# Service difficulty reports: N13990, cancelled Jul 15, 2011

A list on [N13990, cancelled Jul 15, 2011](https://openairdocs.org/deregistered/N13990-2011-07-15.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 · 56 reports

- [SDR C2XA11SH034](https://openairdocs.org/sdr/C2XA11SH034.md): Beam · corroded · Feb 1, 2011 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT CORRODED BETWEEN FR 65 & 68. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH033](https://openairdocs.org/sdr/C2XA11SH033.md): Skin · cracked · Jan 31, 2011 · N13990 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK LT SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 & 80. REPAIRED SKIN IAW EC5330-02352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH032](https://openairdocs.org/sdr/C2XA11SH032.md): Skin · cracked · Jan 31, 2011 · N13990 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK - RT SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 75 & 80. REPAIRED SKIN IAW EC5330-02352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10TY122](https://openairdocs.org/sdr/C2XA10TY122.md): Sensor · contaminated · Sep 9, 2010 · N13990 · Emb EMB145LR · Engine Temperature Indicating System
  > TYS - A/C WAS DIVERTED TO TYS FROM BNA DUE TO E1 OVERTEMP. TYS MAINTENANCE FOUND A LOOSE B-NUT THAT WAS LEAKING HOT AIR ONTO A TEMP SENSOR. TIGHTEN B-NUT AND OPD CHECK GOOD AND WAS RELEASED BACK TO SERVICE.
- [SDR C2XA10IA024](https://openairdocs.org/sdr/C2XA10IA024.md): Control Panel · inoperative · Jan 17, 2010 · N13990 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE CABIN / EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA023](https://openairdocs.org/sdr/C2XA10IA023.md): Battery Pack · discharged · Jan 17, 2010 · N13990 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2314, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NUMBER TWO EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV
- [SDR C2XA10IA022](https://openairdocs.org/sdr/C2XA10IA022.md): Battery Pack · discharged · Jan 17, 2010 · N13990 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2314, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NUMBER TWO EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS
- [SDR C2XA09SH350](https://openairdocs.org/sdr/C2XA09SH350.md): Duct · dirty · Oct 20, 2009 · N13990 · Emb EMB145LR · Cabin Cooling System
  > PACK NR 1 PRODUCES BURNING SMELL WHEN ON. MAINTENANCE PERFORMED EMB-145 FIM TASK 21-20-00-810-801-A. MAINTENANCE ALSO CLEANED NR 1 PACK RAM AIR DUCT. MAINTENANCE REMOVED NR 1 PACK RAM AIR DUCT AND RE-INSTALLED NR 1 PACK RAM AIR DUCT IAW EMB-145 AMM 21-20-04
- [SDR C2XA09TY241](https://openairdocs.org/sdr/C2XA09TY241.md): Bulb · blown · Sep 18, 2009 · N13990 · Emb EMB145LR · Fire Detection
  > TYS - A/C AT GATE IN TYS WHEN CREW COMPLIED WITH FIRE TEST OF THE BAGGAGE COMPARTMENT AND TEST FAIL. MAINTENANCE REMOVED AND REPLACED THE BULBS AND OPS CHECK GOOD IAW EMB AMM 20-13-04. A/C RELEASED BACK TO SERVICE.
- [SDR C2XA09CL073](https://openairdocs.org/sdr/C2XA09CL073.md): O-Ring · deteriorated · May 22, 2009 · N13990 · Emb EMB145LR · Pneumatic Distribution System
  > EWR - FLIGHT 2038 - THE CREW REPORTED A BLEED 1 LEAK IN ROUTE TO MSN. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT O-RINGS IN THE AFT AVIONICS BAY. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09IA120](https://openairdocs.org/sdr/C2XA09IA120.md): Clamp · leaking · May 8, 2009 · N13990 · Emb EMB145LR · Pneumatic Distribution System
  > IAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPPER BLEED DUCT CLAMP IN THE CARGO COMPARTMENT, OPERATIONAL AND LEAK C
- [SDR C2XA09IA119](https://openairdocs.org/sdr/C2XA09IA119.md): O-Ring · blown · May 8, 2009 · N13990 · Emb EMB145LR · Pneumatic Distribution System
  > IAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPPER O-RING IN THE CARGO COMPARTMENT, OPERATIONAL AND LEAK CHECKED WIT
- [SDR C2XA09IA072](https://openairdocs.org/sdr/C2XA09IA072.md): Structure · leaking · Mar 10, 2009 · N13990 · Emb EMB145LR · Wing Miscellaneous Structure
  > DURING CRUISE A REPORT OF FUEL LEAKING FROM THE LEFT WING WAS MADE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FULLY FUELED THE WING TANKS HOWEVER A LEAK COULD NOT BE CONFIRMED. THE AIRCRAFT WAS THEN RETURNED TO SERV
- [SDR C2XA09SH047](https://openairdocs.org/sdr/C2XA09SH047.md): Floor Support · corroded · Feb 1, 2009 · N13990 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LEFT OMEGA BEAM HAS CORROSION AT SECTION AROUND THE CARBON FIBER CROSS-MEMBER AT FRM 19. MAINTENANCE REPAIRED LT OMEGA BEAM AT SECTION AROUND THE CARBON FIBER CROSS-BEAM MEMBER AT FRM 19 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROV
- [SDR C2XA09SH046](https://openairdocs.org/sdr/C2XA09SH046.md): Support · corroded · Feb 1, 2009 · N13990 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CORROSION ON WASTE VALVE SUPPORT BEHIND SERVICE PANEL. MAINTENANCE INSTALLED NEW WASTE DRAIN DUMP VALVE SUPPORT ASSY IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08IA197](https://openairdocs.org/sdr/C2XA08IA197.md): Connector · loose · Aug 26, 2008 · N13990 · Emb EMB145LR · Light System Wiring
  > IAH DURING A CHECK INSPECTION THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MX RECONNECTED A LOOSE PLUG CONNECTED TO THE LIGHT, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2X2008F00020](https://openairdocs.org/sdr/C2X2008F00020.md): Pump · leaking · Aug 14, 2008 · N13990 · Emb EMB145LR · Hydraulic Pump (Electric/Engine), Main
  > ACFT EN ROUTE FROM EWR TO TYS WHEN THE HYD 1 SYSTEM MESSAGE WAS HYD LOW QUANTITY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG DRIVEN HYD PUMP IAW EMB 145AMM 29-10-03 AND REMOVED AND REPLACED THE NR 1 ELECTRIC DRIVEN PUMP IAW EMB 145 AMM 29-10-04. OPS AND L
- [SDR C2XA08CL075](https://openairdocs.org/sdr/C2XA08CL075.md): Connector · loose · Jun 29, 2008 · N13990 · Emb EMB145LR · Light System Wiring
  > DURING ROUTINE MAINTENANCE THE COCKPIT STEP EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTOR ON THE COCKPIT STEP EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. (S)
- [SDR C2XA07IA205](https://openairdocs.org/sdr/C2XA07IA205.md): Connector · loose · Sep 15, 2007 · N13990 · Emb EMB145LR · Light System Wiring
  > EWR - FLIGHT 2762 THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE VICINITY SEAT 1A. FOUND LUMINESCENT LIGHT BULB ARCHING AT CONTACT PINS, LIGHT BULB REMOVED; SYSTEM CHECKED NO ARCHING NO SMELL. A/C RELEASED IAW MEL 33-20-00/1 CAT C CONTROL 129030, AND THE
- [SDR C2XA07RI082](https://openairdocs.org/sdr/C2XA07RI082.md): Light · defective · Sep 14, 2007 · N13990 · Emb EMB145LR · Passenger Compartment Lighting
  > FLT 2754 - YOW - CREW REPORTED ELECTRICAL ODOR FROM SEAT 1A AREA. MX FOUND FLUORESCENT LIGHT ARCING AT CONTACT. MX REMOVED AND REPLACED LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07SH022](https://openairdocs.org/sdr/C2XA07SH022.md): Fitting · corroded · Apr 15, 2007 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON SHEAR CLIPS AT FRAMES 65 & 68. MAINTENANCE REPAIRED SHEAR CLIPS AT FRAMES 65 & 68 IAW EC 5330-01458. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07SH021](https://openairdocs.org/sdr/C2XA07SH021.md): Firewall · chafed · Apr 15, 2007 · N13990 · Emb EMB145LR · Fuselage Main, Bulkhead
  > SHV - DURING C-CHECK MAINTENANCE APU FIREWALL LOWER SECTION HAS RIVET INDENTATION. MAINTENANCE REPAIRED APU FIREWALL AT FRAME 81 LOWER SECTION IAW EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA07SH019](https://openairdocs.org/sdr/C2XA07SH019.md): Floor Support · corroded · Apr 14, 2007 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20 AND FRAME 23. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 20 TO 23 IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA06IA144](https://openairdocs.org/sdr/C2XA06IA144.md): Elevator · malfunctioned · Sep 5, 2006 · N13990 · Emb EMB145LR · Elevator Control System
  > DAL - FLIGHT 2923, THE CREW REPORTED THAT THE ELEVATOR WAS NON-RESPONSIVE UNDER LOAD IN FLIGHT. THE AIRCRAFT LANDED AT DAL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CONTROL CABLE RUNS, ELEVATOR AND TABS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SU
- [SDR C2XA06CL060](https://openairdocs.org/sdr/C2XA06CL060.md): Smoke · detected · Jun 20, 2006 · N13990 · Emb EMB145LR · Air Distribution System
  > CLE FLIGHT 2705 THE CREW REPORTED NR 1 PACK NOISE FROM THE ACM WITH SMELL AND SMOKE FROM THE SIDE VENTS. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 21-51-00/1. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACM.OPERATIONAL CHECKS WERE GOOD..
- [SDR C2XA06IA051](https://openairdocs.org/sdr/C2XA06IA051.md): Retainer · damaged · Mar 28, 2006 · N13990 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > IAH - FLIGHT 2971, THE CREW REPORTED LOSS OF ENGINE TWO OIL QUANTITY AND PRESSURE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE, AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR GENERATOR GARLOCK SEAL. OPERAT
- [SDR C2XA04CL106](https://openairdocs.org/sdr/C2XA04CL106.md): Wire · loose · Oct 11, 2004 · N13990 · Emb EMB145LR · Light System Wiring
  > DURING MAINTENANCE THE NR 2 AND 3 AISLE PATH EMERGENCY LIGHTING WERE INOPERATIVE. RESECURED GROUND WIRE AND SYSTEM CHECKED GOOD.
- [SDR C2XA04BT078](https://openairdocs.org/sdr/C2XA04BT078.md): Light · inoperative · Jul 15, 2004 · N13990 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED, (STRIP OF EMERGENCY AISLE PATH LIGHTS NOT WORKING.) MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 33-50-00/02 CATEGORY C-PLACARD NR 044167 AND RETURNED THE AIRCRAFT TO SERVICE. ON IAD RON 07/16/2004 MAINTENANCE TROUBLESHOT AND REMOVED AND REPLA
- [SDR C2XA03BT114](https://openairdocs.org/sdr/C2XA03BT114.md): Proximity Sensor · faulty · Nov 28, 2003 · N13990 · Emb EMB145LR · Landing Gear Position and Warning
  > CREW REPORTED, AFTER GEAR RETRACTION, LANDING GEAR INDICATED UP. OBVIOUS WIND NOISE SUSPECTED GEAR DOORS DID NOT RETRACT. AIRCRAFT REPORTEDLY HAD EXCESSIVE DRAG IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SEQUENCE PROXIMITY SENSOR IAW
- [SDR C2XA03BT077](https://openairdocs.org/sdr/C2XA03BT077.md): Panel · faulty · Aug 5, 2003 · N13990 · Emb EMB145LR · Smoke Detection
  > EWR CO2879, CREW REPORTED, LAV SMOKE WARNING DURING FLIGHT WITH ASSOCIATED SMOKE ALARM. PERFORMED QRH. NO VISIBLE SIGN OF SMOKE OR FIRE. FLIGHT CONTINUED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTION PANEL IN GALLEY IAW EMB145 AMM 26-14-02
- [SDR C2XA03TY098](https://openairdocs.org/sdr/C2XA03TY098.md): Floor Support · corroded · Jul 27, 2003 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 2C INSPECTION THE LT LAV SIDEWALL FLOOR SUPPORT HAD CORRODED NUT PLATED AND RIVETS FWD AND AFT. MAINTENANCE REMOVED AND REPLACED THE LT LAV FLOOR SUPPORT WITH ALL NEW HARDWARE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WIL
- [SDR C2XA03TY097](https://openairdocs.org/sdr/C2XA03TY097.md): Floorbeam · corroded · Jul 27, 2003 · N13990 · Emb EMB145LR · Fuselage Main, Floor Beam
  > TYS- DURING A SCHEDULED 2C INSPECTION THE LT AND RT AISLE OMEGA BEAM AT THE SECOND CARBON CROSS BAR WAS FOUND CORRODED. MAINTENANCE CUT OUT DAMAGED SECTIONS ON LT AND RT FLOORBEAM, FAB EXTERNAL ANGLE SHIM AND FILLER ALODINED, PRIMED, PAINTED AND INSTALLED FA
- [SDR C2XA03TY095](https://openairdocs.org/sdr/C2XA03TY095.md): Sill · corroded · Jul 23, 2003 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT. SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 9394, FABRICATED AND INSTALLED A DOUBLER. IAW EMB-GST-1927/02A, THE REPAIR WAS SATISFACTORY AND THE A
- [SDR C2XA03TY094](https://openairdocs.org/sdr/C2XA03TY094.md): Sill · corroded · Jul 23, 2003 · N13990 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 9394, FABRICATED AND INSTALLED A DOUBLER IAW-EMB-GST-1927/02A. THE REPAIR WAS SATISFACTORY AND THE AI
- [SDR C2XA03TY093](https://openairdocs.org/sdr/C2XA03TY093.md): Seat Track · corroded · Jul 23, 2003 · N13990 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED INSPECTION THE LW1, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06.
- [SDR C2XA03TY092](https://openairdocs.org/sdr/C2XA03TY092.md): Seat Track · corroded · Jul 23, 2003 · N13990 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED INSPECTION THE ROW 2, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06.
- [SDR C2XA03IA021](https://openairdocs.org/sdr/C2XA03IA021.md): Battery Pack · discharged · Feb 14, 2003 · N13990 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE BATTERY PACK, PERFORMED A OPERATIONAL CHECK AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03IA020](https://openairdocs.org/sdr/C2XA03IA020.md): Battery Pack · discharged · Feb 14, 2003 · N13990 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA02CL173](https://openairdocs.org/sdr/C2XA02CL173.md): Proximity Sensor · failed · Aug 16, 2002 · N13990 · Emb EMB145LR · Landing Gear Position and Warning
  > CLE FLIGHT#3222 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF.A EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.AFTER EXITING RUNWAY THE MESSAGE DISAPPEARED.THEY ALSO REPORTED ENGINE 1 AND 2 THRUST REVERSER DISA
- [SDR C2XA02CL130](https://openairdocs.org/sdr/C2XA02CL130.md): Inverter · faulty · Jun 8, 2002 · N13990 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE FLOOR PROXIMITY STRIP LIGHTS FROM ROW 12 TO LAST ROW WILL NOT ILLUMINATE.MAINTENANCE REPLACED THE #6 EMERGENCY LIGHT AC/DC INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA02CL119](https://openairdocs.org/sdr/C2XA02CL119.md): Odor · detected · May 31, 2002 · N13990 · Emb EMB145LR · Air Distribution System
  > CLE FLIGHT 3248 THE CREW REPORTED THE APU CAUSES A SMELL IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED A OPERATIONAL CHECK OF THE APU AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL237](https://openairdocs.org/sdr/C2XA01CL237.md): Connector · corroded · Dec 4, 2001 · N13990 · Emb EMB145LR · Emergency Equipment
  > CLE FLIGHT#3308 THE CREW REPORTED A BURNING SMELL COMING FROM THE #2 HOT JUG.MAINTENANCE RELEASED AIRCRAFT I/A/W MEL 25-60-02/3.MAINTENANCE CLEARED THE MEL BY REPLACING THE #2 HOT JUG CONNECTOR.OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA01TY115](https://openairdocs.org/sdr/C2XA01TY115.md): Stringer · chafed · Sep 13, 2001 · N13990 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > TYS During a scheduled inspection, Stringer 19R was found chafed at frame 53, Maintenance blended chafed area, performed dye-penetrant inspection, alodined, primed and restored top coat, I.A.W.-EMB-145-GST-2979/01. The repair was satisfactory and the aircraft
- [SDR C2XA01TY114](https://openairdocs.org/sdr/C2XA01TY114.md): Stringer · chafed · Sep 13, 2001 · N13990 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > TYS During a scheduled inspection, Stringer 19L was found chafed at frame 53. Maintenance blended chafed area, performed dye-penetrant inspection, alodined, primed and restored top coat I.A.W.-EMB-GST-2979/01. The repair was satisfactory and the aircraft will
- [SDR C2XA01TY113](https://openairdocs.org/sdr/C2XA01TY113.md): Battery · discharged · Sep 13, 2001 · N13990 · Emb EMB145LR · Emergency Lighting
  > TYS DURING A SCHEDULED INSPECTION, THE EMERGENCY AISLE LIGHTING SYSTEM BATTERY SUPPLY NUMBER 4 WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY, IAW EMB-145-MM-33-50-04. OPERATIONAL CHECKS WERE GOOD. THE REPAIR WAS SATISFACTORY
- [SDR C2XA01TY112](https://openairdocs.org/sdr/C2XA01TY112.md): Beam · corroded · Sep 13, 2001 · N13990 · Emb EMB145LR · Fuselage Main, Floor Beam
  > TYS During a scheduled inspection, The left omega beam was found corroded at frame 20. Maintenance removed damaged area, fabricated repair filler, shims & external angle. Alodined, primed and installed repair parts. I.A.W.-EMB-135/145-SRM-51-40-02, 53-21-10
- [SDR C2XA01TY111](https://openairdocs.org/sdr/C2XA01TY111.md): Attach Fitting · gouged · Sep 13, 2001 · N13990 · Emb EMB145LR · Ailerons
  > TYS DURING A SCHEDULED INSPECTION, THE LEFT AILERON CENTER INBOARD ATTACH FITTING WAS FOUND GOUGED. MAINTENANCE BLENDED OUT THE DAMAGED AREA, PERFORMED DYE-PENETRANT INSPECTION, ALODINED, PRIMED AND PAINTED THE AILERON FITTING IAW-EMB-145-GST-3059/01. THE R
- [SDR C2XA01TY110](https://openairdocs.org/sdr/C2XA01TY110.md): Tube · bent · Sep 13, 2001 · N13990 · Emb EMB145LR · Extinguishing System
  > TYS During a scheduled inspection. The left engine fire extingisher line was found bent. Maintenance removed and replaced the fire extingisher line I.A.W.-EMB-145-MM-26-21-06 and SB # 145-26-0008 page 12 & 13. The repair was satisfactory and the aircraft will
- [SDR C2XA01TY109](https://openairdocs.org/sdr/C2XA01TY109.md): Skin · chafed · Sep 13, 2001 · N13990 · Emb EMB145LR · Cargo/Baggage Doors
  > TYS DURING A SCHEDULED INSPECTION, THE CARGO DOOR SKIN AROUND THE EXTERIOR HANDLE WAS FOUND CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA, PERFORMED DYE-PENETRENT INSPECTION, ALODINED, PRIMED AND PAINTED AREA IAW-EMB-145-GST-3098/01. THE REPAIR WAS SATISFACT
- [SDR C2XA01TY108](https://openairdocs.org/sdr/C2XA01TY108.md): Step · corroded · Sep 6, 2001 · N13990 · Emb EMB145 · Entrance Stairs
  > TYS DURING A SCHEDULED INSPECTION THE FLOOR GUSSET LOCATED AFT OF THE COCKPIT ENTRANCE STEP WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AROUND THE RIVETS. MAINTENANCE TREATED THE CORRODED AREAS AND REMOVED AND REPLACED THE RIVETS IAW EMB-145 SRM 51-40-02 AN

Next page: https://openairdocs.org/deregistered/N13990-2011-07-15/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 = 'N13990' AND deregistration_id = 'N13990-2011-07-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N13990-2011-07-15/reports

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