# Service difficulty reports: N11109, cancelled Mar 10, 2026

A list on [N11109, cancelled Mar 10, 2026](https://openairdocs.org/deregistered/N11109-2026-03-10.md).

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

- [SDR ASOA202003314008](https://openairdocs.org/sdr/ASOA202003314008.md): Connector · detached · Mar 26, 2020 · N11109 · Emb EMB145XR · Light System Wiring
  > IAH - FLIGHT 4328, DURING MX INSPECTION THE LEFT HAND EXTERIOR FWD EMERGENCY LIGHT WAS FOUYND TO BE INOPERATIVE. MAINTENANCE REATTACHED CANNON PLUG P8561, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019121953072](https://openairdocs.org/sdr/ASOA2019121953072.md): Servo · faulty · Dec 15, 2019 · N11109 · Emb EMB145XR · Autopilot System
  > THE CREW REPORTED BAD VIBRATION IN THE YOKE AT FL360 AND.70 MACH. SLOWED AIRCRAFT TO.65 MACH VIBRATION DID NOT GO AWAY. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED ELEVATOR AUTOPILOT SERVO.OPERATIONAL CHECKS WERE GOO
- [SDR ASOA20190624033](https://openairdocs.org/sdr/ASOA20190624033.md): Entertain Sys · odor · Jun 20, 2019 · N11109 · Emb EMB145XR · Buffet/Galleys
  > FLIGHT 4324, THE CREW REPORTED A BURNT WIRE SMELL FROM THE CD AREA IN THE GALLEY. THE AIRCRAFT LANDED IN MFE WITHOUT INCIDENT WHERE MAINTENANCE DEACTIVATED THE CD PLAYER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE C
- [SDR ASOA201905094017](https://openairdocs.org/sdr/ASOA201905094017.md): Skin · corroded · May 9, 2019 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > IAH - DURING MAINTENANCE INSPECTION THE BELLY SKIN WAS FOUND TO BE CORRODED UNDER THE AFT RADIO ALTIMETER BASE. MAINTENANCE REMOVED THE CORROSION, CUT OUT THE DAMAGED SKIN AND PERFORMED A FILLER / DOUBLER REPAIR IN ACCORDANCE WITH TECHNICAL DISPOSITION ETD2019
- [SDR ASOA201801014001](https://openairdocs.org/sdr/ASOA201801014001.md): Smoke Detector · false indication · Jan 1, 2018 · N11109 · Emb EMB145XR · Smoke Detection
  > THE CREW REPORTED A LAVATORY SMOKE WARNING, DURING APPROACH AT 3000FEET. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA201704035030](https://openairdocs.org/sdr/ASOA201704035030.md): Door · out of adjust · Apr 3, 2017 · N11109 · Emb EMB145XR · Passenger/Crew Doors
  > PILOT REPORTED THE MAIN CABIN DOOR HARD TO OPEN. MX ADJUSTED THE DOOR TO FUSELAGE GAP AND OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20170329006V](https://openairdocs.org/sdr/ASOA20170329006V.md): Door Sill · corroded · Mar 29, 2017 · N11109 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LOWER BAGGAGE DOOR SILL BETWEEN FRAMES 65-68 CORRODED. REMOVED AND REPLACED IAW SRM 51-21-06. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20170329005](https://openairdocs.org/sdr/ASOA20170329005.md): Support · corroded · Mar 29, 2017 · N11109 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, TOILET DUMP VALVE SUPPORT FOUND CORRODED (EXTERNAL). REMOVED AND REPLACED THE DUMP VALVE SUPPORT IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151208059](https://openairdocs.org/sdr/ASOA20151208059.md): Bulb · inoperative · Dec 8, 2015 · N11109 · Emb EMB145XR · Emergency Lighting
  > MAINTENANCE DISCOVERED THE FORWARD LT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE R & R BULB WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150302022](https://openairdocs.org/sdr/ASOA20150302022.md): Unknown · odor · Mar 2, 2015 · N11109 · Emb EMB145XR · Air Distribution System
  > THE CREW REPORTED AN ELECTRICAL BURNING ODOR OF VARIOUS INTENSITIES THROUGHOUT THE FLIGHT WITH THE ODOR INCREASING ON FINAL. THE ACFT LANDED WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE ACFT WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20120803060V](https://openairdocs.org/sdr/ASOA20120803060V.md): Skin · cracked · Aug 4, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FRAME 77 SKIN CRACKED NEAR RIVET HEADS. MX PERFORMED REPAIR IAW EC5330-02080, REV A. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120803059](https://openairdocs.org/sdr/ASOA20120803059.md): Skin · cracked · Aug 4, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FRAME 79 SKIN CRACKED NEAR RIVET HEADS. MX PERFORMED REPAIR IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120803058](https://openairdocs.org/sdr/ASOA20120803058.md): Skin · cracked · Aug 4, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RT FRAME 78 SKIN CRACKED AROUND RIVET HEADS. MX PERFORMED REPAIR IAW EC5330-02501 REV ORIG. FILLER AND DOUBLER INSTALLED. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06 AND STRINGERS 5R-6R. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120803057](https://openairdocs.org/sdr/ASOA20120803057.md): Stringer · corroded · Aug 3, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Bulkhead
  > DURING C-CHECK, CORROSION ON STRINGER 21R AROUND RIVETS BETWEEN FRAMES 10-11. MX R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801055V](https://openairdocs.org/sdr/ASOA20120801055V.md): Skin · cracked · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RT FUSELAGE SKIN CRACKED AT FRAME 78 STRINGERS 5-6R. MX REPAIRED SKIN IAW EC5330-02501 REV ORIG., FILLER AND DOUBLER INSTALLLED. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801054V](https://openairdocs.org/sdr/ASOA20120801054V.md): Skin · cracked · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RT FUSELAGE SKIN CRACKED AT FRAME 77 BETWEEN STRINGERS 5-7R. MX REPAIRED RT FUSELAGE SKIN IAW EC5330-02501, REV ORIG, FILLER AND DOUBLER INSTALLED. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801053](https://openairdocs.org/sdr/ASOA20120801053.md): Skin · cracked · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, RT FUSELAGE SKIN CRACKED AT FRAME 77 BETWEEN STRINGERS 8-9R. MX REPAIRED FUSELAGE SKIN CRACKS IAW EC5330-02501, REV ORIG, FILLER AND DOUBLER INSTALLED. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20120801052](https://openairdocs.org/sdr/ASOA20120801052.md): Skin · damaged · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN DAMAGE AT FRAME 77 AND 78 BETWEEN STRINGER 5L AND 7L. MX PERFORMED REPAIR ON FUSELAGE SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801051](https://openairdocs.org/sdr/ASOA20120801051.md): Skin · damaged · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN DAMAGE AT FRAME 78 BETWEEN STRINGER 4L-5L. MX PERFORMED REPAIR ON FUSELAGE SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801050](https://openairdocs.org/sdr/ASOA20120801050.md): Skin · damaged · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN DAMAGED AT FRAME 77 BETWEEN STRINGER 4L AND 5L. MX PERFORMED REPAIR ON FUSELAGE SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120801049](https://openairdocs.org/sdr/ASOA20120801049.md): Skin · damaged · Aug 1, 2012 · N11109 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN DAMAGE AT FRAME 77 BETWEEN STRINGER 8L AND 9L. MX PERFORMED REPAIR ON SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120308037](https://openairdocs.org/sdr/ASOA20120308037.md): Inverter · inoperative · Mar 8, 2012 · N11109 · Emb EMB145XR · Emergency Lighting
  > DURING MX INSPECTION, THE LT EMERGENCY EXIT MARKER LIGHT AT THE AFT LT EMERGENCY EXIT HATCH WAS FOUND TO BE INOPERATIVE. MX R & R THE 4 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH390](https://openairdocs.org/sdr/C2XA10SH390.md): Bracket · corroded · Nov 11, 2010 · N11109 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK FWD LWR CENTER FUEL TUBE BRACKET HAS CORROSION (LEVEL 2 LOCAL) ON VENTRAL TANK. MAINTENANCE PERFORMED REPAIR ON FWD LWR CENTER FUEL TUBE BRACKET ON VENTRAL TANK IAW EC5320-01573. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA259](https://openairdocs.org/sdr/C2XA10IA259.md): Sleeve · leaking · Sep 19, 2010 · N11109 · Emb EMB145XR · Cabin Cooling System
  > IAH - FLIGHT 2020, DURING CLIMB THE CREW REPORTED A PACK 1 VALVE CLOSED MESSAGE ON EICAS. THE AIRCRAFT RETUIRNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED SLEEVE ON THE PACK ONE DUAL TEMP CONTROL VALVE, OPERATIONALLY AND LEAK C
- [SDR C2XA10IA248](https://openairdocs.org/sdr/C2XA10IA248.md): Smoke Detector · inoperative · Sep 8, 2010 · N11109 · Emb EMB145XR · Smoke Detection
  > FLIGHT 3006, DURING PRE-FLIGHT INSPECTION THE BAGGAGE SMOKE DETECTOR WOULD NOT RESET AFTER TESTING. MAINTENANCE REMOVED AND REPLACED THE FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA10IA247](https://openairdocs.org/sdr/C2XA10IA247.md): Detection Sys · malfunctioned · Sep 7, 2010 · N11109 · Emb EMB145XR · Smoke Detection
  > IAH - FLIGHT 2147, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS AND OVERHEAD LIGHT WHILE ON THE GROUND. THE CREW VERIFIED NO SMOKE PRESENT, RESET THE SMOKE DETECTION SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED OFR RETU
- [SDR C2XA10TY119](https://openairdocs.org/sdr/C2XA10TY119.md): Warning System · malfunctioned · Sep 1, 2010 · N11109 · Emb EMB145XR · Door Warning System
  > TYS - A/C WAS DEPARTING CLT WHEN THE BAGGAGE COMPARTMENT LIGHT CAME ON. THE CREW RESET THE SYSTEM AND NO FURTHER ACTION WAS REQUIRED.
- [SDR C2XA10CL079](https://openairdocs.org/sdr/C2XA10CL079.md): A/C Pack · malfunctioned · May 20, 2010 · N11109 · Emb EMB145XR · Cabin Cooling System
  > CLE FLT 2678 THE CREW REPORTED PACK NR 1 QUIT ON ITS OWN FOLLOWED BY A ELECTRICAL SMELL. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF PACK 1. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA10IA032](https://openairdocs.org/sdr/C2XA10IA032.md): Connector · dirty · Jan 21, 2010 · N11109 · Emb EMB145XR · Fire Protection System Wiring
  > IAH - FLIGHT 2758 THE CREW REPORTED THAT THE NUMBER TWO ENGINE FIRE DETECTOR FAIL MESSAGE CAME ON INTERMITTENTLY DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE CLEANED AND RE-SECURED THE CONNECTOR ON THE ENGINE ONE FIRE LOOP, OPE
- [SDR C2XA09CL114](https://openairdocs.org/sdr/C2XA09CL114.md): Valve · faulty · Sep 12, 2009 · N11109 · Emb EMB145XR · Pneumatic Distribution System
  > CLE - FLT 2592 - THE CREW REPORTED A BLEED 1/2 OVERTEMP MESSAGE ON THE ECIAS IN ICING CONDITIONS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED BOTH NR 1 AND NR 2 FAN AIR VALVES. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09RI082](https://openairdocs.org/sdr/C2XA09RI082.md): Light · inoperative · Apr 28, 2009 · N11109 · Emb EMB145XR · Emergency Lighting
  > RIC - DURING ROUTINE MAINTENANCE, MX FOUND LUMINESCENT EMERGENCY EXIT MARKER INOPERATIVE. MX REMOVED AND REPLACED LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI073](https://openairdocs.org/sdr/C2XA09RI073.md): Charger · inoperative · Apr 21, 2009 · N11109 · Emb EMB145XR · Emergency Lighting
  > RIC MX - DURING ROUTINE MAINTENANCE, RIC MX FOUND LT AND RT OVER THE WING EMERGENCY LIGHTS INOPERATIVE. MX REMOVED AND REPLACED NR 4 EMERGENCY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08IA186](https://openairdocs.org/sdr/C2XA08IA186.md): Solenoid · inoperative · Aug 4, 2008 · N11109 · Emb EMB145XR · Landing Gear Door Retract Section
  > IAH-FLIGHT 3044 - THE CREW REPORTED THAT THE NOSE GEAR DOORS WOULD NOT CLOSE. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS AP
- [SDR C2XA08IA0132](https://openairdocs.org/sdr/C2XA08IA0132.md): Control Module · inoperative · May 27, 2008 · N11109 · Emb EMB145XR · Passenger Compartment Lighting
  > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT HALF OF THE CABIN LIGHTS WERE INOP, AND A BURNING SMELL WAS PRESENT. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPRO
- [SDR C2XA07IA231](https://openairdocs.org/sdr/C2XA07IA231.md): Audio Panel · burned · Nov 12, 2007 · N11109 · Emb EMB145XR · Communications System
  > IAH - FLIGHT 2470, DURING CLIMB THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PILOTS DIGITAL AUDIO PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS,
- [SDR C2XA07RI093](https://openairdocs.org/sdr/C2XA07RI093.md): Connector · disconnected · Nov 3, 2007 · N11109 · Emb EMB145XR · Light System Wiring
  > RIC - DURING ROUTINE MAINTENANCE, MX FOUND FORWARD AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX RECONNECTED CONNECTOR P8525 ABOVE FORWARD CABIN CEILING PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07SH081](https://openairdocs.org/sdr/C2XA07SH081.md): Floorbeam · corroded · Oct 4, 2007 · N11109 · Emb EMB145XR · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK CORROSION AROUND NUT PLATE ON RIGHT OMEGA BEAM AT FR23. MAINTENANCE REPAIRED RT OMEGA BEAM AT FR 23 AROUND NUT PLATE IAW EC5320-01228 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA07IA162](https://openairdocs.org/sdr/C2XA07IA162.md): Proximity Switch · inoperative · Jul 5, 2007 · N11109 · Emb EMB145XR · Landing Gear Door Retract Section
  > IAH - FLIGHT 2771, THE CREW REPORTED A LOUD WIND NOISE FROM THE FRONT GEAR DOOR AREA BEGINNING AT CRUISE AT 35,000 FEET. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SEQUENCE PROXIMITY SWITCH, OPERATIONALLY C
- [SDR C2XA07IA150](https://openairdocs.org/sdr/C2XA07IA150.md): Unknown · odor · Jun 23, 2007 · N11109 · Emb EMB145XR · Air Distribution System
  > FLIGHT 2023 - AFTER TAKEOFF, THE CREW NOTICED A FUEL SMELL WITH THE APU RUNNING THE AIR CONDITIONING PACKS. MAINTENANCE PERFORMED SYSTEM CHECKS OF THE APU BLEED SYSTEM AND AIR CONDITIONING PACKS. THE DISCREPANCY COULD NOT BE DUPLICATED AND THE DISCREPANCY WA
- [SDR C2XA07IA128](https://openairdocs.org/sdr/C2XA07IA128.md): Engine · shutdown · May 29, 2007 · N11109 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > AUS - FLIGHT 2081, THE CREW REPORTED AN UNCOMMANDED NR 1 ENGINE SHUTDOWN IN CRUISE. THE AIRCRAFT DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT W
- [SDR C2XA07TY024](https://openairdocs.org/sdr/C2XA07TY024.md): Connector · broken · May 7, 2007 · N11109 · Emb EMB145XR · Light System Wiring
  > TYS DURING A 3A SERVICE/ROUTINE CHECK, THE RIGHT FWD CABIN BULKHEAD EXIT SIGN WAS FOUND INOP. MAINTENANCE FOUND A BAD CONNECTOR. MAINTENANCE REPLACED THE CONNECTOR AND OPS CHECK WERE GOOD IAW EMB 145 SPWM. AIRCRAFT RELEASED BACK TO SERVICE.
- [SDR C2XA06IA200](https://openairdocs.org/sdr/C2XA06IA200.md): Inverter · inoperative · Dec 26, 2006 · N11109 · Emb EMB145XR · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE THE LEFT EMERGENCY EXIT LOWER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHT POWER INVERTER, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY.
- [SDR C2XA06IA129](https://openairdocs.org/sdr/C2XA06IA129.md): Wire · chafed · Aug 16, 2006 · N11109 · Emb EMB145XR · Landing Gear System Wiring
  > IAH - FLIGHT 2239 THE CREW REPORTED A LANDING GEAR AIR/GND FAILURE INDICATION AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A CHAFED WIRE ON THE RT TRAILING ARM WEIGHT IN WHEELS PROX SW
- [SDR C2XA03CL187](https://openairdocs.org/sdr/C2XA03CL187.md): Control Unit · failed · Nov 18, 2003 · N11109 · Emb EMB145XR · Stabilizer Control System
  > CLE FLIGHT 2169 THE CREW REPORTED THAT THE BACK-UP TRIM WAS INOP IN FLIGHT. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA03CL079](https://openairdocs.org/sdr/C2XA03CL079.md): Combustion Liner · wrong part · Mar 25, 2003 · N11109 · Emb EMB145 · Turbine Engine Combustion Section
  > 3/25/03 EXPRESS JET AIRLINES WAS NOTIFIED BY ROLLS ROYCE THAT AIRCRAFT 11109, NR 2 ENGINE HAD THE WRONG P/N COMBUSTION LINER INSTALLED AT THE FACTORY. THE AIRCRAFT WAS FERRIED TO CLEVELAND FOR A ENGINE CHANGE. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL
- [SDR C2XA02IA242](https://openairdocs.org/sdr/C2XA02IA242.md): Control Handle · intermittent · Nov 22, 2002 · N11109 · Emb EMB145 · Landing Gear Selector
  > THE CREW NOTED THAT THE LANDING GEAR WOULD NOT COME UP. AFTER USING QRH, GEAR CAME UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

## 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 = 'N11109' AND deregistration_id = 'N11109-2026-03-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N11109-2026-03-10/reports

---
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