DURING AN INSPECTION, MAINTENANCE FOUND THE TOP SIDE OF THE RUDDER CRACKED PERPENDICULAR AT THE FORWARD RIVET OF THE TOP STATIC WICK MOUNT. THE CRACK WAS 2 INCHES LONG AND THE BASE SKIN IS ONLY.020 INCH THOUSANDS THICK WITH NO REPAIR ALLOWED PER BEECH. FOUN - [SDR S2YA950026](https://openairdocs.org/sdr/S2YA950026.md): Flap Motor · shorted · Oct 22, 1995 · N92SK · Beech 1900D · Trailing Edge Flap Control System > THE FLIGHT CREW NOTICED AN UNKNOWN SOURCE OF SMOKE IN THE CABIN (ACRID SMELL) AND NOTICED THE FLAPS WOULD NOT SELECT 17 OR 35 DEGREES FROM THE FULL UP POSITION. OUTSIDE MAINTENANCE WAS CALLED AND THE MECHANIC C/W THE MAINTENANCE ACTION FOR FLAPS INOP BY PULLI - [SDR S2YA950025](https://openairdocs.org/sdr/S2YA950025.md): Trim · lack of lube · Oct 21, 1995 · N92SK · Beech 1900D · Elevator Tab Control System > AFTER THE FLIGHT CREW ASCENDED TO FLIGHT LEVEL 230, THEY NOTICED THE ELECTRIC ELEVATOR TRIM APPARENTLY FROZE AND WOULD NOT MOVE MANUALLY. THE CREW DECIDED TO TURN BACK TO MKE AND CALL MAINTENANCE. A MECHANIC INSPECTED THE ELEVATOR TRIM SYSTEM, REMOVED VISIBL ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N92SK' AND deregistration_id = 'N92SK-2010-07-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N92SK-2010-07-01/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.