# Service difficulty reports: N13989

A list on [N13989](https://openairdocs.org/aircraft/N13989.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 · 96 reports

- [SDR ASOA2019111164060](https://openairdocs.org/sdr/ASOA2019111164060.md): Wire · broken · Nov 6, 2019 · N13989 · Emb EMB145LR · Light System Wiring
  > IAH - DURING MAINTENANCE INSPECTION THET #3 EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201909234053](https://openairdocs.org/sdr/ASOA201909234053.md): Inverter · inoperative · Sep 23, 2019 · N13989 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 4155, DURING MAINTENANCE INSPECTION THE LEFT HAND OVER WING EXIT SHROUD EXIT MARKER FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE #4 INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2019081547096](https://openairdocs.org/sdr/ASOA2019081547096.md): Mount · corroded · Aug 14, 2019 · N13989 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FORWARD INBOARD ACCESSORY GEARBOX MOUNT POINT CORRODED. REPAIRED AREA IN ACCORDANCE WITH TECHNICAL VARIANCE 204465 BY BLENDING OUT CORROSION AND APPLYING PROTECTIVE AREA.
- [SDR ASOA201908017093](https://openairdocs.org/sdr/ASOA201908017093.md): Skin · delaminated · Aug 1, 2019 · N13989 · Emb EMB145LR · Trailing Edge Flaps
  > A/C IS IN C-CHECK WHEN INSPECTION FOUND THE L/H I/B FLAP WITH AREAS OF IMPACT DAMAGE ON THE LOWER SIDE. UPON FURTHER INSPECTION FOUND THE AREAS TO BE DELAMINATION. REPAIRED THE AREA OF DELAMINATION IAW EMB 145 SRM51-72-03(6). ALL WORK WAS ACCOMPLISHED AND WIL
- [SDR ASOA2018062515159](https://openairdocs.org/sdr/ASOA2018062515159.md): Battery Pack · inoperative · Jun 21, 2018 · N13989 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE AFT EMERGENCY LIGHTS AND OVER WING LIGHTS WERE FOUND NOT TO ILLUMINATE. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201712217033](https://openairdocs.org/sdr/ASOA201712217033.md): Battery Pack · discharged · Dec 18, 2017 · N13989 · Emb EMB145LR · Emergency Lighting
  > FLOOR EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 3 IAW AMM 33-50-04 AND IPC 33-50-04 ITEM 30 FIG 01. OPS CHECKED GOOD.
- [SDR ASOA201712054064](https://openairdocs.org/sdr/ASOA201712054064.md): Battery Pack · weak · Dec 5, 2017 · N13989 · Emb EMB145LR · Emergency Lighting
  > IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR
- [SDR ASOA201712054063](https://openairdocs.org/sdr/ASOA201712054063.md): Battery Pack · weak · Dec 5, 2017 · N13989 · Emb EMB145LR · Emergency Lighting
  > IAH- DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 3 & 4 WERE FOUND TO BE NOT HOLDING A CHANRGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR
- [SDR ASOA20161005055](https://openairdocs.org/sdr/ASOA20161005055.md): Inverter · inoperative · Oct 5, 2016 · N13989 · Emb EMB145LR · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTS WERE INOPERATVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES NR 2, 3, AND 4 ALONG WITH INVERTER NR 6. OPS CHECKED GOOD.
- [SDR ASOA20160919049R](https://openairdocs.org/sdr/ASOA20160919049R.md): Wire · loose · Sep 19, 2016 · N13989 · Emb EMB145LR · Light System Wiring
  > THE AFT CABIN EMERGENCY EXIT OVERHEAD LIGHT INOPERATIVE. INSTALLED A LOOSE WIRE ON INTERIOR EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160916051](https://openairdocs.org/sdr/ASOA20160916051.md): Sign · inoperative · Sep 16, 2016 · N13989 · Emb EMB145LR · Emergency Lighting
  > EXIT SIGN IN CABIN WOULD NOT ILLUMINATE IN EMERGENCY LGT MODE. MAINTNENACE REPLACED THE EXIT SIGN ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA20160424024](https://openairdocs.org/sdr/ASOA20160424024.md): Light · inoperative · Apr 24, 2016 · N13989 · Emb EMB145 · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY LIGHT MID SECTION CEILING LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT ROW FORWARD EMERGENCY LIGHT. OPS CHECKS WERE GOOD.
- [SDR ASOA20160310010R](https://openairdocs.org/sdr/ASOA20160310010R.md): Light · malfunctioned · Mar 10, 2016 · N13989 · Emb EMB145LR · Emergency Lighting
  > THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 18 WAS INOPERATIVE. THE SYSTEM WAS RESET AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150831049](https://openairdocs.org/sdr/ASOA20150831049.md): Light · unknown · Aug 31, 2015 · N13989 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED EXIT LIGHT ABOVE EXIT ROW WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS. OPS CHECKS WERE GOOD.
- [SDR ASOA20150421100](https://openairdocs.org/sdr/ASOA20150421100.md): Fitting · cracked · Apr 21, 2015 · N13989 · Emb EMB145LR · Engine Mount Section
  > DURING C-CK NR 1 ENGINE FWD LOWER YOKE FITTING CRACKED. R & R NR 1 ENGINE FWD LOWER YOKE FITTING IAW EC5450-01142. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150421099V](https://openairdocs.org/sdr/ASOA20150421099V.md): Structure · corroded · Apr 21, 2015 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CK. CARGO DOOR LOWER CUTOUT STRUCTURE IS CORRODED. R & R CARGO DOOR LOWER STRUCTURE IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150420098](https://openairdocs.org/sdr/ASOA20150420098.md): Floor Support · corroded · Apr 20, 2015 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CK. RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EC5320-02031. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150414097](https://openairdocs.org/sdr/ASOA20150414097.md): Frame · cracked · Apr 14, 2015 · N13989 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK. FRAME 10 CRACKED UNDER RT DV WINDOW. REPAIRED FRAME 10 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140309035](https://openairdocs.org/sdr/ASOA20140309035.md): Inverter · inoperative · Mar 9, 2014 · N13989 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE NR 1 EMERGENCY LIGHT INVERTER WAS DISCOVERED INOPERATIVE. MX R & R NR 1 INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130504147](https://openairdocs.org/sdr/ASOA20130504147.md): Beam · corroded · May 4, 2013 · N13989 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK CARGO CUTOUT LOWER BEAM HAS CORROSION (LOCAL LEVEL 2) BETWEEN FRAMES 65-66. MX R & R CARGO LOWER CUTOUT BEAM AT FRAME 65-68 IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130504146](https://openairdocs.org/sdr/ASOA20130504146.md): Structure · corroded · May 4, 2013 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO DOOR FWD LWR INTERNAL CUTOUT CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUTOUT FWD SHEAR CLIP AT FRAME 65 IAW EC5320-01494. FOUND TO BE MAJOR REPAIR IAW EC5320-01494. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130504145](https://openairdocs.org/sdr/ASOA20130504145.md): Skin · damaged · May 4, 2013 · N13989 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK FUSELAGE SKIN FRAMES 15-16 STRINGER 3R-4R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAMES 15-16 STRINGERS 3R-4R IAW SRM 53-23-01 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130504144](https://openairdocs.org/sdr/ASOA20130504144.md): Skin · damaged · May 4, 2013 · N13989 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-3R HAS LIGHTNING STRIKE. MX PERFORMED REPAIR OF FUSELAGE SKIN BETWEEN FRAMES 38-39, STRINGER 1R-3R IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326024C](https://openairdocs.org/sdr/ASOA20130326024C.md): Light · inoperative · Mar 26, 2013 · N13989 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, THE EMERGENCY AISLE PATH LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT AND OPS CHECKED GOOD.
- [SDR ASOA20120813128](https://openairdocs.org/sdr/ASOA20120813128.md): Lamp · inoperative · Aug 11, 2012 · N13989 · Emb EMB145LR · Emergency Lighting
  > EMERGENCY DOME LIGHT AFT OF OVER-WING CEILING EXIT INOPERATIVE. REPLACED BULB OPS CHECK GOOD ACFT, RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20120321033](https://openairdocs.org/sdr/ASOA20120321033.md): Charger · inoperative · Mar 21, 2012 · N13989 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, THE NR 2 EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.
- [SDR C2XA11IA189](https://openairdocs.org/sdr/C2XA11IA189.md): Unknown · malfunctioned · Aug 31, 2011 · N13989 · Emb EMB145LR · Emergency Lighting
  > STL - FLIGHT 3150, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT POWER OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND ALL SWITCHES TO BE SET CORRECTLY, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND
- [SDR C2XA11RI143](https://openairdocs.org/sdr/C2XA11RI143.md): Smoke Detector · defective · Aug 25, 2011 · N13989 · Emb EMB145LR · Smoke Detection
  > FLIGHT 2517 - MHT - FLIGHT CREW REPORTED LAV SMOKE DETECT SYSTEM WOULD NOT TEST. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA11TY095](https://openairdocs.org/sdr/C2XA11TY095.md): Skin · corroded · Jun 27, 2011 · N13989 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > CORROSION ON INTERIOR SKIN BETWEEN FRAMES 14-15, STRINGER 21L-19R. REMOVED AND REPLACED SKIN PANEL IAW EC5330-02440.
- [SDR C2XA11TY094](https://openairdocs.org/sdr/C2XA11TY094.md): Frame · corroded · Jun 26, 2011 · N13989 · Emb EMB145LR · Fuselage Main, Frame
  > AFT FUSELAGE HAS CORROSION ON FRAME 80 UNDER THE APU GENERATOR "L" BAR GROUNDING ATTACHMENT POINT. BLENDED OUT DAMAGE, PERFORMED NDT- NO DEFECTS NOTED. CONTINUED ON WITH REPAIR IAW EC5310-01544.
- [SDR C2XA11TY093](https://openairdocs.org/sdr/C2XA11TY093.md): Guide · worn · Jun 25, 2011 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS - A/C IN FOR C-CHECK WHEN INSPECTION FOUND THE RIGHT O/B ELEVATOR CABLE AND RIGHT I/B RUDDER CABLES CHAFING AGAINST THE TEFLON GUIDE AT FR39, STR 19R-21R. MAINTENANCE CHANGED OUT THEN CABLES AND TELFON GUIDE IAW EC5320--01463. A/C WILL BE RELEASED AT THE
- [SDR C2XA11TY089](https://openairdocs.org/sdr/C2XA11TY089.md): Structure · corroded · Jun 20, 2011 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CARGO DOOR CORRODED ON STRUCTURE FRAME 64 ADJACENT TO CUTOUT. INSTALLED DOUBLER IAW EC5320-01479 REPAIR 3.
- [SDR C2XA11TY059](https://openairdocs.org/sdr/C2XA11TY059.md): Skin · damaged · May 6, 2011 · N13989 · Emb EMB145LR · Elevator, Plate/Skin
  > LT ELEVATOR L/E SKIN HAD A TEAR/CRACK OF 9MM FOUND IN UPPER TIP SKIN AT YH=3022. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW ETD2011-145/02568.
- [SDR C2XA11TY057](https://openairdocs.org/sdr/C2XA11TY057.md): Light · inoperative · May 4, 2011 · N13989 · Emb EMB145LR · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145AMM 33-50-10, OPS CHECK GOOD.
- [SDR C2XA10IA169](https://openairdocs.org/sdr/C2XA10IA169.md): Adc · faulty · Jun 7, 2010 · N13989 · Emb EMB145EP · Air Data Computer
  > FLIGHT 2734 - DURING CRUISE AT 36,000 FEET THE CAPTAIN'S AIRSPEED INDICATION STUCK AT 215 KIAS FOR 10 TO 15 MINUTES. AT THAT TIME THE STANDBY AND FIRST OFFICER'S AIRSPEED INDICATIONS WERE OPERATING NORMALLY. UPON DESCENT THE CREW LOST THE CAPTAINS AND FIRST
- [SDR C2XA09CL112](https://openairdocs.org/sdr/C2XA09CL112.md): Light · malfunctioned · Sep 4, 2009 · N13989 · Emb EMB145LR · Emergency Lighting
  > CLE FLIGHT 2915 THE CREW REPORTED THE LEFT OVERWING EMERGENCY EXIT LIGHT BECOMES ILLUMINATED AFTER NORMAL AIRCRAFT SHUT DOWN. AFTER 7TH POWER DOWN THE LIGHT SEEMED TO OPERATE NORMALLY. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHTS AND OPERATIONAL CHEC
- [SDR C2XA09SH236](https://openairdocs.org/sdr/C2XA09SH236.md): Crossbeam · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CROSSBEAM BETWEEN LT AND CENTER OMEGA BEAM AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM AT FRAME 20 IAW EC5320-01024 REV B AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH235](https://openairdocs.org/sdr/C2XA09SH235.md): Bracket · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CROSSBEAM L-BRACKET AT FRAME 23 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSBEAM L-BRACKET AT FRAME 23 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH234](https://openairdocs.org/sdr/C2XA09SH234.md): Sill · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT FLOOR SILL FRAME 42-47 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED RT FLOOR SILL AT FRAME 42-47 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH233](https://openairdocs.org/sdr/C2XA09SH233.md): Sill · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORRODED NUT PLATES AT FRAMES 20-22. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL NUT PLATES IAW EMB-145 SRM 51-40-09 AND CPM 51-21-07. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH232](https://openairdocs.org/sdr/C2XA09SH232.md): Sill · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SERVICE DOOR FORWARD SILL HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR FORWARD SILL IAW SRM 51-10-03 AND CPM 51-20-06. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH231](https://openairdocs.org/sdr/C2XA09SH231.md): Plate · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SHELL PLATE AT FRAME 22 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH230](https://openairdocs.org/sdr/C2XA09SH230.md): Plate · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SHELL PLATE AT FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED SHELL PLATE AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH229](https://openairdocs.org/sdr/C2XA09SH229.md): Buttstrap · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP FRAMES 20-22 HAS CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BUTTSTRAP AT FRAME 20-22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH228](https://openairdocs.org/sdr/C2XA09SH228.md): Floor Support · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 71. MAINTENANCE COMPLETED THE REMOVAL AND INSTALLATION OF NEW CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 61-71 IAW EMB-145 SRM 53-31-10 AND EC5320-01137 REV ORIG. THE AIR
- [SDR C2XA09SH227](https://openairdocs.org/sdr/C2XA09SH227.md): Beam · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT BEAM CORRODED (LEVEL 2 WIDESPREAD) IN SEVERAL AREAS. MAINTENANCE PERFORMED AND COMPLETED INSTALLATION OF CARGO DOOR LOWER CUTOUT BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH226](https://openairdocs.org/sdr/C2XA09SH226.md): Floor Support · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR IAW EMB-145 SRM 51-10-03 AND CPM 51-20-06. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH225](https://openairdocs.org/sdr/C2XA09SH225.md): Frame · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK RT CARGO FRAME 61 CORRODED (LEVEL 2 LOCAL) AT 15R BEHIND CARBON BEAM. MAINTENANCE PERFORMED REPAIR IAW IC2009-145/05601. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.
- [SDR C2XA09SH224](https://openairdocs.org/sdr/C2XA09SH224.md): Sill · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 69-73 HAS VARIOUS AREAS OF CORROSION (LEVEL 2 WIDESPREAD). MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED REPAIR ON RT FLOOR SILL AT FRAME 69-73 AFFECTED AREAS IAW EMB-145 EC5320-01137 REV ORIG AND SRM 51
- [SDR C2XA09SH223](https://openairdocs.org/sdr/C2XA09SH223.md): Sill · corroded · Aug 1, 2009 · N13989 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT FLOOR SILL AT FRAME 61-66 HAS CORROSION (LEVEL 2 WIDESPREAD) ON SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED NUT PLATES AND COMPLETED REPAIR ON AFFECTED AREAS ON RT FLOOR SILL AT FRAME 61-66 IAW EMB-145 EC5320-01131 REV ORIG AND SRM

Next page: https://openairdocs.org/aircraft/N13989/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 = 'N13989' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N13989/reports

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