# Service difficulty reports: N16963, cancelled Jan 31, 2018

A list on [N16963, cancelled Jan 31, 2018](https://openairdocs.org/deregistered/N16963-2018-01-31.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 · 99 reports

- [SDR ASOA20141221380](https://openairdocs.org/sdr/ASOA20141221380.md): Engine · failed · Dec 21, 2014 · N16963 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > LOST NR 2 ENGINE IN FLIGHT. R & R NR 2 ENGINE IAW AMM 71-00-00. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140803084](https://openairdocs.org/sdr/ASOA20140803084.md): Inverter · inoperative · Aug 3, 2014 · N16963 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE LT SIDE CABIN UPPER EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140622048](https://openairdocs.org/sdr/ASOA20140622048.md): Controller · odor · Jun 22, 2014 · N16963 · Emb EMB145LR · Passenger Compartment Lighting
  > THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN CABIN. MAINTENANCE INSPECTED AND REPLACED THE CABIN LIGHT CONTROLLER. OPS CHECKED GOOD.
- [SDR ASOA20140227024](https://openairdocs.org/sdr/ASOA20140227024.md): Light · inoperative · Feb 27, 2014 · N16963 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, THE FLOOR EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE R & R THE LIGHT AND OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130926378](https://openairdocs.org/sdr/ASOA20130926378.md): Skin · deformed · Sep 25, 2013 · N16963 · Emb EMB145LR · Elevator, Plate/Skin
  > LT ELEVATOR TIP FAIRING UPPER NUT PLATE HOLE IS ELONGATED. CUT-OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A FILLER AND A DOUBLER. PERFORMED BALANCE CHECK OF ELEVATOR.
- [SDR ASOA20130829156](https://openairdocs.org/sdr/ASOA20130829156.md): Skin · cracked · Aug 29, 2013 · N16963 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR75 BELOW STR 2R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2013-145-034022A, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121218092](https://openairdocs.org/sdr/ASOA20121218092.md): Battery · discharged · Dec 18, 2012 · N16963 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX, SEVERAL FORWARD CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR ASOA20120328027R](https://openairdocs.org/sdr/ASOA20120328027R.md): Charger · inoperative · Mar 28, 2012 · N16963 · Emb EMB145LR · Emergency Lighting
  > DURING SCHEDULED ROUTINE INSPECTION, BOTH THE LT & RT SIDE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT SYS BATTERY CHARGER TRAY IAW AMM 33-50-04 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL215](https://openairdocs.org/sdr/C2XA11CL215.md): Wire · broken · Sep 25, 2011 · N16963 · Emb EMB145LR · Pneumatic System Wiring
  > ORD FLT 6062 - THE CREW REPORTED A BLEED 1 AND 2 FAIL MESSAGE IN FLIGHT ALONG WITH A PACK 2 FAIL:ANTI-ICE FAIL AND THE PRESSURIZATION FAILED AS WELL. MAINTENANCE INSPECTED AND FOUND WIRES AT THE HIGH PRESSURE BLEED SWITCH CONNECTOR P 1203 BROKEN. THE WIRES W
- [SDR C2XA11RI155](https://openairdocs.org/sdr/C2XA11RI155.md): Charger · inoperative · Sep 22, 2011 · N16963 · Emb EMB145LR · Emergency Lighting
  > RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 12-19 EMERGENCY LIGHT FLOOR STRIP INTERMITTENT. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR R
- [SDR C2XA11CL176](https://openairdocs.org/sdr/C2XA11CL176.md): Battery · discharged · Jul 31, 2011 · N16963 · Emb EMB145XR · Emergency Lighting
  > MAINTENANCE REPORTED THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11IA152](https://openairdocs.org/sdr/C2XA11IA152.md): Warning System · false activation · Jul 13, 2011 · N16963 · Emb EMB145LR · Landing Gear Position and Warning
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. MAINTENANCE FUNCTIONALLY TESTED THE PROXIMITY SWITCHES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA116](https://openairdocs.org/sdr/C2XA11IA116.md): Control Lever · faulty · Jun 17, 2011 · N16963 · Emb EMB145LR · Landing Gear Selector
  > JAX --- CREW REPORTED, "LANDING GEAR LEVER DISAGREE" EICAS MESSAGE AFTER TAKE OFF THEN TRIED TO RETRACT THE LANDING GEAR. LANDING GEAR WOULD NOT RETRACT. QRH PROCEDURES PERFORMED. LANDED UNDER-WEIGHT. LANDING WAS UNEVENTFUL. MAINTENANCE PERFORMED A GENERA
- [SDR C2XA11IA123](https://openairdocs.org/sdr/C2XA11IA123.md): Control Lever · inoperative · Jun 16, 2011 · N16963 · Emb EMB145LR · Landing Gear Selector
  > IAH - FLIGHT 2296, THE CREW REPORTED THAT THE LANDING GEAR INDICATION WAS THREE RED UP, AND LANDING GEAR MASTER DISAGREE WITH THE LEVER IN THE DOWN POSITION, THE CREW SUCCESSFULLY LOWERED THE LANDING GEAR, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAIN
- [SDR C2XA11IA116SUP](https://openairdocs.org/sdr/C2XA11IA116SUP.md): Control Lever · faulty · Jun 14, 2011 · N16963 · Emb EMB145LR · Landing Gear Selector
  > CREW REPORTED, "LANDING GEAR LEVER DISAGREE" EICAS MESSAGE AFTER TAKEOFF THEN TRIED TO RETRACT LANDING GEAR. LANDING GEAR WOULD NOT RETRACT. QRH PROCEDURES PERFORMED. LANDED UNDER-WEIGHT. LANDING WAS UNEVENTFUL. MAINTENANCE PERFORMED A GENERAL VISUAL INSP
- [SDR C2XA10IA291](https://openairdocs.org/sdr/C2XA10IA291.md): Proximity Sensor · out of adjust · Nov 9, 2010 · N16963 · Emb EMB145LR · Landing Gear Position and Warning
  > IAH - FLIGHT 3090, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR AIR/GRND PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10TY105](https://openairdocs.org/sdr/C2XA10TY105.md): Battery · overtemp · Jul 29, 2010 · N16963 · Emb EMB145LR · Battery/Charger System
  > TYS - A/C WAS IN CLT WHEN NR 2 BATTERY SHOWED OVERTEMP. MAINTENANCE REMOVED AND REPLACED THE 3 AT BATTERY IAW EMB 145 AMM 24-36-01. OPS CHECK WAS GOOD AND RELEASED.
- [SDR C2XA10IA084](https://openairdocs.org/sdr/C2XA10IA084.md): Light · inoperative · Feb 26, 2010 · N16963 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2347, DURING POST FLIGHT INSPECTION THE AISLE PATH LIGHT STRIP AT THE EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR
- [SDR C2XA09SH449](https://openairdocs.org/sdr/C2XA09SH449.md): Skin · cracked · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK, RT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 75-80. REPAIRED SKIN IAW EC 5330-02009. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH448](https://openairdocs.org/sdr/C2XA09SH448.md): Skin · cracked · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK, LT FUSELAGE SKIN HAS CRACKS BETWEEN FR 75-78. REPAIRED SKIN IAW EC 5330-02009. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH445](https://openairdocs.org/sdr/C2XA09SH445.md): Floor Support · corroded · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 39. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH444](https://openairdocs.org/sdr/C2XA09SH444.md): Floor Support · corroded · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 39. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH443](https://openairdocs.org/sdr/C2XA09SH443.md): Floor Support · corroded · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH442](https://openairdocs.org/sdr/C2XA09SH442.md): Floor Support · corroded · Nov 22, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH422](https://openairdocs.org/sdr/C2XA09SH422.md): Bowl · corroded · Nov 11, 2009 · N16963 · Emb EMB145LR · Waste Disposal System
  > SHV - DURING C-CHECK LAV PAN CORRODED (LEVEL 2 LOCAL) FWD WASTE DRAIN VALVE. MAINTENANCE REMOVED AND REPLACED WASTE DRAIN DUMP BOWL ASSY IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH421](https://openairdocs.org/sdr/C2XA09SH421.md): Shear Tie · corroded · Nov 11, 2009 · N16963 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHV - DURING C-CHECK SHEAR CLIP AT FRAME 65 STRINGER 19L-17L HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP AND SPLICE AT FRAME 65 STRINGER 19L-17L IAW EMB-145 EC5320-01494 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH420](https://openairdocs.org/sdr/C2XA09SH420.md): Flange · cracked · Nov 11, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LAV WASTE DRAIN PAN FLANGE IS MISDRILLED AND CRACKED. MAINTENANCE PERFORMED REPAIR OF LAV WASTE DRAIN PAN FLANGE IAW EMB-145 ETD 2009-145/08910. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH419](https://openairdocs.org/sdr/C2XA09SH419.md): Floor Support · corroded · Nov 11, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM AT CARBON CROSSBEAM MEMBER MATING SURFACE HAS CORROSION (LEVEL 2 LOCAL) FRAME 32-33. MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM AT CARBON CROSS MEMBER MATING SURFACE AT FRAME 32-33 IAW EMB-145 SRM 53-00-10. THE A
- [SDR C2XA09SH418](https://openairdocs.org/sdr/C2XA09SH418.md): Bushing · migrated · Nov 11, 2009 · N16963 · Emb EMB145 · Aileron Tabs
  > SHV - DURING C-CHECK RT SPRING TAB OTBD PANEL ATTACH BRACKET INBD HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT SPRING TAB OTBD PANEL ATTACH BRACKET IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH417](https://openairdocs.org/sdr/C2XA09SH417.md): Floor Support · corroded · Nov 11, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM FRAME 29 AT CROSSBEAM ATTACHMENT FLANGE CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED LT OMEGA BEAM FRAME 29 AT CROSSBEAM ATTACHMENT FLANGE IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH414](https://openairdocs.org/sdr/C2XA09SH414.md): Floor Support · corroded · Nov 10, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAMES 15-21. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 51-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH413](https://openairdocs.org/sdr/C2XA09SH413.md): Sill · corroded · Nov 10, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK SERVICE DOOR CENTER FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL) AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH412](https://openairdocs.org/sdr/C2XA09SH412.md): Threshold · corroded · Nov 10, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CARGO DOOR THRESHOLD CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR THRESHOLD IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH410](https://openairdocs.org/sdr/C2XA09SH410.md): Support · corroded · Nov 8, 2009 · N16963 · Emb EMB145LR · Waste Disposal System
  > SHV - DURING C-CHECK, LAV WASTE DRAIN VALVE SUPPORT CORRODED. REMOVED AND REPLACED LAV WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH409](https://openairdocs.org/sdr/C2XA09SH409.md): Floor Support · corroded · Nov 8, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH408](https://openairdocs.org/sdr/C2XA09SH408.md): Floor Support · corroded · Nov 8, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED LT OMEGA BEAM IAW EC5310-01466 AND EMB 145 SRM 53-00-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH407](https://openairdocs.org/sdr/C2XA09SH407.md): Door Frame · corroded · Nov 8, 2009 · N16963 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK, SERVICE DOOR CUTOUT HAS CORROSION UNDER AFT LWR TEFLON GUIDE. REPAIRED SERVICE DOOR CUTOUT IAW ETD2009-145/09007A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH404](https://openairdocs.org/sdr/C2XA09SH404.md): Frame · cracked · Nov 3, 2009 · N16963 · Emb EMB145 · Fuselage Main, Frame
  > SHV - DURING C-CHECK LT FRM 10 UNDER DV WINDOW CUTOUT IS CRACKED. MAINTENANCE REMOVED AND REPLACED FUSELAGE FRAME 10 LT SIDE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH394](https://openairdocs.org/sdr/C2XA09SH394.md): Mount · corroded · Oct 31, 2009 · N16963 · Emb EMB145LR · Engine Mount Section
  > SHV - DURING C-CHECK RT ENGINE FRONT MOUNTING FLANGE HAS ON CORRODED (LEVEL 2 LOCAL) BOLT HOLE. MAINTENANCE CLEANED, REAMED AND POLISHED ONE CORRODED HOLE AT RT ENGINE FRONT MOUNTING FLANGE IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVED FOR RETU
- [SDR C2XA09SH393](https://openairdocs.org/sdr/C2XA09SH393.md): Mount · corroded · Oct 31, 2009 · N16963 · Emb EMB145LR · Engine Mount Section
  > SHV - DURING CHECK LT ENG FRONT MOUNTING FLANGE HAS 24 CORRODED (LEVEL 2 LOCAL) BOLT HOLES. MAINTENANCE CLEANED, REAMED AND POLISHED UP TO 0.306 CORRODED HOLES AT 24 LT ENG MOUNTING FLANGE BOLT HOLES IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVE
- [SDR C2XA09SH391](https://openairdocs.org/sdr/C2XA09SH391.md): Floor Support · corroded · Oct 31, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 58-59. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM BETWEEN FRAMES 58-59 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH390](https://openairdocs.org/sdr/C2XA09SH390.md): Floor Support · corroded · Oct 31, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 39 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 39 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH389](https://openairdocs.org/sdr/C2XA09SH389.md): Floor Support · corroded · Oct 31, 2009 · N16963 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AROUND CARBON CROSSBEAM FR 54. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM AT FR 54 IAW EMB-145 SRM 53-00-10 FIG 202 DET A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09RI128](https://openairdocs.org/sdr/C2XA09RI128.md): Proximity Switch · defective · Jul 12, 2009 · N16963 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 2319 - EWR - FLIGHT CREW REPORTED "AIR GROUND FAIL" MESSAGE ON EICAS WITH ASSOCIATED MESSAGES: AIR GROUND SENSOR FAIL, GROUND IDLE STOP FAIL, AND AOA INOP. EWR MX REMOVED AND REPLACED NOSE WOW A/G PROX SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFUL
- [SDR C2XA09CL080](https://openairdocs.org/sdr/C2XA09CL080.md): Light · malfunctioned · Jun 8, 2009 · N16963 · Emb EMB145LR · Emergency Lighting
  > CLE FLIGHT 2972 - CREW REPORTED CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND RESET SYSTEM. OPERATIONAL CHECK PERFORMED. CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR C2XA09RI114](https://openairdocs.org/sdr/C2XA09RI114.md): Unknown · malfunctioned · Jun 2, 2009 · N16963 · Emb EMB145LR · Emergency Lighting
  > FLIGHT CREW REPORTED CABIN/CABIN EMERGENCY BUTTON ON ICU PANEL ILLUMINATED AND WILL NOT RESET. MX CONTROL INSTRUCTED FLIGHT CREW HOW TO PERFORM SYSTEM RESET. RESET SUCCESSFULL. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2X2008F00025](https://openairdocs.org/sdr/C2X2008F00025.md): Unknown · odor · Sep 2, 2008 · N16963 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED SMOKE OR ELECTRICAL, ODOR IN THE CABIN AND FLIGHTDECK DURING TAXI. THE AC RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINT INSPECTED CONTACTORS, RELAYS AND ELECTRICAL CONNECTIONS IN THE COCKPIT. CHECKED OPERATION FO THE LAV AND CABIN LIG
- [SDR C2XA08RI019](https://openairdocs.org/sdr/C2XA08RI019.md): Inverter · inoperative · Feb 21, 2008 · N16963 · Emb EMB145LR · Emergency Lighting
  > RIC - DURING ROUTINE MAINTENANCE, MX FOUND EXIT ROW LIGHT AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED NR 5 INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL010](https://openairdocs.org/sdr/C2XA08CL010.md): Fuel Control · leaking · Jan 17, 2008 · N16963 · Emb EMB145LR · APU Engine Fuel and Control
  > EWR FLIGHT 2756 - THE CREW REPORTED FUEL FUMES IN THE COCKPIT WHEN THE APU WAS STARTED AND SHUT DOWN. THE APU WAS MEL'ED CONTROL NR 137605. ON 1/18/08 CLE MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL ASSEMBLY P/N 4504616A, S/N 04-02-63, AND THE APU
- [SDR C2XA08CL009](https://openairdocs.org/sdr/C2XA08CL009.md): Solenoid Valve · faulty · Jan 14, 2008 · N16963 · Emb EMB145LR · APU Engine Fuel and Control
  > EWR FLIGHT 2947 - THE CREW REPORTED A FUEL SMELL AFTER APU START ON THE GROUND. THE AIRCRAFT WAS RELEASED IAW MEL CONTROL 137419. ON 1/16/08 CLE MAINTENANCE REMOVED AND REPLACED THE MAIN FUEL SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS R

Next page: https://openairdocs.org/deregistered/N16963-2018-01-31/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 = 'N16963' AND deregistration_id = 'N16963-2018-01-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16963-2018-01-31/reports

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