# Service difficulty reports: N14938, cancelled Mar 15, 2016

A list on [N14938, cancelled Mar 15, 2016](https://openairdocs.org/deregistered/N14938-2016-03-15.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 · 87 reports

- [SDR ASOA20140917117](https://openairdocs.org/sdr/ASOA20140917117.md): Bulb · burned out · Sep 17, 2014 · N14938 · Emb EMB145EP · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE LT WING AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140807105](https://openairdocs.org/sdr/ASOA20140807105.md): Light · inoperative · Aug 7, 2014 · N14938 · Emb EMB145EP · Emergency Lighting
  > DURING A 3A INSPECTION, THE LT EMERGENCY LIGHT ON THE FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140514072](https://openairdocs.org/sdr/ASOA20140514072.md): Attach Fitting · damaged · May 14, 2014 · N14938 · Emb EMB145EP · Ailerons
  > DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THA AFFECTED FITTING, OPERATIONALLY TESTING WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR
- [SDR ASOA2014051400001](https://openairdocs.org/sdr/ASOA2014051400001.md): Attach Fitting · damaged · May 14, 2014 · N14938 · Emb EMB145EP · Ailerons
  > DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THAT AFFECTED FITTING, OPERATIONALLY TESTING WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR
- [SDR ASOA20140319047](https://openairdocs.org/sdr/ASOA20140319047.md): Light · inoperative · Mar 19, 2014 · N14938 · Emb EMB145EP · Emergency Lighting
  > DURING PREFLIGHT, CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHT STRIP AT SEAT 4A WAS INOPERATIVE. R & R EMERGENCY LIGHT AND OPS TESTED WITH NO DEFECTS. APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140311025](https://openairdocs.org/sdr/ASOA20140311025.md): Seal · debonded · Mar 11, 2014 · N14938 · Emb EMB145ER · Cargo/Baggage Doors
  > EXPERIENCED CABIN DEPRESSURIZATION AT ALTITUDE AND THEN DIVERTED. MAINTENANCE FOUND CARGO DOOR RUBBER TRIM SEAL DEBONDED AND HANGING OUT IN THE AIRSTREAM. REINSTALLED CARGO DOOR RUBBER TRIM SEAL IAW AMM 52-30-02. PERFORMED LEAK CHECK ON PRESSURIZATION AND O
- [SDR ASOA20131216223](https://openairdocs.org/sdr/ASOA20131216223.md): Socket · shorted · Dec 16, 2013 · N14938 · Emb EMB145EP · Passenger Compartment Lighting
  > THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN FRONT CABIN. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT SOCKET SHORTED AND MELTED. R & R AFFECTED HARNESS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130716124](https://openairdocs.org/sdr/ASOA20130716124.md): Skin · cracked · Jul 17, 2013 · N14938 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130226025H](https://openairdocs.org/sdr/ASOA20130226025H.md): Skin · cracked · Feb 26, 2013 · N14938 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A.2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AN
- [SDR ASOA20121107123V](https://openairdocs.org/sdr/ASOA20121107123V.md): Sill · corroded · Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE SERVICE DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107122V](https://openairdocs.org/sdr/ASOA20121107122V.md): Hinge Fitting · worn · Nov 7, 2012 · N14938 · Emb EMB145ER · Rudder Structure
  > DURING C-CHECK, THE RUDDER LOWER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX OVERSIZED THE HOLES AND REPLACED THE HAT BUSHINGS IAW EC5540-01178. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107121V](https://openairdocs.org/sdr/ASOA20121107121V.md): Skin · corroded · Nov 7, 2012 · N14938 · Emb EMB145ER · Cargo/Baggage Doors
  > DURING C-CHECK, THE CARGO DOOR LOWER INTERNAL SKIN WAS FOUND TO BE CORRODED AROUND THE BOTTOM NUT PLATES. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107120V](https://openairdocs.org/sdr/ASOA20121107120V.md): Doubler · cracked · Nov 7, 2012 · N14938 · Emb EMB145ER · Vertical Stabilizer
  > DURING C-CHECK THE VERTICAL STAB DOUBLER BETWEEN FRAMES 80-81 AND STRINGERS 1L-1R WAS FOUND TO BE CRACKED. MX R & R THE DOUBLER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107119V](https://openairdocs.org/sdr/ASOA20121107119V.md): Shear Tie · corroded · Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE SHEAR TIE AT FRAME 19 BETWEEN STRINGERS 21L AND 21R WAS FOUND TO BE CORRODED. MX R & R THE SHEAR CLIP IAW EC5320-01713. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107118V](https://openairdocs.org/sdr/ASOA20121107118V.md): Shear Tie · cracked · Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > DURING C-CHECK THE CENTERLINE SHEAR TIE AT FRAME 42, 6:00 POSITION IN THE WING BOX WAS FOUND TO BE CRACKED. MX R & R THE SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121107117](https://openairdocs.org/sdr/ASOA20121107117.md): Skin · corroded · Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-19 AND STRINGERS 21L-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02633. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121001128HS](https://openairdocs.org/sdr/ASOA20121001128HS.md): Wire Harness · chafed · Oct 1, 2012 · N14938 · Emb EMB145EP · Light System Wiring
  > DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. NARROWED DOWN TO CEILING LIGHTS 14A-18A. MX REPAIRED A CHAFED WIRE ON THE CEILING LIGHT AT 18A, OPS CHECKED WITH NO DEFECTS. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121001128](https://openairdocs.org/sdr/ASOA20121001128.md): Light · odor · Oct 1, 2012 · N14938 · Emb EMB145EP · Passenger Compartment Lighting
  > DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. FOUND TO BE CEILING LIGHTS 14A-18A. OPEN
- [SDR ASOA20120906120H](https://openairdocs.org/sdr/ASOA20120906120H.md): Light · overheated · Sep 6, 2012 · N14938 · Emb EMB145EP · Passenger Compartment Lighting
  > THE CREW REPORTED A STRING ELECTRICAL BURNING ODOR AROUND ROW 14. MX INSPECTED THE ACFT AND R & R THE SIDEWALL LIGHT ASSY AT ROW 15 RT, OPS TESTED WITH NO DFECTS, AND THE ACFT WAS APPROVED OFR RETURN TO SERVICE.
- [SDR ASOA20120519077H](https://openairdocs.org/sdr/ASOA20120519077H.md): Unknown · odor · May 19, 2012 · N14938 · Emb EMB145EP · Air Distribution System
  > THE CREW REPORTED THAT AFTER LANDING THERE WAS AN ELECTRICAL BURNING ODOR IN THE CABIN AND COCKPIT THAT WENT AWAY AFTER 3 MINUTES, AND SEEMED TO BE COMING FROM BEHIND THE CAPTAINS SEAT. MX INSPECTED THE ACFT C/W FIM21-20-00-810-801A, AND R & R RELAY K0094 FRO
- [SDR ASOA20120404053](https://openairdocs.org/sdr/ASOA20120404053.md): Tire · failed · Mar 30, 2012 · N14938 · Emb EMB145EP · Tire
  > VIBRATION FROM WHEELS ON ACFT ROTATION. TOWER FLY-BY REVEALED RT MAIN TIRE BLOWN. UPON LANDING, RT MAIN INBD WAS BLOWN. R & R NR 3 & NR 4 MWA.
- [SDR ASOA20120305032](https://openairdocs.org/sdr/ASOA20120305032.md): Power Supply · inoperative · Mar 5, 2012 · N14938 · Emb EMB145EP · Emergency Lighting
  > THE CREW REPORTED EMERGENCY AISLE PATH LIGHTING NR 6, 7, & 8 TO BE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH178](https://openairdocs.org/sdr/C2XA10SH178.md): Floor Support · corroded · May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 54. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH177](https://openairdocs.org/sdr/C2XA10SH177.md): Floor Support · corroded · May 19, 2010 · N14938 · Emb EMB145EP · 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 C2XA10SH176](https://openairdocs.org/sdr/C2XA10SH176.md): Floor Support · corroded · May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH175](https://openairdocs.org/sdr/C2XA10SH175.md): Beam · corroded · May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH174](https://openairdocs.org/sdr/C2XA10SH174.md): Skin · cracked · May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE LT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2L-7L. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED FASTENERS IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH173](https://openairdocs.org/sdr/C2XA10SH173.md): Skin · cracked · May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE RT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED HOLES IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH172](https://openairdocs.org/sdr/C2XA10SH172.md): Frame · cracked · May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Frame
  > SHV - DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L RIGHT BELOW THE LT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH171](https://openairdocs.org/sdr/C2XA10SH171.md): Frame · cracked · May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R WAS FOUND TO BE CRACKED RIGHT BELOW THE RT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH170](https://openairdocs.org/sdr/C2XA10SH170.md): Yoke · cracked · May 18, 2010 · N14938 · Emb EMB145EP · Nacelle/Pylon, Attach Fittings
  > SHV - DURING C-CHECK THE RT ENGINE FORWARD LOWER YOKE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED YOKE IAW EC 5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH164](https://openairdocs.org/sdr/C2XA10SH164.md): Fitting · cracked · May 2, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6R-7R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH163](https://openairdocs.org/sdr/C2XA10SH163.md): Fitting · cracked · May 2, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6L-7L. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 STRINGER 6L-7L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA093](https://openairdocs.org/sdr/C2XA10IA093.md): Brake · malfunctioned · Mar 11, 2010 · N14938 · Emb EMB145EP · Trailing Edge Flap Control System
  > IAH - FLIGHT 2102, THE CREW REPORTED THAT AFTER T/O, RECEIVED A FLAP FAIL MESSAGE ON EICAS WITH THE FLAP LEVER AT 0 DEGREES AND THE FLAPS AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT
- [SDR C2XA10IA058](https://openairdocs.org/sdr/C2XA10IA058.md): Dau · defective · Feb 8, 2010 · N14938 · Emb EMB145EP · Pneumatic Indicating System
  > XNA - FLIGHT 2660, THE CREW REPORTED A BLEED 1 LEAK IN FLIGHT THAT DID NOT GO AWAY. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND RETURNED TO XNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL AND LEAK CHECKS, AND SUBSEQUE
- [SDR C2XA09IA231](https://openairdocs.org/sdr/C2XA09IA231.md): O-Ring · leaking · Sep 13, 2009 · N14938 · Emb EMB145EP · Pneumatic Distribution System
  > IAH - FLIGHT 2264 - THE CREW REPORTED A BLEED ONE LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS AT POSITIONS 17, 19, 23, 25 & 30, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECT
- [SDR C2XA09IA158](https://openairdocs.org/sdr/C2XA09IA158.md): Selector · inoperative · Jun 20, 2009 · N14938 · Emb EMB145EP · Trailing Edge Flap Control System
  > IAH - FLIGHT 2967 - THE CREW REPORTED THAT THE FLAPS FAILED AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR
- [SDR C2XA09SH083](https://openairdocs.org/sdr/C2XA09SH083.md): Accumulator · faulty · Mar 17, 2009 · N14938 · Emb EMB145EP · Hydraulic Power Accumulator, Main
  > SHV - LOUD BANGING NOISE IN WHEEL WELL FOR 30 SEC AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR HYD ACCUMULATOR IAW EMB 145 AMM 32-33-15. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08IA144](https://openairdocs.org/sdr/C2XA08IA144.md): Light · inoperative · Jun 19, 2008 · N14938 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2361, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE FRONT AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA07IA256](https://openairdocs.org/sdr/C2XA07IA256.md): Structure · out of position · Dec 30, 2007 · N14938 · Emb EMB145EP · Emergency Exits
  > IAH - DURING A-CHECK INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR WOULD NOT OPEN. THE METAL TRIM AT THE TOP OF THE DOOR WAS FOUND TO BE CATCHING ON THE OPENING. MAINTENANCE RECONTOURED/TRIMMED THE AFFECTED MATERIAL, OPERATIONALLY CHECKED THE EXIT W
- [SDR C2XA06BT026](https://openairdocs.org/sdr/C2XA06BT026.md): Smoke Detector · faulty · Jun 27, 2006 · N14938 · Emb EMB145EP · Smoke Detection
  > CREW REPORTED LAV SMOKE DETECTOR WARNING ON EICAS WITH APU ON ENGINES OFF. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB145 AMM 26-14-02. OPS CHECK GOOD.
- [SDR C2XA05CL097](https://openairdocs.org/sdr/C2XA05CL097.md): Proximity Sensor · failed · Dec 6, 2005 · N14938 · Emb EMB145EP · Landing Gear Position and Warning
  > CLE FLIGHT NR 2235, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE PRECEEDED BY E1-2 REVERSER DISAGREE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING
- [SDR C2XA05IA112](https://openairdocs.org/sdr/C2XA05IA112.md): Light · inoperative · Oct 10, 2005 · N14938 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH039](https://openairdocs.org/sdr/C2XA05SH039.md): Floor Support · corroded · May 20, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AROUND NUT PLATE BETWEEN FRAMES 22 AND 23. MAINTENANCE REPAIRED LT OMEGA BEAM NUT PLATE AT FRAME 22.5 AND RIVET HOLE CRACK AT FRAME 22 IAW SRM 51-30-01; 51-40-02 AND EC5320-01241. THE AIRCRAFT WAS APPROVED
- [SDR C2XA05SH038](https://openairdocs.org/sdr/C2XA05SH038.md): Skin Panel · lightning strike · May 20, 2005 · N14938 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > DURING C-CHECK VARIOUS LIGHTNING STRIKE ON SKIN PNL 214. MAINTENANCE REPAIR SKIN PNL 214 ABOVE STR 13R AFT FR 1A IAW EC 5330-01465. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA05SH037](https://openairdocs.org/sdr/C2XA05SH037.md): Floor Support · corroded · May 17, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON I/B SIDE FROM FRAME 36 TO FRAME 38. REPAIRED LT OMEGA BEAM AT FRAME 38 IAW EMB 145 SRM 53-21-10, SECTION 2, FIGURE 201, SHEET 3 & EC 5320-01231 (ORIG).
- [SDR C2XA05SH036](https://openairdocs.org/sdr/C2XA05SH036.md): Floor Support · corroded · May 16, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE RT OMEGA BEAM HAS CORROSION AROUND NUT PLATE AT FRAME 23. REPAIRED CORROSION ON RT OMEGA BEAM AROUND NUT PLATE AT FRAME 23 WITH INSTALLATION OF NEW OMEGA BEAM AT FRAME 23 IAW EMB 145 SRM 51-40-02 WITH NUT PLATE INSTALLATION PER EC 532
- [SDR C2XA05SH035](https://openairdocs.org/sdr/C2XA05SH035.md): Floor Support · corroded · May 16, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 & 24. REPAIRED CENTER OMEGA BEAM AT FRAME 24 IAW EMB 145 SRM 53-22-10 PARAGRAPH 2 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH033](https://openairdocs.org/sdr/C2XA05SH033.md): Floor Support · corroded · May 13, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 17-24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05SH032](https://openairdocs.org/sdr/C2XA05SH032.md): Floor Support · corroded · May 12, 2005 · N14938 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 39 TO FRM 45. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FRM 44 IAW SRM 53-21-10, SECTION 2, FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N14938-2016-03-15/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 = 'N14938' AND deregistration_id = 'N14938-2016-03-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14938-2016-03-15/reports

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