# Service difficulty reports: N14947, cancelled Nov 8, 2018 A list on [N14947, cancelled Nov 8, 2018](https://openairdocs.org/deregistered/N14947-2018-11-08.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 · 94 reports - [SDR ASOA20140709096](https://openairdocs.org/sdr/ASOA20140709096.md): Battery · discharged · Jul 9, 2014 · N14947 · Emb EMB145EP · Emergency Lighting > DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130407049H](https://openairdocs.org/sdr/ASOA20130407049H.md): Skin · cracked · Apr 7, 2013 · N14947 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING A-CK INSPECTION, THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STR 1R AND 2R. MX PERFORMED A DOUBLER REPAIR WITH DRAG ANGLE IAW ENGINEERING CHANGE AND RA EC 5330-02353, AND ACFT APPROVED FOR SERVICE. - [SDR ASOA20121107154](https://openairdocs.org/sdr/ASOA20121107154.md): Skin · dented · Nov 6, 2012 · N14947 · Emb EMB145EP · Cargo/Baggage Doors > TWO DENTS ON CARGO DOOR RIGHT ABOVE STR 12L BETWEEN X=22364.2 AND X=22640.2. RECONTOURED BACK TO ORIGINAL SHAPE AND REFINISHED. - [SDR C2XA11IA136](https://openairdocs.org/sdr/C2XA11IA136.md): Light · inoperative · Jun 28, 2011 · N14947 · Emb EMB145EP · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA273](https://openairdocs.org/sdr/C2XA10IA273.md): Ballast · overheated · Oct 21, 2010 · N14947 · Emb EMB145EP · Passenger Compartment Lighting > IAH - FLIGHT 2935, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM SEAT 1A AREA. MAINTENANCE PLACED THE CEILING BALLAST AT ROW 1A ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/22/10 IAH MAINTENANCE REMOVED AND REPLACED - [SDR C2XA10IA267](https://openairdocs.org/sdr/C2XA10IA267.md): Light · overheated · Oct 13, 2010 · N14947 · Emb EMB145EP · Passenger Compartment Lighting > FLIGHT 2804, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR NEAR SEAT 1A, FOLLOWED BY AN INOP READING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE READING LIGHT SOCKET AT 1A TO BE WORN, THE BULB WAS REMOVED AND THE LIGHT PLACED ON - [SDR C2XA10IA264](https://openairdocs.org/sdr/C2XA10IA264.md): Velocity Sensor · inoperative · Oct 5, 2010 · N14947 · Emb EMB145EP · Trailing Flap Position Indicating System > IAH - FLIGHT 2554, THE CREW REPORTED A FLAP FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP VELOCITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP - [SDR C2XA10SH158](https://openairdocs.org/sdr/C2XA10SH158.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM FRAME 23 IAW EMB-145 SRM 53-21-10, SRM 51-40-02 AND SRM 51-30-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH157](https://openairdocs.org/sdr/C2XA10SH157.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 54. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM SUPPORT AT FRAME 54 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI - [SDR C2XA10SH156](https://openairdocs.org/sdr/C2XA10SH156.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 54. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 54 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH155](https://openairdocs.org/sdr/C2XA10SH155.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 49. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CROSSBEAM AT FRAME 49 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH154](https://openairdocs.org/sdr/C2XA10SH154.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 44. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH153](https://openairdocs.org/sdr/C2XA10SH153.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 44 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH152](https://openairdocs.org/sdr/C2XA10SH152.md): Fitting · cracked · Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach Fittings > SHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENG YOKE FWD LWR FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH151](https://openairdocs.org/sdr/C2XA10SH151.md): Fitting · cracked · Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach Fittings > SHV - DURING C-CHECK NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF CRACK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH150](https://openairdocs.org/sdr/C2XA10SH150.md): Bracket · damaged · Apr 25, 2010 · N14947 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK LT AILERON PCA BRACKET I/B FLANGE HAT BUSHINGS MISSING AND HOUSING IS DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH149](https://openairdocs.org/sdr/C2XA10SH149.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 39 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH148](https://openairdocs.org/sdr/C2XA10SH148.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM FRAME 38-39 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH147](https://openairdocs.org/sdr/C2XA10SH147.md): Inlet · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon Miscellaneous Structure > SHV - DURING C-CHECK RT INLET HAS SEVERAL NUT PLATE HOLES THAT ARE CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT INLET NUT PLATE HOLES IAW EC5420-01158. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH146](https://openairdocs.org/sdr/C2XA10SH146.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE INSTALLED DOUBLER ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AREA FRAME 33-34 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA10SH145](https://openairdocs.org/sdr/C2XA10SH145.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAME 33 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH144](https://openairdocs.org/sdr/C2XA10SH144.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH143](https://openairdocs.org/sdr/C2XA10SH143.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 29. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM CARBON CROSSBEAM CUTOUT AT FRAME 29 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH142](https://openairdocs.org/sdr/C2XA10SH142.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 25 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH141](https://openairdocs.org/sdr/C2XA10SH141.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 20. MAINTENANCE PERFORMED REPAIR OF LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH140](https://openairdocs.org/sdr/C2XA10SH140.md): Floor Support · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 25. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 25 CARBON CROSSBEAM AREA IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH139](https://openairdocs.org/sdr/C2XA10SH139.md): Fitting · corroded · Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK BAGGAGE DOOR CUTOUT HAS CORROSION (LEVEL 2 LOCAL) AT FWD LWR CORNER. MAINTENANCE PERFORMED REPAIR OF FRAME 65 SHEAR CLIP AT BAGGAGE DOOR CUTOUT FWD LWR CORNER IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH137](https://openairdocs.org/sdr/C2XA10SH137.md): Fitting · cracked · Apr 17, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach Fittings > SHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT HAS VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE YOKE FWD LOWER PYLON FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA078](https://openairdocs.org/sdr/C2XA10IA078.md): Fcu · inoperative · Feb 23, 2010 · N14947 · Emb EMB145EP · Fuel Indicating System > IAH - FLIGHT 2481, THE CREW REPORTED BOTH FUEL QUANTITY INDICATORS WENT TO DASHES ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FCU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP - [SDR C2XA10IA037](https://openairdocs.org/sdr/C2XA10IA037.md): Battery Pack · discharged · Jan 22, 2010 · N14947 · Emb EMB145EP · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO - [SDR C2XA10IA031](https://openairdocs.org/sdr/C2XA10IA031.md): Ballast · malfunctioned · Jan 21, 2010 · N14947 · Emb EMB145EP · Passenger Compartment Lighting > DFW - FLIGHT 2324 THE CREW REPORTED A FAINT ELECTRICAL BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED SIDEWALL LIGHTS 2A & 3A ON MEL 33-20-00/1 CAT C, AND THE AIRCRAFT WAS APPROVED FOR - [SDR C2XA09IA213](https://openairdocs.org/sdr/C2XA09IA213.md): Hinge · broken · Aug 25, 2009 · N14947 · Emb EMB145EP · Cargo Compartments > IAH - FLIGHT 3040, DURING PREFLIGHT INSPECTION THE CARGO RAMP ASSY WAS FOUND TO HAVE A BROKEN HINGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA146](https://openairdocs.org/sdr/C2XA09IA146.md): Unknown · malfunctioned · Jun 3, 2009 · N14947 · Emb EMB145EP · AC Generator-Alternator > IAH - FLIGHT 2804 - THE CREW REPORTED THE LOSS OF GENERATORS 1, 2, & 4 IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND ALL GENERATORS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVE - [SDR C2XA09IA082](https://openairdocs.org/sdr/C2XA09IA082.md): Connector · disconnected · Mar 17, 2009 · N14947 · Emb EMB145EP · Light System Wiring > IAH - FLIGHT 2803 - DURING PREFLIGHT INSPECTION THE LEFT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-SECURED THE ELECTRICAL CONNECTION TO THE SIGN, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA008](https://openairdocs.org/sdr/C2XA09IA008.md): Uplock · inoperative · Jan 5, 2009 · N14947 · Emb EMB145EP · Landing Gear Retraction/Extension System > FLIGHT 4930, THE CREW REPORTED THAT THE NLG DOORS FAILED TO RETRACT. THE ACFT RETURNED TO ICT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FERRIED IT TO MCI WHERE MX REMOVED AND REPLACED THE NLG UPLOCK BOX, OPS TESTED WITH NO DEFECTS. THE ACFT W - [SDR C2XA09IA007](https://openairdocs.org/sdr/C2XA09IA007.md): Solenoid Valve · inoperative · Jan 4, 2009 · N14947 · Emb EMB145EP · Landing Gear Door Retract Section > DURING MX INSP THE NLG DOORS WERE FOUND TO BE NOT CLOSING. MX REMOVED AND REPLACED THE NLG DOOR SOLENOID VALVE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA006](https://openairdocs.org/sdr/C2XA09IA006.md): Proximity Switch · inoperative · Jan 4, 2009 · N14947 · Emb EMB145EP · Landing Gear Position and Warning > THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON CLIMB OUT WITH THE NOSE GEAR DOWN. THE ACFT RETURNED TO ICT WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE NLG UPLOCK BOX PROXIMITY SWITCHES, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVE - [SDR C2XA08SH165](https://openairdocs.org/sdr/C2XA08SH165.md): Proximity Switch · defective · Dec 29, 2008 · N14947 · Emb EMB145EP · Landing Gear Position and Warning > ON DEPARTURE OUT, NLG WOULD NOT RETRACT. REMOVED AND REPLACED NLG UPLOCK PROXIMITY SWITCH IAW EMB 145 32-63-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08TY058](https://openairdocs.org/sdr/C2XA08TY058.md): Light · inoperative · Jun 13, 2008 · N14947 · Emb EMB145EP · Emergency Lighting > EMERGENCY LIGHT IN MID CEILING, AFT SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB 145 AMM 33-51-01. OPS CHECK GOOD. (S) - [SDR C2XA08IA094](https://openairdocs.org/sdr/C2XA08IA094.md): Skin · cracked · Mar 30, 2008 · N14947 · Emb EMB145EP · Wing, Plate/Skin > IAH - FLIGHT 2695, DURING PREFLIGHT INSPECTION, THE CREW REPORTED CRACKS AT THE SPOILER HINGE POINTS. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETERMINED THAT ONLY THE RIGHT HAND UPPER CENTER HINGE CUTOUT TO HAVE AN 18MM CRACK. THE CRACK WAS PLACED ON DMI FOR - [SDR C2XA08TY036](https://openairdocs.org/sdr/C2XA08TY036.md): Light · inoperative · Mar 18, 2008 · N14947 · Emb EMB145EP · Emergency Lighting > EMERGENCY EXIT ROW OVERHEAD AFT EXIT LIGHT INOP. REPLACED EXIT LIGHT ASSY IAW EMB 145AMM 33-50-13. OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA08RI022](https://openairdocs.org/sdr/C2XA08RI022.md): Electronic Unit · malfunctioned · Feb 18, 2008 · N14947 · Emb EMB145EP · Landing Gear Retraction/Extension System > FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL (LGEU) IAW EMB145 AMM 32-32-01 AND PERFORMED OPERATIONAL - [SDR C2XA08RI021](https://openairdocs.org/sdr/C2XA08RI021.md): Control Lever · faulty · Feb 18, 2008 · N14947 · Emb EMB145EP · Landing Gear Selector > FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM 32-32-02 AND PERFORMED OPERATIONAL CHECK SUCCE - [SDR C2XA07RI094](https://openairdocs.org/sdr/C2XA07RI094.md): Landing Gear · malfunctioned · Nov 6, 2007 · N14947 · Emb EMB145EP · Landing Gear Retraction/Extension System > FLT 2581 - EWR - CREW REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT FOR ABOUT 2 MINUTES AFTER THE GEAR HANDLE WAS SELECTED UP. EWR MX PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR SYSTEM (EXTENSION & RETRACTION) IAW EMB AMM 32-30-00 AND C - [SDR C2XA07SH078](https://openairdocs.org/sdr/C2XA07SH078.md): Floor Support · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK MAINTENANCE FOUND LT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 20 & 23. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRAME 20 & 23 IAW IC 2007-145-06463. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07SH077](https://openairdocs.org/sdr/C2XA07SH077.md): Floor Support · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK MAINTENANCE FOUND RT OMEGA BEAM WITH CORROSION BETWEEN FRAMES 18 & 19. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 18 IAW EMB 145 EC 5510-01381. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07SH076](https://openairdocs.org/sdr/C2XA07SH076.md): Shroud · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK MAINTENANCE FOUND LT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AILERON LOWER SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07SH075](https://openairdocs.org/sdr/C2XA07SH075.md): Shroud · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK MAINTENANCE FOUND LT AILERON UPPER SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED LT AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07SH074](https://openairdocs.org/sdr/C2XA07SH074.md): Shroud · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK MAINTENANCE FOUND RT UPPER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT UPPER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07SH073](https://openairdocs.org/sdr/C2XA07SH073.md): Shroud · corroded · Sep 21, 2007 · N14947 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK MAINTENANCE FOUND RT LOWER AILERON SHROUD WITH CORRODED BONDING PLATES. MAINTENANCE REPAIRED RT LOWER AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. Next page: https://openairdocs.org/deregistered/N14947-2018-11-08/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 = 'N14947' AND deregistration_id = 'N14947-2018-11-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14947-2018-11-08/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.