# Service difficulty reports: N14943, cancelled May 26, 2015

A list on [N14943, cancelled May 26, 2015](https://openairdocs.org/deregistered/N14943-2015-05-26.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 · 108 reports

- [SDR ASOA20131029193H](https://openairdocs.org/sdr/ASOA20131029193H.md): Drag Angle · cracked · Oct 29, 2013 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING 2A INSPECTION THE LT VERTICLE STAB TO FUSELAGE LT DRAG ANGLE WAS FOUND TO HAVE A 20MM CRACK AT FRAME 76. MAINTENANCE R & R THE AFFECTED LT DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131019188](https://openairdocs.org/sdr/ASOA20131019188.md): Light · inoperative · Oct 19, 2013 · N14943 · Emb EMB145EP · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, LEFT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226089](https://openairdocs.org/sdr/ASOA20130226089.md): Skin · corroded · Mar 7, 2013 · N14943 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK THE COCKPIT BELLY SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 18R-19L. MX R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226088](https://openairdocs.org/sdr/ASOA20130226088.md): Beam · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 BETWEEN STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226087](https://openairdocs.org/sdr/ASOA20130226087.md): Shear Tie · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226086](https://openairdocs.org/sdr/ASOA20130226086.md): Shear Angle · corroded · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226085](https://openairdocs.org/sdr/ASOA20130226085.md): Shear Angle · cracked · Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE RIB 1 SHEAR CLIP FROM FRAMES 40-45 WAS FOUND TO BE CRACKED. MX R & R THE SHEAR CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121126147](https://openairdocs.org/sdr/ASOA20121126147.md): Skin · cracked · Nov 26, 2012 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING MX INSPECTION, THE FUSELAGE SKIN AT FR 75 ON EITHER SIDE OF STRINGER 2R WAS FOUND TO HAVE TWO CRACKS ONE APPROX.039" AND 1 APPROX.157" LONG. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 12/02
- [SDR ASOA20121126146](https://openairdocs.org/sdr/ASOA20121126146.md): Skin · cracked · Nov 26, 2012 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING MX INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED ACROSS A RIVET HOLE APPROX 16MM IN LENGTH BETWEEN FRAME 77-78 JUST ABOVE STR 6R. MX INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121126145](https://openairdocs.org/sdr/ASOA20121126145.md): Skin · cracked · Nov 26, 2012 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120824076](https://openairdocs.org/sdr/ASOA20120824076.md): Engine · smoke · Aug 23, 2012 · N14943 · Emb EMB145EP · Engine (Turbine/Turboprop)
  > GROUND CREW REPORTED FLAMES FROM NR 1 ENGINE. ENGINE SMOKING 15 MIN AFTER SHUTDOWN. R & R 1 ENGINE IAW AMM 71-00-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120503066](https://openairdocs.org/sdr/ASOA20120503066.md): Smoke Detector · defective · May 3, 2012 · N14943 · Emb EMB145EP · Smoke Detection
  > THE CREW REPORTED A BAGGAGE SMOKE WARNING ON EICAS. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE FORWARD BAGGAGE SMOKE DETECTOR, OPS TESTED WITH NO
- [SDR C2XA11IA238](https://openairdocs.org/sdr/C2XA11IA238.md): Unknown · odor · Oct 17, 2011 · N14943 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 4586, THE CREW REPORTED WEIRD SMELL DURING ENGINE START. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE STARTS, OPERATIONALLY CHECKED BLEED SYSTEMS ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA287](https://openairdocs.org/sdr/C2XA10IA287.md): Engine · malfunctioned · Nov 9, 2010 · N14943 · Emb EMB145EP · Engine (Turbine/Turboprop)
  > FLIGHT 2561 THE CREW REPORTED A BURNING SMOKE SMELL IN THE CABIN WITH THE NUMBER TWO ENGINE, NUMBER 2 BLEED, AND NUMBER TWO PACK RUNNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY T
- [SDR C2XA10IA286](https://openairdocs.org/sdr/C2XA10IA286.md): Acm · seized · Nov 9, 2010 · N14943 · Emb EMB145EP · Cabin Cooling System
  > IAH - FLIGHT 2561, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON SHORT FINAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA10SH275](https://openairdocs.org/sdr/C2XA10SH275.md): Fitting · corroded · Aug 16, 2010 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5310-01505. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH274](https://openairdocs.org/sdr/C2XA10SH274.md): Floor Support · corroded · Aug 16, 2010 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 33-34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH273](https://openairdocs.org/sdr/C2XA10SH273.md): Floor Support · corroded · Aug 16, 2010 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24-25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH272](https://openairdocs.org/sdr/C2XA10SH272.md): Floor Support · corroded · Aug 16, 2010 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 22-23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01257. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH266](https://openairdocs.org/sdr/C2XA10SH266.md): Beam · corroded · Aug 11, 2010 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA117](https://openairdocs.org/sdr/C2XA10IA117.md): Controller · inoperative · Apr 11, 2010 · N14943 · Emb EMB145EP · Cabin Pressure Controller
  > MEM - FLIGHT 2249, DURING DESCENT THE CREW REPORTED THAT AUTO PRESSURIZATION FAILED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE CREW PLACED THE AUTO PRESSURIZATION ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT
- [SDR C2XA10IA104](https://openairdocs.org/sdr/C2XA10IA104.md): Sign · malfunctioned · Mar 25, 2010 · N14943 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2132, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EXIT SIGN AT SEAT 12C TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH106](https://openairdocs.org/sdr/C2XA10SH106.md): Relay · failed · Mar 23, 2010 · N14943 · Emb EMB145EP · Pneumatic Distribution System
  > FLT 2159 MEM-IAH DIVERT TO AEX - BLEED 1 LOW TEMP/ENG OPEN LIGHT NOT ILLUM IN ICING - SHV RECOVERY. MAINTENANCE PERFORMED ANTI-ICE OPERATIONAL CHECKS IAW EMB-145 AMM 30-00-00 (ALL OPS CHECK GOOD). ALSO, MAINTENANCE REMOVED AND REPLACED RELAY KO528 ON RT RELA
- [SDR C2XA10TY030](https://openairdocs.org/sdr/C2XA10TY030.md): Light · inoperative · Mar 2, 2010 · N14943 · Emb EMB145EP · Emergency Lighting
  > SEAT 12BC OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB145 AMM 33-50-07, OPS CHECK GOOD.
- [SDR C2XA10IA055](https://openairdocs.org/sdr/C2XA10IA055.md): Clamp · defective · Feb 5, 2010 · N14943 · Emb EMB145EP · Compressor Bleed Valve
  > IAH - FLIGHT 2069 THE CREW REPORTED A BLEED ONE LEAK DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD CLAMP ON THE NUMBER ONE ENGINE BLEED VALVE. OPERATIONAL AND LEAK CHECKS WERE COMPL
- [SDR C2XA10IA047](https://openairdocs.org/sdr/C2XA10IA047.md): Duct · leaking · Feb 1, 2010 · N14943 · Emb EMB145EP · Pneumatic Distribution System
  > IAH - FLIGHT 2277, THE CREW REPORTED A BLEED ONE LEAK MESSAGE DURING CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT CARGO WALL "T" DUCT, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED, A
- [SDR C2XA10IA041](https://openairdocs.org/sdr/C2XA10IA041.md): Thermostat · inoperative · Jan 28, 2010 · N14943 · Emb EMB145EP · Compressor Bleed Control
  > IAH - FLIGHT 2413 - THE CREW REPORTED A BLEED 1 LOW TEMP DURING ICING TEST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE BLEED THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE
- [SDR C2XA09IA313](https://openairdocs.org/sdr/C2XA09IA313.md): Inverter · inoperative · Dec 9, 2009 · N14943 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE IN THE REAR OF THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LAST INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR C2XA09IA180](https://openairdocs.org/sdr/C2XA09IA180.md): Proximity Switch · inoperative · Jul 15, 2009 · N14943 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2703 - DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER,
- [SDR C2XA09IA080A](https://openairdocs.org/sdr/C2XA09IA080A.md): Proximity Sensor · inoperative · Jul 15, 2009 · N14943 · Emb EMB145EP · Landing Gear Position and Warning
  > DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE LT MAIN GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER, OPERATIONALLY TESTED WITH NO DEFECTS, AND
- [SDR C2XA09IA022](https://openairdocs.org/sdr/C2XA09IA022.md): Battery Pack · discharged · Jan 23, 2009 · N14943 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING A-CK INSPECTION THE LT FORWARD WING BOX EMERGENCY LIGHT, PAX DOOR EMERGENCY LIGHT, AND EMERGENCY LIGHT ABOVE THE FORWARD F/A SEAT WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 1 EMERGENCY LIGHT BATTERY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS
- [SDR C2XA08IA173](https://openairdocs.org/sdr/C2XA08IA173.md): Unknown · odor · Jul 21, 2008 · N14943 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 2372 - THE FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM ROWS 8-10. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS SUBS
- [SDR C2XA08CL012](https://openairdocs.org/sdr/C2XA08CL012.md): Bleed Valve · faulty · Jan 24, 2008 · N14943 · Emb EMB145EP · Compressor Bleed Valve
  > BWI FLIGHT 2247 - THE CREW REPORTED A NR 1 ENGINE BLEED VALVE FAIL MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XAO8RI007](https://openairdocs.org/sdr/C2XAO8RI007.md): Generator · inoperative · Dec 26, 2007 · N14943 · Emb EMB145ER · AC Generator-Alternator
  > FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETU
- [SDR C2XA08RI006](https://openairdocs.org/sdr/C2XA08RI006.md): Gcu · inoperative · Dec 26, 2007 · N14943 · Emb EMB145ER · AC Regulator
  > FLT 3142 - EWR - CREW REPORTED APU GENERATOR AND GENERATOR NR 1 OFF BUSS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED APU GCU AND GENERATOR NR 1 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETU
- [SDR C2XA07RI104](https://openairdocs.org/sdr/C2XA07RI104.md): Wire · chafed · Dec 8, 2007 · N14943 · Emb EMB145ER · Light System Wiring
  > FLT 2616 - RIC - CREW REPORTED PAX DETECTED ELECTRIC TYPE OF SMOKE. RIC MX FOUND ELECTRIC EMERGENCY SIGN AT ROW 3BC WITH BARE WIRE EXPOSED. MX REPAIRED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07RI101](https://openairdocs.org/sdr/C2XA07RI101.md): Relay · failed · Nov 21, 2007 · N14943 · Emb EMB145ER · Smoke Detection
  > FLIGHT 2929 - EWR - CREW REPORTED BAGG SMOKE LIGHT ON, BUT NO VISUAL SMOKE IN CARGO BAY. EWR MX REMOVED AND REPLACED BAGG SMOKE TEST RELAY AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07SH083](https://openairdocs.org/sdr/C2XA07SH083.md): Floorbeam · corroded · Oct 13, 2007 · N14943 · Emb EMB145EP · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-13. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA07IA093](https://openairdocs.org/sdr/C2XA07IA093.md): Connector · loose · Apr 20, 2007 · N14943 · Emb EMB145EP · Light System Wiring
  > IAH - FLIGHT 2277, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WORKED INTERMITTENTLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA06IA127](https://openairdocs.org/sdr/C2XA06IA127.md): Power Supply · discharged · Jul 31, 2006 · N14943 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2415, THE CREW REPORTED THAT THE LT FUSELAGE EXTERIOR LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05IA116](https://openairdocs.org/sdr/C2XA05IA116.md): Inverter · inoperative · Oct 18, 2005 · N14943 · Emb EMB145EP · Light System Wiring
  > IAH - FLIGHT 2418, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LOWER AFT LEFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT
- [SDR C2XA05SH088](https://openairdocs.org/sdr/C2XA05SH088.md): Hinge · worn · Jul 21, 2005 · N14943 · Emb EMB145EP · Horizontal Stabilizer Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND HAT BUSHING HOUSING AT ATTACHMENT FITTING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I IS WORN. MAINTENANCE REPAIRED HAT BUSHING HOUSING FOR UPPER HYDRAULIC ACTUATOR ON RUDDER I I/A/W EC 5540-01043 REV A. AIRCRAFT WAS APPROVED
- [SDR C2XA05SH087](https://openairdocs.org/sdr/C2XA05SH087.md): Hinge · cracked · Jul 21, 2005 · N14943 · Emb EMB145EP · Horizontal Stabilizer Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND RUDDER II UPPER MIDDLE ATTACHMENT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER MIDDLE ATTACHMENT BRACKET (HINGE FITTING) I/A/W EC 5540-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH086](https://openairdocs.org/sdr/C2XA05SH086.md): Floor Support · corroded · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM FLOOR SUPPORT FLANGE HAS CORROSION BETWEEN FRAMES 20-24. MAINTENANCE REMOVED & REPLACED LT OMEGA BEAM FROM FRAMES 20-23 I/A/W EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH085](https://openairdocs.org/sdr/C2XA05SH085.md): Floor Support · corroded · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM LOWER FLANGE IS CORRODED BETWEEN FRAMES 53-59. MAINTEANACE REPAIRED LOWER FLANGE AT FRAME 54 I/A/W EMB 145 SRM 53-00-10 & EC 5320-01140. INSTALLED NEW NUTPLATES I/A/W EC 5320-01137. PREPPED, PRIMED & PAINTED A
- [SDR C2XA05SH084](https://openairdocs.org/sdr/C2XA05SH084.md): Floor Support · corroded · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAMES 11-23 I/A/W EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH083](https://openairdocs.org/sdr/C2XA05SH083.md): Floor Support · corroded · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRAMES 38-46. MAINTENANCE REPAIRED LT OMEGA BEAM BETWEEN FRAMES 38 & 46 I/A/W EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH082](https://openairdocs.org/sdr/C2XA05SH082.md): Skin Panel · lightning strike · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB. MAINTENANCE REPAIRED LIGHTNING STRIKES AT LOWER RT WING, NEAR PNL 631 AB I/A/W EC 5330-01480, REPAIR FIGURES NR 5 7 & 6. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH081](https://openairdocs.org/sdr/C2XA05SH081.md): Skin Panel · lightning strike · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTNING STRIKE AT FRAME 23 STR 17R. MAINTENANCE REPAIRED LIGHTNING STRIKE AT FRAME 23 STR 17R I/A/W EC 5330-01480, REPAIR FIGURE #1. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH080](https://openairdocs.org/sdr/C2XA05SH080.md): Skin Panel · lightning strike · Jul 21, 2005 · N14943 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV-DURING C-CHECK MAINTENANCE FOUND LIGHTENING STRIKE AT FRAMES 21-22, STR 18R. MAINTENANCE REPAIRED LIGHTENING STRIKES AT FRAMES 21-22, STR 18R I/A/W EC 5330-01480, REPAIR FIGURE NR 2. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N14943-2015-05-26/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 = 'N14943' AND deregistration_id = 'N14943-2015-05-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14943-2015-05-26/reports

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