# Service difficulty reports: N8925E, cancelled Aug 3, 2010 A list on [N8925E, cancelled Aug 3, 2010](https://openairdocs.org/deregistered/N8925E-2010-08-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DALA105929945](https://openairdocs.org/sdr/DALA105929945.md): Battery · discharged · Mar 17, 2010 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 & 18-21 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE APPROPRIATE BATTERIES IN THE DIFFERENT APPLICABLE LOCATIONS. OPERATIONAL CHECK WAS GOOD. - [SDR DALA102449945](https://openairdocs.org/sdr/DALA102449945.md): Battery Pack · weak · Feb 1, 2010 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-7 AND THE RT OVERWING EMERGENCY EXIT SIGN WERE WEAK. MX REPLACED THE BATTERIES AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CHECK. - [SDR NWAA094349945](https://openairdocs.org/sdr/NWAA094349945.md): Battery · discharged · Dec 16, 2009 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-11 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. - [SDR NWAA091079945](https://openairdocs.org/sdr/NWAA091079945.md): Power Supply · inoperative · Apr 4, 2009 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE CHECK, MX FOUND THAT ALL THREE OF THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYS. (K) - [SDR NWAA091069945](https://openairdocs.org/sdr/NWAA091069945.md): Actuator · intermittent · Apr 3, 2009 · N8925E · Doug DC931 · Drag Control Actuator > ON APPROACH, AS THE FLIGHT CREW WAS CONFIGURING THE ACFT FOR LANDING, AN UNCOMMANDED ROLL OF THE ACFT TO THE LT OCCURRED WHEN THE SPEED BRAKES WERE USED. THE ACFT COMPLETED A NORMAL LANDING WITHOUT FURTHER DIFFICULTIES. MX FUNCTIONALLY CHECKED THE SPOILER SY - [SDR 0302109945](https://openairdocs.org/sdr/0302109945.md): Skin · corroded · Oct 30, 2003 · N8925E · Doug DC931 · Fuselage Main, Plate/Skin > DURING M-CHECK FOUND CRACK IN SKIN AT NR 6 FORWARD STOP OF DOOR 1L. REPAIRED PER EA 99-196420. - [SDR 0103289945](https://openairdocs.org/sdr/0103289945.md): Skin · wrinkled · Mar 29, 2001 · N8925E · Doug DC931 · Fuselage Main, Plate/Skin > DURING AN H-CHECK AT ATLANTA, WAVINESS AND SKIN MISMATCH WERE FOUND IN THE AREA OF THE ALTERNATE STATIC PORT. IN ORDER TO CORRECT THE DISCREPANCY, THE FUSELAGE SKIN WAS TRIMMED OUT. HOWEVER, THE FLUSH SKIN REPAIR PER THE DC-9 SRM, CHAPTER 53-04, FIGURE 12C C - [SDR 0002809944](https://openairdocs.org/sdr/0002809944.md): Battery Pack · discharged · Jul 27, 2000 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. - [SDR 9903819945](https://openairdocs.org/sdr/9903819945.md): Connector · dirty · Sep 12, 1999 · N8925E · Doug DC931 · Emergency Lighting > DURING PERIODIC CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS ON CATWALK INOPERATIVE. CLEANED CORROSION FROM CATWALK STRIP CONNECTOR, OPERATIONAL CHECK NORMAL. - [SDR 9903589945](https://openairdocs.org/sdr/9903589945.md): Battery Pack · discharged · Sep 7, 1999 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9903579945](https://openairdocs.org/sdr/9903579945.md): Battery Pack · discharged · Sep 3, 1999 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9809169945](https://openairdocs.org/sdr/9809169945.md): Overheat Sensor · failed · May 13, 1998 · N8925E · Doug DC931 · Overheat Detection > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TAIL COMPARTMENT OVERHEAT SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. - [SDR 9804809945](https://openairdocs.org/sdr/9804809945.md): Wire · broken · Mar 22, 1998 · N8925E · Doug DC931 · Light System Wiring > DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 12, 13, AND 14 INOPERATIVE. REPAIRED BROKEN WIRING, OPERATIONAL CHECK NORMAL. - [SDR 9805289945](https://openairdocs.org/sdr/9805289945.md): Bracket · cracked · Mar 4, 1998 · N8925E · Doug DC931 · Fuselage Miscellaneous Structure > DURING H-CHECK, FOUND SHEAR TIE FITTING CRACKED AT FS 639 AT LONGERON 29L. REPLACED SHEAR TIE FITTING PER SRM 51-30-2. - [SDR 9716389945](https://openairdocs.org/sdr/9716389945.md): Battery Pack · discharged · Sep 1, 1997 · N8925E · Doug DC931 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND AFT CEILING AND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. - [SDR 9713709945](https://openairdocs.org/sdr/9713709945.md): Air Cycle Mach · leaking · Jul 12, 1997 · N8925E · Doug DC931 · Cabin Cooling System > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AT 29,000 FEET. CREW SHUT DOWN LEFT PACK AND CABIN PRESSURE BEGAN TO RISE. CREW DECLARED AN EMERGENCY AND DESCENT WAS MADE TO 10,000 FEET. FLIGHT WAS DIVERTED TO MEM, AIRCRAFT LANDED WITHOUT INCIDENT. MAI - [SDR 9713219945](https://openairdocs.org/sdr/9713219945.md): Gasket · blown · Jul 3, 1997 · N8925E · Doug DC931 · Pneumatic Indicating System > TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO BNA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BLOWN GASKET AT AIR CONDITIONING SUPPLY TEMPERATURE HIGH SENSOR, OPERATIO - [SDR 9705579945](https://openairdocs.org/sdr/9705579945.md): Anti Ice Valve · malfunctioned · Mar 18, 1997 · N8925E · Doug DC931 · Airfoil Anti/De-ice System > AIRFOIL ICE PROTECTION PRESSURE ABNORMAL AND PRESSURE HIGH LIGHTS ILLUMINATED WITH TAIL DEICE SELECTED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAIL ANTI-ICE VALVE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED T - [SDR 9626299945](https://openairdocs.org/sdr/9626299945.md): Tailcone · out of adjust · Dec 10, 1996 · N8925E · Doug DC931 · Aerodynamic Fairings > DURING PERIODIC CHECK, TAILCONE RELEASE FORCE EXCEEDED MAXIMUM LIMITS ON FUNCTION DROP CHECK. ADJUSTED PER CITEXT 09-5350-1-0021, SECOND TEST WAS WITHIN LIMITS. - [SDR 9626229945](https://openairdocs.org/sdr/9626229945.md): Frame · elongated hole · Dec 6, 1996 · N8925E · Doug DC931 · Fuselage Main, Frame > DURING PERIODIC CHECK, FOUND FRAME AT FS 1038 BETWEEN LONGERONS 13L AND 14L WITH AN ELONGATED HOLE FROM BRACE ROD ATTACH FITTING. REPAIRED FRAME PER EA 99-111-14. - [SDR 9621499945](https://openairdocs.org/sdr/9621499945.md): Gen Contl Pnl · failed · Oct 7, 1996 · N8925E · Doug DC931 · AC Generation System > RIGHT GENERATOR DROPPED OFF LINE ACCOMPANIED BY AC CROSSTIE LOCKOUT AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR CONTROL PANEL. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. - [SDR 9619819945](https://openairdocs.org/sdr/9619819945.md): Door Track · dirty · Sep 15, 1996 · N8925E · Doug DC931 · Door Warning System > AFTER TAKEOFF RECEIVED AN E/E DOOR WARNING INDICATION, LIGHT EXTINGUISHED AFT PRESSURIZATION. RETURNED TO SDF WITHOUT FURTHER INCIDENT. RECYCLED THE DOOR, CLEANED DEBRIS FROM THE DOOR TRACK AND RESET THE PLUG ON THE SWITCH, CHECKED OK. - [SDR 9618189945](https://openairdocs.org/sdr/9618189945.md): Door · not seated · Aug 21, 1996 · N8925E · Doug DC931 · Electrical/Electronic Compartment Doors > AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. WIND NOISE WAS ALSO COMING FROM NOSE GEAR AREA. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. NOTE: FORWARD ACCESSORY COMPARTMENT DOOR LIGHT ILLUMINATED SEVERAL TIMES ON FINAL. MAINTENANCE FOUND E/E COMPA - [SDR 9615039945](https://openairdocs.org/sdr/9615039945.md): Bleed Air · leaking air · Jul 11, 1996 · N8925E · Doug DC931 · APU Bleed Air System > DURING CLIMBOUT, PASSENGERS REPORTED A FUEL LIKE SMELL IN CABIN. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT APU WAS BLEEDING RESIDUAL OIL INTO AIR CONDITIONING SYSTEM, APU WAS CHANGED ON 10JUL96. REPLACED COALESCER BAGS, LEAK - [SDR 9603489945](https://openairdocs.org/sdr/9603489945.md): Schrader Valve · failed · Feb 11, 1996 · N8925E · Doug DC931 · Nose/Tail Landing Gear Strut/Axle > DURING CLIMBOUT, THE AIRCRAFT WOULD NOT SHIFT FROM GROUND MODE TO FLIGHT MODE. AIRCRAFT WAS UNABLE TO PRESSURIZE AND NOSE WHEEL WAS STEERABLE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT FLAT. REPLACED SCHR - [SDR 9601019945](https://openairdocs.org/sdr/9601019945.md): Press Reg Vlv · malfunctioned · Jan 16, 1996 · N8925E · Doug DC931 · Airfoil Anti/De-ice System > DURING FLIGHT, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING WING ANTI-ICE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED ICE PROTECTION PRE - [SDR 9518529945](https://openairdocs.org/sdr/9518529945.md): Thermal Switch · failed · Nov 19, 1995 · N8925E · Doug DC931 · Cabin Temperature Control System > DURING CLIMB, THE LEFT PACK OVERHEATED AND SMOKE ACCUMULATED IN THE FLIGHT DECK AND CABIN. DEACTIVATED THE LEFT PACK. FLIGHT RETURNED TO ROC AND LANDED WITHOUT INCIDENT. REPLACED THE THERMAL SHUTOFF SWITCH. OPERATIONAL CHECK OK. - [SDR 9514489945](https://openairdocs.org/sdr/9514489945.md): Indication · malfunctioned · Sep 24, 1995 · N8925E · Doug DC931 · Leading Edge Slat Position Indicating System > DURING APPROACH INTO MSP, AFTER SLATS AND FLAPS WERE EXTENDED FOR LANDING, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTENDED LIGHT. SLATS WERE VISUALLY CONFIRMED TO BE IN EXTENDED POSITION AND AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMEN - [SDR 9514449945](https://openairdocs.org/sdr/9514449945.md): Retract Mech · malfunctioned · Sep 21, 1995 · N8925E · Doug DC931 · Leading Edge Slat Control System > DURING SLAT EXTENSION ON APPROACH INTO MSP, SLAT EXTEND LIGHT BEGAN FLICKERING, THEN EXTINGUISHED AND SLAT DISAGREEMENT LIGHT ILLUMINATED. PERFORMED MISSED APPROACH AND CAPTAIN DECLARED AN EMERGENCY. SUCCESSFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT WITH - [SDR 9509419945](https://openairdocs.org/sdr/9509419945.md): Windshield · delaminated · Jun 9, 1995 · N8925E · Doug DC931 · Flight Compartment Windows > LEFT COCKPIT WINDSHIELD CRACKED EN ROUTE DFW TO MSP. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO STL, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. FOUND CAPTAIN'S WINDSHIELD DELAMINATED ON ALL SIDES. REPLACED WINDSHIELD AND TEMPERATURE CONTROLLER. - [SDR 9504089945](https://openairdocs.org/sdr/9504089945.md): Bracket · cracked · Mar 10, 1995 · N8925E · Doug DC931 · Vertical Stabilizer > DURING LINE CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR, RIGHT SIDE ABOVE THE RUDDER LEADING EDGE. REPAIRED PER XEA X9-53-82. - [SDR 9503179945](https://openairdocs.org/sdr/9503179945.md): Strut · deflated · Feb 26, 1995 · N8925E · Doug DC932 · Nose/Tail Landing Gear Strut/Axle > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED GROUND SHIFT LINKAGE AND CABLES WITH NO PROBLEMS FOUND. PERFORMED FULL SERVICE OF NOSE LANDING GEAR STRUT. AIRCRAFT RETU - [SDR 9502249945](https://openairdocs.org/sdr/9502249945.md): Studs · corroded · Feb 8, 1995 · N8925E · Doug DC931 · Trailing Edge Flaps > DURING PERIODIC CHECK, FOUND CORROSION ON NR 2 FLAP HINGE ATTACH STUDS. REPAIRED PER XEA X9-27-9. - [SDR 9502119945](https://openairdocs.org/sdr/9502119945.md): Hinge · corroded · Feb 2, 1995 · N8925E · Doug DC931 · Trailing Edge Flaps > DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE MOUNTING HOLES, WS 251. REPLACED HINGE FITTING PER CITEXT 09-5740-1-9800. - [SDR 9500939945](https://openairdocs.org/sdr/9500939945.md): Bulkhead · corroded · Jan 13, 1995 · N8925E · Doug DC931 · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, FOUND CORROSION IN FS 110 BULKHEAD TUNNEL AT LONGERON 27R, 6 INCHES UP FROM BOTTOM CORNER. REPAIRED PER XEA X9-53-50. - [SDR 9500869945](https://openairdocs.org/sdr/9500869945.md): Hinge Fitt · corroded · Jan 12, 1995 · N8925E · Doug DC931 · Wing, Control Surface Attach Fittings > DURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WING NR 2 FLAP HINGE FITTING OUTBOARD FASTENER BORES. REPAIRED PER XEA X9-9-27-9. - [SDR 9502449945](https://openairdocs.org/sdr/9502449945.md): Hinge · corroded · Jan 11, 1995 · N8925E · Doug DC931 · Trailing Edge Flaps > DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-12. - [SDR 9500509945](https://openairdocs.org/sdr/9500509945.md): Fitting · cracked · Jan 9, 1995 · N8925E · Doug DC931 · Wing Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CRACK IN CENTER WING TANK FITTING XCW O, BETWEEN WING STRINGERS 17 - 18. REPLACED FITTING PER SRM 51-10-4. - [SDR 9500499945](https://openairdocs.org/sdr/9500499945.md): Keel Beam · cracked · Jan 9, 1995 · N8925E · Doug DC931 · Fuselage Main, Keel > DURING PERIODIC CHECK, FOUND 10 INCH CRACK AND CORROSION IN RIGHT SIDE KEEL BEAM FS 604 - 637 BETWEEN LONGERON 28R - 29R. REPLACED BEAM PER SRM 51-30-2. - [SDR 9500479945](https://openairdocs.org/sdr/9500479945.md): Spar Chord · cracked · Jan 7, 1995 · N8925E · Doug DC931 · Horizontal Stabilizer, Spar/Rib > DURING PERIODIC CHECK, FOUND CRACKS IN THE HORIZONTAL STABILIZER AFT SPAR 'T' CAPS LEFT SIDE LOWER (XHS 205-211) AND RIGHT SIDE UPPER (XHS 188). REPAIRED BOTH PER SRM 55-02. - [SDR 9500469945](https://openairdocs.org/sdr/9500469945.md): Fitting · cracked · Jan 7, 1995 · N8925E · Doug DC931 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CRACKS IN ATTACH FITTINGS FS 996 AT LONGERONS 27R, 24L, AND AT INTERCOSTAL BETWEEN LONGERON 27L AND 28L. REPLACED ALL FITTINGS PER SRM 51-30. ## 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 = 'N8925E' AND deregistration_id = 'N8925E-2010-08-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8925E-2010-08-03/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.