# Service difficulty reports: N95S, cancelled Sep 22, 1999 A list on [N95S, cancelled Sep 22, 1999](https://openairdocs.org/deregistered/N95S-1999-09-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 9809679105](https://openairdocs.org/sdr/9809679105.md): Controller · failed · Jun 29, 1998 · N95S · Doug DC915 · Cabin Pressure Controller > AT FL290, THE CABIN PRESSURE BEGAN CLIMBING 1500 FEET PER MINUTE. THE FLIGHT CREW CLOSED THE OUTFLOW VALVE, CHECKED FOR CLOSED CROSSFEED VALVES, FOLLOWED EMERGENCY CHECK LIST, AND INITIATED AN EMERGENCY DESCENT TO FL100. THE OXYGEN MASK AUTO DEPLOY SYSTEM OP - [SDR 9800799105](https://openairdocs.org/sdr/9800799105.md): Circuit Breaker · tripped · Jan 11, 1998 · N95S · Doug DC915 · Stabilizer Control System > PRIMARY TRIM FAILED AFTER TAKEOFF. SECONDARY SYSTEM OPERATED NORMALLY. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A PHASE CIRCUIT BREAKER POPPED BEHIND FORWARD FLIGHT ATTENDANT SEAT. RESET CIRCUIT BREAKER, OPERATIONAL CHECK O - [SDR 9721279105](https://openairdocs.org/sdr/9721279105.md): Frame · cracked · Oct 29, 1997 · N95S · Doug DC915 · Fuselage Main, Frame > DURING L-CHECK, FOUND A CRACK IN CANTED FRAME AT FS 895, LONGERON 4L. REPAIRED PER EA 91-151790. - [SDR 9720309105](https://openairdocs.org/sdr/9720309105.md): Panel · cracked · Oct 27, 1997 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT LEFT OUTBOARD VERTICAL SUPORT FS 106. REPAIRED PER EA 91-151781. - [SDR 9720299105](https://openairdocs.org/sdr/9720299105.md): Panel · cracked · Oct 25, 1997 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE PREVIOUS REPAIR FS 83. REPAIRED PER EA 91-151780. - [SDR 9707309105](https://openairdocs.org/sdr/9707309105.md): Clips · out of adjust · Apr 7, 1997 · N95S · Doug DC915 · Aerodynamic Fairings > DURING LINE CHECK, FOUND EXCESSIVE FORCE REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. CLEANED AND LUBED LATCH PIN ASSEMBLIES AND INTERNAL HANDLE. ALSO, ADJUSTED CLIPS AND OPERATIONAL CHECK OK. - [SDR 9701589105](https://openairdocs.org/sdr/9701589105.md): Door Jamb · dirty · Jan 24, 1997 · N95S · Doug DC915 · Cargo/Baggage Doors > AFTER TAKEOFF, THE CABIN WOULD NOT PRESSURIZE. APPROXIMATELY SIX MINUTES AFTER TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED FOR APPROXIMATELY TWO MINUTES. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND DEBRIS IN AFT CARGO DOOR JAMB. REMOVED DEBRIS - [SDR 9700599501](https://openairdocs.org/sdr/9700599501.md): Fuel Control · malfunctioned · Jan 11, 1997 · N95S · Doug DC915 · APU Engine Fuel and Control > DURING CLIMB, APU AUTO SHUTDOWN. NR 1 ENGINE GENERATOR ON MEL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE APU FUEL CONTROL, LEAK CHECK GOOD. - [SDR 9700599105](https://openairdocs.org/sdr/9700599105.md): Fuel Control · malfunctioned · Jan 11, 1997 · N95S · Doug DC915 · APU Engine Fuel and Control > DURING CLIMB, APU AUTO SHUTDOWN. NBR 1 ENGINE GENERATOR ON MEL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE APU FUEL CONTROL, LEAK CHECK GOOD. - [SDR 9626609105](https://openairdocs.org/sdr/9626609105.md): Engine · failed · Dec 16, 1996 · N95S · Doug DC915 · Engine (Turbine/Turboprop) > DURING CLIMB AT 1000 FEET AGL, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS AND A CONTAINED FAILURE OF THE LEFT ENGINE. CREW FOLLOWED COM EMERGENCY PROCEDURES. RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. - [SDR 9621549105](https://openairdocs.org/sdr/9621549105.md): Bulkhead Doubler · cracked · Sep 13, 1996 · N95S · Doug DC915 · Fuselage Main, Bulkhead > DURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD -13 DOUBLER UPPER DOOR JAMB. REPAIRED DOUBLER (P/N 5910130-13) PER EA 91-111229. - [SDR 9619469105](https://openairdocs.org/sdr/9619469105.md): Power Supply · inoperative · Sep 6, 1996 · N95S · Doug DC915 · Emergency Lighting > DURING LINE CHECK, FOUND THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT POWER SUPPLIES. OPERATIONAL CHECK OK. - [SDR 9619459105](https://openairdocs.org/sdr/9619459105.md): Batteries · discharged · Sep 6, 1996 · N95S · Doug DC915 · Emergency Lighting > DURING LINE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERIES. OPERATIONAL CHECK OK. - [SDR 9614489105](https://openairdocs.org/sdr/9614489105.md): Frame · cracked · Jun 27, 1996 · N95S · Doug DC915 · Fuselage Main, Frame > DURING LINE CHECK, FOUND A CRACK EXTENDING APPROXIMATELY HALF WAY THROUGH THE FS 180 FRAME BETWEEN LONGERONS 6L TO 7L. REPAIRED FRAME PER SRM 53-03 FIG 36, SHEETS 1 AND 2. - [SDR 9608239105](https://openairdocs.org/sdr/9608239105.md): Battery Pack · discharged · Apr 11, 1996 · N95S · Doug DC915 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK GOOD. - [SDR 9605189105](https://openairdocs.org/sdr/9605189105.md): Fitting · cracked · Feb 26, 1996 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL FITTING FS 642 OUTBOARD OF LONGERON 29R. REPLACED FITTING REF 51-30. - [SDR 9605179105](https://openairdocs.org/sdr/9605179105.md): Fittings · corroded · Feb 25, 1996 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON THE FS 642 LEFT KEEL FITTINGS AT LONGERON 30 AND OUTBOARD OF LONGERON 29L. REPLACED BOTH FITTINGS PER SRM 51-30-5. - [SDR 9605149105](https://openairdocs.org/sdr/9605149105.md): Fitting · corroded · Feb 20, 1996 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON THE LEFT LAVATORY FITTING ON THE AFT SIDE OF THE FS 817 FRAME. REPLACED FITTING PER SRM 51-30-3. - [SDR 9600129105](https://openairdocs.org/sdr/9600129105.md): Unsafe Light · illuminated · Jan 4, 1996 · N95S · Doug DC915 · Landing Gear Position and Warning > DURING APPROACH INTO FAR, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EXECUTED GO-AROUND AND RECYCLED GEAR. ALL INDICATIONS WERE NORMAL AFTER THIRD CYCLE. AIRCRAFT LANDED WITHOUT INCIDENT. CHECKED NOSE GEAR DOWNLOCK SWITCH AND ALL C - [SDR 9520409105](https://openairdocs.org/sdr/9520409105.md): Transponder · malfunctioned · Dec 13, 1995 · N95S · Doug DC915 · Stall Warning System > STALL WARNING AND STICK SHAKER ACTIVATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT STALL WARNING TRANSDUCER, FLAP POSITION TRANSMITTER, AND YAW DAMPER ACTUATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR 9514769105](https://openairdocs.org/sdr/9514769105.md): Clips · out of adjust · Sep 16, 1995 · N95S · Doug DC915 · Aerodynamic Fairings > DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. - [SDR 9513519105](https://openairdocs.org/sdr/9513519105.md): Skin · delaminated · Aug 30, 1995 · N95S · Doug DC915 · Spoilers > DURING LINE CHECK, FOUND DELAMINATION IN THE RIGHT INBOARD SPOILER. REPLACED SPOILER PER CITEXT 90-2760-1-9901. - [SDR 9507729105](https://openairdocs.org/sdr/9507729105.md): Rib · cracked · May 5, 1995 · N95S · Doug DC915 · Spoilers > DURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD SPOILER FITTING (RIB CAP). REPLACED RIB CAP. - [SDR 9504799105](https://openairdocs.org/sdr/9504799105.md): Skin · loose fasteners · Mar 26, 1995 · N95S · Doug DC915 · Rudder, Plate/Skin > DURING LINE CHECK, FOUND APPROXIMATELY 40 - 50 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS. - [SDR 9502929105](https://openairdocs.org/sdr/9502929105.md): Intercostal · cracked · Feb 18, 1995 · N95S · Doug DC915 · Fuselage Miscellaneous Structure > DURING LINE CHECK, FOUND ONE.5 INCH CRACK IN VERTICAL INTERCOSTAL, FORWARD CARGO DOOR JAMB FS 351. REPLACED INTERCOSTAL PER EA 91-096933. - [SDR 9502669105](https://openairdocs.org/sdr/9502669105.md): Dnlock Sw · malfunctioned · Feb 11, 1995 · N95S · Doug DC915 · Landing Gear Position and Warning > DURING APPROACH INTO MSP, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON GEAR EXTENSION. CONFIRMED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION AND AIRCRAFT LANDED WITHOUT INCIDENT. 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 = 'N95S' AND deregistration_id = 'N95S-1999-09-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N95S-1999-09-22/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.