# Service difficulty reports: N19554, cancelled Mar 3, 2022 A list on [N19554, cancelled Mar 3, 2022](https://openairdocs.org/deregistered/N19554-2022-03-03.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 · 58 reports - [SDR ASOA2020050414017](https://openairdocs.org/sdr/ASOA2020050414017.md): Battery Pack · discharged · May 1, 2020 · N19554 · Emb EMB145LR · Emergency Lighting > IAH- FLIGHT 4289 DURING MAINTENANCE INSPECTION THE R/H EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT POWERSUPPLY BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR - [SDR ASOA20200205004](https://openairdocs.org/sdr/ASOA20200205004.md): Lamp · odor · Feb 1, 2020 · N19554 · Emb EMB145LR · Emergency Lighting > PILOT REPORTED ELECTRICAL SMELL BY SEAT 4CD AND 5CD. ITEM PLACED ON MEL. ON 2/3/20 MX REMOVED AND REPLACED SIDEWALL LAMP AND RESEATED CONNECTOR WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2018091845203](https://openairdocs.org/sdr/ASOA2018091845203.md): Inverter · defective · Sep 14, 2018 · N19554 · Emb EMB145LR · Emergency Lighting > PILOT REPORTED "FLOOR PATH EMERG LIGHT A/C LEFT AT WINDOW EXIT AND EXIT CEILING BACK SIDE OF LIGHT CAME ON IN FLIGHT" MX REMOVED AND REPLACED THE NR 5 INVERTER AND BATTERY CHARGER ASSEMBLY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201807257142](https://openairdocs.org/sdr/ASOA201807257142.md): Brace · scored · Jul 25, 2018 · N19554 · Emb EMB145LR · Main Landing Gear > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RT MLG SIDE BRACE FWD AFT FITTING BEARING BORE SCORED AND HAD A SMALL AREA OF CORROSION. ALL WORK WAS ACCOMPLISHED BY MAINTENANCE IAW ETD 2018-145-076914. CORROSION WAS A LEVEL ONE IN SIZE AND WAS CLEANED. A/C WI - [SDR ASOA201807257141](https://openairdocs.org/sdr/ASOA201807257141.md): Bearing · worn · Jul 25, 2018 · N19554 · Emb EMB145LR · Vertical Stabilizer > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND EVIDENCE OF SOME WEAR ON THE VERTICAL STAB BORES OR SPHERICAL BEARINGS. MAINTENANCE PERFORMED OPS CHECKS OF BOTH DIHEDRAL AND FOUND TO BE GOOD IAW AMM 51-50-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END O - [SDR ASOA201807237139](https://openairdocs.org/sdr/ASOA201807237139.md): Trunnion · corroded · Jul 21, 2018 · N19554 · Emb EMB145LR · Main Landing Gear Attach Section > LT AND RT MLG AFT TRUNNION FITTINGS INTERNAL DIAMETER HAS CORROSION. COMPLETED REWORK OF THE MLG TRUNNION IN ACCORDANCE WITH ETD 2018-145-079169. - [SDR ASOA201807177131](https://openairdocs.org/sdr/ASOA201807177131.md): Skin · damaged · Jul 17, 2018 · N19554 · Emb EMB145LR · Elevator, Plate/Skin > TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT ELEVATOR LOWER OUTBOARD FLANGE AT SCREW HOLE DAMAGED. MAINTENANCE REPAIRED DAMAGED AREA BY CUTTING OUT DAMAGE AND FABRICATING AND INSTALLING A REPAIR IAW ETD 2018-145-073219. ALL WORK ACCOMPLISHED AND WILL - [SDR ASOA201807177130](https://openairdocs.org/sdr/ASOA201807177130.md): Skin · dented · Jul 17, 2018 · N19554 · Emb EMB145LR · Wing, Plate/Skin > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A DENT IN THE NR 2 LEADING EDGE LEFT WING. MAINTENANCE REPAIRED AREA BY CUTTING OUT THE DENT AND FABRICATED A DOUBLER AND REPAIRED AREA IAW SRM 57-40-00 FIGURE 201, SHEET 2. ALL WORK ACCOMPLISHED AND WILL BE RE - [SDR ASOA201807177129](https://openairdocs.org/sdr/ASOA201807177129.md): Skin · cracked · Jul 17, 2018 · N19554 · Emb EMB145LR · Fuselage Main, Plate/Skin > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LEFT REAR EXTERNAL FUSELAGE BETWEEN FRAME 75 AND 76,STRINGER 2L TO 4L CRACKED. MAINTENANCE PERFORMED A REPAIR AT THIS AREA IAW SRM 53-31-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHEC - [SDR ASOA201807177128](https://openairdocs.org/sdr/ASOA201807177128.md): Stringer · cracked · Jul 17, 2018 · N19554 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK AT STRINGER 2L AND FRAME 75. MAINTENANCE REPAIRED AREA IAW ETD 2018-145-077021. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA201807097122](https://openairdocs.org/sdr/ASOA201807097122.md): Fitting · worn · Jul 9, 2018 · N19554 · Emb EMB145LR · Rudder Structure > A/C IS IN C-CHECK WHEN INSPECTION FOUND RUDDER 1 UPPER ACTUATOR ATTACH POINT UPPER LUG HAT BUSHING MISSING AND FELL OUT. MAINTENANCE FOUND THE ATTACH POINT ELONGATED, THEY REAM HOLE AND PLACED AN OVERSIZED BUSHING IAW SRM 55-00-00. ALL WORK ACCOMPLISHED AND WI - [SDR ASOA201807257140](https://openairdocs.org/sdr/ASOA201807257140.md): Frame · cracked · Jun 29, 2018 · N19554 · Emb EMB145LR · Fuselage Main, Frame > CP SIDE FRAME ABOVE WS SIDE POST CRACKED. SPLICED IN NEW SECTION OF FRAME ABOVE WS SIDE POST IN ACCORDANCE WITH ETD 2018-145-072956. - [SDR ASOA20160522050](https://openairdocs.org/sdr/ASOA20160522050.md): Inverter · inoperative · May 22, 2016 · N19554 · Emb EMB145LR · Emergency Lighting > FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT ON THE BULKHEAD AT SEAT 3D WAS INOPERATIVE. THE ACFT WAS FERRIED WHERE MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVI - [SDR ASOA20160324019](https://openairdocs.org/sdr/ASOA20160324019.md): Battery · inoperative · Mar 24, 2016 · N19554 · Emb EMB145 · Emergency Lighting > EMERGENCY FLOOR LIGHTS AT ROW 8-11 AND EXIT LIGHT AT OVERWING EXITS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD. - [SDR ASOA20151201068C](https://openairdocs.org/sdr/ASOA20151201068C.md): Power Supply · faulty · Dec 1, 2015 · N19554 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED EMERGENCY LIGHTS REMAIN ON AT ROW 5-18. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD. - [SDR ASOA20141121135](https://openairdocs.org/sdr/ASOA20141121135.md): Relay · inoperative · Nov 21, 2014 · N19554 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT ON EICAS AND EXT/BAGG PUSHBUTTON. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND RESECURED A LOOSE WIRE ON THE SMOKE DETECTOR PANEL, AND R & R RELAYS K - [SDR ASOA20141121134](https://openairdocs.org/sdr/ASOA20141121134.md): Relay · inoperative · Nov 21, 2014 · N19554 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT ON EICAS AND EXT/BAG PUSHBUTTON. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND RESECURED A LOOSE WIRE ON THE SMOKE DETECTOR PANEL, AND R & R RELAYS K0 - [SDR ASOA20141113115](https://openairdocs.org/sdr/ASOA20141113115.md): Light · inoperative · Nov 12, 2014 · N19554 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHT INOPERATIVE. R & R LIGHT. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20140616071](https://openairdocs.org/sdr/ASOA20140616071.md): Inverter · inoperative · Jun 16, 2014 · N19554 · Emb EMB145LR · Emergency Lighting > DURING MX INSPECTION THE EMERGENCY LIGHT BELOW THE COCKPIT STEP WAS DISCOVERED INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT SYS INVERTER AND LIGHT ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140424082](https://openairdocs.org/sdr/ASOA20140424082.md): Power Supply · inoperative · Apr 23, 2014 · N19554 · Emb EMB145LR · Emergency Lighting > LEFT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY. OPS CHECKED GOOD. - [SDR ASOA20140419036](https://openairdocs.org/sdr/ASOA20140419036.md): Bolt · sheared · Apr 19, 2014 · N19554 · Emb EMB145LR · Engine (Turbine/Turboprop) > DURING FLIGHT, AFTER A SERIES OF BUMPS OR WHAT SOUNDED LIKE A BACKFIRE. NR 2 ENGINE ITT SPIKED INTO THE RED FOLLOWED BY NR 2 ENGINE OUT. RESTART WAS SUCCESSFUL, FOLLOWED SHORTLY BY REPEAT OF UNCOMMANDED ENGINE SHUTDOWN. THE ACFT LANDED WITHOUT FURTHER INCIDE - [SDR ASOA20140207022](https://openairdocs.org/sdr/ASOA20140207022.md): Bearing · migrated · Feb 7, 2014 · N19554 · Emb EMB145LR · Ailerons > DURING C CHECK, INSPECTION FOUND RT AILERON PCA ATTACHMENT BRACKET BEARING MIGRATED. MAINTENANCE R & R THE RT PCA BRACKET IAW EC 5750-01177. - [SDR ASOA20130612059](https://openairdocs.org/sdr/ASOA20130612059.md): Roller · out of adjust · Jun 12, 2013 · N19554 · Emb EMB145LR · Passenger/Crew Doors > PILOT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MX ADJUSTED THE MAIN CABIN DOOR ROLLERS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130427043R](https://openairdocs.org/sdr/ASOA20130427043R.md): Charger · faulty · Apr 27, 2013 · N19554 · Emb EMB145LR · Emergency Lighting > CREW REPORTED SECTIONS OF THE FLOOR EMERGENCY LIGHTS TURNING ON AND OFF INTERMITTENTLY. MX R & R THE NR 3 BATTERY CHARGER ASSY AND BATTERY PACK WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20121009080](https://openairdocs.org/sdr/ASOA20121009080.md): Contactor · faulty · Oct 9, 2012 · N19554 · Emb EMB145LR · Light System Wiring > F/A SMELLED ELECTRIC BURNING ODOR AFTER LANDING. MX INSPECTED AND REPLACED NOSE LANDING LIGHT CONTACTOR K0237. OPS CHECKED WERE GOOD. - [SDR ASOA20111212014](https://openairdocs.org/sdr/ASOA20111212014.md): Generator · faulted · Dec 12, 2011 · N19554 · Emb EMB145LR · AC Generator-Alternator > DURING CLIMB THE CREW REPORTED THAT THE NR 3 GENERATOR DROPPED OFF LINE. THE ACFT WAS OPERATING WITH THE NR1 GENERATOR ON MEL AND WITH THE NR 3 DROPPING OFF LINE ELECTED TO RETURN TO DEPARTURE WHERE THE ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE NR3 GENERA - [SDR C2XA11TY163](https://openairdocs.org/sdr/C2XA11TY163.md): Skin · damaged · Oct 24, 2011 · N19554 · Emb EMB145LR · Wing, Plate/Skin > AIRCRAFT STRUCK BY LIGHTNING. PERFORMED LIGHTNING STRIKE INSPECTION IAW EMB 145 5-50-01. REMOVED AND REPLACED DAMAGE RIVET AT FRAME 8 STRINGER 16L-17L. REPAIRED TOP AFT OF RT WING TIP. REMOVED AND REPLACED RT ELEVATOR TIP FAIRING. REPAIRED O/B FLAP TRAILI - [SDR C2XA11RI166](https://openairdocs.org/sdr/C2XA11RI166.md): Battery · discharged · Oct 13, 2011 · N19554 · Emb EMB145LR · Emergency Lighting > FLT 6145 IAD SECTION OF AISLE PATH LIGHTING INOP AROUND EMERGENCY EXIT ROW 12 NOTED. IAD MX REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04 WITH OPERATION CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11CL230](https://openairdocs.org/sdr/C2XA11CL230.md): Charger · faulty · Oct 13, 2011 · N19554 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED THE AILE PATH EMERGENCY LIGHTS AT ROW 8 THRU 12 WILL NOT GO OFF. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11IA231](https://openairdocs.org/sdr/C2XA11IA231.md): Connector · dirty · Oct 4, 2011 · N19554 · Emb EMB145LR · Light System Wiring > MCI - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHTS OVER BOTH EXITS AND THE AISLE PATH LIGHTS FROM RO 8 TO 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTORS ON INVERTERS NUMBER 4 AND 5, OPERATIONALLY TESTED WITH NO DEFECTS AND THE - [SDR C2XA11CL178](https://openairdocs.org/sdr/C2XA11CL178.md): Battery · discharged · Jul 31, 2011 · N19554 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE AT THE EXIT ROW. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11TY038](https://openairdocs.org/sdr/C2XA11TY038.md): Smoke Detector · activated · Mar 23, 2011 · N19554 · Emb EMB145LR · Smoke Detection > LAV SMOKE INDICATION ON THE EICAS SHORTLY AFTER TAKEOFF. FOGGY CABIN/POSSIBLY DE-ICING FLUID IN AIR CONDITIONING SYSTEM. PERFORMED ENGINE RUNS IAW RR MM71-00-80 AND COULD NOT DUPLICATE AND LEAK CHECK WAS GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE - [SDR C2XA10RI087](https://openairdocs.org/sdr/C2XA10RI087.md): Trim Switch · broken · Jun 24, 2010 · N19554 · Emb EMB145LR · Stabilizer Control System > FLIGHT 2476 - EWR - FLIGHT CREW REPORTED BACK UP PITCH TRIM SWITCH INOPERATIVE. CREW PERFORMED AIR RETURN UNEVENTFULLY. EWR MX REMOVED AND REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10IA173](https://openairdocs.org/sdr/C2XA10IA173.md): Control Module · faulty · Jun 13, 2010 · N19554 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED THAT WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARMED POSITION THE CABIN EMERGENCY LIGHTS WOULD COME ON. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT'S LIGHT CONTROL MODULE, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DIS - [SDR C2XA10SH180](https://openairdocs.org/sdr/C2XA10SH180.md): Attach Bracket · worn · May 20, 2010 · N19554 · Emb EMB145LR · Ailerons > SHV - DURING C-CHECK THE RT AILERON PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH179](https://openairdocs.org/sdr/C2XA10SH179.md): Skin · cracked · May 20, 2010 · N19554 · Emb EMB145LR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK THE AFT RT SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FRAME 79 AND STRINGER 4R. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC5330-02130. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09CL139](https://openairdocs.org/sdr/C2XA09CL139.md): Switch · inoperative · Oct 28, 2009 · N19554 · Emb EMB145LR · Pneumatic Distribution System > CLE FLT 2580 - THE CREW REPORTED A BLEED 1 VALVE CLOSED MESSAGE AFTER TAKEOFF. COULD NOT GET THE NR 1 BLEED VALVE TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA09TY058](https://openairdocs.org/sdr/C2XA09TY058.md): Tube · leaking · Apr 3, 2009 · N19554 · Emb EMB145LR · Engine Bleed Air System > AIRCRAFT ON CLIMBOUT FROM EWR TO TYS REACH A HIGH ITT. MAINTENANCE REPLACED THE RT COMPRESSOR AIR TUBE ON THE E1 IAW ROLLS ROYCE MM 75-00-00, OPS AND LEAK CHECKS WERE GOOD AND RETURN TO SERVICE. - [SDR C2XA07ON050](https://openairdocs.org/sdr/C2XA07ON050.md): Valve · malfunctioned · Dec 21, 2007 · N19554 · Emb EMB145 · Air Distribution System > FLT 421 - SMF TO GEG - FLIGHT CREW REPORTED PACK 1 VALVE FAILED TO CLOSED NUMEROUS TIMES ON CLIMB. MX PERSONNEL REMOVED AND REPLACED NR 1 PACK VALVE, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE. - [SDR C2XA07ON021](https://openairdocs.org/sdr/C2XA07ON021.md): Connector · unsecure · Sep 3, 2007 · N19554 · Emb EMB145LR · Light System Wiring > FLT 524 - MCI TO RDU - DURING PREFLIGHT CK, FLIGHT CREW DISCOVERED THE EMERGENCY LIGHTS WILL NOT SHUT OFF. MX PERSONNEL INSPECTED AND FOUND CONNECTOR ON NR 3 EMERGENCY BATTERY NOT PROPERLY SECURED. MX PERSONNEL RESECURED AND OPERATIONALLY CHECK EMERGENCY LIG - [SDR C2XA07IA195](https://openairdocs.org/sdr/C2XA07IA195.md): Battery Pack · discharged · Sep 2, 2007 · N19554 · Emb EMB145LR · Emergency Lighting > MCI - DURING MAINTENANCE INSPECTION THE NUMBER 5 & 6 AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED - [SDR C2XA07IA185](https://openairdocs.org/sdr/C2XA07IA185.md): Power Supply · discharged · Aug 9, 2007 · N19554 · Emb EMB145LR · Emergency Lighting > AUS - FLIGHT 308, DURING PREFLIGHT INSPECTION AN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY FOR THE EMERGENCY EXIT ROWS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO - [SDR C2XA07IA182](https://openairdocs.org/sdr/C2XA07IA182.md): Battery Pack · discharged · Aug 2, 2007 · N19554 · Emb EMB145LR · Emergency Lighting > AUS - DURING MAINTENANCE INSPECTION, THE FORWARD THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R - [SDR C2XA07BT019](https://openairdocs.org/sdr/C2XA07BT019.md): Battery · discharged · Feb 19, 2007 · N19554 · Emb EMB145LR · Emergency Lighting > EWR LOG SQUAWK FLT 2665 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW EMB145 AMM 37-50-04. OPS CHECK GOOD. - [SDR C2XA06SH008](https://openairdocs.org/sdr/C2XA06SH008.md): Frame · corroded · Jan 28, 2006 · N19554 · Emb EMB145LR · Cargo/Baggage Doors > SHV - DURING C-CHECK THE CARGO DOOR INTERNAL FRAME WAS FOUND TO BE CORRODED AROUND A NUT PLATE. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01131. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA06SH007](https://openairdocs.org/sdr/C2XA06SH007.md): Firewall · chafed · Jan 28, 2006 · N19554 · Emb EMB145LR · APU Cowling/Containment > SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O`CLOCK POSITION. MAINTENANCE BLENDED OUT THE DAMAGED AREA AND PERFORMED A SHIM REPAIR IAW CONTINENTAL EXPRESS EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA05BT082](https://openairdocs.org/sdr/C2XA05BT082.md): Bulb · blown · Nov 19, 2005 · N19554 · Emb EMB145LR · Emergency Lighting > DURING SERVICE AND ROUTINE INSPECTION CHECK, MAINTENANCE FOUND THAT THE LEFT OVERWING EMERGENCY LIGHT WAS NOT WORKING. REMOVED AND REPLACED BULB IN LEFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, OPS CHECKED GOOD. - [SDR C2XA04TY044](https://openairdocs.org/sdr/C2XA04TY044.md): Sill · corroded · Mar 4, 2004 · N19554 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR FWD SILL HAS AREAS OF CORROSION. MAINT BLENDED AFT AREA AND FOUND TO BE WITHIN LIMITS; ALODINED, PRIMED, PAINTED, BLENDED FWD AND FOUND TO BE OUT OF LIMITS, FABBED DOUBLER, ALODINED, PRIMED, PAINTED AND I - [SDR C2XA04TY043](https://openairdocs.org/sdr/C2XA04TY043.md): Plate · corroded · Mar 4, 2004 · N19554 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS DURING A SCHEDULED 1C INSPECTION THE FWD DIGITAL PLATE HAD AREAS OF CORROSION. MAINT CUT THE DAMAGED AREA OUT, FAB DOUBLERS AND DRILLED HOLES ON NEW FWD DIGITAL, INSTALL AND PRIMED DOUBLERS AND NEW DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCO - [SDR C2XA04TY042](https://openairdocs.org/sdr/C2XA04TY042.md): Stiffener · cracked · Mar 4, 2004 · N19554 · Emb EMB145LR · APU Cowling/Containment > TYS DURING A SCHEDULED 1C INSPECTION THE RT UPPER STIFFENER ON THE APU FIREWALL WAS FOUND CRACKED. MAINT FABBED A DOUBLER AND STOPPED DRILL CRACK. INSTALL DOUBLER AT RT UPPER STIFFENER ON THE APU FIREWALL IAW EMB 135/145 SRM 55-32-13. ALL WORK WAS ACCOMPLI Next page: https://openairdocs.org/deregistered/N19554-2022-03-03/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 = 'N19554' AND deregistration_id = 'N19554-2022-03-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N19554-2022-03-03/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.