# Service difficulty reports: N847LS, cancelled Oct 19, 2004 A list on [N847LS, cancelled Oct 19, 2004](https://openairdocs.org/deregistered/N847LS-2004-10-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2003F00630](https://openairdocs.org/sdr/2003F00630.md): Probe · loose · Oct 31, 2003 · N847LS · Frchld SA227DC · Fire Detection > ENGINE FIRE WARNING LIGHT FOR THE NR 2 ENGINE CAME ON DURING CLIMB-OUT AS CREW COMPLETED CHECKLIST. AS THE CREW STARTED EMERGENCY CHECKLIST PROCEDURES, THE FIRE LIGHT WENT OUT. CREW COMPLETED APPLICABLE EMERGENCY CHECKLIST ITEMS, AND RETURNED TO STATION. CREW - [SDR BSA2002F00000](https://openairdocs.org/sdr/BSA2002F00000.md): Acm · failed · Sep 17, 2002 · N847LS · Frchld SA227DC · Cabin Cooling System > AFTER LANDING, SMOKE/OIL MIST FILLED THE CABIN. CREW SHUT DOWN AIRCRAFT AND EVACUATED THE PASSENGER ON THE TAXI WAY. ACM FAILURE. IMPELLER WAS FOUND LOOSE IN THE HOUSING. INITIALLY DEFERRED THE RIGHT BLEED SYSTEM IAW MEL. THE ACM WAS NOT SERVICED ON THE LA - [SDR 98ZZZX743](https://openairdocs.org/sdr/98ZZZX743.md): Relay · inoperative · Jan 18, 1998 · N847LS · Frchld SA227DC · AC Generation System > DFW/ELD - FLT 1253 - WHILE IN CRUISE AT FL 170, CREW RECEIVED RT GEN FAIL LIGHT. QRH CONSULTED AND GENERATOR SWITCH - OFF - RESET - ON INSTRUCTIONS FOLLOWED. GEN CAME BACK ON-INE. APPROX 3 MINUTES LATER, RT GEN FAIL LIGHT AGAIN ILLUMINATED. QRH WAS FOLLOW - [SDR 98ZZZX285](https://openairdocs.org/sdr/98ZZZX285.md): Hydraulic Line · cracked · Jan 9, 1998 · N847LS · Frchld SA227DC · Hydraulic System, Main > DFW/ELD - FLT 1251 - WHILE IN CRUISE 30 MINUTES INTO FLIGHT, BOTH HYD LIGHTS ILLUMINATED. CREW NOTICED GAUGES BLEEDING DOWN. BLEED DOWN STOPPED WHEN GAUGES WERE IN YELLOW ARC. CREW FOLLOWED ABNORMAL CHECKLIST AND CONTACTED MAINT AND FLIGHT DISPATCH. CREW A - [SDR ASE97012](https://openairdocs.org/sdr/ASE97012.md): Hydraulic Line · cracked · Jan 2, 1998 · N847LS · Frchld SA227DC · Hydraulic System, Main > FLT 1217 - DFW-HOT - ON APPROACH IN TO HOT, OBSERVED A HYDRAULIC PRESSURE FLUCTUATION. CREW MANUALLY EXTENDED LANDING GEAR AND LANDED IN HOT WITHOTU INCIDENT. UPON ARRIVAL, CREW NTOED OBVIOUS SIGNS OF LEAKAGE IN LEFT WHEEL WELL. MAINTENANCE CONTROL WAS NOTI - [SDR ASE97010](https://openairdocs.org/sdr/ASE97010.md): Hydraulic Line · cracked · Dec 31, 1997 · N847LS · Frchld SA227DC · Hydraulic System, Main > DFW-WDG - FLT 1265 - ON APPROACH IN TO WDG, AIRCRAFT EXPERIENCED TOTAL HYDRAULIC FAILURE. CREW MANUALLY EXTENDED LANDING GEAR AND LANDED IN WDG WITHOUT INCIDENT. UPON ARRIVAL, CREW NOTED OBVIOUS SIGNS OF LEAKAGE IN RIGHT WHEEL WELL. MAINTENANCE CONTROL WAS - [SDR ASE97011](https://openairdocs.org/sdr/ASE97011.md): Hyd Line · cracked · Dec 28, 1997 · N847LS · Frchld SA227DC · Hydraulic System, Main > DRT-TRC - FLT 1265 - ON APPROACH IN TO TRC, A/C EXPERIENCED TOTAL HYD PRESS LOSS. LOSS OF PRESS CONFIRMED BY ANNUNCIATOR PANEL LIGHTS. CREW MANUALLY EXTENDED L/G AND LANDED IN TRC W/O INCIDENT. UPON ARRIVAL, CREW NOTED OBVIOUS SIGNS OF LEAKAGE IN RT WHEEL W - [SDR 97ZZZM776](https://openairdocs.org/sdr/97ZZZM776.md): Starter Gen · failed · Jul 15, 1997 · N847LS · Frchld SA227DC · Starter-Generator > RIGHT GENERATOR FAIL LIGHT CAME ON INFLIGHT. AIRCRAFT DIVERTED TO HOT, MAINTENANCE REMOVED AND REPLACED THE RIGHT STARTER GENERATOR. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR 96ZZZM1569](https://openairdocs.org/sdr/96ZZZM1569.md): Tube · cracked · Nov 26, 1996 · N847LS · Frchld SA227DC · Hydraulic System, Main > EN ROUTE TO DFW, THE AIRCRAFT LOST ALL HYDRAULIC PRESSURE. CAPTAIN PUMPED GEAR DOWN USING THE EMERGENCY EXTENSION SYSTEM. AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. ON INSPECTION, A CRACKED HYDRAULIC LINE WAS FOUND TO BE THE PROBLEM. THE LINE WAS REP - [SDR 96ZZZM1495](https://openairdocs.org/sdr/96ZZZM1495.md): Connector · loose · Nov 1, 1996 · N847LS · Frchld SA227DC · Visual Omnirange (VOR) System > A/C DIVERTED TO HOT DUE TO RADAR MALFUNCTION. ON APPROACH, THE CAPT REPORTED BOTH VOR'S WERE NOT FUNCTIONING PROPERLY AND THE CEILING WAS TOO LOW FOR AN ADF APPROACH, CAPT ASKED MEM CTR FOR VECTORS TO NEAREST VFR AIRPORT AND DIVERTED TO FSM. AN AVIONICS SHO - [SDR 96ZZZM1171](https://openairdocs.org/sdr/96ZZZM1171.md): Oil Press Tube · cracked · Jun 27, 1996 · N847LS · Frchld SA227DC · Propeller Controlling System > WHILE EN ROUTE FROM HOT TO DFW, THE CAPTAIN NOTICED THAT THE OIL PRESSURE ON THE RIGHT ENGINE WAS DROPPING RAPIDLY. THE FLIGHT CREW THEN SHUTDOWN AND SECURED THAT ENGINE. THE AIRCRAFT THEN LANDED AT DFW WITHOUT FURTHER INCIDENT. ON INSPECTION, IT WAS FOUND - [SDR 96ZZZM1021](https://openairdocs.org/sdr/96ZZZM1021.md): Bearing · failed · May 28, 1996 · N847LS · Frchld SA227DC · Turbine Engine Accessory Drive > AFTER LANDING AT ROW, THE CHIP DETECTOR LIGHT CAME ON. THE PILOT COMPLETED A NORMAL SHUTDOWN WITH NO FURTHER INDICATIONS. AFTER INSPECTING THE CHIP DETECTOR, IT WAS DETERMINED A FAILURE HAD TAKEN PLACE IN THE GEARBOX. AFTER INSPECTING THE GEARBOX, IT WAS FO - [SDR 96ZZZX1448](https://openairdocs.org/sdr/96ZZZX1448.md): Hyd Line · leaking · Feb 7, 1996 · N847LS · Frchld SA227DC · Hydraulic System, Main > JBR/ELD - WHILE EN ROUTE, AIRCRAFT LOST ALL HYDRAULIC PRESSURE. THE PILOT DIVERTED TO HOT AND LANDED WITHOUT FURTHER INCIDENT. ON INSPECTION, MAINTENANCE FOUND THE LT MAIN PRESSURE LINE FROM THE HYDRAULIC PUMP TO THE FIREWALL HAD A HOLE IN IT AT A BEND. THE - [SDR 96ZZZX1449](https://openairdocs.org/sdr/96ZZZX1449.md): Hyd Line · leaking · Feb 6, 1996 · N847LS · Frchld SA227DC · Hydraulic System, Main > DURING PRE-FLIGHT, PILOT NOTICED A LARGE PUDDLE OF HYDRAULIC FLUID UNDER THE RT ENGINE AND VERY LITTLE FLUID IN THE SIGHT GLASS. THE PILOT WAS INSTRUCTED TO FERRY ACFT TO HOT FROM RUI WITH THE GEAR DOWN AND FLAPS UP. ON ARRIVAL AT HOT, MAIN PRESSURE LINE FRO - [SDR 96ZZZX656](https://openairdocs.org/sdr/96ZZZX656.md): Hydraulic Line · cracked · Dec 18, 1995 · N847LS · Frchld SA227DC · Hydraulic System, Main > HOT/STL - AFTER GAINING CRUISE ALTITUDE EN ROUTE, THE PILOT NOTICED THAT HYDRAULIC PRESSURE WAS FALLING AND DID FALL OFF COMPLETELY. THE PILOT THEN DIVERTED AND RETURNED TO HOT, LANDING WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THE RIGHT ENGINE MAIN HYDR - [SDR 96ZZZX119](https://openairdocs.org/sdr/96ZZZX119.md): Tube · cracked · Oct 1, 1995 · N847LS · Frchld SA227DC · Engine Oil Distribution (Airframe Furnished) > DFW/ROW - WHILE EN ROUTE, RT ENGINE LOST ALL OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO ABI AND LANDED WITHOUT FURTHER INCIDENT. ON INSPECTION OF THE ENGINE, AN OIL PRESSURE LINE WAS FOUND CRACKED. THIS LINE WAS A POST-DATED SB 77-0 ## 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 = 'N847LS' AND deregistration_id = 'N847LS-2004-10-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N847LS-2004-10-19/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.