# Service difficulty reports: N613US, cancelled Feb 2, 2005 A list on [N613US, cancelled Feb 2, 2005](https://openairdocs.org/deregistered/N613US-2005-02-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0203576613](https://openairdocs.org/sdr/0203576613.md): Module · malfunctioned · Oct 23, 2002 · N613US · Boeing 747251B · AC Generation System > DURING FLIGHT, AN ELECTRICAL ODOR EMITTED AND THE NR 1 FIELD OFF AND GEN OPEN LIGHT ILLUMINATED. DISCONNECTED THE NR 1 CSD AND THE BURNING SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE CSD OIL TEMPERATURE INDI - [SDR 0200356613](https://openairdocs.org/sdr/0200356613.md): Ballast · malfunctioned · Feb 8, 2002 · N613US · Boeing 747251B · Passenger Compartment Lighting > DURING FLIGHT, GALLEY NR 5 WORK LIGHT CONTROL BOX EMITTED SMOKE. PULLED CIRCUIT BREAKER AND SMOKE DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED BALLAST AND SOCKET INSIDE LIGHT CONTROL BOX. OPERATIONAL CHECK GOOD. - [SDR 0104506613](https://openairdocs.org/sdr/0104506613.md): Skin Panel · corroded · Dec 5, 2001 · N613US · Boeing 747251B · Fuselage Main, Plate/Skin > During line check found corrosion on skin panel at lap splice from BS 1835-1961, stringer 12R. Repaired per EA 66-187305. - [SDR 0100916613](https://openairdocs.org/sdr/0100916613.md): Engine · stalled · Mar 1, 2001 · N613US · Boeing 747251B · Turbine Engine Compressor Section > DURING LANDING ROLLOUT (NKT) WHILE COMING OUT OF REVERSE THRUST, THE NR 4 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 1291C AND THE CONTROL TOWER REPORTED FLAMES FROM THE ENGINE. THE CREW FOLLOWED ENGINE FIRE PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. MAINTE - [SDR 0100366613](https://openairdocs.org/sdr/0100366613.md): Pin · installed · Feb 3, 2001 · N613US · Boeing 747251B · Landing Gear Retraction/Extension System > DURING CLIMB, THE NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT DUMPED 120,000 LBS OF FUEL AND RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REMOVED THE NOSE LANDING GEAR GROUND LOCK SAFETY PIN. OPERATIONAL CHECK NORMAL. - [SDR 0003526613](https://openairdocs.org/sdr/0003526613.md): Stringer · cracked · Aug 22, 2000 · N613US · Boeing 747251B · Fuselage Main, Longeron/Stringer > DURING M CHECK FOUND CRACK ON RT STRINGER NR 7 AT BS 1164. REPAIRED PER EA 66-162151. - [SDR 9804966613](https://openairdocs.org/sdr/9804966613.md): Engine · malfunctioned · Mar 24, 1998 · N613US · Boeing 747251B · Engine (Turbine/Turboprop) > DURING CRUISE, THE CREW NOTICED THE NR 3 ENGINE OIL CONSUMPTION TO BE UNUSUALLY HIGH. THE OIL CONSUMPTION DECREASED WITH LOWER POWER SETTINGS SO THE AIRCRAFT DIVERTED TO MSP FOR MAINTENANCE. THE ENGINE WAS NOT SHUT DOWN AND THE FLIGHT WAS COMPLETED WITHOUT F - [SDR 9802296613](https://openairdocs.org/sdr/9802296613.md): Engine · flamed out · Feb 6, 1998 · N613US · Boeing 747251B · Engine (Turbine/Turboprop) > JUST BEFORE TOP OF DESCENT AT FL370, THE NR 4 ENGINE FLAMED OUT. THE ENGINE WAS RESTARTED NORMALLY AT FL310 AND PERFORMED WITHOUT ANY PROBLEMS FOR THE REMAINEDER OF THE FLIGHT. MAINTENANCE VISUALLY INSPECTED THE ENGINE WITH NO DEFECTS NOTED. THE ENGINE FUEL - [SDR 9803726613](https://openairdocs.org/sdr/9803726613.md): Skin · corroded · Feb 4, 1998 · N613US · Boeing 747251B · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON SKIN AT FS 2020 BETWEEN STR 43R TO 44R. REPAIRED PER EA 66-154323. - [SDR 9802996613](https://openairdocs.org/sdr/9802996613.md): Longeron · cracked · Jan 29, 1998 · N613US · Boeing 747251B · Fuselage Main, Longeron/Stringer > DURING PERIODIC CHECK, FOUND CRACK IN STR 42L AT FS 1740. REPAIRED PER EA 66-155129. - [SDR 9801626613](https://openairdocs.org/sdr/9801626613.md): Fitting · corroded · Jan 25, 1998 · N613US · Boeing 747251B · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT END FITTINGS FOR STR 48L, 49L, 50L, AND 51L AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02634. - [SDR 9801616613](https://openairdocs.org/sdr/9801616613.md): Fitting · corroded · Jan 25, 1998 · N613US · Boeing 747251B · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD END FITTINGS FOR STR 48L TO 51L AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02634. - [SDR 9801606613](https://openairdocs.org/sdr/9801606613.md): Fitting · corroded · Jan 25, 1998 · N613US · Boeing 747251B · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD END FITTINGS FOR STR 46R, 50R, AND 51R AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02634. - [SDR 9801596613](https://openairdocs.org/sdr/9801596613.md): Fitting · corroded · Jan 25, 1998 · N613US · Boeing 747251B · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT END FITTINGS FOR STR 49R TO 51R AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02634. - [SDR 9722006613](https://openairdocs.org/sdr/9722006613.md): Battery Pack · discharged · Nov 24, 1997 · N613US · Boeing 747251B · Emergency Lighting > DURING LINE CHECK, FOUND C-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK GOOD. - [SDR 9720276613](https://openairdocs.org/sdr/9720276613.md): Latch · out of adjust · Oct 31, 1997 · N613US · Boeing 747251B · Cargo/Baggage Doors > DURING CLIMB, THE AFT CARGO DOOR ILLUMINATED AND AIRCRAFT FAILED TO PRESSURIZE. FLIGHT RETURNED TO BKK AFTER DUMPING 5000 LBS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE OUT OF POSITION. ADJUSTED LATCH AND LOCK. - [SDR 9701576613](https://openairdocs.org/sdr/9701576613.md): Battery Pack · discharged · Jan 26, 1997 · N613US · Boeing 747251B · Emergency Lighting > DURING LINE CHECK, FOUND THE 'E' ZONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY SUPPLY, OPERATIONAL CHECK GOOD. - [SDR 9627736613](https://openairdocs.org/sdr/9627736613.md): Bulkhead Chord · cracked · Dec 21, 1996 · N613US · Boeing 747251B · Nacelle/Pylon, Bulkhead/Firewall > DURING CHECK, FOUND NR 4 STRUT AFT BULKHEAD VERTICAL T-CHORD CRACKED VERTICALLY TWO INCHES FROM TOP RIGHT SIDE. REPLACED VERTICAL T-CHORD PER EA 66-120269 AND EA 66-120281. - [SDR 9627806613](https://openairdocs.org/sdr/9627806613.md): Floorbeam · cracked · Dec 11, 1996 · N613US · Boeing 747251B · Fuselage Main, Floor Beam > DURING CHECK, FOUND CRACK ON UPPER DECK FLOOR BEAM WEB. REPAIRED PER EA 66-120233. - [SDR 9621656613](https://openairdocs.org/sdr/9621656613.md): Bulkhead Fitting · cracked · Oct 2, 1996 · N613US · Boeing 747251B · Nacelle/Pylon, Bulkhead/Firewall > DURING P-CHECK, FOUND A CRACK IN THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD TO FRONT SPAR ATTACH FITTING AT NACELLE STA 221. REPLACED FITTING (P/N 65B91314-3). - [SDR 9621636613](https://openairdocs.org/sdr/9621636613.md): Bulkhead Web · cracked · Oct 1, 1996 · N613US · Boeing 747251B · Nacelle/Pylon, Bulkhead/Firewall > DURING P-CHECK, FOUND A 1.5 INCH CRACK IN THE NR 1 PYLON LOWER BULKHEAD WEB AT NACELLE STA 210. REPAIRED WEB PER EA 66-106410. - [SDR 9621576613](https://openairdocs.org/sdr/9621576613.md): Floor Beam · corroded · Sep 24, 1996 · N613US · Boeing 747251B · Fuselage Main, Floor Beam > DURING P-CHECK, FOUND CORROSION ON THE BS 520 UPPER DECK FLOOR BEAM UPPER CHORD FROM LBL 40 TO 50. REPAIRED CHORD (P/N 65B10936-12) PER EA 66-106402. - [SDR 9618916613](https://openairdocs.org/sdr/9618916613.md): Compressor · stalled · Aug 29, 1996 · N613US · Boeing 747251B · Turbine Engine Compressor Section > EN ROUTE, THE NR 4 ENGINE EXPERIENCED COMPRESSOR STALL AT TOP OF DESCENT. CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE. DECLARED EMERGENCY AND CONTINUED FLIGHT TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED METAL IN TAILPIPE. THE - [SDR 9613126613](https://openairdocs.org/sdr/9613126613.md): Wire · failed · Jun 14, 1996 · N613US · Boeing 747251B · Light System Wiring > DURING LINE CHECK, FOUND DOOR SLIDE AND OVERHEAD EMERGENCY LIGHTS DEFECTIVE AT DOOR 1R. REPAIRED WIRE, OPERATIONAL CHECK GOOD. - [SDR 9609316613](https://openairdocs.org/sdr/9609316613.md): Actuator · iced up · Apr 24, 1996 · N613US · Boeing 747251B · Aileron Control System > DURING CRUISE, THE AIRCRAFT WOULD NOT TURN, APPLIED A MODERATE AMOUNT OF PRESSURE TO FREE AILERONS. AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. REMOVED ICE FROM THE CENTRAL CONTROL ACTUATOR LOAD LIMITER. REPLACED THE NR 2 PACK WATER SEPARATOR COA - [SDR 9603116613](https://openairdocs.org/sdr/9603116613.md): Engine · high oil use · Feb 12, 1996 · N613US · Boeing 747251B · Turbine Engine Oil System > EN ROUTE, THE NR 1 ENGINE HAD HIGH OIL CONSUMPTION. CREW DUMPED 15,000 LBS OF FUEL AND DIVERTED TO SFO WITHOUT FURTHER INCIDENT. AIRCRAFT IS SCHEDULED FOR NR 1 ENGINE CHANGE. - [SDR 9521656613](https://openairdocs.org/sdr/9521656613.md): Engine · malfunctioned · Dec 27, 1995 · N613US · Boeing 747251B · Engine Fuel and Control > DURING CRUISE, THE NR 3 ENGINE ROLLED BACK TWICE WITH EGT, N1 AND FUEL FLOW GOING TO BOTTOM OF SCALE. WHEN THE THRUST LEVER WAS ADVANCED, ALL READINGS RETURNED TO NORMAL AND THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. FUEL PRESSURES WERE CHECKED, THE FUEL PU - [SDR 9517376613](https://openairdocs.org/sdr/9517376613.md): Battery Pack · discharged · Nov 3, 1995 · N613US · Boeing 747251B · Emergency Lighting > DURING CHECK, FOUND THE EMERGENCY LIGHT AT DOOR 5R INOPERATIVE. REPLACED THE BATTERY PACK, PERFORMED FUNCTIONAL CHECK AND UNIT CHECKED NORMAL. - [SDR 9516916613](https://openairdocs.org/sdr/9516916613.md): Prbcv · malfunctioned · Oct 26, 1995 · N613US · Boeing 747251B · Compressor Bleed Valve > DURING TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. A RE-LIGHT WAS ACCOMPLISHED, BUT THE POWER LEVER COULD NOT BE ADVANCED WITHOUT THE COMPRESSOR STALLING. THE ENGINE WAS SHUT DOWN AGAIN DURING APPROACH AN - [SDR 9516716613](https://openairdocs.org/sdr/9516716613.md): Flap · damaged · Oct 19, 1995 · N613US · Boeing 747251B · Leading Edge Devices > AFTER FLIGHT ARRIVAL, MAINTENANCE DISCOVERED THAT A LARGE SECTION OF THE NR 11 LEADING EDGE FLAP WAS MISSING. NO OTHER DAMAGE WAS FOUND. REPLACED FLAP PER MM 27-81-01, PG 401. CHECKED OK. (STA AMS). - [SDR 9507216613](https://openairdocs.org/sdr/9507216613.md): Bulkhead · cracked · Apr 29, 1995 · N613US · Boeing 747251B · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, FOUND A CRACK AND CORROSION IN THE SLANTED PRESSURE PANEL LOWER EDGE FS 1241, RBL 76. REPAIRED PER EA 66-97906. - [SDR 9506556613](https://openairdocs.org/sdr/9506556613.md): Skin · cracked · Apr 25, 1995 · N613US · Boeing 747251B · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, THE NOSE WHEEL WELL ACCESS RIGHT FORWARD HINGE FAIRING WAS FOUND CRACKED. REMOVED CRACK FROM OUTER SKIN, STOP DRILLED CRACK ON INNER SKIN. INSTALLED DOUBLER AND TRIPLER AND QUADRUPLER PER SA 5311-01064-6. - [SDR 9506416613](https://openairdocs.org/sdr/9506416613.md): Blkhd Web · corroded · Apr 24, 1995 · N613US · Boeing 747251B · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, THE LEFT BODY GEAR WHEEL WELL BULKHEAD WEB AT FS 1480 WAS FOUND CORRODED. REMOVED CORROSION, ROTO PEENED, TREATED, PRIMED, AND INSTALLED STRUCTURE PER EA 66-98011. - [SDR 9506286613](https://openairdocs.org/sdr/9506286613.md): Floor Beam · corroded · Apr 20, 1995 · N613US · Boeing 747251B · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, THE FLOOR BEAM AT FS 660, BL 0 WAS FOUND CORRODED. REPLACED FLOOR BEAM FROM RBL 56 TO LBL 47 AT FS 66 PER EA 66-98000. - [SDR 9506276613](https://openairdocs.org/sdr/9506276613.md): Carriage · cracked · Apr 20, 1995 · N613US · Boeing 747251B · Trailing Edge Flaps > DURING PERIODIC CHECK, THE RIGHT INBOARD TRAILING EDGE FLAP NR 5 CARRIAGE THRUST BEARING BORE WAS FOUND CORRODED AND CRACKED. MACHINED CORROSION, COMPLETED HFEC, FLAP PEENED BORE, AND INSTALLED WET BUSHING, BORE TREATED AND PRIMED PER EA 66-97885. - [SDR 9506216613](https://openairdocs.org/sdr/9506216613.md): Bracket · cracked · Apr 18, 1995 · N613US · Boeing 747251B · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CRACKED SHEAR TIE BETWEEN STR 10R AND 11R, FS 1220. REMOVED CRACKED SHEAR TIE, FABRICATED REPAIR, AND INSTALLED. - [SDR 9506226613](https://openairdocs.org/sdr/9506226613.md): Floorbeam · corroded · Apr 13, 1995 · N613US · Boeing 747251B · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, THE MAIN DECK FLOORBEAM WAS FOUND CORRODED ON THE UPPER SURFACE OF UPPER CHORD AT FS 660, LBL 56. MAXIMUM DEPTH OF CORROSION AFTER BLEND-OUT WAS BEYOND 50 PERCENT OF FLANGE THICKNESS AT SEVERAL AREAS. FLOORBEAM UPPER CHORD IS MADE OF. ## 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 = 'N613US' AND deregistration_id = 'N613US-2005-02-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N613US-2005-02-02/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.