N268UE, cancelled Dec 19, 2005

Service difficulty reports · 94

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 = 'N268UE' AND deregistration_id = 'N268UE-2005-12-19'
  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 SWIA200516008Seat Track · corrodedLT SIDE CABIN FLOOR SEAT TRACK FWD END HAS CORROSION, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FORWARD END OF LT SIDE CABIN FLOOR SEAT TRACK IAW EMB120 MM 53-01-05.Nov 4, 2005 · N268UE · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200516007Seat Track · corrodedLT SIDE FWD SHORT SEAT TRACK CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT SIDE FWD SHORT SEAT TRACK IAW EMB120 MM 53-01-05.Nov 4, 2005 · N268UE · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200515762Light · inoperativeEMERGENCY LIGHT 1ST FRONT ONE ON GROUND STRIP OUT. REPLACED 1ST FRONT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.Oct 25, 2005 · N268UE · Emb EMB120ER · Emergency LightingSDR SWIA200515643Annunciator · malfunctionedNUMEROUS FLAP MALFUNCTIONS -DISAGREEMENT ON LANDING APPROACH, CONTROL FAULT ON TAXI. REPLACED FLAP ANNUNCIATOR, OPERATIONAL CHECK GOOD.Oct 1, 2005 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200515577Selector · malfunctionedCREW REPORTED AN INTERMITTENT FLAP CONTROL FAULT. REPLACED FLAP CONTROL HANDLE ASSY. OPERATIONAL CHECK GOOD IAW 27-50-00.Sep 19, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200515348Actuator · malfunctionedFLAP CONTROL FAULT DURING EXTENSION. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.Jul 24, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200515267Control Unit · malfunctionedFLAP DISAGREEMENT WHEN FLAPS WERE SELECTED TO 45 DEGREES. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00.Jul 7, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200514673Rod End · out of adjustFLAP DISAGREEMENT OCCURRED WHEN SELECTING FLAPS FROM 25 DEGREES TO 45 DEGREES. LUBED LEFT AND RIGHT OUTBOARD FLAP ROLLERS, CLEANED FLAP TRACKS, ADJUSTED LEFT FLAP ACTUATOR ROD END IN IAW MM 27-50-04, OPERATIONAL CHECK GOOD IAW MM 27-50-00.Mar 2, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200514622Annunciator · malfunctionedON APPROACH, WHEN SELECTING FLAPS, RECEIVED CONTROL FAULT WITH FLAP DISAGREE. REMOVED AND REPLACED ANNUNCIATOR ASSY, OPERATIONAL CHECK GOOD.Feb 17, 2005 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200414317Actuator · failedINBOARD CONTROL FAULT, ASYMMETRY FLAPS SETTING 25. REMOVED AND REPLACED RT INBOARD FLAP ACTUATOR ASSY WITH SERVICEABLE UNIT IAW 27-50-00, OPERATIONAL CHECK GOOD.Dec 26, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200414264Actuator · malfunctionedFLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT OUTBOARD FLAP ACTUATOR, FLAP SELECTOR LEVER AND FLAP CONTROL UNIT IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD. PN 320300-1007 SN OFF 1113PN 120-64207-615 SN OFF 280040-316 PN OFF 307500-1017 SN OFF 0216.Dec 15, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200414170Actuator · malfunctionedWHEN FLAPS ARE RETRACTED INTERMITTENT CONTROL FAULT. REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.Dec 4, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200414046Actuator · malfunctionedNACELLE FLAPS CREATE CONTROL FAULT - DO NOT EXTEND WITH INBOARD AND OUTBOARD FLAPS. MEGGED ALL FLAP ACTUATORS CONNECTORS IAW EMB MM 27-50-00. REPLACED FLAP ANNUNCIATOR. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE ACTUATOR PER MM 27-50-Nov 1, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200414025Control Unit · malfunctionedCONTROL FAULT WITH ASSOCIATED MAP WARNING LIGHTS CAME ON DURING TAXI AND ONCE DURING APPROACH. REPLACED FCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.Oct 24, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200414003Actuator · malfunctionedRECEIVED FLAP CONTROL FAULTS. REPLACED RIGHT NACELLE ACTUATOR WITH SERVICEABLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD.Oct 22, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200413921Actuator · malfunctionedFLAP CONTROL FAULT WITH THE INBOARD PAIR FLASHING. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.Oct 11, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200413888Connector · dirtyAFTER SELECTING FLAPS 15 DEGREES, FLAP WARNING CONTROL FAULT ASSOC WITH FLAP AND ADV SWS ON MAP PANEL. CLEANED FLAP TRACKS AND CONNECTORS. ALL SYSTEM'S OPERATIONAL CHECK GOOD.Oct 1, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200413638Stringer · crackedLEFT HAND WING STRINGER 10 CRACKED BY RIB 5. ITEM FOUND AT C-CHECK.Jul 29, 2004 · N268UE · Emb EMB120ER · Wing, Longeron/StringerSDR SWIA200413895Floor Support · crackedLEFT FLOOR PROP AT FRAME 13 CRACKED. REPAIRED LEFT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10 PAGES 214 - 220.Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA200413894Frame · crackedRIGHT FLOOR PROP AT FRAME 13 CRACKED. ITEM FOUND AT C-CHECK. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10.Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, FrameSDR SWIA200413893Rib · crackedAFT OF DV CAPTAIN'S SIDE FRAME 13 HAS CRACKED RIB (MARKED). ITEM FOUND AT C-CHECK. REMOVED AND REPLACED CRACKED RIB ON FRAME 13 BEHIND CAPTAIN'S DV WINDOW WITH A SERVICEABLE UNIT.Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, Longeron/StringerSDR SWIA200413892Stringer · crackedLEFT WING FUEL CELL STRINGER CRACKED FORWARD OF INBOARD DEFUEL PANEL (MARKED). ITEM FOUND AT C-CHECK. COMPLIED WITH LEFT WING STRINGER NR 10 BETWEEN RIB NR 5 AND RIB NR 6 REPAIR PER SRM 57-20-03.Jul 24, 2004 · N268UE · Emb EMB120ER · Wing, Longeron/StringerSDR SWIA200413891Window Frame · crackedF/O'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON F/O'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED.Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, StructureSDR SWIA200413890Window Frame · crackedCAPTAIN'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON CAPTAIN'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED.Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, StructureSDR SWIA200413437Actuator · malfunctionedREPEATEDLY RECEIVE FLAP DISAGREEMENT WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW EMB 120 MM 27-50-09. OPERATIONAL CHECK GOOD.Jun 13, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200413090Computer · malfunctionedWHEN AUTOPILOT IS SELECTED TO FIRST OFFICER'S SIDE, AUTOPILOT TRIES TO CAPTURE LOCALIZER WHEN STILL FULL SCALE (AT LEAST 1.5 MILES OFF COURSE). REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD.Mar 26, 2004 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200412875Computer · malfunctionedON ROTATION AUTO PILOT FAIL & TRIM FAIL, MAP ILLUMINATED WITH ASSOCIATED TRIPLE CHIME AND AURAL WARNING. BOTH FCP'S SHOWED TRIM AND AP WARNINGS. AUTOPILOT PANEL INDICATED T, AP, R, E, TRIM. WOULD NOT RESET. CAPTAIN'S EADI SHOWED FD. REMOVED AND REPLACED NFeb 6, 2004 · N268UE · Emb EMB120ER · Integrated Flight SystemSDR SWIA200412820Support · crackedA 7 INCH CRACK IN RIGHT WING INBOARD LEADING EDGE SUPPORT. DISCOVERED DURING LINE INSPECTION. REPLACED RIGHT WING INBOARD LEADING EDGE INBOARD SUPPORT IAW SRM 51-40-02.Jan 29, 2004 · N268UE · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200412791Computer · malfunctionedON TWO OCCASIONS THE YAW DAMPNER CAPTAIN'S SIDE DISENGAGED, HOWEVER THE AUTO PILOT REMAINS ON EVEN AFTER LANDING THEN TURNING OFF THE AUTO PILOT, YAW DISENGAGED REMAINS ILLUMINATED. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKS GOOD PER MM 22-11-00.Jan 14, 2004 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200312709Servo · malfunctionedINFLIGHT GOT TRIM FAIL LIGHT ON FCP AND AURAL WARNING, PERFORMED QRH PROCEDURE, STILL GOT TRIM FAIL. ELECTRIC TRIM DOES NOT WORK, MANUAL TRIM WORKS FREE AND SMOOTH. REPLACED PITCH TRIM SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-11-00.Dec 20, 2003 · N268UE · Emb EMB120ER · Autopilot Trim ServoSDR SWIA200312652Control Box · malfunctionedCAPTAIN'S AND FIRST OFFICER'S AUTOPILOT INOP. REPLACED AP TRANSFER BOX AS REQUIRED. SYSTEM OPS CHECK GOOD IAW CH 22-10-00 EMB 120 MM.Dec 4, 2003 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200312553Computer · malfunctionedFD FLAG ON F/O ADI. CANNOT ENGAGE YAW WITH AP TRANSFER SELECT ON F/O SIDE. REPLACED NR 1 APC-69B AUTOPILOT COMPUTER. OPS CHECK GOOD AT THIS TIME.Oct 23, 2003 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200312456Actuator · malfunctionedRECEIVED FLAP CONTROL FAULT MULTIPLE TIMES EN ROUTE. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-00. OPS AND LEAK CHECKS GOOD. S/N OFF: 0214Sep 28, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200312373Computer · malfunctionedF/O'S A/P - F/D INTERMITTENTLY DISCONNECTED INFLIGHT WITH ASSOCIATE A/P FAILED. REPLACED NR 2 A/P COMPUTER. INSTALLED NEW PINS/SOCKETS ON PITCH TRANSFER RELAYS K0311, K0310, K0312 AND K0256. INSTALLED NEW RELAY SOCKETS FOR RELAYS K0310 AND K0312 AND REPLACEAug 28, 2003 · N268UE · Emb EMB120ER · Autopilot ComputerSDR SWIA200312363Computer · malfunctionedDURING CLIMB AND DESCENT FLIGHT DIRECTOR V-BARS BECAME ERRATIC AND AP FOLLOWED ERRATIC MOVEMENTS. BOTH WORKED NORMALLY DURING CRUISE. REPLACED CAPTAIN'S AHRS COMPUTER AND REPAIRED WIRING TO NR 2 DPU FAN CONNECTOR. BOTH AUTOPILOTS AND FLIGHT DIRECTOR SYSTEMSAug 26, 2003 · N268UE · Emb EMB120ER · Integrated Flight SystemSDR SWIA200312275Control Unit · malfunctionedON THE GROUND FLAP AND ADVANCED SWS ON MAP ILLUMINATED WITH CONTROL FAULT ON FLAP PANEL AND SECOND NAC BAR FLASHING. REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.Aug 19, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200312274Servo · malfunctionedDURING FLIGHT CONTROL COLUMNS BEGIN TO OSCILLATE FOLLOWED BY AUTOPILOT FAIL ON MAP AND AP ON FCP. HAPPENED ON BOTH CAPT AND FO SIDE. REPLACED PITCH DATA RELAYS K0312 & K0256 (CAPT'S SIDE). REPLACED AILERON SERVO AND AP TRANSFER BOX. AP AND AP TRANSFER OPS Aug 19, 2003 · N268UE · Emb EMB120ER · Autopilot Main ServoSDR SWIA200312228Control Handle · malfunctionedCONTROL FAULT ON NACELLE FLAPS. REPLACED FLAP CONTROL HANDLE. OPS CHECK GOOD. SN OFF: 200513-308Aug 4, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200312227Pin · backed outAUTOPILOT DISCONNECTED IN FLIGHT WITH 'AUTOPILOT FAIL' ON MAP AND 'AP' ON AUTOPILOT CONTROL PANEL. WHEN AP DISCONNECTED, A/C FELT OUT OF TRIM IN ROLL. DISCONNECT OCCURED WITH FO FLYING. MEL 22-11-1A. FOUND PIN 12 AT J2 OF NR 2 AUTO PILOT COMPUTER RACK RECEAug 3, 2003 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200312146Roller · damagedAFTER TAKEOFF, FLAPS WOULD NOT RETRACT TO FULL UP POSITION. QRH PROCEDURE FOLLOWED BUT WITH NO RESULT. DISAGREEMENT OBSERVED. REPLACED ROLLER AND BRACKET ON LT OUTBOARD FLAP GAP FAIRING.Jun 27, 2003 · N268UE · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200312075Connector · failedINBOARD FLAPS DISAGREEMENT ON LIGHT BAR, CONTROL FAULT ILLUMINATED ON O/H PANEL, FLAP INDICATOR SHOWED ZERO DEGREES (ALL DURING TAXI OUT). REPLACED CONNECTOR P1756 AND P1757 AS REQUIRED. ALSO MEGGED SYSTEM WIRING. NO DEFECTS NOTED. SYSTEM OPS CHECK GOOD IAJun 7, 2003 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200312000Actuator · malfunctionedCREW REPORTS CONTROL FAULT ON INBOARD FLAPS.REMOVED AND REPLACED RT IB FLAP ACTUATOR IAW 27-50-07. REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW 27-50-01. PN OFF/ON 120-64207-615 SN OFF 280040-316. FUNCTIONAL TEST AND OPS CHECK GOOD.May 19, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200311965Control Unit · malfunctionedON INITIAL POWER UP OF THE AIRCRAFT, A FLAP CONTROL FAULT CAME ON AND WOULD NOT RESET UNTIL THE BIT AND THE PST BUTTONS WERE PUSHED. REMOVED AND REPLACED VERSION II FCU AND ANNUNCIATOR UNIT WITH SERVICEABLE VERSION I FCU AND ANNUNCIATOR UNIT. OPS CHECK GOODMay 10, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200311871Control Unit · malfunctionedFLAP CONTROL FAULT IN CRUISE. ONE SEGMENT NAC FLASHING, REST OK. FLAP CONTROL FAULT WHEN 25 DEGREES OF FLAPS SELECTED AT APPROXIMATELY 15 DEGREES OF FLAPS, REMAINDER OK. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB120 MM 27-50-06. OPS CHECK GOOD.Apr 10, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200311864Computer · malfunctionedON TAKEOFF ROLL AT 90 KTS (INTERMITTENTLY) AND LANDING ROLL TRIM FAIL ILLUMINATION ON MAP AND MASTER CAUTION SYSTEM. REMOVED FIRST OFFICER'S AUTOPILOT COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECK GOOD.Mar 30, 2003 · N268UE · Emb EMB120ER · Autopilot SystemSDR SWIA200311824Light · inoperativeFLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW THREE INOP. REPLACED A BAD FUSE. OPS CHECK GOOD.Mar 4, 2003 · N268UE · Emb EMB120ER · Emergency LightingSDR SWIA200211450Servo · malfunctionedDISTINCT BUMP OR GRAB FELT IN LT RUDDER WHEN LEFT RUDDER IS PRESSED. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO IAW MM 22-10-05. SYSTEM TESTS GOOD.Nov 8, 2002 · N268UE · Emb EMB120ER · Autopilot Main ServoSDR SWIA200211449Wire Harness · malfunctionedLANDING GEAR WOULD NOT EXTEND, USED ELECTRICAL OVERRIDE. RH MLG GREEN ''A'' LIGHT REMAINS ON. REMOVED AND REPLACED RIGHT MAIN DOWNLOCK ''A'' PROXIMITY SENSOR HARNESS IAW MM 32-61-01. OPS CHECK GOOD.Nov 8, 2002 · N268UE · Emb EMB120ER · Landing Gear System WiringSDR SWIA200211234Line · leakingLOST OIL PRESSURE AFTER TAKEOFF ON UPWIND LEG. REDUCED POWER. LANDED ON RWY 10, SHUT DOWN ENGINE AFTER LANDING. FOUND LOWER OIL COOLER HOSE ON LEFT ENGINE TO HAVE A HOLE. REMOVED AND REPLACED LEFT ENGINE OIL COOLER HOSE IAW MM 79-21-05. DOWNLOAD AND REVIESep 18, 2002 · N268UE · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)SDR SWIA200211144Computer · malfunctionedAUTOPILOT DID AN UNCOMMANDED ROLL TO THE LEFT WHEN SELECTED TO CAPTAIN'S SIDE. DISENGAGED AND RE-ENGAGED AUTOPILOT AND IT HAPPENED AGAIN. CAPTAIN'S FLIGHT DIRECTOR COMMANDED MULTIPLE UNWANTED PITCH CHANGES WHILE IN LEVEL FLIGHT (AUTOPILOT WAS NOT ENGAGED). Aug 19, 2002 · N268UE · Emb EMB120ER · Integrated Flight System
Back to N268UE, cancelled Dec 19, 2005