N8923E, cancelled Jul 28, 2010

Service difficulty reports · 46

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N8923E' AND deregistration_id = 'N8923E-2010-07-28'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR NWAA 1459929Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12/15 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.May 2, 2009 · N8923E · Doug DC931 · Emergency LightingSDR NWAA09159929Skin · crackedDURING L-CHECK, FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 14. TEMPORARY REPAIRED ACCOMPLISHED IAW EA99-214503, SEC I. SECTION II FURTHER TEMPORARY REPAIR TO BE DONE WITHIN 4000 FLIGHT HOURS AFTER SECTION I ACCOMPLISHMENT. SECTION III REQUIRES INSPECTJan 7, 2009 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR NWAA084519929Duct · defectiveON APPROACH INTO YYZ AFTER FLIGHT CREW SET THE LEADING EDGE SLATS TO EXTEND, FLAPS AT ZERO, THE AMBER SLAT DISAGREEMENT LIGHT ILLUMINATED AND AN UNCOMMANDED ROLL OF THE ACFT TO THE LT OCCURRED. THE SLATS WERE RETRACTED WITHOUT DIFFICULTY, THE FLAPS EXTENDED TOct 7, 2008 · N8923E · Doug DC931 · Airfoil Anti/De-ice SystemSDR NWAA084179929Connector · corrodedDURING LINE CHECK MX FOUND THAT 2 OF THE 3 EMERGENCY PATHWAY LIGHTS IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MX FOUND THE CATWALK LIGHTS CONNECTOR BETWEEN THE SECOND AND THIRD EEPL WAS CORRODED. AFTER IT WAS CLEANED AND SECURED THE LIGHTS TESTED AS FUNCTIONSep 4, 2008 · N8923E · Doug DC931 · Light System WiringSDR NWAA081499929Switch · failedDURING THE LANDING APPROACH INTO MBS, THE CREW SMELLED SMOKE AND WITNESSED SPARKS AND MOLTEN METAL COMING FROM UNDERNEATH THE INSTRUMENT PANEL. THE LANDING WAS ACCOMPLISHED WITHOUT FURTHER TROUBLE BUT CREW REQUESTED THAT CFR MEET UP WITH THE AIRCRAFT. AIRCRAApr 12, 2008 · N8923E · Doug DC931 · Light System WiringSDR NWAA080909929Actuator · malfunctionedAIRCRAFT RETURNED TO A SAFE LANDING AFTER PILOT EXPERIENCED HORIZONTAL STABILIZER PROBLEMS DURING CLIMB-OUT. FIRST OFFICER HAD SELECTED STABILIZER TRIM AND WAS UNABLE TO STOP THE STABILIZER FROM CONTINUOUSLY MOVING, OSCILLATING UP AND DOWN PAST THE DESIRED POMar 10, 2008 · N8923E · Doug DC931 · Stabilizer Control SystemSDR NWAA073759929Control System · out of rigWHEN THE SLATS WERE SELECTED TO EXTEND DURING THE APPROACH FOR LANDING, THE BLUE "SLAT DISAGREE" LIGHT ILLUMINATED AND WAS ACCOMPANIED BY AN AIRCRAFT ROLL TO THE RIGHT. THE FLAP/SLAT COMBINATION WAS RECYCLED AND THE FIRST OFFICER VISUALLY VERIFIED FLAPS HAD Nov 4, 2007 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR NWAA073579929Slat System · unknownON APPROACH FOR LANDING AT ABOUT 200 KTS, THE YELLOW "SLAT DISAGREEMENT" LIGHT ILLUMINATED WHEN SLATS WERE SELECTED TO EXTEND. THE AIRCRAFT ALSO EXPERIENCED AN UNCOMMANDED ROLL TO THE RIGHT WHEN THE LEADING EDGE SLATS FAILED TO DEPLOY SYMMETRICALLY. AS THE AOct 23, 2007 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR NWAA072489929Skin · crackedDURING "H" CHECK, FOUND CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF FORWARD SERVICE DOOR JAMB . REPAIRED PER EA 99-209601 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3,000 CYCLES AFTER SECTION I ACCOMPLISHMENT.Jul 6, 2007 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR NWAA072479929Skin · crackedDURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT FORWARD UPPER CORNER OF THE FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-209598 SECTION I SECTION II TO BE ACCOMPLISHED ON OR BEFORE 2 YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT.Jul 5, 2007 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR NWAA072469929Skin · crackedDURING "H" CHECK FOUND CRACK IN RT FUSELAGE SKIN AT UPPER LEFT CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-209597 SECT I SECT II TO BE ACCOMPLISHED ON OR BEFORE TWO YEARS OR 3000 CYCLES AFTER SECTION I ACCOMPLISHMENT.Jul 5, 2007 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR 0501259929Wire · chafedEMERGENCY LIGHTS REMAIN ON WHEN SWITCHED OFF AND C/B POPS. FOUND WIRING CHAFED BEHIND OVERHEAD BINS. REPAIRED WIRING AND RECHARGED BATTERY PACKS. CHECKS GOOD. Aug 14, 2005 · N8923E · Doug DC931 · Light System WiringSDR 0401119929Frame · crackedDURING M-CHECK FOUND CRACK IN FRAME AT BS 598 L24L. REPAIRED PER EA 99-199088.May 16, 2004 · N8923E · Doug DC931 · Fuselage Main, FrameSDR 0301179929Duct · lack of lubeDURING SLAT EXTENSION ROLL, SLAT DISAGREEMENT ANNUNCIATOR STAYED ON. COMPLIED WITH COM PROCEDURE AND SLATS RETRACTED NORMALLY. AN UNEVENTFUL LANDING WAS MADE AT MKE. MAINTENANCE INSPECTED THE SLAT SYSTEM BUT FOUND NO DEFECTS AND COULD NOT DUPLICATE THE PROBJun 23, 2003 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR 0204019929Duct · lack of lubeWhen the slats were extended the aircraft rolled and the "Slat Disagreement" light illuminated. After about 2 minutes the light extinguished and the aircraft flew normally. Landing at YYG was without incident. No mention of COM procedures. Maintenance found noDec 10, 2002 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR 0204029929DuctDuring approach the aircraft rolled left on slat extension. "Slat Disagreement" light was illuminated. COM procedures were performed and the aircraft landed uneventfully. Maintenance replaced a T-Duct in the left wing. The aircraft was returned to service.Dec 8, 2002 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR 0103979929Flange · crackedEO 5230-01119 installs a hold open latch on the fwd end of the fwd cargo door to minimize the the possibility of inadvertant closure. However, investigation has revealed cracking of the cargo door flange. EA 99-186086Oct 18, 2001 · N8923E · Doug DC931 · Cargo/Baggage DoorsSDR 0003679929Slat · stuckSLAT DISAGREEMENT ANNUNCIATOR ILLUMINATED ON APPROACH TO MEM. THE AIRCRAFT ROLLED TO THE LEFT WHEN RIGHT SLAT EXTENDED BEFORE THE LEFT, THEN ROLLED TO THE RIGHT WHEN THE LEFT SLAT CAUGHT UP RESULTING IN A SAFE LANDING. MAINTENANCE DETERMINED THAT A LEFT ''T'Oct 8, 2000 · N8923E · Doug DC931 · Leading Edge Slat Position Indicating SystemSDR 0001289929Angle · crackedVERTICAL STABILIZER LOWER ATTACH ANGLE CRACKED AT RIGHT SIDE, NEAR AFT END. REPAIRED DAMAGED AREA AND CONFIRMED. REPAIRED IAW SRM 53-05 AND EA 99-175537. LP''S 1424295, 1423937Apr 11, 2000 · N8923E · Doug DC931 · Vertical StabilizerSDR 0000209929Duct · lack of lubeON APPROACH INTO CLT, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE LEFT ON SLAT EXTENSION. FLIGHT CREW DECLARED A YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICATED LEFT SLAT T DUCT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETJan 27, 2000 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR 9808459929Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES FROM THE RETAINING CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.May 5, 1998 · N8923E · Doug DC931 · Aerodynamic FairingsSDR 9720399929Cables · out of adjustAIRCRAFT ROLLED TO THE LEFT UPON SLAT EXTENSION. SLAT EXTEND TOOK LONGER THAN NORMAL TO ILLUMINATE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT SLAT CABLES OUT OF RIG. RIGGED SLAT SYSTEM CABLES, OPERATIONAL CHECK NORMAL.Oct 29, 1997 · N8923E · Doug DC931 · Leading Edge Slat Control SystemSDR 9709139929Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.May 5, 1997 · N8923E · Doug DC931 · Emergency LightingSDR 9708629929Bulkhead · crackedDURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 110 AT RIGHT INBOARD FITTING. REPAIRED PER EA 99-112886.Apr 29, 1997 · N8923E · Doug DC931 · Fuselage Main, BulkheadSDR 9708489929Release Mech · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ADJUSTED TAIL CONE RELEASE LATCHES, OPERATIONAL CHECK OK.Apr 29, 1997 · N8923E · Doug DC931 · Aerodynamic FairingsSDR 9708639929Bulkhead · crackedDURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD AT FS 110 AT RIGHT OUTBOARD FITTING. REPAIRED PER EA 99-112886.Apr 28, 1997 · N8923E · Doug DC931 · Fuselage Main, BulkheadSDR 9709549929Bulkhead · corrodedDURING L CHECK, FOUND CORROSION ON THE HORIZONTAL FLANGE AT THE T-CAP FS 110 BETWEEN LONGERONS 26L AND 27L. REPAIRED PER EA 99-112892.Apr 27, 1997 · N8923E · Doug DC931 · Fuselage Main, BulkheadSDR 9708739929Bulkhead · crackedDURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 110 AT LEFT OUTBOARD FITTING. REPAIRED PER EA 99-112886.Apr 26, 1997 · N8923E · Doug DC931 · Fuselage Main, BulkheadSDR 9709539929Skin · corrodedDURING L CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 310 BETWEEN AFT MOUNT HOLES ON UPPER AFT LOOP ANTENNA. REPAIRED PER EA 99-112904.Apr 1, 1997 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9705609929Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHT DIM. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.Mar 17, 1997 · N8923E · Doug DC931 · Emergency LightingSDR 9702929929Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND BOTH AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 11, 1997 · N8923E · Doug DC931 · Emergency LightingSDR 9702169929Switch · malfunctionedFLAP/RUDDER STOP INOPERATIVE, LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP POSITION SWITCH S1-351. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.Feb 3, 1997 · N8923E · Doug DC931 · Trailing Flap Position Indicating SystemSDR 9623049929Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL.Oct 27, 1996 · N8923E · Doug DC931 · Emergency LightingSDR 9616079929Fuel Line · disconnectedFUEL BEGAN VENTING FROM LEFT WING EN ROUTE DCA-MSP. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. FORWARD AND AFT RIGHT FUEL PRESSURE LIGHTS WOULD NOT EXTINGUISH AFTER LANDING. MAINTENANCE FOUND FUEL LINE AT FORWARD RIGHT FUEL BOOST PUMP DISCONNECTED Jul 27, 1996 · N8923E · Doug DC931 · Fuel Boost PumpSDR 9610449929T/O Warning · soundedTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL AT 30 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. HORN WAS SILENCED AFTER SPOILERS WERE CYCLED. MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM TEST PER MAINTENANCE MANUAL 27-00, CODE 4, PG 215, SYSTEM CHECKED May 12, 1996 · N8923E · Doug DC931 · Central WarningSDR 9606249929Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Mar 17, 1996 · N8923E · Doug DC931 · Emergency LightingSDR 9606089929Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND ALL OVERWING EXIT EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL.Mar 13, 1996 · N8923E · Doug DC931 · Emergency LightingSDR 9600249929Power Supply · inoperativeDURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD.Jan 8, 1996 · N8923E · Doug DC931 · Emergency LightingSDR 9600239929Battery · dischargedDURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD.Jan 5, 1996 · N8923E · Doug DC931 · Emergency LightingSDR 9518079929Windshield · crackedMSP-YQR - DURING CRUISE AT FL350, THE FIRST OFFICER'S OUTER WINDSHIELD CRACKED. ACFT RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED THE WINDSHIELD AND WINDOW HEAT CONTROLLER, CHECKED OK.Nov 14, 1995 · N8923E · Doug DC931 · Flight Compartment WindowsSDR 9518259929Boost Pump · malfunctionedDURING CLIMB, FUEL WAS PUMPING INTO RIGHT FUEL TANK AND WAS UNABLE TO CROSSFEED FUEL WITH FUEL IN CENTER TANK. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSTALLED NEW BOOST PUMP VOLUTE AND OPERATIONAL CHECK GOOD.Nov 9, 1995 · N8923E · Doug DC931 · Fuel Boost PumpSDR 9515049929Engine · low powerDURING TAKEOFF, THE NR 1 ENGINE DID NOT REACH TAKEOFF POWER. ABORTED TAKEOFF AND RETURNED TO THE GATE. RERIGGED AND TRIMMED BOTH ENGINES AND OPERATIONAL CHECK GOOD.Oct 1, 1995 · N8923E · Doug DC931 · Fuel Controlling SystemSDR 9513689929Circuit Breaker · poppedDURING APPROACH INTO DTW, FLAPS INDICATED AN ASYMMETRICAL CONDITION ON FLAP EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND ACCOMPLISHED AN UNEVENTFUL LANDING USING SLATS ONLY. FOUND LEFT INSTRUMENT TRANSFORMER CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, CYSep 2, 1995 · N8923E · Doug DC931 · Trailing Flap Position Indicating SystemSDR 9513189929Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR CUTOUT, LOWER INTERNAL DOUBLER BENEATH THE SEAL DEPRESSOR. REPAIRED PER EA 99-94734.Jul 27, 1995 · N8923E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9513169929Skin · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN FS 197 AT LONGERON 22L. REPAIRED SKIN PER EA 99-94700.Jul 13, 1995 · N8923E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9513159929Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 30 AT FS 813. REPAIRED LONGERON PER EA 99-97390.Jul 12, 1995 · N8923E · Doug DC931 · Fuselage Main, Longeron/Stringer
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