# Service difficulty reports: N14960, cancelled Aug 6, 2015

A list on [N14960, cancelled Aug 6, 2015](https://openairdocs.org/deregistered/N14960-2015-08-06.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 · 86 reports

- [SDR ASOA20140918080](https://openairdocs.org/sdr/ASOA20140918080.md): Engine · leaking · Sep 18, 2014 · N14960 · Emb EMB145LR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED BAD FUME ODOR FROM BLEED NR 1, MOST INTENSE WITH HIGH THRUST SETTING CHANGES. APU USED AS ALTERNATE BLEED SOURCE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPS CHECKED GOOD.
- [SDR ASOA20140913102](https://openairdocs.org/sdr/ASOA20140913102.md): Switch · shorted · Sep 13, 2014 · N14960 · Emb EMB145LR · Passenger Compartment Lighting
  > CREW REPORTED PSU LIGHT AT 6D SMOKING AND FLICKERING COULD NOT TURN OFF. MAINTENANCE R & R 6D PSU LIGHT WITH NO FIX. DISCONNECTED SWITCH AND PLACED ON NEF CB02. MX R & R 6D PSU LIGHT SWITCH WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140912101](https://openairdocs.org/sdr/ASOA20140912101.md): Unknown · odor · Sep 12, 2014 · N14960 · Emb EMB145LR · Cabin Cooling System
  > PILOT REPORTED ODOR OF BURNING OIL FROM NR 1 PACK WHEN IT IS POWERED BY ENGINE BLEED. MAINTENANCE PERFORMED TROUBLESHOOTING IAW AMM 21-20-00. PERFORMED ENGINE 1 AND 2 HIGH POWER RUNS WITH NO BURNING ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140810093](https://openairdocs.org/sdr/ASOA20140810093.md): Actuator · loose · Aug 10, 2014 · N14960 · Emb EMB145LR · Flight Control System
  > DURING FLIGHT, CREW FELT LIGHT VIBRATION IN THE FLIGHT CONTROLS DURING FLIGHT AND RETURNED TO BASE. ACFT WAS FERRIED, WHERE MAINTENANCE PERFORMED CABLE TENSIONS AND FUNCTIONAL TEST OF THE AILERON, RUDDER AND ELEVATOR, FOUND THE AILERON CABLE SLIGHTLY OUT OF
- [SDR ASOA20140616088](https://openairdocs.org/sdr/ASOA20140616088.md): Unknown · odor · Jun 16, 2014 · N14960 · Emb EMB145LR · Air Distribution System
  > ACFT WAS FERRIED FOR SMOKE IN CABIN WHEN PACKS WERE SELECTED. MAINTENANCE CHANGED OUT THE CARBON SEAL ON THE NR 1 ENGINE IAW MM 72-00-00-200. OPS AND LEAK CHECKED GOOD. PERFORMED AN AIR DUCT OIL DECONTAMINATION IAW AMM 21-20-00. R & R THE ACM IAW AMM 21-51
- [SDR ASOA20140604063](https://openairdocs.org/sdr/ASOA20140604063.md): Acm · odor · Jun 4, 2014 · N14960 · Emb EMB145LR · Cabin Cooling System
  > PILOT REPORTED A STRONG ODOR COMING FROM PACK NR 1. MX R & R THE NR 1 ACM WITH OPS CHECK GOOD AND NO ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140223027H](https://openairdocs.org/sdr/ASOA20140223027H.md): A/C Pack · malfunctioned · Feb 23, 2014 · N14960 · Emb EMB145LR · Cabin Cooling System
  > IT WAS REPORTED THAT THE NR 2 PACK WAS MAKING LOUD NOISE AND ODORS. R & R THE NR 2 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131221140R](https://openairdocs.org/sdr/ASOA20131221140R.md): Wire Harness · arced · Dec 21, 2013 · N14960 · Emb EMB145LR · Light System Wiring
  > CREW REPORTED THE CEILING LIGHT OVER ROW 1A WAS PRODUCING A BURNING ODOR. MX R & R THE ELECTRICAL HARNESS NR ROW 1A WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131013117](https://openairdocs.org/sdr/ASOA20131013117.md): Inverter · inoperative · Oct 13, 2013 · N14960 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION, EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT INOPERATIVE. MX R & R INVERTER & OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130617061](https://openairdocs.org/sdr/ASOA20130617061.md): Unknown · odor · Jun 17, 2013 · N14960 · Emb EMB145LR · Air Distribution System
  > CREW REPORTED A ODOR IN THE CABIN LIKE BURNING PLASTIC. MX PERFORMED PASSENGER CABIN LIGHT TEST WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326107](https://openairdocs.org/sdr/ASOA20130326107.md): Shear Tie · corroded · Mar 28, 2013 · N14960 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK SHEAR TIE AT FRAME 68 BETWEEN STRINGER 18L-17L IS CORRODED. MX REPAIRED SHEAR TIE IAW SRM 51-20-01 AND CPM 51-21-06. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326106](https://openairdocs.org/sdr/ASOA20130326106.md): Skin · corroded · Mar 28, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326104](https://openairdocs.org/sdr/ASOA20130326104.md): Stringer · corroded · Mar 28, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, COCKPIT STRINGER 21R CORRODED. MX R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326103](https://openairdocs.org/sdr/ASOA20130326103.md): Stringer · corroded · Mar 28, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK COCKPIT STRINGER 21L CORRODED. MX REPAIRED OF STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326102](https://openairdocs.org/sdr/ASOA20130326102.md): Stringer Splice · corroded · Mar 28, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER SPLICE 21L CORRODED BETWEEN FRAMES 12-13. MX PERFORMED REPAIR ON STRINGER SPLICE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326101](https://openairdocs.org/sdr/ASOA20130326101.md): Threshold · corroded · Mar 27, 2013 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAME 68 CORRODED AROUND NUTPLATES. MX PERFORMED REPAIR ON CARGO DOOR THRESHOLD TRIANGULAR PLATE AT FRAME 68 IAW EC5320-01479, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326100](https://openairdocs.org/sdr/ASOA20130326100.md): Plate · corroded · Mar 27, 2013 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CARGO THRESHOLD TRIANGULAR PLATE AT FRAME 65 CORRODED. (LOCAL LEVEL 2) AROUND NUTPLATES. MX PERFORMED REPAIR ONCARGO COMP THRESHOLD TRIANGULAR PLATE AT FRAME 65 IAW EC5320-01479, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326099](https://openairdocs.org/sdr/ASOA20130326099.md): Structure · corroded · Mar 27, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK CARGO DOOR CUTOUT LWR MEMBER CORRODED. MX PERFORMED REPAIR ON CARGO DOOR CUT-OUT LWR MEMBER IAW SRM 51-20-01 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326098V](https://openairdocs.org/sdr/ASOA20130326098V.md): Shear Angle · corroded · Mar 27, 2013 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CORRODED SHEAR CLIP ON RT CROSSBEAM FRAME 65. MX PERFORMED REPAIR ON FRAME 65 RH CROSSBEAM SHEAR CLIP IAW EC5320-01494A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326097V](https://openairdocs.org/sdr/ASOA20130326097V.md): Floor Support · corroded · Mar 27, 2013 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK LT OMEGA BEAM FLANGE CORRODED (LOCAL LEVEL 2) BETWEEN FRAMES 18-23. MX PERFORMED REPAIR FOR LT OMEGA BEAM FLANGE AT FRAME 20 IAW SRM 53-00-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130326096](https://openairdocs.org/sdr/ASOA20130326096.md): Frame · gouged · Mar 26, 2013 · N14960 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK FRAME 60 AT STRINGER 5L GOUGED. MX PERFORMED REPAIR AT FRAME 60 STRINGER 5L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120220020](https://openairdocs.org/sdr/ASOA20120220020.md): Controller · faulty · Feb 20, 2012 · N14960 · Emb EMB145LR · Windshield/Door Rain/Ice Removal
  > THE CREW REPORTED AN 115 VOLT, AC BUSS FAILED ALONG WITH SMOKE ODOR. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD.
- [SDR C2XA11TY097](https://openairdocs.org/sdr/C2XA11TY097.md): Light · inoperative · Jun 29, 2011 · N14960 · Emb EMB145LR · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHT INOP. REPLACED LAMP IAW EMB 145 AMM33-50-05. OPS CHECK GOOD.
- [SDR C2XA11RI097](https://openairdocs.org/sdr/C2XA11RI097.md): Starter · vibration · May 27, 2011 · N14960 · Emb EMB145LR · Engine Starter
  > FLIGHT 2260 - EWR - FLIGHT CREW REPORTED ENGINE NR 1 HIGH VIBRATION ON TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PLACED ITEM ON DMI FOR 50 FLIGHT HOURS. ACFT WAS APPROVED TO RETURN TO SERVICE. FURTHER TROUBLESHOOTING REVEALED VIBRA
- [SDR C2XA11CL138](https://openairdocs.org/sdr/C2XA11CL138.md): Starter · faulty · May 27, 2011 · N14960 · Emb EMB145LR · Engine Starter
  > EWR FLT 2260 THE CREW REPORTED A NR 1 ENGINE HIGH VIBRATION ON TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR TURBINE STARTER. PERFORMED ENGINE VIBRATION SURVEY AND COMPLIED WITH CMC DOWNLOAD. OPERATION
- [SDR C2XA11SH067](https://openairdocs.org/sdr/C2XA11SH067.md): Fitting · cracked · Mar 15, 2011 · N14960 · Emb EMB145LR · Nacelle/Pylon, Attach Fittings
  > SHV - DURING C-CHECK NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REMOVED AND REPLACED NR 1 ENG YOKE FITTING IAW EC5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH065](https://openairdocs.org/sdr/C2XA11SH065.md): Floor Support · corroded · Mar 13, 2011 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK RT OMEGA BEAM AT FRAME 18 IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH064](https://openairdocs.org/sdr/C2XA11SH064.md): Doubler · damaged · Mar 13, 2011 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK BOUBLER AT FRAME 22 IS CORRODED (LEVEL 2 LOCAL) AND BENT. MAINTENANCE PERFORMED REPAIR ON DOUBLER AT FRAME 22 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10CL196](https://openairdocs.org/sdr/C2XA10CL196.md): Controller · faulty · Dec 10, 2010 · N14960 · Emb EMB145LR · Cabin Pressure Controller
  > CLE FLT 2690 THE CREW REPORTED THE PRESSURIZATION WAS INOPERATIVE IN BOTH MANUAL AND AUTO. THE AIRCRAFT DIVERTED INTO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA10CL165](https://openairdocs.org/sdr/C2XA10CL165.md): Brake · overheated · Nov 1, 2010 · N14960 · Emb EMB145LR · Brake
  > DAY - FLT 2693 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE AFTER TAKEOFF. THE LEFT BRAKE SHOWED FULL HOT. THE BRAKES WERE COOLED PER THE QRH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BRAKE AND BRAKE TEMP SENSOR. O
- [SDR C2XA10IA243](https://openairdocs.org/sdr/C2XA10IA243.md): Connector · loose · Sep 6, 2010 · N14960 · Emb EMB145LR · Light System Wiring
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A AND 12A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10IA242](https://openairdocs.org/sdr/C2XA10IA242.md): Connector · loose · Sep 6, 2010 · N14960 · Emb EMB145LR · Light System Wiring
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD LIGHTS AT EXIT ROWS TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT SIGNS AT 3A AND 12A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA290](https://openairdocs.org/sdr/C2XA09IA290.md): Inverter · inoperative · Nov 16, 2009 · N14960 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE LOWER FORWARD SERVICE DOOR EXIT IDENTIFIER AND NR 1 FLOOR PROX LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER AT CONNECTOR P8527, OPERATIONALLY TESTED WITH NO DEFECTS, A
- [SDR C2XA09RI1137](https://openairdocs.org/sdr/C2XA09RI1137.md): Flap · overspeed · Aug 7, 2009 · N14960 · Emb EMB145LR · Trailing Edge Flap Control System
  > FLIGHT 2527 - EWR - FLIGHT CREW REPORTED FLAP OVER SPEED IN CRUISE (FLAP 9 AT 290 KNOTS FOR 5 MINUTES). EWR INSPECTION DEPARTMENT PERFORMED FLAP OVER SPEED INSPECTION AND FOUND NO DAMAGES. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI115](https://openairdocs.org/sdr/C2XA09RI115.md): Outflow Valve · inoperative · Jun 3, 2009 · N14960 · Emb EMB145LR · Pressure Regulator/Outflow Valve
  > FLIGHT CREW REPORTED CABIN AUTO PRESSURIZATION SYS OPERATED ABNORMALLY ON DESCENT. CREW LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09SH081](https://openairdocs.org/sdr/C2XA09SH081.md): Floor Support · corroded · Mar 16, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FR 49. MAINTENANCE REPAIRED CORRODED AREA ON LT OMEGA BEAM (CORRODED AREA) AT FRM 49 IAW IC2009-145/00816. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRC
- [SDR C2XA09SH080](https://openairdocs.org/sdr/C2XA09SH080.md): Floor Support · corroded · Mar 16, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT FR 29. MAINTENANCE COMPLETED INSTALLATION OF REPAIR FOR LT OMEGA BEAM AT FRM 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH079](https://openairdocs.org/sdr/C2XA09SH079.md): Floor Support · corroded · Mar 16, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE CORRODED FRM 25 AT COMPOSITE CROSSBEAM. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09SH078](https://openairdocs.org/sdr/C2XA09SH078.md): Floor Support · corroded · Mar 16, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 44. MAINTENANCE REPAIRED LT OMEGA BEAM IAW IC2009-145/00816. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH077](https://openairdocs.org/sdr/C2XA09SH077.md): Stringer · corroded · Mar 16, 2009 · N14960 · Emb EMB145 · Fuselage Main, Longeron/Stringer
  > SHV - DURING C-CHECK STR 17R FRMS 16-24 HAS CORROSION. MAINTENANCE REMOVED AND COMPLETED INSTALLATION OF STR 17R AT FRMS 16-24 BY INSTALLING HI-LOKS AT STRINGER SPLICE AT FR 16.5 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH076](https://openairdocs.org/sdr/C2XA09SH076.md): Smoke Detector · inoperative · Mar 16, 2009 · N14960 · Emb EMB145 · Smoke Detection
  > SHV - DURING C-CHECK LAV SMOKE DETECTOR TEST PANEL HAS NO POWER. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB-145 AMM 26-14-01. OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH074](https://openairdocs.org/sdr/C2XA09SH074.md): Floor Support · corroded · Mar 10, 2009 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW IC 2009-145/00816. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH071](https://openairdocs.org/sdr/C2XA09SH071.md): Floor Support · corroded · Mar 1, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FRM 33. MAINTENANCE COMPLETED REPAIR OF LT OMEGA BEAM AT FRM 33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09SH069](https://openairdocs.org/sdr/C2XA09SH069.md): Floor Support · corroded · Mar 1, 2009 · N14960 · Emb EMB145 · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM FRM 25, CORRODED AT COMPOSITE CROSSBEAM. MAINTENANCE REPAIRED CENTER OMEGA BEAM FRM 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08TY031](https://openairdocs.org/sdr/C2XA08TY031.md): Connector · loose · Feb 25, 2008 · N14960 · Emb EMB145LR · Light System Wiring
  > THE AFT FACING PORTION OF THE CEILING EMERGENCY EXIT SIGN AT SEAT 12 IS INOP. RESECURED THE CONNECTOR, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA07SH033](https://openairdocs.org/sdr/C2XA07SH033.md): Floor Support · corroded · Jun 10, 2007 · N14960 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK MAINTENANCE FOUND LEFT OMEGA BEAM FROM FRAME 18 TO 23 WITH CORROSION. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FRAME 18 TO 23 IAW SRM 51-40-02. PAINTED & INSTALLED NUT PLATES IAW EC 5320-01140 & EC 5320-01137. AIRCRAFT WAS APPROVED TO RE
- [SDR C2XA07SH032](https://openairdocs.org/sdr/C2XA07SH032.md): Panel · corroded · Jun 10, 2007 · N14960 · Emb EMB145LR · Wing, Plate/Skin
  > SHV - DURING C-CHECK MAINTENANCE FOUND OVER THE WING TO FUSELAGE PNL 195 WITH CORRODED BONDING STRAPS. MAINTENANCE REPAIRED PNL 195 IAW EC 5750-01315, AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07CL020](https://openairdocs.org/sdr/C2XA07CL020.md): Switch · leaking · Feb 7, 2007 · N14960 · Emb EMB145LR · Brake Anti-Skid Section
  > EWR FLIGHT 2996 THE CREW REPORTED HYDRAULIC SYSTEM NR 2 FAILURE. TOTAL LOSS OF SYSTEM NR 2 FLUID. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 SYSTEM BRAKE PRESSURE SWITCH LEAKING. THE SWITCH
- [SDR C2XA06IA197](https://openairdocs.org/sdr/C2XA06IA197.md): Proximity Switch · faulty · Dec 21, 2006 · N14960 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > BNA - FLT 2278 THE CREW REPORTED THAT THE NOSE GEAR DOORS DID NOT CLOSE UNTIL REACHING AN ALTITUDE OF 11,000 FT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK PROXIMITY SWITCH. THE LANDING GEAR DOORS WERE OPERATIONALLY CHECKED AND THE AIRCRAFT RETURNED TO
- [SDR C2XA05IA141](https://openairdocs.org/sdr/C2XA05IA141.md): Battery Pack · discharged · Dec 12, 2005 · N14960 · Emb EMB145 · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE AND FOUR EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR

Next page: https://openairdocs.org/deregistered/N14960-2015-08-06/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 = 'N14960' AND deregistration_id = 'N14960-2015-08-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14960-2015-08-06/reports

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