# Service difficulty reports: N17185 A list on [N17185](https://openairdocs.org/aircraft/N17185.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR JJBA20220112022](https://openairdocs.org/sdr/JJBA20220112022.md): Cable · out of limits · Jan 12, 2022 · N17185 · Emb EMB145XR · Rudder Control System > LEFT RUDDER AP SERVO CABLE CONNECTION FOUND TO BE OUT OF LIMITS. ADJUSTED LEFT RUDDER AP SERVO CABLE. TENSION CHECK SAT. - [SDR JJBA202201182021](https://openairdocs.org/sdr/JJBA202201182021.md): Cable · out of limits · Jan 12, 2022 · N17185 · Emb EMB145XR · Rudder Control System > RIGHT RUDDER AP SERVO CABLE CONNECTION FOUND TO BE OUT OF LIMITS. ADJSUTED RIGHT RUDDER AP SERVO CABLE. TENSION CHECK SAT. - [SDR JJBA20210529032](https://openairdocs.org/sdr/JJBA20210529032.md): Bulb · inoperative · May 29, 2021 · N17185 · Emb EMB145XR · Emergency Lighting > MCD AND SERVICE DOOR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R BULB AT SERVICE DOOR EMERGENCY LIGHT. OPS CHECK SAT. REMOVED MCD EXTERNAL EMERGENCY LIGHT HOUSING AND OBSERVED GROUND CONNECTION LOOSE. R&R BULB. OPS CHECK FAILED. RESURED GROUND CONNECTION. OPS C - [SDR ASOA2020032405011](https://openairdocs.org/sdr/ASOA2020032405011.md): Fuse · blown · Mar 20, 2020 · N17185 · Emb EMB145XR · Emergency Lighting > PILOT REPORTED EMERGENCY LIGHT NEXT TO THE GALLEY IS NOT WORKING. MX REMOVED AND REPLACED FUSE 9 AT BATTERY TRAY #1 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201911297135](https://openairdocs.org/sdr/ASOA201911297135.md): Support Plate · corroded · Nov 29, 2019 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > VENTRAL TANK FORWARD O/B SKIN FUEL LINE SHROUD SUPPORT DOUBLER CORRODED. REMOVED CORRODED BRACKET, REMOVED PREVIOUSLY INSTALLED REPAIR, CUT-OUT DAMAGED AREA ON RIB 1, FABRICATED REPAIR PARTS AND INSTALLED. IAW ETD2019-145-155071. AIRCRAFT STILL IN C CHECK. - [SDR ASOA2019111907134](https://openairdocs.org/sdr/ASOA2019111907134.md): Rib · cracked · Nov 19, 2019 · N17185 · Emb EMB145XR · Wing Spar > TYS A/C IS IN FOR A C-CHECK INSPECTION WHEN MAINTENANCE FOUND THE L/H WING AT RIB 21 CRACKED. MAINTENANCE REPAIRED THE RIB 21 IAW ETD 2019-145-153596. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA201705155075](https://openairdocs.org/sdr/ASOA201705155075.md): Mechanism · out of adjust · May 15, 2017 · N17185 · Emb EMB145XR · Passenger/Crew Doors > CREW REPORTED CABIN DOOR WILL NOT OPEN FROM INSIDE. MX ADJUSTED DOOR OPEN AND CLOSE MECHANISM WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201704123077](https://openairdocs.org/sdr/ASOA201704123077.md): Floorbeam · corroded · Apr 12, 2017 · N17185 · Emb EMB145XR · Fuselage Main, Floor Beam > CENTER FUSELAGE 4 RT FLOORBEAM UNDER GUSSET CORRODED AT ANCHOR NUT LOCATION. 61 REPAIRED IAW ETD2017-145-028579. HFEC PERFORMED WITH NO FAULT FOUND. - [SDR ASOA201704113076](https://openairdocs.org/sdr/ASOA201704113076.md): Frame · corroded · Apr 12, 2017 · N17185 · Emb EMB145XR · Cargo/Baggage Doors > CARGO DOOR AFT AND FWD L-SHAPE CORRODED. BAGGAGE DOOR AFT L-SHAPE REPROTECTED IAW 51-21-05/04. BAGGAGE DOOR FWD L-SHAPE CORROSION REMOVED IAW 53-31-04. HFEC PERFORMED WITH NO FAULT FOUND. - [SDR ASOA201704113075](https://openairdocs.org/sdr/ASOA201704113075.md): Bulkhead · cracked · Apr 11, 2017 · N17185 · Emb EMB145XR · Fuselage Main, Bulkhead > LEFT WHEEL WELL AFT BULKHEAD CRACKED UPEER OUTBOARD CORNER. THE BULKHEAD UPPER OUTBOARD CORNER WAS REPAIRED IAW SRM 53-23-12 AND ETD2017-145-027457. - [SDR ASOA201704113074](https://openairdocs.org/sdr/ASOA201704113074.md): Bulkhead · cracked · Apr 11, 2017 · N17185 · Emb EMB145XR · Fuselage Main, Bulkhead > R/H WHEELWELL AFT BULKHEAD CRACKED UPPER OUTBOARD CORNER. RT WHEEL WELL AFT BULKHEAD UPPER OUTBOARD CORNER REPAIRED IAW SRM 53-23-12 AND ETD2017-145-027457. HFEC PERFORMED WITH NO FAULTS FOUND. - [SDR ASOA201704113073](https://openairdocs.org/sdr/ASOA201704113073.md): Support · cracked · Apr 11, 2017 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > WING TO BODY FAIRING ANGLE CRACKED AT RT TOP NR 1 AFT END. THE ANGLE WAS REPAIRED IAW SRM 53-21-12 AND ETD2017-145-027506. - [SDR ASOA201704113072](https://openairdocs.org/sdr/ASOA201704113072.md): Skin · corroded · Apr 11, 2017 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > CORROSION FOUND ON FUSELAGE SKIN AROUND AFT RADIO ALTIMETER AT FRAME 68. SKIN AREA UNDER AFT RADIO ALT ANTENNA REPAIRED IAW ETD2017-145-027855. AFT RADIO ALT ANTENNA BASE AND SUPPORT REPLACED. HFEC PERFORMED ON REPAINTED AREA WITH NO FAULT. - [SDR ASOA201704113071](https://openairdocs.org/sdr/ASOA201704113071.md): Skin · corroded · Apr 11, 2017 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > FUSELAGE SKIN UNDER RADIO ALTIMETER ANTENNA BASE CORRODED, BETWEEN FRAMES 65 & 66. BLENDED IAW ETD2017-145-027855. HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT FOUND. - [SDR ASOA201704053068](https://openairdocs.org/sdr/ASOA201704053068.md): Floor Support · corroded · Apr 5, 2017 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > RIGHT OTBD FLOOR SUPPORT AT FRAMES 49 AND 51 CORRODED. REPLACED IAW SRM 51-40-02.. - [SDR ASOA201704053067](https://openairdocs.org/sdr/ASOA201704053067.md): Floor Support · corroded · Apr 5, 2017 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > LEFT OTBD FLOOR SUPPORT AT FRAME 51 CORRODED. REPLACED IAW SRM 51-40-02. - [SDR ASOA20160228015H](https://openairdocs.org/sdr/ASOA20160228015H.md): Battery Pack · discharged · Feb 28, 2016 · N17185 · Emb EMB145XR · Emergency Lighting > DURING MAINTENANCE INSPECTION THE RT & LT FORWARD EXTERIOR OVERWING LIGHTS AND THE FWD AISLE EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS AP - [SDR ASOA20160202003](https://openairdocs.org/sdr/ASOA20160202003.md): Inverter · abnormal · Feb 2, 2016 · N17185 · Emb EMB145XR · Emergency Lighting > THE FWD SIDE EMERGENCY LIGHTS AT THE OVERWING EXIT WAS REPORTED INOPERATIVE. MAINTENANCE R & R NR 6 INVERTER FOR EMERGENCY LIGHT SYS WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140917281](https://openairdocs.org/sdr/ASOA20140917281.md): Skin · cracked · Sep 17, 2014 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > DURING C-CHECK, LT FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 79. LEFT FUSELAGE SKIN WAS REPAIRED IAW EC5330-02940. - [SDR ASOA20140917280](https://openairdocs.org/sdr/ASOA20140917280.md): Skin · cracked · Sep 17, 2014 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > DURING C-CHECK, RT FUSELAGE SKIN IS CRACKED AROUND RIVET AT FRAME 79. REPAIRED FUSELAGE SKIN IAW EC5330-02940. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140917279](https://openairdocs.org/sdr/ASOA20140917279.md): Door Sill · corroded · Sep 17, 2014 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING A C-CHECK. CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT CENTER SILL. REPAIRED SERVICE DOOR CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140913277](https://openairdocs.org/sdr/ASOA20140913277.md): Threshold · corroded · Sep 13, 2014 · N17185 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK, CARGO CUTOUT THRESHOLD CORRODED, LOCAL LEVEL 2, FRAMES 65-68. MAINTENANCE R & R CARGO CUTOUT THRESHOLD BETWEEN FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140913276](https://openairdocs.org/sdr/ASOA20140913276.md): Valve · corroded · Sep 13, 2014 · N17185 · Emb EMB145XR · Waste Disposal System > DURING C-CHECK, TOILET WASTE VALVE SUPPORT HAS CORROSION. MAINTENANCE R & R TOILET WASTE VALVE SUPPORT ASSY IAW SRM 51-40-02 AND IS DETERMINED TO BE MAJOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140913275V](https://openairdocs.org/sdr/ASOA20140913275V.md): Bushing · migrated · Sep 13, 2014 · N17185 · Emb EMB145XR · Rudder Structure > DURING C-CHECK, RUDDER II UPPER CENTER HINGE HAS A MIGRATED HAT BUSHING, SECOND FROM TOP. MAINTENANCE R & R RUDDER II UPPER CENTER HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140913274](https://openairdocs.org/sdr/ASOA20140913274.md): Bushing · migrated · Sep 13, 2014 · N17185 · Emb EMB145XR · Rudder Structure > DURING C-CHECK, LOWER RUDDER ACTUATOR FITTING HAT BUSHING MISSING AT RUDDER I. MAINTENANCE R & R LOWER RUDDER ACTUATOR FITTING AT RUDDER I IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131129134](https://openairdocs.org/sdr/ASOA20131129134.md): Inverter · inoperative · Nov 29, 2013 · N17185 · Emb EMB145XR · Emergency Lighting > PILOT REPORTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE R & R NR 1 EMERGENCY LIGHT INVERTER WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140224033](https://openairdocs.org/sdr/ASOA20140224033.md): Skin · scratched · Feb 24, 2013 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > DURING WALKAROUND INSPECTION, A SCRATCH WAS DISCOVERED IN THE AFT FUSELAGE SKIN BETWEEN FRAMES 69-70 AND EXTENDING BETWEEN STRINGERS 14L-15L. MAINTENANCE BLENDED THE DAMAGE AND INSTALLED A REPAIR DOUBLER IAW DER APPROVED TECHNICAL DISPOSITION ETD2014-145-01608 - [SDR ASOA20120814061](https://openairdocs.org/sdr/ASOA20120814061.md): Inverter · inoperative · Aug 14, 2012 · N17185 · Emb EMB145XR · Emergency Lighting > DURING MX INSP THE LT LOWER INTERIOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. MX R & R NR 5 INVERTER AND SIGN WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2012010900001](https://openairdocs.org/sdr/ASOA2012010900001.md): Landing Gear · malfunctioned · Jan 9, 2012 · N17185 · Emb EMB145XR · Landing Gear Retraction/Extension System > TOWER REPORTED TO DEPARTURE THAT THE LT MLG NOT FULLY RETRACTED ON T/O. THE CREW REPORTED NORMAL INDICATIONS IN THE COCKPIT WITH ALL GEAR UP AND LOCKED. THE CREW MAINTAINED THE ACFT BELOW 250 KIAS AS A PRECAUTION. THE ACFT LANDED IN WITHOUT INCIDENT, WHERE M - [SDR C2XA11RI154](https://openairdocs.org/sdr/C2XA11RI154.md): Connector · disconnected · Sep 17, 2011 · N17185 · Emb EMB145XR · Light System Wiring > RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND SEAT 12A LOWER EXIT EMERGENCY LIGHT INOPERATIVE. MX FOUND THE CONNECTOR FOR THE LIGHT TO BE LOOSE. MX RECONNECTED LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA164](https://openairdocs.org/sdr/C2XA11IA164.md): Sensor · inoperative · Jul 29, 2011 · N17185 · Emb EMB145XR · Fuel Quantity Sensor > IAH - FLIGHT 2053, THE CREW REPORTED A FUEL CONFIG DISAGREE MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE VENTRAL TANK LOW LEVEL SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS - [SDR C2XA10TY168](https://openairdocs.org/sdr/C2XA10TY168.md): Smoke Detector · defective · Oct 25, 2010 · N17185 · Emb EMB145XR · Emergency Lighting > TYS - A/C JUST CAME OUT OF C-CHECK WHEN THE LAV SMOKE DETECTOR WOULDN'T TEST. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW AMM 26-14-01. OPS CHECK GOOD AND RELEASED TO SERVICE. - [SDR C2XA10CL160](https://openairdocs.org/sdr/C2XA10CL160.md): Wire · burned · Oct 22, 2010 · N17185 · Emb EMB145XR · Electrical Power System Wiring > DURING MAINTENANCE THE APU GENERATOR WIRE WAS FOUND BURNED UNDER THE CARGO FLOOR. THE WIRE WAS BURNED AT THE MANUFACTURE SPLICE WHERE THE WIRE CHANGES FROM COPPER TO ALUMINUM. MAINTENANCE REPLACED THE WIRE WHICH RUNS FROM LEFT POWER CONTROL BOX IN THE COCKPI - [SDR C2XA10TY166](https://openairdocs.org/sdr/C2XA10TY166.md): Rib · bent · Oct 21, 2010 · N17185 · Emb EMB145XR · Elevator, Spar/Rib > LT ELEVATOR CLOSING-RIB CAP IS BENT APPROX 10 INCHES FROM LEADING EDGE. MAINTENANCE INDUCED DAMAGE. PERFORMED DOUBLER AND FILLER REPAIR, FABRICATION, ALODINE, PRIME, PAINT AND INSTALL ALL IAW ETD2010-145/09760. - [SDR C2XA10CL111](https://openairdocs.org/sdr/C2XA10CL111.md): Generator · failed · Jul 13, 2010 · N17185 · Emb EMB145XR · AC Generator-Alternator > THE CREW REPORTED A GENERATOR 2 BEARING FAIL MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND REPLACED THE NR 2 GENERATOR. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10TY037](https://openairdocs.org/sdr/C2XA10TY037.md): Skin · dented · Mar 11, 2010 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > DENT ON LT SIDE OF FUSELAGE FRAME 19 & 20 JUST AFT OF MAIN DOOR STR 11L & 12L. REPAIRED DENT IAW EC 5330-02087. CUT OUT DAMAGE, INSTALLED FABRICATED FILLER, INSTALLED FABRICATED EXTERNAL DOUBLER. - [SDR C2XA10TY036](https://openairdocs.org/sdr/C2XA10TY036.md): Skin · dented · Mar 11, 2010 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > DENT ON LT SIDE OF FUSELAGE FRAME 19 & 20 JUST AFT OF MAIN DOOR STR 12L & 13L. REPAIRED DENT IAW EC 5330-02087. CUT OUT DAMAGE, INSTALLED FABRICATED FILLER, INSTALLED FABRICATED INTERNAL DOUBLER. - [SDR C2XA09TY222](https://openairdocs.org/sdr/C2XA09TY222.md): Skin · damaged · Aug 13, 2009 · N17185 · Emb EMB145XR · Fuselage Main, Plate/Skin > AIRCRAFT HAS LIGHTNING STRIKE BURN DAMAGE ON FUSELAGE SKIN AT FRM 20 STR 19L, FRM 13 STR 20L AND FRM 9 STR 18L. DRILLED DAMAGE, INSTALLED RIVET AND WASHER, PRESSURE CHECKED GOOD. ALL WORK C/W IAW 145XR SRM 53-00-01 & EMB135/145 CPM 51-21-07. - [SDR C2XA08ON109](https://openairdocs.org/sdr/C2XA08ON109.md): Duct Clamp · missing · Mar 30, 2008 · N17185 · Emb EMB145XR · Pneumatic Distribution System > FLT 0412 - SAN - FLIGHT CREW ABORTED T/O DUE TO NR 1 ENG EXCEEDANCE ON TAKEOFF ROLL. MX INSPECTED BLEED DUCTS AND COMPRESSOR BLEED AIR DUCTING ON ENGINE AND FOUND CLAMP MISSING ON COMPRESSOR DISCHARGE TUBE. INSTALLED NEW CLAMP OPERATIONALLY AND LEAK CHECKED - [SDR C2XA07ON046](https://openairdocs.org/sdr/C2XA07ON046.md): Smoke Detector · inoperative · Dec 27, 2007 · N17185 · Emb EMB145XR · Smoke Detection > FLT MX - TYS - WHILE PERFORMING PLANNED MX INSPECTION THE NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. MX PERSONNEL REMOVED AND REPLACED NR 2 BAGGAGE SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDI - [SDR C2XA07ON048](https://openairdocs.org/sdr/C2XA07ON048.md): Pressure Switch · faulty · Dec 17, 2007 · N17185 · Emb EMB145XR · Rudder Control System > FLT 7652 - LAX TO LAX - FLIGHT CREW REPORTED RUDDER OVERBOOST ON CLIMBOUT OF ONT. MX PERSONNEL REMOVED AND REPLACED NR 1 RUDDER PRESSURE SWITCH. OPERATIONALLY CHECKED GOOD AND A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. - [SDR C2XA07IA220](https://openairdocs.org/sdr/C2XA07IA220.md): Smoke Warning · malfunctioned · Oct 9, 2007 · N17185 · Emb EMB145XR · Smoke Detection > IAH - FLIGHT 537, THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON CLIMB. THE CARGO FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGAGE SMOKE DE ## 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 = 'N17185' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N17185/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.