# Service difficulty reports: N85SK, cancelled Jul 10, 2008 A list on [N85SK, cancelled Jul 10, 2008](https://openairdocs.org/deregistered/N85SK-2008-07-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR S2YA07004](https://openairdocs.org/sdr/S2YA07004.md): Spar Cap · cracked · Apr 29, 2007 · N85SK · Beech 1900D · Wing Spar > ON 04/29/07 DURING INSPECTION REQUIRED BY AD 2006-18-51 SKYWAY MAINTENANCE FOUND A CRACK ON RIGHT WING AFT SPAR, LOWER SPAR CAP AFT FLANGE AT WING STATION 117 INCHES. THE CRACK RAN FROM THE AFT EDGE TO A RIVET HOLE. THE DAMAGE WAS REPAIRED IAW RAYTHEON AIRCR - [SDR S2YA06005](https://openairdocs.org/sdr/S2YA06005.md): Unknown · malfunctioned · Jul 17, 2006 · N85SK · Beech 1900D · Cabin Pressure Control System > DURING FLIGHT 1070 MKE TO SDF AT FL 210 THE CREW GOT A CABIN HIGH INDICATION. THE CREW DECLARED AN EMERGENCY AND DID AN EMERGENCY DESCENT. THE A/C DECOMPRESSED SLOWLY AND BY FL 100 THE A/C HAD NO PRESSURIZATION. BOTH THE CREW AND PASSENGER DONNED OXYGEN MAS - [SDR S2YA05071](https://openairdocs.org/sdr/S2YA05071.md): Uplock Switch · inoperative · Oct 31, 2005 · N85SK · Beech 1900D · Landing Gear Position and Warning > ON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE RED IN TRANSIT LIGHT STAYED ILLUMINATED AFTER THE GEAR WAS SELECTED UP AND APPARENTLY DID FULLY RETRACT. THE RELEASE WAS AMENDED AND THE AC CONTINUED WITHOUT STOPPING. MX REPLACED THE NOSE GEAR UPLOCK SWITCH AND - [SDR S2YA05019](https://openairdocs.org/sdr/S2YA05019.md): Switch · malfunctioned · Feb 25, 2005 · N85SK · Beech 1900D · Trailing Edge Flap Control System > FLT 1071 - SDF-MKE - AFTER TAKEOFF, THE CREW WAS UNABLE TO RAISE THE FLAPS, PERFORMED AIR TURN BACK TO SDF. THE FLAPS WHERE RETRACTED USING THE BYPASS SWITCH AND THE SYSTEM WAS MEL'D. THE MEL WAS CLEAR BY ADJUSTING THE RT FLAP SAFETY SWITCH AND REPLACING THE - [SDR S2YA04046](https://openairdocs.org/sdr/S2YA04046.md): Annunciator · false activation · Dec 7, 2004 · N85SK · Beech 1900D · Door Warning System > SHORTLY AFTER TAKEOFF, THE CREW NOTICED AN AIR STAIR DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. AFTER MX CONSULTATION, THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX CLEANED AND INSPECT - [SDR S2YA04036](https://openairdocs.org/sdr/S2YA04036.md): Battery · discharged · Oct 4, 2004 · N85SK · Beech 1900D · Emergency Lighting > DURING FLIGHT, THE CREW NOTED THE BATTERY WAS NOT CHARGING SINCE THE BATTERY CHANGE LIGHT HAD STAYED ON SINCE START UP AND WAS STILL DRAWING 10-20 AMPS. INSTEAD STRANDING THE AC, THE DECISION WAS MADE TO PERFORMED AN AIR-TURN-BACK. MX CHARGED THE BATTERY AN - [SDR S2YA04011](https://openairdocs.org/sdr/S2YA04011.md): Module · failed · Apr 28, 2004 · N85SK · Beech 1900D · Air Data Computer > BEFORE FLIGHT, THE CREW NOTED THE TAWS FAILED RIGHT AFTER REACHING TAKE-OFF POWER. THE CREW ABORTED THE TAKE-OFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND COULD NOT CLEAR AN (ADC 1 INVALID) MESSAGE ON THE TAWS. MX REPLACED THE AIR DATA MODULE AN - [SDR S2YA02031](https://openairdocs.org/sdr/S2YA02031.md): Propeller · leaking · Aug 8, 2002 · N85SK · Beech 1900D · Propeller Assembly > SHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW NOTICED OIL ON THE RIGHT NACELLE. THE MADE AND AIR TURN BACK. MECHANIC INSPECTED THE ENGINE AND REPLACED THE PROP FOR LEAKING. - [SDR S2YA01002](https://openairdocs.org/sdr/S2YA01002.md): Motor · inoperative · Jan 19, 2001 · N85SK · Beech 1900D · Landing Gear Retraction/Extension System > FLT 1900 - MKG-MKE - DURING APPROACH, THE CRWE SELECTED GEAR DOWN BUT DID ACHEIVE DOWN AND LOCKED. THE CREW EMERGENCY HAND PUMPED THE GEAR DOWN AND GOT THREE GREEN. JUST TO BE SURE THE CREW MADE A FLY-BY TO CONFIRM THE GEAR DOWN AND AN UNEVENTFUL LANDING IN - [SDR S2YA98021](https://openairdocs.org/sdr/S2YA98021.md): Wire · chafed · Aug 11, 1998 · N85SK · Beech 1900D · Electrical Power System Wiring > A FLT CREW HAD WRITTEN UP THE LT AC BUS AS FAILING INFLIGHT. MAINTENANCE INSPECTED THE A/C AND FOUND FOUR WIRES CHAFFING IN THE LT FORWARD LEADING EDGE WING ROOT WS 29.06. THE WIRES WERE CHAFFING ON A GUIDE PLATE THAT ROUTES THE WIRES THROUGH PART OF THE LEA - [SDR S2YA98003](https://openairdocs.org/sdr/S2YA98003.md): Switch · dirty · Jan 13, 1998 · N85SK · Beech 1900D · Door Warning System > MKE/CLE - FLT 1158 - DURING FLIGHT, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE CREW DIVERTED TO THE NEAREST SUITABLE AIRPORT, LAN. AFTER A SAFE LANDING, THE ANNNUNCIATOR WAS PLACED ON MEL. THE FLIGHT THEN CONTINUED ON TO CLE. ON 1-14-98, MAINTENANCE CLEAR - [SDR S2YA97010](https://openairdocs.org/sdr/S2YA97010.md): Bulb · failed · Mar 6, 1997 · N85SK · Beech 1900D · Landing Gear Position and Warning > MKE/GRR - FLT 1833 - FLIGHT CREW SELECTED THE LANDING GEAR DOWN ON FINAL APPROACH. WHEN THE LANDING GEAR EXTENDED, THE RT MAIN GEAR DOWN AND LOCKED ANNUNCIATOR DID NOT ILLUMINATE. THE CREW PERFORMED ALL NECESSARY LANDING GEAR CHECKS, THEN MADE A SAFE LANDIN - [SDR S2YA97009](https://openairdocs.org/sdr/S2YA97009.md): Downlock Switch · dirty · Feb 6, 1997 · N85SK · Beech 1900D · Landing Gear Position and Warning > SBN/MKE - FLT 1161 - DURING THE LANDING APPROACH INTO MKE, CREW HAD TO CYCLE THE LANDING GEAR 3 TIMES IN ORDER TO GET A NOSE GEAR DOWN AND LOCKED INDICATION. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED AT MKE WITHOUT INCIDENT. WHEN MAINTENANCE TROUBLESH - [SDR 97ZZZX1809](https://openairdocs.org/sdr/97ZZZX1809.md): Nav Contl Head · inoperative · Nov 1, 1996 · N85SK · Beech 1900D · Visual Omnirange (VOR) System > DURING 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 7 - [SDR 97ZZZX1804](https://openairdocs.org/sdr/97ZZZX1804.md): Comp Contl Head · inoperative · Nov 1, 1996 · N85SK · Beech 1900D · VHF Communications System > DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE; 6,578.5 HRS FROM N - [SDR S2YA960020](https://openairdocs.org/sdr/S2YA960020.md): Fire Loop · shorted · Jul 29, 1996 · N85SK · Beech 1900D · Fire Detection > THE CREW OF FLT NR 1077.3 GRB-MKE - LANDED IN MKE AND DURING TAXI TO THE GATE THEY NOTICED THE LEFT FIRE WARNING T-HANDLE ANNUNCIATOR LIGHTS FLICKERED AND THEN STAYED 'ON'. THE CREW STOPPED THE AIRCRAFT, PROCEEDED TO BLOW THE FIRE BOTTLE AND DEBOARDED THE AIR - [SDR S2YA950012](https://openairdocs.org/sdr/S2YA950012.md): Switch · failed · Jun 11, 1995 · N85SK · Beech 1900D · Propeller Controlling System > THE PROP SYNCROPHASER BECAME INOP DUE TO AN ON/ON SWITCH BEING USED INSTEAD OF AN ON/OFF SWITCH. BEECH IS USING A THREE-POLE SWITCH AND THE ONE BARE UNPROTECTED TERMINAL HAS POWER SWITCHED TO IT WHEN YOU THINK IT IS SELECTED TO THE OFF POSITION. THIS HAS OCC - [SDR 95ZZZX2341](https://openairdocs.org/sdr/95ZZZX2341.md): Transfer Tube · chafed · Feb 16, 1995 · N85SK · Beech 1900D · Aircraft Fuel Distribution System > FOUND FUEL LEAKING FROM LT WHEELWELL, MAINTENANCE OPENED UP THE INNER FENDER ASSEMBLY AND FOUND MAIN GEAR UPLOCK SWITCH, WIRE BUNDLE HAD CHAFED THROUGH THE FUEL TRANSFER TUBE ASSEMBLY JUST INBOARD OF THE FUEL CROSS-TRANSFER VALVE. THE LINE WAS REMOVED ADN REP ## 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 = 'N85SK' AND deregistration_id = 'N85SK-2008-07-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N85SK-2008-07-10/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.