# Service difficulty reports: N13969, cancelled Jul 31, 2021

A list on [N13969, cancelled Jul 31, 2021](https://openairdocs.org/deregistered/N13969-2021-07-31.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 3 · 105 reports

- [SDR ASOA20141030122](https://openairdocs.org/sdr/ASOA20141030122.md): Light · damaged · Oct 30, 2014 · N13969 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140806253](https://openairdocs.org/sdr/ASOA20140806253.md): Beam · corroded · Aug 6, 2014 · N13969 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140806252](https://openairdocs.org/sdr/ASOA20140806252.md): Stringer · cracked · Aug 6, 2014 · N13969 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 13. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140805250](https://openairdocs.org/sdr/ASOA20140805250.md): Hinge Fitting · worn · Aug 5, 2014 · N13969 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK THE LT ELEVATOR INBD HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140805249V](https://openairdocs.org/sdr/ASOA20140805249V.md): Fitting · cracked · Aug 5, 2014 · N13969 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK, THE RT OTBD FLAP INBD ROOT FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5750-01628. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140805248V](https://openairdocs.org/sdr/ASOA20140805248V.md): Yoke · worn · Aug 5, 2014 · N13969 · Emb EMB145LR · Engine Mount Section
  > DURING C-CHECK THE RT ENGINE FWD UPPER YOKE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE PERFORMED A REAMING REPAIR AND INSTALLED AN OVERSIZED BUSHING IAW SRM 54-50-16. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140725234](https://openairdocs.org/sdr/ASOA20140725234.md): Yoke · cracked · Jul 25, 2014 · N13969 · Emb EMB145LR · Engine Mount Section
  > DURING C-CHECK, THE RT ENGINE FORWARD LOWER MOUNT YOKE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE YOKE IAW EC5450-01094. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140724233](https://openairdocs.org/sdr/ASOA20140724233.md): Skin · cracked · Jul 24, 2014 · N13969 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE FORWARD FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE TOP OF THE WINDSHIELD AND LT DV WINDOW LATERAL POST. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01804. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140314043](https://openairdocs.org/sdr/ASOA20140314043.md): Flapper Bearing · leaking · Mar 14, 2014 · N13969 · Emb EMB145LR · Aircraft Fuel Distribution System
  > DURING TAKEOFF ROLL, A FUEL LEAK WAS REPORTED COMING FROM THE LT WING WHERE THE OTBD FLAP MEETS THE AILERON. THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R THE OTBD FLAPPER VALVE IN THE LT WING. LEAK CHECKS PERFORMED S
- [SDR ASOA20131221141](https://openairdocs.org/sdr/ASOA20131221141.md): Charger · inoperative · Dec 21, 2013 · N13969 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131003075](https://openairdocs.org/sdr/ASOA20131003075.md): Seal · faulty · Oct 3, 2013 · N13969 · Emb EMB145LR · Cargo/Baggage Doors
  > CREW REPORTED A SLOW CABIN PRESSURE LOSS AT FL 310. CABIN ALTITUDE WENT UP TO 14,600 FT IN EMERGENCY DESCENT. MX REPLACED THE CARGO DOOR TRIM SEAL. CABIN OXYGEN GENERATORS REPLACED. OPS CHECKED PRESSURIZATION SYS GOOD. ACFT RELEASED TO SERVICE.
- [SDR ASOA20130510046](https://openairdocs.org/sdr/ASOA20130510046.md): Window Frame · cracked · May 10, 2013 · N13969 · Emb EMB145LR · Fuselage Main, Structure
  > DURING POST FLIGHT WALKAROUND, CREW REPORTED FINDING A FUSELAGE SKIN CRACK ON THE LT DV WINDOW UPPER FRAME AREA. MX PERFORMED REPAIR ON UPPER BEAM ATTACHED TO DV WINDOW AND WINDSHIELD POST ON LT SIDE IAW SRM 51-40-02. SHV MX ALSO PERFORMED REPAIR ON LT DV
- [SDR ASOA20130324020C](https://openairdocs.org/sdr/ASOA20130324020C.md): Controller · faulty · Mar 24, 2013 · N13969 · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > THE CREW REPORTED A BURNING ELECTRICAL ODOR ON DESCENT IN COCKPIT/CABIN ASSOCIATED WITH WINDSHIELD HEAT NOT WORKING. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD TEMP CONTROLLER. OPS CHECKS WERE GOOD.
- [SDR ASOA20121004089](https://openairdocs.org/sdr/ASOA20121004089.md): Control Unit · faulty · Oct 4, 2012 · N13969 · Emb EMB145LR · Landing Gear Brake System
  > ON TAXI, BRAKES REQUIRED 50-60 PERCENT ACTUATION ON PEDALS TO ENGAGE FOLLOWED BY BRAKE DEGRADED MESSAGE WHICH CLEARED. ON GATE RETURN, BRAKES COMPLETELY FAILED ABOVE 5 KTS. AND REQUIRED USE OF EMERGENCY BRAKE. MX R & R THE BRAKE CONTROL UNIT WITH TAXI AND OP
- [SDR ASOA20120822075](https://openairdocs.org/sdr/ASOA20120822075.md): Stringer · corroded · Aug 22, 2012 · N13969 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 21L CORRODED FR. 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120822074](https://openairdocs.org/sdr/ASOA20120822074.md): Stringer · corroded · Aug 22, 2012 · N13969 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > STRINGER 21R CORRODED FR 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120822073](https://openairdocs.org/sdr/ASOA20120822073.md): Support · corroded · Aug 22, 2012 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LOWER CARGO DOOR CUT OUT SUPPORT CORRODED. R & R CARGO DOOR LOWER CUT OUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120822072](https://openairdocs.org/sdr/ASOA20120822072.md): Support · corroded · Aug 22, 2012 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LT EMERGENCY EXIT LOWER SUPPORT CORRODED. REPAIRED LT EMERGENCY EXIT IAW EC5220-01041. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120822071](https://openairdocs.org/sdr/ASOA20120822071.md): Skin · corroded · Aug 22, 2012 · N13969 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SERVICE DOOR CUT OUT HAS CORROSION AT FR 22. REPAIRED IAW EC5310-01373. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120117006](https://openairdocs.org/sdr/ASOA20120117006.md): Battery Pack · inoperative · Jan 17, 2012 · N13969 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED ROW 1-7 EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED, CHARGED, AND RE-INSTALLED NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA206](https://openairdocs.org/sdr/C2XA11IA206.md): Light · malfunctioned · Sep 10, 2011 · N13969 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2127, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE ROW 123 A & C SIDE PANEL EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI140](https://openairdocs.org/sdr/C2XA11RI140.md): Track · obstructed · Aug 22, 2011 · N13969 · Emb EMB145LR · Flight Compartment Windows
  > FLIGHT 6029 - IAD - FLIGHT CREW REPORTED FO DV WINDOW NOT CLOSED IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. IAD MX FOUND DEBRIS ON THE DV WINDOW TRACK. MX REMOVED DEBRIS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO
- [SDR C2XA11RI138](https://openairdocs.org/sdr/C2XA11RI138.md): Anti-Ice Valve · inoperative · Aug 15, 2011 · N13969 · Emb EMB145LR · Airfoil Anti/De-ice System
  > FLIGHT 2169 - EWR - FLIGHT CREW REPORTED WING ANTI ICE FAIL DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED WING 1 ANTI ICE VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVI
- [SDR C2XA11TY047](https://openairdocs.org/sdr/C2XA11TY047.md): Relay · inoperative · Apr 20, 2011 · N13969 · Emb EMB145LR · Rudder Control System
  > RUDDER HARD OVER PROTECTION MESSAGE ON EICAS. R & R RELAY K0774. OPS CHECK GOOD. CLOSED
- [SDR C2XA10IA333](https://openairdocs.org/sdr/C2XA10IA333.md): Light · inoperative · Dec 10, 2010 · N13969 · Emb EMB145LR · Emergency Lighting
  > MCI - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI154](https://openairdocs.org/sdr/C2XA10RI154.md): Bracket · broken · Dec 7, 2010 · N13969 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 3134 - EWR - FLIGHT CREW REPORTED AFT EMERGENCY LIGHT BRACKET BROKEN. EWR MX REMOVED AND REPLACED BRACKET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10SH243](https://openairdocs.org/sdr/C2XA10SH243.md): Skin · cracked · Jul 20, 2010 · N13969 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2L-8L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02182. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA10SH242](https://openairdocs.org/sdr/C2XA10SH242.md): Skin · cracked · Jul 20, 2010 · N13969 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO HAVE CRACKS AT FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02182. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA10SH241](https://openairdocs.org/sdr/C2XA10SH241.md): Fitting · worn · Jul 20, 2010 · N13969 · Emb EMB145LR · Vertical Stabilizer Miscellaneous Structure
  > SHV - DURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 AT 12:00 POSITION WAS FOUND TO HAVE ELONGATED BOLT HOLES AND CAUSING FRETTING WITH ADJACENT SKIN PANELS. MAINTENANCE PERFORMED REPAIRS TO THAT AREA IAW EC5310-01317 AND EC5310-01521. THE AIRCRA
- [SDR C2XA10SH240](https://openairdocs.org/sdr/C2XA10SH240.md): Skin · corroded · Jul 20, 2010 · N13969 · Emb EMB145LR · Cargo/Baggage Doors
  > SHV - DURING C-CHECK THE CARGO DOOR LOWER INNER SKIN WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH239](https://openairdocs.org/sdr/C2XA10SH239.md): Stringer · corroded · Jul 20, 2010 · N13969 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01522. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH238](https://openairdocs.org/sdr/C2XA10SH238.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH237](https://openairdocs.org/sdr/C2XA10SH237.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH236](https://openairdocs.org/sdr/C2XA10SH236.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH235](https://openairdocs.org/sdr/C2XA10SH235.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH234](https://openairdocs.org/sdr/C2XA10SH234.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH233](https://openairdocs.org/sdr/C2XA10SH233.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH232](https://openairdocs.org/sdr/C2XA10SH232.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH231](https://openairdocs.org/sdr/C2XA10SH231.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH230](https://openairdocs.org/sdr/C2XA10SH230.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH229](https://openairdocs.org/sdr/C2XA10SH229.md): Floor Support · corroded · Jul 15, 2010 · N13969 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI084](https://openairdocs.org/sdr/C2XA10RI084.md): Unknown · odor · Jun 22, 2010 · N13969 · Emb EMB145LR · Air Distribution System
  > FLIGHT 3063 - EWR - FLIGHT CREW REPORTED BURNING PLASTIC SMELL DURING FLIGHT. EWR MX PERFORMED FIM TASK FOR ABNORMAL SMELL IN COCKPIT AND COULD NOT DUPLICATE ANY SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10IA114](https://openairdocs.org/sdr/C2XA10IA114.md): Unknown · malfunctioned · Apr 7, 2010 · N13969 · Emb EMB145LR · Smoke Detection
  > ATL - FLIGHT 2432, THE CREW REPORTED A BAGG SMOKE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED THE BAGG SMOKE DETECTOR, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT W
- [SDR C2XA10CL012](https://openairdocs.org/sdr/C2XA10CL012.md): Connector · corroded · Jan 26, 2010 · N13969 · Emb EMB145LR · Engine Exhaust System Wiring
  > DAY FLT 2234 THE CREW REPORTED A NR 2 T/R DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED AND TAXIED BACK TO THE GATE. MAINTENANCE PLACED THE T/R SYSTEM ON MEL AND RELEASED THE AIRCRAFT FOR SERVICE. NR 2 PYLON CONNECT P1770 WAS REPLACED AND OPERATIONAL CHECK
- [SDR C2XA09RI088](https://openairdocs.org/sdr/C2XA09RI088.md): Potentiometer · defective · May 2, 2009 · N13969 · Emb EMB145LR · Landing Gear Steering System
  > FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DISCONNECT TRIGGER AND BROUGHT ACFT TO STOP. CREW WAS UNABLE TO USE TILLER NOR CLEAN STEERING INOP ME
- [SDR C2XA09RI087](https://openairdocs.org/sdr/C2XA09RI087.md): Manifold · defective · May 2, 2009 · N13969 · Emb EMB145LR · Landing Gear Steering System
  > FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DISCONNECT TRIGGER AND BROUGHT ACFT TO STOP. CREW WAS UNABLE TO USE TILLER NOR CLEAN STEERING INOP ME
- [SDR C2XA09RI049](https://openairdocs.org/sdr/C2XA09RI049.md): Unknown · odor · Apr 3, 2009 · N13969 · Emb EMB145LR · Air Distribution System
  > FLIGHT 4932 - EWR - FLIGHT CREW REPORTED STRONG ODOR OF SMOKE IN THE COCKPIT SHORTLY AFTER INITIAL DESCENT. EWR MX RAN PACKS, PRESSURIZED AIRCRAFT, TURNED W/S HEAT ON AND HYDRAULIC PUMPS. NO SMELL WAS DETECTED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI050](https://openairdocs.org/sdr/C2XA09RI050.md): Unknown · odor · Apr 2, 2009 · N13969 · Emb EMB145LR · Air Distribution System
  > FLIGHT - 2554 - EWR-JAX - FLIGHT CREW DIVERTED TO SAV DUE TO LIGHTNING STRIKE ACCOMPANIED WITH STRONG BURNING SMELL IN COCKPIT. MX INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF LIGHTNING STRIKE. FLIGHT CREW RAN PNEUMATIC SYSTEMS AND COULD NOT DUPLICATE SMELL IN
- [SDR C2XA08TY104](https://openairdocs.org/sdr/C2XA08TY104.md): Light · inoperative · Sep 10, 2008 · N13969 · Emb EMB145LR · Emergency Lighting
  > ACFT WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED LIGHT IAW AMM 33-50-09. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. (K)
- [SDR C2XA08RI138](https://openairdocs.org/sdr/C2XA08RI138.md): Light · inoperative · Sep 8, 2008 · N13969 · Emb EMB145LR · Emergency Lighting
  > RIC MX DURING ROUTINE INSPECTION RIC MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. RIC MX R&R EMERGENCY LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N13969-2021-07-31/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 = 'N13969' AND deregistration_id = 'N13969-2021-07-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13969-2021-07-31/reports

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