# Service difficulty reports: N16541 A list on [N16541](https://openairdocs.org/aircraft/N16541.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 · 79 reports - [SDR JJBA20220306007](https://openairdocs.org/sdr/JJBA20220306007.md): Proximity Switch · loose · Mar 6, 2022 · N16541 · Emb EMB145LR · Landing Gear System > LG AIR GROUND FAIL MESSAGE ON LANDING AT 50FT. PERFORMED TROUBLESHOOTING. FOUND PROXIMITY SWITCH BRACKET ON RH MAIN LANDING GEAR LEG LOOSE. BRACKET BOLT WAS BROKEN. REMOVED AND ADJUSTED BRACKET AND REMOVED AND REPLACED TWO PROXIMITY SWITCH SENSORS. OPS CHECK G - [SDR JJBA2022022006021](https://openairdocs.org/sdr/JJBA2022022006021.md): Lamp · inoperative · Feb 26, 2022 · N16541 · Emb EMB145LR · Emergency Lighting > EMERGENCY CEILING LIGHT ON CEILING PANEL 253CLC INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT ON CEILING PANEL 253CLC. - [SDR JJBA202201184023](https://openairdocs.org/sdr/JJBA202201184023.md): Light · inoperative · Jan 14, 2022 · N16541 · Emb EMB145LR · Emergency Lighting > COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT. OPS CHECK SAT - [SDR JJBA20210929054](https://openairdocs.org/sdr/JJBA20210929054.md): Battery Pack · inoperative · Sep 29, 2021 · N16541 · Emb EMB145LR · Emergency Lighting > LH FWD WING/FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH FWD EMERGENCY LIGHT LAMP. OPS CHECK FAIL. SUSPECTED EMERGENCY BATTERY #1 NEEDS TO BE REPLACED. REMOVED AND REPLACED BPS #1. OPS CHECK SAT - [SDR JJBA20210923036](https://openairdocs.org/sdr/JJBA20210923036.md): Battery Pack · inoperative · Sep 23, 2021 · N16541 · Emb EMB145XR · Emergency Lighting > MULTIPLE EMERGENCY LIGHTS AFT OF EXIT ROW ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK SAT. - [SDR JJBA20210808027](https://openairdocs.org/sdr/JJBA20210808027.md): Brake Assy · leaking · Aug 8, 2021 · N16541 · Emb EMB145LR · Landing Gear Brake System > HYD 1 LOW QUANTITY ADVISORY CAME ON IN CRUISE. TRANSFERRED HYDRAULIC FLUID FROM #2 SYSTEM TO #1 SYSTEM. DUE TO HYD 1 LOW ADVISORY MESSAGE, R&R OUTBOARD BRAKES. OPS CHECK SAT. LEAK CHECK GOOD. - [SDR JJBA20210414050](https://openairdocs.org/sdr/JJBA20210414050.md): Sealant · missing · Apr 14, 2021 · N16541 · Emb EMB145LR · Main Landing Gear > SEALANT MISSING FROM RIGHT LANDING GEAR NUT WHERE MAIN BRACE STRUT AND LOWER SIDE ARM CONNECT. APPLIED SEALANT TO RLG NUT. - [SDR JJBA2021370003](https://openairdocs.org/sdr/JJBA2021370003.md): Armrest · cracked · Mar 7, 2021 · N16541 · Emb EMB145XR · Passenger Compartment Equipment > ARMREST STRUCTURE CRACKED ON PAX SEAT 10A. REMOVED AND REPLACED SEAT 10A INBOARD ARMREST STRUCTURE (SPREADER). - [SDR JJBA20210212040](https://openairdocs.org/sdr/JJBA20210212040.md): None · none · Feb 12, 2021 · N16541 · Emb EMB145LR · Fuselage Structure (General) > FUSELAGE SKIN DAMAGED AT FR29 TO FR31 BETWEEN S12R TO S13R. REMOVED DAMAGED FUSELAGE SKIN STR 13R FR 29R TO 31R. LOCATED AND DRILLED REPAIR DOUBLER AND FILLER. TRIMMED AND DEBURRED REPAIR FILLER AND REPAIR DOUBLER AND COUNTERSUNK REPAIR DOUBLER. TREATED AND PR - [SDR JJBA20210206020](https://openairdocs.org/sdr/JJBA20210206020.md): Shear Tie · damaged · Feb 6, 2021 · N16541 · Emb EMB145LR · Fuselage Internal Mounting Structure > SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12R AND 13R. REPAIRED SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12 AND 13R BY STEPPING FASTENER SIZE HOLD UP 1/32 ORG HOLE SIZE IS 5/32 AND IS NOW 3/16. TREATED AND PRIMED FASTENER HOLE. INSTALLED FASTENER. - [SDR JJBA20210205019](https://openairdocs.org/sdr/JJBA20210205019.md): Skin · damaged · Feb 5, 2021 · N16541 · Emb EMB145LR · Fuselage Main, Plate/Skin > FUSELAGE SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R. REPAIRED CENTER FUSELAGE II SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R. - [SDR ASOA201907143038](https://openairdocs.org/sdr/ASOA201907143038.md): Light · inoperative · Jul 14, 2019 · N16541 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED AISLE PATH EMERGENCY LIGHT AFT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT AILSE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD - [SDR ASOA2018121073071](https://openairdocs.org/sdr/ASOA2018121073071.md): Engine · leaking · Dec 7, 2018 · N16541 · Emb EMB145LR · Engine (Turbine/Turboprop) > THE CREW REPORTED ON CLIMBOUT AT 6000 FEET LAV SMOKE WARNING ON EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE #1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. - [SDR ASOA2018120763069](https://openairdocs.org/sdr/ASOA2018120763069.md): Control Panel · faulty · Dec 6, 2018 · N16541 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED @1000' LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR PANEL AMD OPERATIONAL CHECKS WERE GOOD. - [SDR ASOA2018112874067](https://openairdocs.org/sdr/ASOA2018112874067.md): Acm · frozen · Nov 27, 2018 · N16541 · Emb EMB145LR · Cabin Cooling System > IAH - THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPEVCTED THE AIRCRAFT, REMOVED AND REPLACED THE #1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCTRAFT WAS APPROVED FOR RETURN TO SE - [SDR ASOA2018090495181](https://openairdocs.org/sdr/ASOA2018090495181.md): Connector · disconnected · Aug 29, 2018 · N16541 · Emb EMB145LR · Light System Wiring > DURING MX INSPECTION THE ROW 18 CEILING AFT EXIT SIGN WAS FOUND INOP. MX INSTALLED CONNECTORS ON ROW 18 AFT EXIT SIGN WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024041](https://openairdocs.org/sdr/ASOA201706024041.md): Skin · dented · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING C-CHECK INSPECTION, THE CENTER FUSELAGE RT SKIN WAS FOUND WAS FOUND TO BE DENTED 3.5 INCH FWD OF FRAME 24 AND 1 INCH BELOW STRINGER 15R. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A REPAIR DOUBLER AND THE AIRCRAFT WAS APPROVED FOR RE - [SDR ASOA201706024040](https://openairdocs.org/sdr/ASOA201706024040.md): Frame · cracked · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Frame > DURING C-CHECK INSPECTION, THE UPPER FRAME 10 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED AT A RIVET LOCATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME SECTION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024039](https://openairdocs.org/sdr/ASOA201706024039.md): Crossbeam · cracked · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Structure > DURING A C-CHECK INSPECTION, THE NLG UPLOCK BOX CROSSBEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024033S](https://openairdocs.org/sdr/ASOA201706024033S.md): Gusset · corroded · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING A C-CHECK INSPECTION, THE LEFT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND RPELACED THE AFFECTED GUSSET AND TYHE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024035](https://openairdocs.org/sdr/ASOA201706024035.md): Crossbeam · corroded · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Structure > DURING A C-CHECK INSPECTION, THE CENTER AISLE CROSSBEAM SUPPORT AT FRAME 20 WAS FOUND TO HAVE BARE METAL AND CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024034](https://openairdocs.org/sdr/ASOA201706024034.md): Gusset · corroded · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING A C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT GUSSET AT FRAMES 60 - 61 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201706024033](https://openairdocs.org/sdr/ASOA201706024033.md): Gusset · corroded · Jun 2, 2017 · N16541 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING A C-CHECK INSPECTION, THE LT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201705304037](https://openairdocs.org/sdr/ASOA201705304037.md): Frame · damaged · May 30, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Frame > DURING A C-CHECK INSPECTION, FRAME 72 WAS FOUND TO BE DAMAGED BETWEEN STRINGERS 15 & 16R. MAINTENANCE REMOVED THE DAMAGED. - [SDR ASOA201705294036](https://openairdocs.org/sdr/ASOA201705294036.md): Skin · damaged · May 29, 2017 · N16541 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING A C-CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO HAVE A SMALL NICK AT FRAME 68 BETWEEN STRINGERS 10 & 11L. MAINTENANCE BLENDED THE AFFECTED AREA IAW ETD2017-145-045392, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201704077006](https://openairdocs.org/sdr/ASOA201704077006.md): Wire · broken · Apr 7, 2017 · N16541 · Emb EMB145LR · Light System Wiring > A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE FOUND A BROKEN WIRE AND SPLICE THE WIRE BACK IAW SWPM 20-21-OO. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE. - [SDR ASOA20160317013](https://openairdocs.org/sdr/ASOA20160317013.md): Lamp · arced · Mar 17, 2016 · N16541 · Emb EMB145LR · Passenger Compartment Lighting > A BURNING PLASTIC ODOR REPORTED FROM THE GALLEY NEAR THE OVERHEAD LIGHT. MX R & R THE LIGHT BLUBS AT SEAT 1 A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150912052R](https://openairdocs.org/sdr/ASOA20150912052R.md): Control Panel · faulty · Sep 12, 2015 · N16541 · Emb EMB145LR · Emergency Lighting > PILOT REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE R & R THE F/A CONTROL PANEL ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150831048R](https://openairdocs.org/sdr/ASOA20150831048R.md): Battery Pack · shorted · Aug 31, 2015 · N16541 · Emb EMB145LR · Emergency Equipment > AN ELECTRICAL BURNING ODOR WAS REPORTED IN THE COCKPIT. MAINTENANCE PERFORMED INSPECTION OF COCKPIT AREA AND FOUND CAPTAIN`S FLASHLIGHT TO BE CAUSE AND PLACED ON MEL. MAINTENANCE R & R CAPTAIN`S FLASHLIGHT BATTERY WITH OPS CHECK GOOD. ACFT APPROVED FOR RETU - [SDR ASOA20150807044R](https://openairdocs.org/sdr/ASOA20150807044R.md): Valve · odor · Aug 7, 2015 · N16541 · Emb EMB145LR · Pneumatic Distribution System > PILOT REPORTED BLEED 1 & 2 OVERTEMP IN ICING THEN ODOR OF SOMETHING BURNING. MAINTENANCE R & R NR 1 ENGINE FAN AIR VALVE, FAN AIR THERMOSTATS 1 & 2, A HIGH STAGE PRESSURE SWITCH WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20141212099](https://openairdocs.org/sdr/ASOA20141212099.md): Sign · no test · Dec 12, 2014 · N16541 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE, THE CEILING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EXIT LOCATOR SIGN. OPS CHECKED GOOD. - [SDR ASOA20140414062](https://openairdocs.org/sdr/ASOA20140414062.md): Pitot System · contaminated · Apr 14, 2014 · N16541 · Emb EMB145LR · Pitot/Static System > CREW REPORTED AT FL 370 A NOTICEABLE ICE BUILD UP ON THE UNPROTECTED SURFACES AS WELL AS THE TAT. SHORTLY AFTER IAS AND ALT INSTRUMENTS BEGAN TO FAIL FOLLOWED BY A NR 2 PACK OVERHEAT MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND BEGAN AN IMMEDIATE - [SDR ASOA20131211137R](https://openairdocs.org/sdr/ASOA20131211137R.md): Light · inoperative · Dec 11, 2013 · N16541 · Emb EMB145LR · Emergency Lighting > DURING SCHEDULED MAINTENANCE INSPECTION, THE CENTER AISLE EMERGENCY LIGHTS FROM SEAT 1A-3A WERE FOUND INOPERATIVE. MAINTENCE R & R THE CENTER AISLE LIGHT STRIP WITH OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130506035](https://openairdocs.org/sdr/ASOA20130506035.md): None · none · May 6, 2013 · N16541 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED EMERGENCY LIGHT NOT ARMED MESSAGE APPEARED WITH NO REASON. REPORTED 2 EMERGENCY LIGHTS WOULD NOT TURN ON. MX INSPECTED AND RESET ACFT SYS AND OPS CHECKS WERE GOOD. NO DEFECT FOUND. - [SDR ASOA20130402123V](https://openairdocs.org/sdr/ASOA20130402123V.md): Beam · corroded · Apr 3, 2013 · N16541 · Emb EMB145LR · Fuselage Main, Structure > DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT MAIN BEAM CORRODED. FRAMES 65-68. BEAM R & R IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130123243T](https://openairdocs.org/sdr/ASOA20130123243T.md): Attach Fitting · damaged · Jan 21, 2013 · N16541 · Emb EMB145LR · Vertical Stabilizer, Attach Fittings > VERTICAL STAB RT AND LT MOUNT LUGS WORN BEYOND LIMITS. OVERSIZED RT AND LT VERTICAL STAB BEARING HOUSINGS TO 1ST REWORK DIMENSIONS AND INSTALLED BUSHINGS. - [SDR C2XA11CL204](https://openairdocs.org/sdr/C2XA11CL204.md): Light · inoperative · Sep 11, 2011 · N16541 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE 4TH AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11CL120](https://openairdocs.org/sdr/C2XA11CL120.md): Proximity Switch · faulty · May 8, 2011 · N16541 · Emb EMB145LR · Landing Gear Position and Warning > EWR FLT 2038 THE CREW REPORTED DURING GEAR RETRACTION RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MESSAGE DID NOT CLEAR. ALSO STATED ON INITAL ATTEMPT TO RETRACT THE GEAR THE HANDLE WOULD NOT MOVE TO THE UP POSITION BUT AFTER A SECOND OR TW - [SDR C2XA11CL118](https://openairdocs.org/sdr/C2XA11CL118.md): Connector · corroded · May 6, 2011 · N16541 · Emb EMB145LR · Flight Control System Wiring > DAY FLT 5857 THE CREW REPORTED THE SPOILERS DEPLOYED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT SPEED BRAKE PROXIMITY SWITCH AND CONNECTOR P1166. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11TY053](https://openairdocs.org/sdr/C2XA11TY053.md): Dau · malfunctioned · May 1, 2011 · N16541 · Emb EMB145LR · Central Computers > L/G AIR/GROUND FAIL MESSAGE ON EICAS. RECEIVED MESH PROX TRAILING ARM IAW EMB 145AMM 32-63-05 AND REMOVED AND REPLACED DAU NR 1 IAW EMB 145AMM 31-41-01 OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA11CL093](https://openairdocs.org/sdr/C2XA11CL093.md): Electronic Unit · faulty · Apr 9, 2011 · N16541 · Emb EMB145LR · Landing Gear Position and Warning > ORD FLT 6112 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER GEAR EXTENSION. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR DOWNLOCK A PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. THE WARNING INDICATION REOCCURRED ON FLT 5837. MAINTENA - [SDR C2XA11CL040](https://openairdocs.org/sdr/C2XA11CL040.md): Smoke Detector · failed · Feb 6, 2011 · N16541 · Emb EMB145LR · Smoke Detection > DURING ROUTINE MAINTENANCE THE FORWARD CARGO SMOKE DETECTOR FAILED THE TASK CARD CHECK. LED STAYS ON ALL THE TIME. MAINTENANCE REPLACED THE SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10CL124](https://openairdocs.org/sdr/C2XA10CL124.md): Proximity Switch · out of adjust · Aug 3, 2010 · N16541 · Emb EMB145LR · Landing Gear Position and Warning > CLE FLT 5658 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT GEAR WOW PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10CL086](https://openairdocs.org/sdr/C2XA10CL086.md): Warning System · activated · Jun 5, 2010 · N16541 · Emb EMB145 · Fuel Pressure Indicator > IAD FLT 5687 THE CREW REPORTED A ENGINE 2 LOW FUEL PRESSURE WARNING ON TAKEOFF ROLL WHILE ON PUMP A. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL PROCEDURES. SUPPLEMENT TO FOLLOW. - [SDR C2XA09CL100](https://openairdocs.org/sdr/C2XA09CL100.md): Connector · loose · Jul 21, 2009 · N16541 · Emb EMB145LR · Light System Wiring > DURING ROUTINE MAINTENANCE, THE LEFT OVERWING EMERGENCY LIGHT EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE EXIT SIGN CONNECTOR. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA09SH171](https://openairdocs.org/sdr/C2XA09SH171.md): Attach Bracket · damaged · Jun 7, 2009 · N16541 · Emb EMB145LR · Wing, Attach Fittings > DURING C-CK. RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED ATTACHMENT BRACKET IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09RIO90](https://openairdocs.org/sdr/C2XA09RIO90.md): Control Panel · inoperative · May 4, 2009 · N16541 · Emb EMB145LR · Audio Integrating System > FLIGHT 3064 - RIC - FLIGHT CREW REPORTED THAT NAV NR 1 AND NAV NR 2 DASHED OUT - NO NAV INFLIGHT. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFUL. RIC MX REMOVED AND REPLACED NR 1 AUDIO CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT - [SDR C2XA09CL024](https://openairdocs.org/sdr/C2XA09CL024.md): Thrust Reverser · faulty · Mar 5, 2009 · N16541 · Emb EMB145LR · Engine Thrust Reverser > CLE FLIGHT 2767 - THE CREW REPORTED AN ENGINE 2 THRUST REVERSER DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00. ON 03/10/09 MAINTENANCE REPLACED THE NR 2 T/R AND OPERATIONA - [SDR C2XA09IA004](https://openairdocs.org/sdr/C2XA09IA004.md): Controller · malfunctioned · Jan 3, 2009 · N16541 · Emb EMB145LR · Cabin Pressure Controller > THE CREW REPORTED, LEVEL AT FL360 RAPID DECOMPRESSION CABIN ALT REACHED 12,000. THE ACFT LANDED WITHOUT INCIDENT WHERE MX REMOVED AND REPLACED THE DIGITAL CONTROLLER, OPERATIONALLY TESTED AITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08IA271](https://openairdocs.org/sdr/C2XA08IA271.md): Fire Loop · chafed · Dec 29, 2008 · N16541 · Emb EMB145LR · Fire Detection > IAH - FLIGHT 2386, THE CREW REPORTED A NUMBER ONE ENGINE FIRE DETECTOR FAIL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL TESTS WERE SATISFACTORY, AND THE AIRCRAFT W Next page: https://openairdocs.org/aircraft/N16541/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 = 'N16541' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N16541/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.