# Service difficulty reports: N918RW, cancelled Oct 24, 2007 A list on [N918RW, cancelled Oct 24, 2007](https://openairdocs.org/deregistered/N918RW-2007-10-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR NWAA072449953](https://openairdocs.org/sdr/NWAA072449953.md): Unknown · unknown · Jul 10, 2007 · N918RW · Doug DC931 · Cabin Pressure Control System > CABIN CREW REPORTED A PRESSURE LEAK TYPE SQUEAL COMING FROM THE AFT EMERGENCY ESCAPE HATCH. WHEN FLIGHT CREW REDUCED THRUST THE CABIN ALTITUDE CLIMBED UNCONTROLLABLY. THE PILOT PERFORMED A RAPID DESCENT TO A LOWER ALTITUDE AND CONTINUED TO SCHEDULED DESTINAT - [SDR 0700219953](https://openairdocs.org/sdr/0700219953.md): Compressor · stalled · Jan 21, 2007 · N918RW · Doug DC931 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL, AT APPROXIMATELY 100KTS, NR 1 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED AND THE AIRCRAFT SKIDDED OFF THE RUNWAY. THE AIRCRAFT IS BEING REPAIRED AND THE NR 1 ENGINE IS BEING REPLACED. - [SDR 0401909953](https://openairdocs.org/sdr/0401909953.md): Stiffener · cracked · Sep 22, 2004 · N918RW · Doug DC931 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CRACKS IN VERTICAL STIFFENERS AT BS 756 L28R, L28L AND ABOVE L26L. REPAIRED PER EA 99-200337. - [SDR 0401189953](https://openairdocs.org/sdr/0401189953.md): Controller · intermittent · Jul 15, 2004 · N918RW · Doug DC931 · Cabin Pressure Controller > FLIGHT CREW WAS NOT ABLE TO CONTROL THE PRESSURIZATION WITH AUTOMATIC CONTROL AFTER TAKEOFF, UTILIZED MANUAL CONTROL. MANUAL CONTROL FAILED AND THE OUTFLOW VALVE WENT FULL OPEN AT FL230. EMERGENCY DESCENT TO 10,000 FT AND THEN NORMAL DESCENT TO 6,000 FT. CA - [SDR 0300509953](https://openairdocs.org/sdr/0300509953.md): Skin · corroded · Mar 7, 2003 · N918RW · Doug DC931 · Fuselage Main, Plate/Skin > During "L" check found cracks in fuselage nose skin BS 69.5 fastener holes. Repaired per EA 99-190934. - [SDR 9810469953](https://openairdocs.org/sdr/9810469953.md): Angle · cracked · Nov 6, 1998 · N918RW · Doug DC931 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CRACK AT FORWARD ENTRY DOOR JAMB LOWER DEPRESSOR ANGLES FS 180. REPAIRED PER EA 99-160834 (P/N 5957094-1). - [SDR 9808119953](https://openairdocs.org/sdr/9808119953.md): Batteries · discharged · May 1, 1998 · N918RW · Doug DC931 · Emergency Lighting > DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS BETWEEN ROWS 9 THRU 11 AND AT LEFT FORWARD OVERWING EMERGENCY EXIT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9808109953](https://openairdocs.org/sdr/9808109953.md): Power Supply · inoperative · May 1, 1998 · N918RW · Doug DC931 · Emergency Lighting > FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS BETWEEN ROWS 8 THRU 10 WOULD NOT EXTINGUISH WITH SWITCH IN OFF POSITION. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9805169953](https://openairdocs.org/sdr/9805169953.md): Battery Pack · discharged · Mar 25, 1998 · N918RW · Doug DC931 · Emergency Lighting > FLIGHT ATTENDANT REPORTED FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9805129953](https://openairdocs.org/sdr/9805129953.md): Computer · failed · Mar 25, 1998 · N918RW · Doug DC931 · Stall Warning System > STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 STALL WARNING COMPUTER AND TRANSDUCER, OPERATIONAL CHECK NORMAL. - [SDR 9723399953](https://openairdocs.org/sdr/9723399953.md): Battery Pack · discharged · Dec 15, 1997 · N918RW · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9723349953](https://openairdocs.org/sdr/9723349953.md): Battery Pack · discharged · Dec 15, 1997 · N918RW · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9713899953](https://openairdocs.org/sdr/9713899953.md): Temp Sensor · failed · Jul 16, 1997 · N918RW · Doug DC931 · Overheat Detection > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TEMPERATURE SENSOR, OPERATIONAL CHECK NORMAL. - [SDR 9713569953](https://openairdocs.org/sdr/9713569953.md): Slide · failed test · Jul 10, 1997 · N918RW · Doug DC931 · Escape Slide > DURING PERIODIC CHECK, MAIN CABIN DOOR EMERGENCY EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. - [SDR 9624339953](https://openairdocs.org/sdr/9624339953.md): Strap · cracked · Nov 12, 1996 · N918RW · Doug DC931 · Nacelle/Pylon Structure > DURING LINE CHECK, FOUND A BROKEN NR 2 PYLON UPPER AFT ENGINE MOUNT STRAP. ALSO, FOUND CRACKS IN THE PYLON WEB LOWER CHANNEL 10 OUTBOARD FROM THE FUSELAGE AT THE LOWER ENGINE MOUNT STRAP AND IN THE UPPER INBOARD PYLON TO FUSELAGE ATTACH ANGLE 15 FORWARD OF TH - [SDR 9618579953](https://openairdocs.org/sdr/9618579953.md): Generator · failed · Aug 26, 1996 · N918RW · Doug DC931 · AC Generator-Alternator > RIGHT ENGINE GENERATOR TRIPPED OFF LINE AFTER TAKEOFF. RIGHT GEN OFF LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR, OPERATIONAL CHECK NORMAL. - [SDR 9613619953](https://openairdocs.org/sdr/9613619953.md): Fitting · corroded · Jun 16, 1996 · N918RW · Doug DC931 · Fuselage Miscellaneous Structure > DURING LINE CHECK, FOUND CORROSION ON THE LONGERON 23L END FITTING AT FS 980 TO 995. REPLACED FITTING PER SRM 51-30-2, 51-30-5. - [SDR 9604289953](https://openairdocs.org/sdr/9604289953.md): Batteries · discharged · Feb 22, 1996 · N918RW · Doug DC931 · Emergency Lighting > DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. - [SDR 9602109953](https://openairdocs.org/sdr/9602109953.md): O-Ring · split · Jan 28, 1996 · N918RW · Doug DC931 · Fuel Boost Pump > DURING CLIMB AFTER CENTER TANK WAS EMPTY, THE RIGHT FUEL PRESSURE LOW LIGHT ILLUMINATED. RIGHT FUEL INDICATION DID NOT DECREASE AND THE LEFT FUEL INDICATION WAS DECREASING AT THE RATE OF EQUAL TO BOTH ENGINE BURNS. ACCOMPLISHED COCKPIT OPERATING MANUAL PROCE - [SDR 9520359953](https://openairdocs.org/sdr/9520359953.md): Pt2 Probe · malfunctioned · Dec 8, 1995 · N918RW · Doug DC931 · Fuel Controlling System > NR 1 ENGINE EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE PT2 LINE, LEAK CHECKED THE PT2 SYSTEM AND REPLACED THE NOSE DOME/PT2 PROBE ASSEMBLY. SUBSEQUENT RUNUP WAS SATISFACTORY. - [SDR 9520349953](https://openairdocs.org/sdr/9520349953.md): Epr Indicator · failed · Dec 8, 1995 · N918RW · Doug DC931 · Engine Pressure Ratio (EPR) > NR 1 EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND PERFORMED A TAKEOFF POWER ASSURANCE RUN. THE NR 1 EPR SYSTEM OPERATION WAS NORMAL ON RUNUP. - [SDR 9520269953](https://openairdocs.org/sdr/9520269953.md): Compressor · stalled · Dec 6, 1995 · N918RW · Doug DC931 · Turbine Engine Compressor Section > ONE OR BOTH ENGINES EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES. THE NR 1 ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. SNOW AND SLUSH INGESTION IS SUSPECTED AS - [SDR 9514359953](https://openairdocs.org/sdr/9514359953.md): Fuel Press Sw · failed · Sep 14, 1995 · N918RW · Doug DC931 · Fuel Pressure Indicating > WHEN TAKEOFF POWER WAS APPLIED, THE NR 2 ENGINE INLET FUEL PRESSURE LOW WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE SYSTEM WAS PLACED ON MEL AND AIRCRAFT CONTINUED IN SERVICE. SUBSEQUENT REPLACEMENT OF THE L - [SDR 9514689953](https://openairdocs.org/sdr/9514689953.md): Longeron · cracked · Sep 13, 1995 · N918RW · Doug DC931 · Fuselage Main, Longeron/Stringer > DURING H-CHECK, FOUND A ONE INCH CRACK IN LONGERON 17R, FS 945 BOTH FRAME ATTACH POINTS. REPAIRED LONGERON (P/N 5911427-9), PER EA 99-100870. - [SDR 9514269953](https://openairdocs.org/sdr/9514269953.md): Release Syst · out of adjust · Sep 11, 1995 · N918RW · Doug DC931 · Aerodynamic Fairings > DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ADJUSTED THE CLIPS AND RELEASE, SYSTEM CHECKED OK. - [SDR 9513999953](https://openairdocs.org/sdr/9513999953.md): Fitting · corroded · Sep 6, 1995 · N918RW · Doug DC931 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 758 TO 760. REPLACED END FITTING PER SRM 53-02 FIG 12. - [SDR 9515499953](https://openairdocs.org/sdr/9515499953.md): Skin · corroded · Sep 5, 1995 · N918RW · Doug DC931 · Fuselage Main, Plate/Skin > DURING H-CHECK, FOUND CORROSION IN THE INNER SKIN AT FS 639, LONGERON 18L. REPAIRED PER EA 99-10973. - [SDR 9514589953](https://openairdocs.org/sdr/9514589953.md): Longeron · corroded · Aug 31, 1995 · N918RW · Doug DC931 · Fuselage Main, Longeron/Stringer > DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT THE FS 570 SPLICE. REPAIRED SPLICE (P/N 5920319-504), PER EA 99-97125. - [SDR 9513709953](https://openairdocs.org/sdr/9513709953.md): Fitting · cracked · Aug 31, 1995 · N918RW · Doug DC931 · Cargo/Baggage Doors > DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FRAME AND FITTING LOCATED IN THE UPPER FORWARD ACCESS NR 1. REPLACED THE FITTING. - [SDR 9513499953](https://openairdocs.org/sdr/9513499953.md): Hinge · corroded · Aug 28, 1995 · N918RW · Doug DC931 · Trailing Edge Flaps > DURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE STUD HOLES. REPLACED HINGE PER CITEXT 09-5740-1-9800. - [SDR 9513289953](https://openairdocs.org/sdr/9513289953.md): Fittings · corroded · Aug 26, 1995 · N918RW · Doug DC931 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND CORROSION ON FRAME FITTINGS FORWARD AND AFT OF THE GALLEY SERVICE DOOR FS 168 AND FS 200. REPLACED FITTINGS PER SRM 51-10-04. - [SDR 9510819953](https://openairdocs.org/sdr/9510819953.md): Connector · malfunctioned · Jul 13, 1995 · N918RW · Doug DC931 · Engine Oil Temperature > CLIMBING OUT OF MSP, THE NR 1 OIL TEMPERATURE INDICATED 170 DEGREES, THEN BEGAN FLUCTUATING BETWEEN 100 TO 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE CANNON PLUG ON THE OIL TEMPERATURE SENSOR, SYSTEM CHECK OK. - [SDR 9510799953](https://openairdocs.org/sdr/9510799953.md): Temp Sensor · malfunctioned · Jul 13, 1995 · N918RW · Doug DC931 · Engine Oil Temperature > CLIMBOUT OF MSP, THE NR 1 ENGINE OIL TEMPERATURE WAS FLUCTUATING AND SEEMED TO STABILIZE AT 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR, SYSTEM OPERATION APPEARED TO BE NORMAL. AIRCRAFT R - [SDR 9510059953](https://openairdocs.org/sdr/9510059953.md): Indication · malfunctioned · Jun 15, 1995 · N918RW · Doug DC931 · Leading Edge Slat Position Indicating System > SLAT EXTEND, BLUE LIGHT DID NOT ILLUMINATE WITH FLAPS EXTENDED TO 15 DEGREES FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PULLED AND RESET SLAT EXTEND SWITCH CIRCUIT BREAKERS, CYCLED SLATS SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SER - [SDR 9509449953](https://openairdocs.org/sdr/9509449953.md): Pressurization · malfunctioned · Jun 13, 1995 · N918RW · Doug DC931 · Cabin Pressure Control System > AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED CHECK OF AUTO AND MANUAL PRESSURIZATION SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. - [SDR 9503769953](https://openairdocs.org/sdr/9503769953.md): Vert Gyro · malfunctioned · Mar 9, 1995 · N918RW · Doug DC931 · Attitude Gyro and Indicating System > CAPTAIN'S ATTITUDE INDICATOR GYRO FLAG APPEARED DURING CLIMB-OUT. PITCH WENT TO 15 DEGREES AND LOCKED. FLIGHT RETURNED TO GTF AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S VERTICAL GYRO AND ADI. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR 9502819953](https://openairdocs.org/sdr/9502819953.md): Fuel Tank · venting · Feb 16, 1995 · N918RW · Doug DC931 · Fuel Storage > FUEL BEGAN VENTING FROM THE RIGHT MAIN TANK EN ROUTE MSP-HPN. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. PERFORMED BACKFLUSH PROCEDURE PER MM 28-20-0. AIRCRAFT RETURNED TO SERVICE. - [SDR 9502799953](https://openairdocs.org/sdr/9502799953.md): Fuel Sys · venting · Feb 15, 1995 · N918RW · Doug DC931 · Fuel Storage > FUEL BEGAN LEAKING FROM LEFT WING ENROUTE HPN-MSP. FUEL WAS VENTING FROM THE RIGHT TANK AT A RATE OF 800 POUNDS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROB - [SDR 9501799953](https://openairdocs.org/sdr/9501799953.md): Wing · fuel leak · Feb 15, 1995 · N918RW · Doug DC931 · Aircraft Fuel Distribution System > FUEL BEGAN LEAKING FROM LEFT WING EN ROUTE HPN-MSP. FUEL WAS VENTING FROM RIGHT TANK AT A RATE OF 800 LBS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBLEMS WE ## 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 = 'N918RW' AND deregistration_id = 'N918RW-2007-10-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N918RW-2007-10-24/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.