# Service difficulty reports: N268UE, cancelled Dec 19, 2005

A list on [N268UE, cancelled Dec 19, 2005](https://openairdocs.org/deregistered/N268UE-2005-12-19.md).

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

Page 1 of 2 · 94 reports

- [SDR SWIA200516008](https://openairdocs.org/sdr/SWIA200516008.md): Seat Track · corroded · Nov 4, 2005 · N268UE · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > LT 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.
- [SDR SWIA200516007](https://openairdocs.org/sdr/SWIA200516007.md): Seat Track · corroded · Nov 4, 2005 · N268UE · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > LT 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.
- [SDR SWIA200515762](https://openairdocs.org/sdr/SWIA200515762.md): Light · inoperative · Oct 25, 2005 · N268UE · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHT 1ST FRONT ONE ON GROUND STRIP OUT. REPLACED 1ST FRONT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515643](https://openairdocs.org/sdr/SWIA200515643.md): Annunciator · malfunctioned · Oct 1, 2005 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating System
  > NUMEROUS FLAP MALFUNCTIONS -DISAGREEMENT ON LANDING APPROACH, CONTROL FAULT ON TAXI. REPLACED FLAP ANNUNCIATOR, OPERATIONAL CHECK GOOD.
- [SDR SWIA200515577](https://openairdocs.org/sdr/SWIA200515577.md): Selector · malfunctioned · Sep 19, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > CREW REPORTED AN INTERMITTENT FLAP CONTROL FAULT. REPLACED FLAP CONTROL HANDLE ASSY. OPERATIONAL CHECK GOOD IAW 27-50-00.
- [SDR SWIA200515348](https://openairdocs.org/sdr/SWIA200515348.md): Actuator · malfunctioned · Jul 24, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT DURING EXTENSION. REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515267](https://openairdocs.org/sdr/SWIA200515267.md): Control Unit · malfunctioned · Jul 7, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT WHEN FLAPS WERE SELECTED TO 45 DEGREES. REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00.
- [SDR SWIA200514673](https://openairdocs.org/sdr/SWIA200514673.md): Rod End · out of adjust · Mar 2, 2005 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP 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.
- [SDR SWIA200514622](https://openairdocs.org/sdr/SWIA200514622.md): Annunciator · malfunctioned · Feb 17, 2005 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating System
  > ON APPROACH, WHEN SELECTING FLAPS, RECEIVED CONTROL FAULT WITH FLAP DISAGREE. REMOVED AND REPLACED ANNUNCIATOR ASSY, OPERATIONAL CHECK GOOD.
- [SDR SWIA200414317](https://openairdocs.org/sdr/SWIA200414317.md): Actuator · failed · Dec 26, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > INBOARD CONTROL FAULT, ASYMMETRY FLAPS SETTING 25. REMOVED AND REPLACED RT INBOARD FLAP ACTUATOR ASSY WITH SERVICEABLE UNIT IAW 27-50-00, OPERATIONAL CHECK GOOD.
- [SDR SWIA200414264](https://openairdocs.org/sdr/SWIA200414264.md): Actuator · malfunctioned · Dec 15, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP 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.
- [SDR SWIA200414170](https://openairdocs.org/sdr/SWIA200414170.md): Actuator · malfunctioned · Dec 4, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > WHEN FLAPS ARE RETRACTED INTERMITTENT CONTROL FAULT. REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414046](https://openairdocs.org/sdr/SWIA200414046.md): Actuator · malfunctioned · Nov 1, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > NACELLE 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-
- [SDR SWIA200414025](https://openairdocs.org/sdr/SWIA200414025.md): Control Unit · malfunctioned · Oct 24, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > CONTROL FAULT WITH ASSOCIATED MAP WARNING LIGHTS CAME ON DURING TAXI AND ONCE DURING APPROACH. REPLACED FCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414003](https://openairdocs.org/sdr/SWIA200414003.md): Actuator · malfunctioned · Oct 22, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > RECEIVED FLAP CONTROL FAULTS. REPLACED RIGHT NACELLE ACTUATOR WITH SERVICEABLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413921](https://openairdocs.org/sdr/SWIA200413921.md): Actuator · malfunctioned · Oct 11, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WITH THE INBOARD PAIR FLASHING. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413888](https://openairdocs.org/sdr/SWIA200413888.md): Connector · dirty · Oct 1, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > AFTER 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.
- [SDR SWIA200413638](https://openairdocs.org/sdr/SWIA200413638.md): Stringer · cracked · Jul 29, 2004 · N268UE · Emb EMB120ER · Wing, Longeron/Stringer
  > LEFT HAND WING STRINGER 10 CRACKED BY RIB 5. ITEM FOUND AT C-CHECK.
- [SDR SWIA200413895](https://openairdocs.org/sdr/SWIA200413895.md): Floor Support · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LEFT FLOOR PROP AT FRAME 13 CRACKED. REPAIRED LEFT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10 PAGES 214 - 220.
- [SDR SWIA200413894](https://openairdocs.org/sdr/SWIA200413894.md): Frame · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, Frame
  > RIGHT FLOOR PROP AT FRAME 13 CRACKED. ITEM FOUND AT C-CHECK. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10.
- [SDR SWIA200413893](https://openairdocs.org/sdr/SWIA200413893.md): Rib · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, Longeron/Stringer
  > AFT 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.
- [SDR SWIA200413892](https://openairdocs.org/sdr/SWIA200413892.md): Stringer · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Wing, Longeron/Stringer
  > LEFT 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.
- [SDR SWIA200413891](https://openairdocs.org/sdr/SWIA200413891.md): Window Frame · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, Structure
  > F/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.
- [SDR SWIA200413890](https://openairdocs.org/sdr/SWIA200413890.md): Window Frame · cracked · Jul 24, 2004 · N268UE · Emb EMB120ER · Fuselage Main, Structure
  > CAPTAIN'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.
- [SDR SWIA200413437](https://openairdocs.org/sdr/SWIA200413437.md): Actuator · malfunctioned · Jun 13, 2004 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > REPEATEDLY 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.
- [SDR SWIA200413090](https://openairdocs.org/sdr/SWIA200413090.md): Computer · malfunctioned · Mar 26, 2004 · N268UE · Emb EMB120ER · Autopilot System
  > WHEN 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.
- [SDR SWIA200412875](https://openairdocs.org/sdr/SWIA200412875.md): Computer · malfunctioned · Feb 6, 2004 · N268UE · Emb EMB120ER · Integrated Flight System
  > ON 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 N
- [SDR SWIA200412820](https://openairdocs.org/sdr/SWIA200412820.md): Support · cracked · Jan 29, 2004 · N268UE · Emb EMB120ER · Wing Miscellaneous Structure
  > A 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.
- [SDR SWIA200412791](https://openairdocs.org/sdr/SWIA200412791.md): Computer · malfunctioned · Jan 14, 2004 · N268UE · Emb EMB120ER · Autopilot System
  > ON 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.
- [SDR SWIA200312709](https://openairdocs.org/sdr/SWIA200312709.md): Servo · malfunctioned · Dec 20, 2003 · N268UE · Emb EMB120ER · Autopilot Trim Servo
  > INFLIGHT 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.
- [SDR SWIA200312652](https://openairdocs.org/sdr/SWIA200312652.md): Control Box · malfunctioned · Dec 4, 2003 · N268UE · Emb EMB120ER · Autopilot System
  > CAPTAIN'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.
- [SDR SWIA200312553](https://openairdocs.org/sdr/SWIA200312553.md): Computer · malfunctioned · Oct 23, 2003 · N268UE · Emb EMB120ER · Autopilot System
  > FD 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.
- [SDR SWIA200312456](https://openairdocs.org/sdr/SWIA200312456.md): Actuator · malfunctioned · Sep 28, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > RECEIVED 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: 0214
- [SDR SWIA200312373](https://openairdocs.org/sdr/SWIA200312373.md): Computer · malfunctioned · Aug 28, 2003 · N268UE · Emb EMB120ER · Autopilot Computer
  > F/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 REPLACE
- [SDR SWIA200312363](https://openairdocs.org/sdr/SWIA200312363.md): Computer · malfunctioned · Aug 26, 2003 · N268UE · Emb EMB120ER · Integrated Flight System
  > DURING 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 SYSTEMS
- [SDR SWIA200312275](https://openairdocs.org/sdr/SWIA200312275.md): Control Unit · malfunctioned · Aug 19, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > ON 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.
- [SDR SWIA200312274](https://openairdocs.org/sdr/SWIA200312274.md): Servo · malfunctioned · Aug 19, 2003 · N268UE · Emb EMB120ER · Autopilot Main Servo
  > DURING 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
- [SDR SWIA200312228](https://openairdocs.org/sdr/SWIA200312228.md): Control Handle · malfunctioned · Aug 4, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > CONTROL FAULT ON NACELLE FLAPS. REPLACED FLAP CONTROL HANDLE. OPS CHECK GOOD. SN OFF: 200513-308
- [SDR SWIA200312227](https://openairdocs.org/sdr/SWIA200312227.md): Pin · backed out · Aug 3, 2003 · N268UE · Emb EMB120ER · Autopilot System
  > AUTOPILOT 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 RECE
- [SDR SWIA200312146](https://openairdocs.org/sdr/SWIA200312146.md): Roller · damaged · Jun 27, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flaps
  > AFTER 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.
- [SDR SWIA200312075](https://openairdocs.org/sdr/SWIA200312075.md): Connector · failed · Jun 7, 2003 · N268UE · Emb EMB120ER · Trailing Flap Position Indicating System
  > INBOARD 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 IA
- [SDR SWIA200312000](https://openairdocs.org/sdr/SWIA200312000.md): Actuator · malfunctioned · May 19, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Actuator
  > CREW 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.
- [SDR SWIA200311965](https://openairdocs.org/sdr/SWIA200311965.md): Control Unit · malfunctioned · May 10, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > ON 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 GOOD
- [SDR SWIA200311871](https://openairdocs.org/sdr/SWIA200311871.md): Control Unit · malfunctioned · Apr 10, 2003 · N268UE · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP 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.
- [SDR SWIA200311864](https://openairdocs.org/sdr/SWIA200311864.md): Computer · malfunctioned · Mar 30, 2003 · N268UE · Emb EMB120ER · Autopilot System
  > ON 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.
- [SDR SWIA200311824](https://openairdocs.org/sdr/SWIA200311824.md): Light · inoperative · Mar 4, 2003 · N268UE · Emb EMB120ER · Emergency Lighting
  > FLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW THREE INOP. REPLACED A BAD FUSE. OPS CHECK GOOD.
- [SDR SWIA200211450](https://openairdocs.org/sdr/SWIA200211450.md): Servo · malfunctioned · Nov 8, 2002 · N268UE · Emb EMB120ER · Autopilot Main Servo
  > DISTINCT 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.
- [SDR SWIA200211449](https://openairdocs.org/sdr/SWIA200211449.md): Wire Harness · malfunctioned · Nov 8, 2002 · N268UE · Emb EMB120ER · Landing Gear System Wiring
  > LANDING 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.
- [SDR SWIA200211234](https://openairdocs.org/sdr/SWIA200211234.md): Line · leaking · Sep 18, 2002 · N268UE · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)
  > LOST 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 REVIE
- [SDR SWIA200211144](https://openairdocs.org/sdr/SWIA200211144.md): Computer · malfunctioned · Aug 19, 2002 · N268UE · Emb EMB120ER · Integrated Flight System
  > AUTOPILOT 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).

Next page: https://openairdocs.org/deregistered/N268UE-2005-12-19/reports.md?page=2

## 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 = 'N268UE' AND deregistration_id = 'N268UE-2005-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N268UE-2005-12-19/reports

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