# Service difficulty reports: N18114 A list on [N18114](https://openairdocs.org/aircraft/N18114.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR RAIA2019100740002](https://openairdocs.org/sdr/RAIA2019100740002.md): Pump · leaking · Oct 4, 2019 · N18114 · Emb EMB145XR · Hydraulic Pump (Electric/Engine), Main > SYSTEM 2 HYDRAULIC LOST FLUID IN FLIGHT. R & R THE NR 2 ENGINE HYD PUMP DUE TO A LEAK. LEAK AND OPS CHECKED GOOD. - [SDR RAIA201909070001](https://openairdocs.org/sdr/RAIA201909070001.md): Light · cracked · Sep 7, 2019 · N18114 · Emb EMB145XR · Emergency Lighting > FLOOR PATH LIGHTING AT 4C/D IS CRACKED. REMOVED & REPLACED FLOOR PATH LIGHTING AT 4 C/D. - [SDR RAIA201907050001](https://openairdocs.org/sdr/RAIA201907050001.md): Warning System · false activation · Jul 5, 2019 · N18114 · Emb EMB145XR · Drag Control System > HIGH SPEED ABORT AT 90 KIAS. MASTER WARNING SPOILERS OPEN---- LOG PAGE 382906 C/W HIGH ENERGY STOP INSP NO FAULTS FOUND- LOG PAGE 382907 CLEANED AND INSP SPOILER PROX SENSOR AND SYSTEM, OPS CHECK GOOD. - [SDR RAIA201905070001](https://openairdocs.org/sdr/RAIA201905070001.md): Garlock Seal · leaking · May 7, 2019 · N18114 · Emb EMB145XR · Turbine Engine Oil System > E2 SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE AND LOW QUANITY. OIL PRESSURE DROPPED TO 34 PSI AND 3 QTS. AT COMMANDED SHUT DOWN PSI INDICATED 8 PSI AND 2 QTS. R/R NR 2 ENG ATS GARLOCK SEAL. LEAK CHECK GOOD. - [SDR RAIA2019041270001](https://openairdocs.org/sdr/RAIA2019041270001.md): Oxygen Bottle · leaking · Apr 7, 2019 · N18114 · Emb EMB145XR · Crew Oxygen System > LOW O2 EICAS MESSAGE IN FLIGHT. DIVERTED. LESS THAN 400 PSI ON OXYGEN WHEN CHECKED ON MFD BEFORE AIRCRAFT SHUTDOWN. R & R CREW OXYGEN BOTTLE. OPS CHECK GOOD. - [SDR RAIA201903080001](https://openairdocs.org/sdr/RAIA201903080001.md): Fire Loop · failed · Mar 8, 2019 · N18114 · Emb EMB145XR · Fire Detection > E1 FIRE DETECT FAIL IN FLIGHT. REMOVED AND REPLACED ENG 1 FIRE DETECTION LOOP. OPS CHECK GOOD. - [SDR RAIA201810180002](https://openairdocs.org/sdr/RAIA201810180002.md): Door Sill · cracked · Oct 18, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT FLOOR SILL BETWEEN FR53 AND FR59 IS CRACKED. REMOVED AND REPLACED RT FLOOR SILL AT FR53 AND FR59. - [SDR RAIA201810120004](https://openairdocs.org/sdr/RAIA201810120004.md): Door Sill · corroded · Oct 12, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT FUSELAGE FLOOR ATTACHMENT FLANGE CORRODED AT FR 40-41. REMOVE AND REPLACE RT FLOOR SILL AT FR36-41. - [SDR RAIA201810080005](https://openairdocs.org/sdr/RAIA201810080005.md): Door Sill · corroded · Oct 8, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > LT FLOOR SILL BETWEEN FR28 AND FR29 HAS CORROSION. REMOVED AND REPLACED LT FLOOR SILL AT FR28 AND FR29. - [SDR RAIA201810060004](https://openairdocs.org/sdr/RAIA201810060004.md): Door Sill · corroded · Oct 6, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CORROSION ON RT FLOOR ATTACH FLANGE AT FR50 AND FR51. REMOVED AND REPLACED RT FLOOR SILL AT FR 50 AND FR51. - [SDR RAIA201810060003](https://openairdocs.org/sdr/RAIA201810060003.md): Door Sill · corroded · Oct 6, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > LIGHT SURFACE CORROSION ON LT FLOOR ATTACH FLANGE BETWEEN FR31-32 AND FR37-38. BLENDED FLOOR SILLS FR37-38 IN LIMITS, FR31-32 OUT OF LIMITS. REMOVED AND REPLACED LT FLOOR SILL AT FR 31-32. - [SDR RAIA2018102460002](https://openairdocs.org/sdr/RAIA2018102460002.md): Door Sill · corroded · Oct 6, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CORROSION ON LT FLOOR ATTACH FLANGE AT FR50. REMOVED AND REPLACED LT FLOOR SILL AT FR 50. - [SDR RAIA2018102460001](https://openairdocs.org/sdr/RAIA2018102460001.md): Door Sill · corroded · Oct 6, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CORROSION FOUND ON FLOOR ATTACH FLANGE RT SIDE BETWEEN FR 41 AND FR 48. REMOVED AND REPLACED FLOOR SILL ON RT SIDE BETWEEN FR41 AND FR48. - [SDR RAIA2018102450001](https://openairdocs.org/sdr/RAIA2018102450001.md): Crossbeam · cracked · Oct 5, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > AFT AVIONICS COMP CROSSBEAM IS CRACKED. REMOVED AND REPLACED CROSSBEAM. - [SDR RAIA2018102440002](https://openairdocs.org/sdr/RAIA2018102440002.md): Fitting · cracked · Oct 4, 2018 · N18114 · Emb EMB145XR · Nacelle/Pylon, Attach Fittings > NR 2 ENG FWD YOKE LOWER FWD MOUNT LINKAGE FITTING INDICATION OF POSSIBLE CRACK AT UPPER INSIDE RADIUS. REMOVED AND REPLACED NR 2 ENG FWD YOKE FWD MOUNT LINKAGE FITTING REF EO-EMB145-54-010-0. - [SDR RAIA2018102440001](https://openairdocs.org/sdr/RAIA2018102440001.md): Support Bracket · cracked · Oct 4, 2018 · N18114 · Emb EMB145XR · Passenger/Crew Doors > PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED DOOR HANDLE SUPPORT BRACKET. - [SDR RAIA2018102430006](https://openairdocs.org/sdr/RAIA2018102430006.md): Door Sill · chafed · Oct 3, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT FLOOR SILL IN CARGO BAY HAS CHAFE MARKS AROUND NUT PLATE HOLES BETWEEN FR61 AND FR65. REMOVED AND REPLACED RT FLOOR SILL BETWEEN FR61 AND FR65. - [SDR RAIA2018102430005](https://openairdocs.org/sdr/RAIA2018102430005.md): Support · cracked · Oct 3, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CARGO DOOR HOLD OPEN ROD SUPPORT IS CRACKED. REMOVED AND REPLACED CARGO DOOR ROD CUP SUPPORT. - [SDR RAIA2018102430004](https://openairdocs.org/sdr/RAIA2018102430004.md): Frame · scratched · Oct 3, 2018 · N18114 · Emb EMB145XR · Fuselage Main, Frame > FR 61 HAS SCRATCHES AROUND NUT PLATE HOLES. REMOVED AND REPLACED FR 61 LOWER PARTITION DOUBLED. - [SDR RAIA2018102430003](https://openairdocs.org/sdr/RAIA2018102430003.md): Frame · chafed · Oct 3, 2018 · N18114 · Emb EMB145XR · Fuselage Main, Frame > FR 70 CHAFED BY STRINGER 11R. BLENDED OUT DAMAGE TO FR 70 REF. ETD2018-145-105368. - [SDR RAIA2018102430002](https://openairdocs.org/sdr/RAIA2018102430002.md): Plate · chafed · Oct 3, 2018 · N18114 · Emb EMB145XR · Nacelle/Pylon Miscellaneous Structure > RT PYLON FWD YOKE GUSSET PLATE HAS CHAFE DAMAGE. REMOVED AND REPLACED RT PYLON FWD GUSSET PLATE. - [SDR RAIA2018102430001](https://openairdocs.org/sdr/RAIA2018102430001.md): Handle · cracked · Oct 3, 2018 · N18114 · Emb EMB145XR · Electrical/Electronic Compartment Doors > REAR ELECTRONIC COMP DOOR HANDLE IS BENT AND POSSIBLY CRACKED. REMOVED AND REPLACED DOOR HANDLE. - [SDR RAIA2018102420003](https://openairdocs.org/sdr/RAIA2018102420003.md): Gusset · corroded · Oct 2, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT LAV FLOOR GUSSET HAS CORROSION AROUND FWD NUT PLATE. REMOVED AND REPLACED RT LAV FLOOR GUSSET. - [SDR RAIA2018102420002](https://openairdocs.org/sdr/RAIA2018102420002.md): Door Sill · corroded · Oct 2, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT LAV FLOOR SILL HAS CORROSION AROUND AFT NUT PLATE. REMOVED AND REPLACED RT LAV FLOOR SILL. - [SDR RAIA2018102420001](https://openairdocs.org/sdr/RAIA2018102420001.md): Floor Support · corroded · Oct 2, 2018 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > BEAM AT FR 20 BETWEEN CTR AND LT OMEGA BEAMS HAS CORROSION. REMOVED AND REPLACED CTR AND LT OMEGA BEAMS AT FR 20. - [SDR RAIA2018082830002](https://openairdocs.org/sdr/RAIA2018082830002.md): Switch · malfunctioned · Aug 23, 2018 · N18114 · Emb EMB145XR · Door Warning System > CARGO DOOR OPEN EICAS MESSAGE. REPLACED THE CARGO DOOR WARNING SWITCH, OPS CHECKED GOOD. - [SDR RAIA201703210002](https://openairdocs.org/sdr/RAIA201703210002.md): Coupling · broken · Mar 21, 2017 · N18114 · Emb EMB145XR · Air Distribution System > PACK 2 CLOSES WITH NO EICAS MESSAGE ASSOCIATED NOSE FROM CABIN FLOOR. FOUND DUCT BLOWN ON #2 PACK REPLACED COUPLING. OPS CHECK GOOD. - [SDR RAIA201610200001](https://openairdocs.org/sdr/RAIA201610200001.md): Switch · failed · Oct 20, 2016 · N18114 · Emb EMB145XR · Stabilizer Control System > EICAS MASTER WARNING PITCH TRIM MAIN INOPERATIVE. REMOVED AND REPLACED CAPTAIN`S PITCH TRIM SWITCH AND PERFORMED OPS CHECKED GOOD ON PITCH TRIM, NO DEFECTS NOTED. - [SDR RAIA201603030001](https://openairdocs.org/sdr/RAIA201603030001.md): Duct · leaking · Mar 3, 2016 · N18114 · Emb EMB145XR · Pneumatic Distribution System > BLEED 2 LEAK. R & R BLEED DUCT CONNECTING TO AIRSTART DUCT ON NR 2 SYSTEM. LEAK CHECK GOOD. - [SDR RAIA201603010003](https://openairdocs.org/sdr/RAIA201603010003.md): Bleed Valve · leaking · Mar 1, 2016 · N18114 · Emb EMB145XR · Compressor Bleed Valve > BLEED 2 LEAK. LOCKED BLEED VALVE CLOSED. PERFORMED OPS CHECK OF 2 BLEED SYS, NO DEFECTS NOTED. - [SDR RAIA201512280002](https://openairdocs.org/sdr/RAIA201512280002.md): Outflow Valve · slow · Dec 28, 2015 · N18114 · Emb EMB145XR · Pressure Regulator/Outflow Valve > SLOW CABIN DEPRESSURIZATION AT FL 230 AFTER CONFIGING TO NORMAL WITH ANTI-ICE ON. R & R PNUEMATIC OUTFLOW VALVE. OPS CHECK GOOD. - [SDR RAIA201512280001](https://openairdocs.org/sdr/RAIA201512280001.md): Warning Message · false activation · Dec 28, 2015 · N18114 · Emb EMB145XR · Pneumatic Distribution System > BLEED 2 OVERTEMP IN FLIGHT, CONDUCTED GROUND RUN OPS TEST. OPS CHECK GOOD. - [SDR RAIA201507220001](https://openairdocs.org/sdr/RAIA201507220001.md): Bolt · loose · Jul 22, 2015 · N18114 · Emb EMB145XR · Turbine Engine Accessory Drive > NR 1 ENGINE LOST 7 QTS OF OIL AFTER 35 MINUTES OF FLYING. CREW COMPLETED PRECAUTIONARY NR 1 ENGINE SHUTDOWN, CONTINUED TO FOR EMERGENCY LANDING. MAINTENANCE INSPECTED AND FOUND A LOOSE BOLT ON ACCESSORY GEAR BOX PLUG, RESECURED BOLT AND PLUG, OPS AND LEAK CH - [SDR ASOA20150114009](https://openairdocs.org/sdr/ASOA20150114009.md): Door Sill · corroded · Jan 14, 2015 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CARGO DOOR CUTOUT CENTER SILL HAS CORROSION. R & R CARGO DOOR CUTOUT CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150112007](https://openairdocs.org/sdr/ASOA20150112007.md): Floor Support · corroded · Jan 12, 2015 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > LEFT OMEGA BEAM CORRODED AT FRAME 59. REPAIRED LEFT OMEGA BEAM IAW EC 5310-01473. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130228026](https://openairdocs.org/sdr/ASOA20130228026.md): Inverter · inoperative · Feb 28, 2013 · N18114 · Emb EMB145XR · Emergency Lighting > DURING A-CHECK INSPECTION, THE LT OVERWING EMERGENCY EXIT DOOR LOWER INTERNAL LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 5 INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11CL149](https://openairdocs.org/sdr/C2XA11CL149.md): Wire Harness · defective · Jun 21, 2011 · N18114 · Emb EMB145XR · Fire Protection System Wiring > CLE FLT 5835 THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. REPLACED THE NR 1 ENGINE EXTERNAL HARNESS AND THE NR 1 ENGINE FIRE LOOP AND THE NR 1 PYLON FIRE LOOP. OPERATIONAL CHECKS - [SDR C2XA11CL147](https://openairdocs.org/sdr/C2XA11CL147.md): Dau · intermittent · Jun 20, 2011 · N18114 · Emb EMB145XR · Fire Detection > THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL ON TAKEOFF. MAINTENANCE INSPECTED AND PERFORMED STEPS OF FIM 26-11-00-810-803A INCLUDING ALL ELECTRICAL STEPS LISTED. NO FAULTS FOUND. REPLACED THE NR 1 DATA ACQUISITION UNIT. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11CL146](https://openairdocs.org/sdr/C2XA11CL146.md): Control Module · faulty · Jun 18, 2011 · N18114 · Emb EMB145XR · Fire Detection > ORD FLT 5887 THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL MESSAGE ON CLIMBOUT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10CL034](https://openairdocs.org/sdr/C2XA10CL034.md): Light · inoperative · Feb 23, 2010 · N18114 · Emb EMB145XR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP ON THE RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA09IA287](https://openairdocs.org/sdr/C2XA09IA287.md): Actuator · inoperative · Nov 10, 2009 · N18114 · Emb EMB145XR · Stabilizer Control System > IAH - FLIGHT 2116, THE CREW REPORTED A PITCH TRIM MAIN INOP EICAS MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCR - [SDR C2XA09RI186](https://openairdocs.org/sdr/C2XA09RI186.md): Wire Harness · damaged · Oct 30, 2009 · N18114 · Emb EMB145XR · Landing Gear System Wiring > FLIGHT 2807 - EWR - FLIGHT CREW REPORTED NR 1 BRAKE TEMP INDICATION IN RED AT TAKE OFF. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LT BRAKE HARNESS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVE - [SDR C2XA07IA207](https://openairdocs.org/sdr/C2XA07IA207.md): Panel · inoperative · Sep 15, 2007 · N18114 · Emb EMB145XR · Instrument Panel > IAH - FLIGHT 2163, THE CREW REPORTED LANDING GEAR LEVER, BACKLIGHTING PANEL, UP POSITION WILL NOT ILUMINATE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED BACKLIGHTING PANEL ON LANDING GEAR LEVER, OPERATIONALLY - [SDR C2XA06TY025](https://openairdocs.org/sdr/C2XA06TY025.md): Floor Support · corroded · Apr 30, 2006 · N18114 · Emb EMB145XR · Fuselage Miscellaneous Structure > CENTER OMEGA BEAM IN GALLEY FROM FRAME 18-23 IS CORRODED. REMOVED AND REPLACED CENTER OMEGA BEAM IN GALLEY IAW EMB145 XR SRM 57-40-02. - [SDR C2XA05SD019](https://openairdocs.org/sdr/C2XA05SD019.md): Flashlight · inoperative · Apr 29, 2005 · N18114 · Emb EMB145XR · Emergency Equipment > SDF - F/O'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA03BT109](https://openairdocs.org/sdr/C2XA03BT109.md): Connector · fire · Nov 19, 2003 · N18114 · Emb EMB145XR · Electrical Connectors > CREW REPORTED, GPU CAUGHT FIRE AT CONNECTOR END AND BURNED AIRCRAFT AT GPU RECEPTICAL (GPU WAS ARCHING WHEN GPU CORD WAS PULLED). MAINTENANCE INSPECTED FUSELAGE AND GPU RECEPTICAL AND FOUND NO DAMAGE. OPS CHECKED AIRCRAFT FOR EICAS MESSAGES AND CONDITION. O - [SDR C2XA03IA052](https://openairdocs.org/sdr/C2XA03IA052.md): Inverter · inoperative · May 20, 2003 · N18114 · Emb EMB145 · Emergency Lighting > DURING POSTFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT ON ROW SEAT TWELVE (12) FORWARD EXIT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED F - [SDR C2XA03IA004](https://openairdocs.org/sdr/C2XA03IA004.md): Controller · inoperative · Jan 11, 2003 · N18114 · Emb EMB145 · Cabin Pressure Controller > DURING CLIMBOUT THE CREW NOTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW DECLARED EMERGENCY, RETURNED TO IAH AND LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE DIGITAL CONTROLLER, PERFORMED A OPERATIONAL CHECK AND NO DEFECTS NOTED - [SDR C2XA02IA250](https://openairdocs.org/sdr/C2XA02IA250.md): Light · disconnected · Dec 14, 2002 · N18114 · Emb EMB145 · Emergency Lighting > DURING PREFLIGHT THE CREW NOTED THAT THE SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE CONNECTED THE EMERGENCY LIGHT TO THE CONNECTOR, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ## 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 = 'N18114' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N18114/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.