# Service difficulty reports: N13929, cancelled Dec 29, 2015

A list on [N13929, cancelled Dec 29, 2015](https://openairdocs.org/deregistered/N13929-2015-12-29.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 · 112 reports

- [SDR ASOA20130713115](https://openairdocs.org/sdr/ASOA20130713115.md): Skin · cracked · Jul 16, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.
- [SDR ASOA20130713120](https://openairdocs.org/sdr/ASOA20130713120.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130713119](https://openairdocs.org/sdr/ASOA20130713119.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR78 BELOW S4L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130713118H](https://openairdocs.org/sdr/ASOA20130713118H.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR 77 ABOVE S6L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130713117](https://openairdocs.org/sdr/ASOA20130713117.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR77 BELOW STR 04L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.
- [SDR ASOA20130713116](https://openairdocs.org/sdr/ASOA20130713116.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 BELOW STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130713114](https://openairdocs.org/sdr/ASOA20130713114.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR78 BETWEEN STRINGERS 5 & 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130713113](https://openairdocs.org/sdr/ASOA20130713113.md): Skin · cracked · Jul 13, 2013 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > DURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR77 STRINGER 04R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/2013.
- [SDR ASOA20121209166](https://openairdocs.org/sdr/ASOA20121209166.md): Inverter · inoperative · Dec 9, 2012 · N13929 · Emb EMB145EP · Emergency Lighting
  > GALLEY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20120820112H](https://openairdocs.org/sdr/ASOA20120820112H.md): Unknown · odor · Aug 20, 2012 · N13929 · Emb EMB145EP · Air Distribution System
  > THE CREW REPORTED A BURNING ODOR IN THE CABIN NOTICED BY THE F/A. MX INSPECTED THE ACFT AND WAS UNABLE TO DUPLICATE ANY BURNING ODOR OR SMELL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120124012](https://openairdocs.org/sdr/ASOA20120124012.md): Sign · inoperative · Jan 24, 2012 · N13929 · Emb EMB145EP · Emergency Lighting
  > THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 1A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11ASH134](https://openairdocs.org/sdr/C2XA11ASH134.md): Skin · corroded · Sep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 18R-20R IS CORRODED. MAINTENANCE PERFORMED REPAIR ON INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 17R-21L IAW EC5330-02474. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH133](https://openairdocs.org/sdr/C2XA11SH133.md): Skin Splice · corroded · Sep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L-19L CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L- 19L IAW EMB-145 CPM 51-21-00. THE AIRCRAFT WAS APPROVED
- [SDR C2XA11SH132](https://openairdocs.org/sdr/C2XA11SH132.md): Skin Splice · corroded · Sep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14-15, STRINGERS 20L-15R CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON CIRCUMFERENTIAL SPLICE BETWEEN FRAMES 13-15, STRINGERS 20L-15R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPRO
- [SDR C2XA11SH131](https://openairdocs.org/sdr/C2XA11SH131.md): Stringer · corroded · Sep 8, 2011 · N13929 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STRINGER 21L BETWEEN FRAMES 11-12 IS CORRODED. MAINTENANCE REMOVED AND REPLACED STRINGER 21L FRAME 9-13 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH130](https://openairdocs.org/sdr/C2XA11SH130.md): Skin · corroded · Sep 7, 2011 · N13929 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R HAS IMPROPERLY PAINTED SKIN AND CORROSION IN UNPAINTED AREAS. MAINTENANCE PERFORMED REPAIR ON SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RET
- [SDR C2XA11SH129](https://openairdocs.org/sdr/C2XA11SH129.md): Bushing · migrated · Sep 7, 2011 · N13929 · Emb EMB145LR · Spoilers
  > SHV - DURING C-CHECK RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET HAS MIGRATING HAT BUSHING. MAINTENANCE PERFORMED REPAIR ON RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET IAW EMB-145 AMM 27-62-05, OPERATIONAL CHECK GOO
- [SDR C2XA11SH128](https://openairdocs.org/sdr/C2XA11SH128.md): Crossbeam · corroded · Sep 7, 2011 · N13929 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM AT FRAME 20 IAW ETD 2011-145-103674. THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR C2XA11SH127](https://openairdocs.org/sdr/C2XA11SH127.md): Skin · corroded · Sep 7, 2011 · N13929 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK CORROSION FOUND ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 57-58, STRINGER 21L-21R. MAINTENANCE PERFORMED REPAIR ON INTERNAL FUSELAGE SKIN, BETWEEN FRAMES 57-58 STRINGER 21L-21R IAW EC5330-02475. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER
- [SDR C2XA11SH121](https://openairdocs.org/sdr/C2XA11SH121.md): Frame · cracked · Aug 24, 2011 · N13929 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK THE RT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 10R-11R, DIRECTLY BELOW THE RT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XAII1A105](https://openairdocs.org/sdr/C2XAII1A105.md): Trim Switch · malfunctioned · Jun 8, 2011 · N13929 · Emb EMB145EP · Stabilizer Control System
  > IAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPL
- [SDR C2XA11IA104](https://openairdocs.org/sdr/C2XA11IA104.md): Trim Switch · shorted · Jun 8, 2011 · N13929 · Emb EMB145EP · Stabilizer Control System
  > IAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPL
- [SDR C2XA11IA044](https://openairdocs.org/sdr/C2XA11IA044.md): Power Supply · inoperative · Mar 8, 2011 · N13929 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2913, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH AND EXIT ROW SIGN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APP
- [SDR C2XA11IA047](https://openairdocs.org/sdr/C2XA11IA047.md): Connector · loose · Mar 8, 2011 · N13929 · Emb EMB145EP · Light System Wiring
  > IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA11IA043](https://openairdocs.org/sdr/C2XA11IA043.md): Battery Pack · discharged · Mar 7, 2011 · N13929 · Emb EMB145EP · Emergency Lighting
  > IAH - FLIGHT 2093, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA296](https://openairdocs.org/sdr/C2XA10IA296.md): Power Supply · inoperative · Nov 18, 2010 · N13929 · Emb EMB145EP · Emergency Lighting
  > IAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON WHEN THE AIRCRAFT WAS DOWN POWERED WITH ALL SWITCHES IN CORRECT POSITIONS. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE
- [SDR C2XA10IA245](https://openairdocs.org/sdr/C2XA10IA245.md): Unknown · odor · Sep 4, 2010 · N13929 · Emb EMB145EP · Air Distribution System
  > IAH - FLIGHT 2104, THE CREW REPORTED A STRONG ODOR AFTER T/O. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED BOTH ENGINES WITH NO DEFECTS OR ODORS FOUND, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA10IA179](https://openairdocs.org/sdr/C2XA10IA179.md): Light · inoperative · Jun 18, 2010 · N13929 · Emb EMB145EP · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE NR 4 AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHT STRIP ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IAH MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE
- [SDR C2XA10IA144](https://openairdocs.org/sdr/C2XA10IA144.md): Skin · cracked · May 12, 2010 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > IAH - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA120](https://openairdocs.org/sdr/C2XA10IA120.md): Ballast · overheated · Apr 15, 2010 · N13929 · Emb EMB145EP · Lighting System
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE BALLAST 2A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA207](https://openairdocs.org/sdr/C2XA09IA207.md): Ballast · burned · Aug 19, 2009 · N13929 · Emb EMB145EP · Passenger Compartment Lighting
  > FLIGHT 2195, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE LAV. MAINTENANCE INSPECTED THE LAV, AND REMOVED THE LIGHT BULB FROM THE LAV CEILING LIGHT, AND PLACED THE LAV LIGHTING ON NEF-LV-05 CAT "D" CTL NUMBER 176224, AND TH
- [SDR C2XA09SH104](https://openairdocs.org/sdr/C2XA09SH104.md): Frame · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Main, Frame
  > DURING C-CHECK. FR 75 SHOWS SIGNS OF CORROSION BTW STR 2L-2R. REPAIRED FR 75 IAW EC 5310-01317. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH103](https://openairdocs.org/sdr/C2XA09SH103.md): Stringer · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STR 21L CORRODED BTW FR 65-66. REPAIRED STR 21L IAW IC 2009-145/01544. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH102](https://openairdocs.org/sdr/C2XA09SH102.md): Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Main, Attach Fittings
  > DURING C-CHECK, TOILET WASTE DRAIN VALVE SUPPORT CORRODED. REPAIRED TOILET WASTE DRAIN SUPPORT IAW SRM 53-31-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH101](https://openairdocs.org/sdr/C2XA09SH101.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 33. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH100](https://openairdocs.org/sdr/C2XA09SH100.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 33. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH099](https://openairdocs.org/sdr/C2XA09SH099.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 38. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH098](https://openairdocs.org/sdr/C2XA09SH098.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 29. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH097](https://openairdocs.org/sdr/C2XA09SH097.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED CENTER OMEGA BEAM IAW EMS 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH096](https://openairdocs.org/sdr/C2XA09SH096.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 59. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH095](https://openairdocs.org/sdr/C2XA09SH095.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 59. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH094](https://openairdocs.org/sdr/C2XA09SH094.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 49. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH093](https://openairdocs.org/sdr/C2XA09SH093.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 54. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH092](https://openairdocs.org/sdr/C2XA09SH092.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 49. REPAIRED LT OMEGA AT FR 49 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH091](https://openairdocs.org/sdr/C2XA09SH091.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 44. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH090](https://openairdocs.org/sdr/C2XA09SH090.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM FLANGE HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM AT FR 29 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH089](https://openairdocs.org/sdr/C2XA09SH089.md): Floor Support · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED OMEGA BEAM AT FR 23 IAW IC 2009-145/01857. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH088](https://openairdocs.org/sdr/C2XA09SH088.md): Splice · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LONGITUDINAL SPLICE CORRODED BETWEEN FR 61-66 STR 19L-20L. REPAIRED SPLICE IAW EMB 145 SRM 51-14-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH087](https://openairdocs.org/sdr/C2XA09SH087.md): Skin · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 70-73 STR 19L-19R. REPAIRED SKIN IAW EMB 145 SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH086](https://openairdocs.org/sdr/C2XA09SH086.md): Skin · corroded · Mar 25, 2009 · N13929 · Emb EMB145EP · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 60-61. REPLACED SKIN IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N13929-2015-12-29/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 = 'N13929' AND deregistration_id = 'N13929-2015-12-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13929-2015-12-29/reports

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