# Service difficulty reports: N14930, cancelled Feb 28, 2020

A list on [N14930, cancelled Feb 28, 2020](https://openairdocs.org/deregistered/N14930-2020-02-28.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 · 142 reports

- [SDR ASOA20140413043](https://openairdocs.org/sdr/ASOA20140413043.md): Door Frame · cracked · Apr 13, 2014 · N14930 · Emb EMB145ER · Cargo/Baggage Doors
  > CARGO DOOR AFT FRAME LOWER INSIDE CORNER HAS A CRACKED NUTPLATE. REPAIRED IAW EC5230-01326. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413042](https://openairdocs.org/sdr/ASOA20140413042.md): Firewall · cracked · Apr 13, 2014 · N14930 · Emb EMB145ER · APU Cowling/Containment
  > DURING C-CHECK, APU FIREWALL CRACKED AT UPPER LT MOUNT. REPAIRED IAW EC5330-02578, REV B. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413041](https://openairdocs.org/sdr/ASOA20140413041.md): Housing · worn · Apr 13, 2014 · N14930 · Emb EMB145ER · Horizontal Stabilizer Structure
  > DURING C-CHECK, HORIZONTAL STAB HINGE FITTING HOUSINGS IS OUT OF LIMITS. REPAIRED IAW SRM 55-30-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413040V](https://openairdocs.org/sdr/ASOA20140413040V.md): Floor Support · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CENTER OMEGA BEAM CORRODED ON LOWER SIDE AT FRAME 59. MAINTENANCE PERFORMED REPAIR IAW EC5310-01473. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413039](https://openairdocs.org/sdr/ASOA20140413039.md): Shear Tie · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED, AT FRAME 65, STRINGER 17L. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140413038](https://openairdocs.org/sdr/ASOA20140413038.md): Beam · corroded · Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Main, Structure
  > DURING C-CHECK, CARGO LOWER BEAM FROM FRAMES 65-68 HAS CORROSION. MAINTENANCE R & R LOWER BEAM IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130225024](https://openairdocs.org/sdr/ASOA20130225024.md): Inverter · inoperative · Feb 25, 2013 · N14930 · Emb EMB145EP · Emergency Lighting
  > DURING MX INSPECTION, THE PASSENGER CABIN FWD EMERGENCY EXIT LOCATING SIGN ON 253CLC FAILED TO ILLUMINATE. MX R & R THE AFFECTED SIGN EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130219020](https://openairdocs.org/sdr/ASOA20130219020.md): Connector · disconnected · Feb 19, 2013 · N14930 · Emb EMB145EP · Light System Wiring
  > THE CREW REPORTED THE EXIT SIGN OVERWING EXIT WOULD NOT ILLUMINATE. MX INSPECTED THE ACFT AND RECONNECTED THE SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120122015](https://openairdocs.org/sdr/ASOA20120122015.md): Floor Support · corroded · Jan 22, 2012 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CHECK. CENTER OMEGA BEAM CORRODED AT FR 20. REPLACED OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120121014](https://openairdocs.org/sdr/ASOA20120121014.md): Skin · cracked · Jan 21, 2012 · N14930 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING C-CHECK. CRACKS AROUND RIVETS ON RT FUSELAGE SKIN AT FR 75. REPAIRED SKIN CRACKS IAW EC 5330-02353. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120121013](https://openairdocs.org/sdr/ASOA20120121013.md): Mount · cracked · Jan 21, 2012 · N14930 · Emb EMB145EP · Engine Mount Section
  > DURING C-CHECK. RT FWD LOWER ENGINE MOUNT CRACKED. R & R RT LOWER FWD ENGINE MOUNT IAW EC 5450-01028. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120117012](https://openairdocs.org/sdr/ASOA20120117012.md): Floor Support · corroded · Jan 17, 2012 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 49. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120117011](https://openairdocs.org/sdr/ASOA20120117011.md): Floor Support · corroded · Jan 17, 2012 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CK. LEFT OMEGA BEAM CORRODED AT FR 44. REPAIRED OMEGA BEAM IAW EC 5310-01466. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA252](https://openairdocs.org/sdr/C2XA11IA252.md): Inverter · inoperative · Nov 3, 2011 · N14930 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING NR 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
- [SDR C2XA11IA177](https://openairdocs.org/sdr/C2XA11IA177.md): Battery Pack · discharged · Aug 10, 2011 · N14930 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2886, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING IN THE BACK HALF OF THE AIRCRAFT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFEC
- [SDR C2XA11IA149](https://openairdocs.org/sdr/C2XA11IA149.md): Damper Plate · damaged · Jul 8, 2011 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > IAH - DURING MAINTENANCE INSPECTION THE APU FIREWALL WAS FOUND TO HAVE SEVERAL DAMAGED VIBRATION ABSORPTION PADS. MAINTENANCE REPAIRED THE VIBRATION ABSORPTION PADS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA177](https://openairdocs.org/sdr/C2XA10IA177.md): Battery · overheated · Jun 18, 2010 · N14930 · Emb EMB145EP · Battery/Charger System
  > IAH - FLIGHT 3121, THE CREW REPORTED A BATTERY TWO OVER-TEMP ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RE
- [SDR C2XA10IA070](https://openairdocs.org/sdr/C2XA10IA070.md): Selector · malfunctioned · Feb 17, 2010 · N14930 · Emb EMB145EP · Landing Gear Selector
  > IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, AND LANDING GEAR ELECTRONICS UN
- [SDR C2XA10IA069](https://openairdocs.org/sdr/C2XA10IA069.md): Electronic Unit · defective · Feb 17, 2010 · N14930 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2102, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, AND LANDING GEAR ELECTRONICS UN
- [SDR C2XA10IA061](https://openairdocs.org/sdr/C2XA10IA061.md): Selector · inoperative · Feb 11, 2010 · N14930 · Emb EMB145EP · Landing Gear Selector
  > DFW - FLIGHT 2114 DURING CLIMB THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE, AND THREE RED X'S ON THE EICAS. THE AIRCRAFT RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACE
- [SDR C2XA09IA282](https://openairdocs.org/sdr/C2XA09IA282.md): A/C Pack · overheated · Nov 3, 2009 · N14930 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 2030, DURING TAXI THE CREW REPORTED THAT THE NUMBER ONE PACK OVERHEATED WITH A BURNING ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 PACK ON MEL, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA09IA229](https://openairdocs.org/sdr/C2XA09IA229.md): Seal · defective · Sep 12, 2009 · N14930 · Emb EMB145EP · Flight Compartment Windows
  > IAH - DURING CLIMB THE CREW REPORTED A LOUD NOISE AND VIBRATION FROM THE WINDSHIELD AREA. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CAPTAINS HUMPSEAL ON DMI, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA09IA208](https://openairdocs.org/sdr/C2XA09IA208.md): Connector · burned · Aug 20, 2009 · N14930 · Emb EMB145EP · Light System Wiring
  > FLIGHT 2526, DURING TAXI THE CREW REPORTED A STRONG ELECTRICAL PLASTIC BURNING ODOR COMING FROM THE GALLEY AREA. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LIGHT SOCKET ON THE CEILING LIGHT AT ROW 1A, TO BE BURNED
- [SDR C2XA09IA168](https://openairdocs.org/sdr/C2XA09IA168.md): Electronic Unit · inoperative · Jun 29, 2009 · N14930 · Emb EMB145EP · Landing Gear Position and Warning
  > IAH - FLIGHT 2605 - THE CREW REPORTED A LANDING GEAR DISAGREE ON CLIMBOUT AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, (LGEU), OPERATIONALLY
- [SDR C2XA09IA164](https://openairdocs.org/sdr/C2XA09IA164.md): Control Handle · inoperative · Jun 25, 2009 · N14930 · Emb EMB145EP · Landing Gear Selector
  > IAH - FLIGHT 2104 - THE CREW REPORTED WHEN COMMANDED GEAR SW TO UP, GEAR DID NOT RETRACT. TEN TO FIFTEEN SECONDS LATER CREW RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS, AND THE GEAR RETRACTED, AND EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO IAH
- [SDR C2XA09SH164](https://openairdocs.org/sdr/C2XA09SH164.md): Floor Support · corroded · May 13, 2009 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED LT OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH163](https://openairdocs.org/sdr/C2XA09SH163.md): Sill · corroded · May 13, 2009 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CHECK. BAGGAGE DOOR CUTOUT LOWER SILL HAS CORROSION. REPAIRED CARGO LOWER SILL IAW IC 2009-145/03445. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH162](https://openairdocs.org/sdr/C2XA09SH162.md): Floor Support · corroded · May 13, 2009 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LT OMEGA BEAM HAS CORROSION FR 19-21. REPAIRED RT OMEGA BEAM IAW IC2009-145/00907. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH160](https://openairdocs.org/sdr/C2XA09SH160.md): Fitting · cracked · May 4, 2009 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK FRAME 80 HAS CRACKED SHEAR CLIP BETWEEN STR 6-7R. MAINTENANCE REMOVED AND REPLACED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STR 6-7R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH159](https://openairdocs.org/sdr/C2XA09SH159.md): Hinge Bracket · worn · May 4, 2009 · N14930 · Emb EMB145EP · Wing, Control Surface Attach Fittings
  > SHV - DURING C-CHECK RT AILERON NR 2 HINGE FROM O/B HAS MIGRATED BUSHINGS. REMOVED AND REPLACED RT AILERON NR 2 HINGE FROM O/B SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH158](https://openairdocs.org/sdr/C2XA09SH158.md): Support Bracket · worn · May 4, 2009 · N14930 · Emb EMB145EP · Wing, Control Surface Attach Fittings
  > SHV - DURING C-CHECK RT AILERON NR 1 HINGE FROM O/B HAS MIGRATED BUSHING. MAINTENANCE REMOVED AND REPLACED RT AILERON NR 1 HINGE FROM O/B SUPPORT BRACKET ASSY (WITH NEW BUSHINGS) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH157](https://openairdocs.org/sdr/C2XA09SH157.md): Support Bracket · damaged · May 4, 2009 · N14930 · Emb EMB145EP · Ailerons
  > SHV - DURING C-CHECK RT AILERON MOST O/B HINGE BRACKET I/B HOUSING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON MOST O/B HINGE SUPPORT BRACKET ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA095](https://openairdocs.org/sdr/C2XA09IA095.md): Actuator · slow · Apr 6, 2009 · N14930 · Emb EMB145EP · Landing Gear Actuator
  > IAH - FLIGHT 2798, THE CREW REPORTED THE LANDING GEAR TOOK OVER 30 SECONDS TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS. THE
- [SDR C2XA09IA067](https://openairdocs.org/sdr/C2XA09IA067.md): Light · inoperative · Feb 26, 2009 · N14930 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA047](https://openairdocs.org/sdr/C2XA09IA047.md): Wire · shorted · Feb 13, 2009 · N14930 · Emb EMB145EP · Electrical Power System Wiring
  > GPT - FLIGHT 2304 - THE CREW REPORTED AN ELECTRICAL BURNING SMELL BEING EMITTED FROM THE ELECTRICAL PANEL BEHIND THE CAPTAINS SEAT. THE AIRCRAFT LANDED AT GPT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND WIRE W179-0001-00 TO THE CENTRAL DC
- [SDR C2XA08IA129](https://openairdocs.org/sdr/C2XA08IA129.md): Wire · broken · May 14, 2008 · N14930 · Emb EMB145EP · Light System Wiring
  > IAH - DURING MAINTENANCE INSPECTION THE 2ND AISLE PATH LIGHT STRIP ON THE FLOOR WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI
- [SDR C2XA08TY033](https://openairdocs.org/sdr/C2XA08TY033.md): Skin · cracked · Mar 7, 2008 · N14930 · Emb EMB145EP · Wing, Plate/Skin
  > A 1.26 LONG CRACK WAS DISCOVERED ON THE LT WING UPPER TRAILING EDGE SKIN ADJACENT TO THE CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01140. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08IA013](https://openairdocs.org/sdr/C2XA08IA013.md): Sensor · burned · Jan 7, 2008 · N14930 · Emb EMB145EP · Pitot/Static Anti-Ice System
  > IAH - FLIGHT 2137, WHILE "SITTING AT THE GATE" THE CREW REPORTED A BURNT SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PITOT NUMBER ONE CURRENT SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S
- [SDR C2XA07IA257](https://openairdocs.org/sdr/C2XA07IA257.md): Skin · cracked · Dec 27, 2007 · N14930 · Emb EMB145EP · Wing, Plate/Skin
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT WING SKIN TO BE CRACKED AT THE SPOILER HINGE POINT. THE CRACK WAS INSPECTED AND PLACED ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING FINAL CORRECTIVE ACTI
- [SDR C2XA07SH096](https://openairdocs.org/sdr/C2XA07SH096.md): Hydraulic Line · ruptured · Nov 29, 2007 · N14930 · Emb EMB145 · Hydraulic System, Main
  > SHV - FLT 2395, DURING CLIMB AND UPON MOVING THE LANDING GEAR SELECTOR TO RETRACT THE CREW OBSERVED A HYDRAULIC SYSTEM 1 ADVISORY. THE CREW MOVED THE LANDING GEAR SELECTOR BACK TO EXTEND AND PERFORMED THE ABNORMAL INDICATION PROCEDURES. THE AIRCRAFT MADE AN
- [SDR C2XA07TY054](https://openairdocs.org/sdr/C2XA07TY054.md): Bulb · inoperative · Sep 21, 2007 · N14930 · Emb EMB145EP · Emergency Lighting
  > EMERGENCY LIGHT IN SERVICE DOOR AND AT SEAT 12 BC AT TOP INOP. REMOVED AND REPLACED BULBS IAW EMB 145 AMM 33-50-00, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA06SH120](https://openairdocs.org/sdr/C2XA06SH120.md): Skin · corroded · Nov 4, 2006 · N14930 · Emb EMB145EP · Horizontal Stabilizer, Plate/Skin
  > SHV - DURING C-CHECK THE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS FOUND TO BE ERRODED AND HAVE PITTING CORROSION ON THE UPPER AND LOWER SURFACES. MAINTENANCE REMOVED AND REPLACED THE LEFT HORIZONTAL STABILIZER LEADING EDGE IAW EMB 145 AMM 55-15-00. THE AI
- [SDR C2XA06SH121](https://openairdocs.org/sdr/C2XA06SH121.md): Intake · corroded · Nov 1, 2006 · N14930 · Emb EMB145EP · Engine Air Intake System
  > SHV - DURING C-CHECK THE NR 2 ENGINE INTAKE FLANGE WAS FOUND TO BE CORRODED AROUND THE BOLT HOLES. MAINTENANCE REMOVED AND REPLACED THE INTAKE IAW EMB 145 AMM 71-60-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH118](https://openairdocs.org/sdr/C2XA06SH118.md): Floor Support · corroded · Oct 31, 2006 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 24 AND 29. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED SHIM FILLER REPAIRS AT FR 24 AND 29 IAW EMB 145 SRM 53-00-10, PG 212, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR C2XA06SH117](https://openairdocs.org/sdr/C2XA06SH117.md): Floor Support · corroded · Oct 31, 2006 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE CLEANED THE AREAS OF CORROSION AND FOUND THE DAMAGE TO BE OUT OF LIMITS AT FRAME 24 AND FRAME 29. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED SHIM
- [SDR C2XA06SH116](https://openairdocs.org/sdr/C2XA06SH116.md): Floor Support · corroded · Oct 30, 2006 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED AROUND THE NUT PLATE HOLES. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER/FILLER REPAIR IAW EC5320-01257, REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH119](https://openairdocs.org/sdr/C2XA06SH119.md): Floor Support · corroded · Oct 30, 2006 · N14930 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 203 DET A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06IA095](https://openairdocs.org/sdr/C2XA06IA095.md): Bearing · failed · Jun 18, 2006 · N14930 · Emb EMB145EP · Engine (Turbine/Turboprop)
  > VCT - FLIGHT 2482, THE CREW REPORTED A LAV SMOKE WARNING FOLLOWED BY A LOW OIL PRESSURE INDICATION, AND AN ENGINE 2 FIRE WARNING. THE CREW SHUTDOWN THE NUMBER TWO ENGINE, AND DIVERTED TO VCT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND
- [SDR C2XA05IA064](https://openairdocs.org/sdr/C2XA05IA064.md): Relay · failed · Apr 27, 2005 · N14930 · Emb EMB145ER · Landing Gear Position and Warning
  > IAH - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL ON TAKEOFF AND A WEIGHT ON WHEEL FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0453 & K0352, OPERATIONALLY CHECKED WITH NO DEFECTS, THE
- [SDR C2XA05IA063](https://openairdocs.org/sdr/C2XA05IA063.md): Control Unit · inoperative · Apr 26, 2005 · N14930 · Emb EMB145ER · Landing Gear Retraction/Extension System
  > CRP - THE CREW REPORTED THAT DURING TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AN

Next page: https://openairdocs.org/deregistered/N14930-2020-02-28/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 = 'N14930' AND deregistration_id = 'N14930-2020-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14930-2020-02-28/reports

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