# Service difficulty reports: N14916

A list on [N14916](https://openairdocs.org/aircraft/N14916.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 · 59 reports

- [SDR ASOA201904247039](https://openairdocs.org/sdr/ASOA201904247039.md): Skin · cracked · Apr 24, 2019 · N14916 · Emb EMB145LR · Nacelle/Pylon, Plate/Skin
  > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE RIGHT ENGINE PYLON/B SIDE SKIN CRACKED IN TWO PLACES. MAINTENANCE REPAIRED THE CRACK AT THE PYLON FIREWALL IAW ECTC ETD 2019-145048086. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK
- [SDR ASOA201904237038](https://openairdocs.org/sdr/ASOA201904237038.md): Skin · chafed · Apr 23, 2019 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > A/C IS IN C-CHECK WHEN INSPECTION FOUND A CHAFE AT FRAME 70 BETWEEN STRINGER12R AND 13R. MAINTENANCE PERFORMED REPAIR PROCEDURES IAW ECTC ETD2019-145-048747.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201905167048](https://openairdocs.org/sdr/ASOA201905167048.md): Door Frame · corroded · Apr 22, 2019 · N14916 · Emb EMB145LR · Fuselage Main, Structure
  > SERVICE DOOR CUT-OUT CORRODED BELOW AFT LOWER STOP. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER. AIRCRAFT WAS IN C CHECK BUT IS NOW RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA201811247185](https://openairdocs.org/sdr/ASOA201811247185.md): Fcu · faulty · Nov 23, 2018 · N14916 · Emb EMB145LR · APU Engine Fuel and Control
  > HEAVY EXHAUST GAS SMELL AFTER STARTING THE APU. REMOVED AND REPLACED THE APU FUEL SOLENOID VALVE IAW HSMM 49-31-02 AND FCU IAW HSMM 49-32-01. OPS AND LEAK CHECKS WERE SATISFACTORY.
- [SDR ASOA201808304045](https://openairdocs.org/sdr/ASOA201808304045.md): Connector · broken · Aug 30, 2018 · N14916 · Emb EMB145LR · Light System Wiring
  > SHV - FLIGHT 4309 THE CREW REPORTED SMOKE IN THE FLIGHT DECK AND DIVERTED TO SHV. THE AIRCRAFT LANDED IN SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE MAGNETIC COMPASS LIGHTING CONNECTOR ON MEL 33-10-00 CAT C AND THE AIRCRAFT WAS
- [SDR ASOA201803284018](https://openairdocs.org/sdr/ASOA201803284018.md): Battery Pack · discharged · Mar 30, 2018 · N14916 · Emb EMB145LR · Emergency Lighting
  > THE AISLE EMERGENCY LIGHTING BETWEEN SEATS 8 - 18 WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160912050C](https://openairdocs.org/sdr/ASOA20160912050C.md): Light · inoperative · Sep 12, 2016 · N14916 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP BY ROW 9 AND 10 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND OPS CHECKS WERE GOOD.
- [SDR ASOA20160410034](https://openairdocs.org/sdr/ASOA20160410034.md): Bulb · burned · Apr 10, 2016 · N14916 · Emb EMB145LR · Passenger Compartment Lighting
  > THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LIGHT BULB AT SEAT 8A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140718225](https://openairdocs.org/sdr/ASOA20140718225.md): Floor Support · corroded · Jul 18, 2014 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 43-44. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01958. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140718224V](https://openairdocs.org/sdr/ASOA20140718224V.md): Floor Support · corroded · Jul 18, 2014 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140718223V](https://openairdocs.org/sdr/ASOA20140718223V.md): Floor Support · corroded · Jul 18, 2014 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140718222](https://openairdocs.org/sdr/ASOA20140718222.md): Floor Support · corroded · Jul 18, 2014 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 33-34 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140718221](https://openairdocs.org/sdr/ASOA20140718221.md): Beam · corroded · Jul 18, 2014 · N14916 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130416029](https://openairdocs.org/sdr/ASOA20130416029.md): Light · inoperative · Apr 16, 2013 · N14916 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, THE EMERGENCY LIGHT STRIP BY SEATS 1A/ 2A WOULD NOT TURN ON. MX REPLACED THE AISLE PATH LIGHT STRIP. OPS CHECKS WERE GOOD.
- [SDR ASOA20120917105V](https://openairdocs.org/sdr/ASOA20120917105V.md): Sill · corroded · Sep 17, 2012 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL CORRODED FR 65-66. MX R & R CARGO DOOR CUTOUT LOWER SILL BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201112120017](https://openairdocs.org/sdr/ASOA201112120017.md): Unknown · odor · Dec 12, 2011 · N14916 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED A STRONG JET FUEL ODOR DURING APU START. MX PERFORMED APU OPS CHECKS AND NO FUEL ODOR WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR C2XA10IA269](https://openairdocs.org/sdr/C2XA10IA269.md): Connector · dirty · Oct 18, 2010 · N14916 · Emb EMB145LR · Light System Wiring
  > IAH - FLIGHT 2093, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN
- [SDR C2XA10IA254](https://openairdocs.org/sdr/C2XA10IA254.md): Fmu · defective · Sep 15, 2010 · N14916 · Emb EMB145LR · Fuel Controlling System
  > IAH - FLIGHT 3151, THE CREW REPORTED A LOW N1 MASTER WARNING ON TAKEOFF ROLE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO FPMU, OPERATIONALLY AND LEAK CHEC
- [SDR C2XA10SH290](https://openairdocs.org/sdr/C2XA10SH290.md): Floor Support · corroded · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR AND INSTALLED A DOUBLER ON RT OMEGA BEAM AT FRAME 23 IAW EC5320-01443 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH289](https://openairdocs.org/sdr/C2XA10SH289.md): Structure · corroded · Sep 8, 2010 · N14916 · Emb EMB145LR · Service Doors
  > SHV - DURING C-CHECK SERVICE DOOR BOTTOM NUT PLATE HOLES CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FROM AFFECTED AREA OF SERVICE DOOR BOTTOM NUT PLATE HOLES FOUND TO BE WITHIN LIMITS IAW EC5210-01154. RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM
- [SDR C2XA10SH288](https://openairdocs.org/sdr/C2XA10SH288.md): Structure · corroded · Sep 8, 2010 · N14916 · Emb EMB145LR · Passenger/Crew Doors
  > SHV - DURING C-CHECK PAX DOOR BOTTOM 4 NUT PLATE HOLES FOR MAIN LINER CORRODED (LEVEL 2 LOCAL). MAINTENANCE REMOVED CORROSION FOR AFFECTED AREA OF PAX DOORS NUT PLATES FOR MAIN LINERS FOUND TO BE WITHIN LIMITS IAW EC5210-01154. RESTORED ORIGINAL FINISH TO TH
- [SDR C2XA10SH287](https://openairdocs.org/sdr/C2XA10SH287.md): Floor Support · corroded · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 22. MAINTENANCE PERFORMED REPAIR AT RT OMEGA BEAM AT FRAME 22 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH286](https://openairdocs.org/sdr/C2XA10SH286.md): Skin · damaged · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK 10 WORKING RIVETS FRM 77 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR OF WORKING RIVETS AT FRM 77 BETWEEN STR'S 3L-8L IAW EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH285](https://openairdocs.org/sdr/C2XA10SH285.md): Skin · damaged · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK 2 WORKING RIVETS FRM 78 BETWEEN STR'S 5L-6L. MAINTENANCE PERFORMED REPAIR AT FRM 78 BETWEEN STR'S 5L-6L WORKING RIVETS IAW EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH284](https://openairdocs.org/sdr/C2XA10SH284.md): Skin · damaged · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK 4 WORKING RIVETS FRM 79 BETWEEN STR'S 3L-8L. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN WORKING RIVETS AT FRM 79 STR'S 3L-8L IAW EMB-145 EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH283](https://openairdocs.org/sdr/C2XA10SH283.md): Skin · damaged · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK 7 WORKING RIVETS FRM 79 BETWEEN STR'S 3R-7R. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN FRM 79 STR'S 3R-7R IAW EMB-145 EC5330-02224. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH282](https://openairdocs.org/sdr/C2XA10SH282.md): Skin · cracked · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK FOUND CRACK ON APU FIREWALL AROUND 3 O'CLOCK POSITION. MAINTENANCE REPAIRED CRACKS ON APU FIREWALL 3 O'CLOCK POSITION IAW EMB-145 EC5330-02226. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH281](https://openairdocs.org/sdr/C2XA10SH281.md): Skin · cracked · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK APU FIREWALL (EXT SKIN) HAS CRACKS FROM RT UPPER MOUNT AT STIFFENER ENDS AND FROM RIVET HEADS TO RT LOWER MOUNT, AND (2) EACH ON LT SIDE AT 9 O'CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL IAW EMB-145 EC 5330-02226. THE AIRCRAFT WAS
- [SDR C2XA10SH280](https://openairdocs.org/sdr/C2XA10SH280.md): Sill · cracked · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND APPLIED SEALANT IAW EMB-145 SRM 51-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH279](https://openairdocs.org/sdr/C2XA10SH279.md): Beam · cracked · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM HAS CORROSION (LEVEL 2 LOCAL) FRM 65-68. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR CUTOUT LWR BEAM FRM 65-68 AND RESTORED TO ORIG FINISH IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR C2XA10SH278](https://openairdocs.org/sdr/C2XA10SH278.md): Frame · cracked · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 10 STR 10R-9R CRACKED. MAINTENANCE REMOVED AND REPLACED FRM 10 BETWEEN STR 9R-13R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH277](https://openairdocs.org/sdr/C2XA10SH277.md): Sill · corroded · Sep 8, 2010 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02 AND APPLIED SEALANT IAW EMB-145 SRM 51-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI109](https://openairdocs.org/sdr/C2XA10RI109.md): O-Ring · defective · Aug 21, 2010 · N14916 · Emb EMB145LR · Pneumatic Distribution System
  > FLIGHT 3085 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN / BLEED NR 1 LEAK WITH APU RUNNING. EWR MX REMOVED AND REPLACED O-RINGS AT JOINTS 25 AND 23. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10RI047](https://openairdocs.org/sdr/C2XA10RI047.md): Control Unit · inoperative · Mar 27, 2010 · N14916 · Emb EMB145LR · Stabilizer Control System
  > FLIGHT 2961 - EWR - FLIGHT CREW REPORTED MAIN AND BACK UP PITCH TRIM INOPERATIVE ON CLIMBOUT. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY.
- [SDR C2XA09RI193](https://openairdocs.org/sdr/C2XA09RI193.md): Light · inoperative · Nov 17, 2009 · N14916 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2543 - EWR - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHT OVERWING EXIT INOPERATIVE. MX REMOVED AND REPLACED AISLE PATH LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09CL070](https://openairdocs.org/sdr/C2XA09CL070.md): Light · malfunctioned · May 16, 2009 · N14916 · Emb EMB145LR · Emergency Lighting
  > YYZ - FLIGHT 3117 - THE CREW REPORTED THE EMERGENCY LIGHTS DID NOT WORK. THE CREW RESET AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA09CL065](https://openairdocs.org/sdr/C2XA09CL065.md): Charger · inoperative · May 16, 2009 · N14916 · Emb EMB145LR · Emergency Lighting
  > FLIGHT NR 3117, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MX INSPECTED AND REPLACED THE NR3 EMERGENCY LIGHT BATTERY AND CHARGER. OPS CHECKS WERE GOOD.
- [SDR C2XA09RI019](https://openairdocs.org/sdr/C2XA09RI019.md): Inverter · inoperative · Jan 27, 2009 · N14916 · Emb EMB145LR · Emergency Lighting
  > RIC - DURING ROUTINE MX, RIC MX FOUND EMERGENCY LIGHT EXIT SIGN AFT GALLEY BULKHEAD INOPERATIVE. MX R&R NR 3 INVERTER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL137](https://openairdocs.org/sdr/C2XA08CL137.md): Control Unit · faulty · Dec 26, 2008 · N14916 · Emb EMB145LR · Stabilizer Control System
  > CLE FLT 2345 - THE CREW REPORTED A PITCH TRIM MAIN INOP MESSAGE IN FLIGHT. THE CREW RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA08TY138](https://openairdocs.org/sdr/C2XA08TY138.md): Light · inoperative · Dec 9, 2008 · N14916 · Emb EMB145 · Emergency Lighting
  > EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP. R&R LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE
- [SDR C2X2008F00017](https://openairdocs.org/sdr/C2X2008F00017.md): Skin · gouged · Aug 4, 2008 · N14916 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > ACFT CURRENTLY IN A C-CHECK STATUS AND THE LT FUSELAGE WAS FOUND GOUGED AND DENTED AT FR19. MAINTENANCE CUT OUT THE AREA AND FABRICATED A NEW REPAIR IAW EC5330-01824. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (S)
- [SDR C2XA07IA214](https://openairdocs.org/sdr/C2XA07IA214.md): Control Unit · inoperative · Oct 1, 2007 · N14916 · Emb EMB145LR · Landing Gear Brake System
  > IAH - FLIGHT 2802, DURING TAXI THE CREW REPORTED A BRAKE OUTBOARD MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETUR
- [SDR C2XA07TY032](https://openairdocs.org/sdr/C2XA07TY032.md): Control Lever · inoperative · Jun 28, 2007 · N14916 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > BNA - FLIGHT NR 2175 - AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT AND CYCLE PROCEDURE PER QRC DID NOT WORK AND A/C DIVERTED INTO TYS. TYS REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB 145 AMM 32-32-02-400-801A AND EVERYTHING. OPS CHECKED GOOD I
- [SDR C2XA05IA062](https://openairdocs.org/sdr/C2XA05IA062.md): Light · inoperative · Apr 22, 2005 · N14916 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2690, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN INTERPHONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CABIN INTERPHONE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA03BT067](https://openairdocs.org/sdr/C2XA03BT067.md): Bulb · burned out · Jun 15, 2003 · N14916 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE INSPECTION, MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT AND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULBS IAW EMB145 MM 33-50-05 AND 33-50-10. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO S
- [SDR C2XA03BT027](https://openairdocs.org/sdr/C2XA03BT027.md): Light · faulty · Feb 7, 2003 · N14916 · Emb EMB145LR · Emergency Lighting
  > BTV---CO2002, DURING 2A INSPECTION, MAINTENANCE FOUND FLOOR EMERGENCY LIGHT STRIP 2ND FROM THE REAR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED #7 FLOOR PROXIMITY EMERGENCY LIGHT STRIP IAW EMB145 AMM #33-50-12. OPS. CHECKED GOOD.
- [SDR C2XA02IA253](https://openairdocs.org/sdr/C2XA02IA253.md): Battery · discharged · Dec 29, 2002 · N14916 · Emb EMB145LR · Emergency Lighting
  > BNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE #1 EMERGENCY LIGHT BATTERY WOULD NOT HOLD CHARGE. BNA- MAINTENANCE REMOVED AND REPLACED THE #1 EMERGENCY LIGHT BATTERY,PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, NO DEFECTS NOTED, AND, TH
- [SDR C2XA02SH138](https://openairdocs.org/sdr/C2XA02SH138.md): Beam · corroded · Dec 6, 2002 · N14916 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C CHECK, THE LT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAITENACE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2A02SH136](https://openairdocs.org/sdr/C2A02SH136.md): Butt Strap · corroded · Dec 6, 2002 · N14916 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV- DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 16 AND 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA02SH139](https://openairdocs.org/sdr/C2XA02SH139.md): Plate · gouged · Dec 6, 2002 · N14916 · Emb EMB145LR · Nacelle/Pylon, Main Frame
  > SHV-DURING C CHECK, NR 1 ENGINE, FOWARD PYLON YOKE GUSSET PLATE WAS FOUND TO HAVE A GOUGE BY LOWER ENGINE MOUNT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5420-01038. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Next page: https://openairdocs.org/aircraft/N14916/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 = 'N14916' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14916/reports

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