# Service difficulty reports: N12922, cancelled Jan 10, 2019 A list on [N12922, cancelled Jan 10, 2019](https://openairdocs.org/deregistered/N12922-2019-01-10.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 3 · 107 reports - [SDR ASOA20160826069](https://openairdocs.org/sdr/ASOA20160826069.md): Acm · frozen · Aug 26, 2016 · N12922 · Emb EMB145LR · Cabin Cooling System > THE CREW REPORTED SMOKE IN THE CABIN WITH A PACK 2 OVERHEAT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, R & R THE NR 1 ACM, AND BOTH Y-DUCTS ON THE LT AND RT PACKS. OPS CHECKS WERE PERFORMED WITHOUT DEFECT, AND THE ACFT WAS APPROV - [SDR ASOA20160626030](https://openairdocs.org/sdr/ASOA20160626030.md): Acm · seized · Jun 26, 2016 · N12922 · Emb EMB145LR · Cabin Cooling System > PILOT REPORTED A PACK 2 OVERHEAT AND PACK 2 VALVE FAIL MESSAGE ON EICAS. PACK 2 OVERHEAT QRH SAID TO SHUTOFF PACK FOR 3 MINUTES. DURING 3 MINUTE PACK SHUTDOWN, SMOKE ENTERED COCKPIT FROM DV WINDOW VENTS. CABIN SMOKE IAC & QRH COMPLIED WITH. WHEN RECIRCULAT - [SDR ASOA20160225015C](https://openairdocs.org/sdr/ASOA20160225015C.md): Inverter · inoperative · Feb 25, 2016 · N12922 · Emb EMB145 · Emergency Lighting > DURING ROUTINE MAINTENANCE THE FORWARD EXIT ROW EMERGENCY SIGN WOULD NOT TEST. MAINTENANCE REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD. - [SDR ASOA20160201008](https://openairdocs.org/sdr/ASOA20160201008.md): Acm · faulty · Feb 1, 2016 · N12922 · Emb EMB145 · Cabin Cooling System > THE CREW REPORTED UPON ACTIVATION OF NR 1 PACK, OBSERVED SMOKE AND A BURNING ODOR IN THE FLIGHT DECK. CREW REPORTED HEARING ABNORMALLY LOUD AND UNUSUAL NOISES AND PASSENGER IN SEAT 1A REPORTED SMOKE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AIR CYCLE MACH - [SDR ASOA2016010700003](https://openairdocs.org/sdr/ASOA2016010700003.md): Frame Splice · corroded · Jan 7, 2016 · N12922 · Emb EMB145LR · Fuselage Main, Frame > DURING C-CHECK, RIVETS AT CIRCUMFERENTIAL SPLICE SHOW SIGNS OF CORROSION FRAME 13. INSTALLED FILLER AND 2 DOUBLERS AT FRAME 13 SPLICE IAW SRM 53-00-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201601040011](https://openairdocs.org/sdr/ASOA201601040011.md): Beam · corroded · Jan 4, 2016 · N12922 · Emb EMB145LR · Fuselage Main, Structure > DURING C-CHECK, BAGGAGE DOOR CUTOUT LOWER BEAM HAS CORROSION, FR 65-68. R & R BAGGAGE DOOR CUTOUT LOWER BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150506043H](https://openairdocs.org/sdr/ASOA20150506043H.md): Firewall · cracked · May 6, 2015 · N12922 · Emb EMB145LR · APU Cowling/Containment > DURING MAINTENANCE INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LT BOTTOM FRAME ATTACHMENT POINT. MAINTENANCE REMOVED THE DAMAGED SECTION OF FIREWALL AND PERFORMED A FILLER/DOUBLER REPAIR IAW SRM 53-32-12, AND THE ACFT WAS APPROVED FOR RETURN T - [SDR ASOA20150506042](https://openairdocs.org/sdr/ASOA20150506042.md): Firewall · cracked · May 6, 2015 · N12922 · Emb EMB145LR · APU Cowling/Containment > DURING MAINTENANCE INSPECTION, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT BOTTOM FRAME ATTACHMENT POINT. MAINTENANCE REMOVED THE DAMAGED SECTION OF FIREWALL AND PERFORMED A FILLER/DOUBLER REPAIR IAW SRM 53-32-12, AND THE ACFT WAS APPROVED FOR RETURN T - [SDR ASOA20150409035](https://openairdocs.org/sdr/ASOA20150409035.md): Smoke Detector · false activation · Apr 9, 2015 · N12922 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED A SMOKE INDICATION FROM THE CARGO BAY, THE QRH WAS FOLLOWED AND THE CARGO FIRE BOTTLES WERE DISCHARGED. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, FOUND NO EVIDENCE OF SMOKE OR FIRE, OPERATIONALLY TESTED THE CARG - [SDR ASOA20150217010](https://openairdocs.org/sdr/ASOA20150217010.md): Display · odor · Feb 17, 2015 · N12922 · Emb EMB145LR · Central Display > PILOT REPORTED THE F/O PFD CIRCUIT BREAKER TRIPPED IN FLIGHT WITH AN ELECTRICAL BURNING ODOR NOTICED. MAINTENANCE R & R THE NR 2 PFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140904094](https://openairdocs.org/sdr/ASOA20140904094.md): Unknown · odor · Sep 4, 2014 · N12922 · Emb EMB145LR · Air Distribution System > CREW REPORTED A BURNING ODOR DURING DECENT AND AGAIN DURING LANDING. MX PERFORMED AN OPS CHECK OF THE AIR CONDITIONING PACKS AND COULD NOT DUPILCATE ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140814107](https://openairdocs.org/sdr/ASOA20140814107.md): Engine · odor · Aug 14, 2014 · N12922 · Emb EMB145LR · Engine (Turbine/Turboprop) > THE CREW REPORTED A MUSTY ODOR WHEN EITHER BLEED ENGINE NR 1 OR NR 2 SELECTED BUT GOES AWAY WHEN APU IS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140814066C](https://openairdocs.org/sdr/ASOA20140814066C.md): Unknown · odor · Aug 14, 2014 · N12922 · Emb EMB145LR · Air Distribution System > THE CREW REPORTED FAINT OIL BURNING ODOR FROM NR 2 PACK DURING CLIMB AND DESCENT. BLEED SOURCE WAS NR 2 ENGINE. OPEN - [SDR ASOA20140124020](https://openairdocs.org/sdr/ASOA20140124020.md): Frame · corroded · Jan 24, 2014 · N12922 · Emb EMB145LR · Fuselage Main, Frame > DURING C-CHECK. APU GROUNDING SHUNT BAR WAS FOUND CORRODED AT FRAME 80. MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER AT FRAME 80 FOR THE GROUNDING BAR MOUNT IAW EC 5310-01544, REV C. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHEC - [SDR ASOA20140124019T](https://openairdocs.org/sdr/ASOA20140124019T.md): Frame · cracked · Jan 24, 2014 · N12922 · Emb EMB145LR · Fuselage Main, Frame > DURING C-CHECK, FRAME 10 WAS FOUND CRACKED UNDER F/O WINDOW. MAINTENANCE R & R THE CRACKED FRAME IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA20140123018](https://openairdocs.org/sdr/ASOA20140123018.md): Skin · corroded · Jan 23, 2014 · N12922 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING C-CHECK, MULTIPLE AREAS OF CORROSION FOUND ON THE INTERIOR BELLY SKIN AT FRAMES 17-19 AND STRINGERS 21L-22R. MAINTENANCE CUTOUT THE DAMAGE AREA, FABRICATED AND INSTALL A FILLER,SHIM AND A REPAIR DOUBLER IAW EC 5320-01890. ALL WORK ACCOMPLISHED AND WIL - [SDR ASOA20140123017T](https://openairdocs.org/sdr/ASOA20140123017T.md): Structure · cracked · Jan 23, 2014 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C-CHECK, A CRACK WAS FOUND AT FRAME 20, S3L IN THE COASTAL REINFORCEMENT. MAINTENANCE R & R COASTAL REINFORCEMENT IAW SRM 51-40-02. - [SDR ASOA20140123015T](https://openairdocs.org/sdr/ASOA20140123015T.md): Floor Support · corroded · Jan 23, 2014 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C CHECK, FOUND RT OMEGA BEAM GUSSET AT FRAME 61 WAS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED A NEW OMEGA BEAM IAW SRM 51-40-02. - [SDR ASOA20140123014](https://openairdocs.org/sdr/ASOA20140123014.md): Threshold · corroded · Jan 23, 2014 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING C CHECK, CORROSION WAS FOUND AROUND NUTPLATE HOLES IN SERVICE DOOR THRESHOLD BETWEEN FRAMES 20 - 22. MAINTENANCE R & R THE CORRODED THRESHOLD IAW SRM 51-40-02. - [SDR ASOA20131008115](https://openairdocs.org/sdr/ASOA20131008115.md): Inverter · inoperative · Oct 9, 2013 · N12922 · Emb EMB145LR · Emergency Lighting > DURING SCHEDULED MX INSPECTION THE LT OVERWING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. MX R & R INVERTER, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130807060](https://openairdocs.org/sdr/ASOA20130807060.md): Unknown · unknown · Aug 7, 2013 · N12922 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHTS OVER THE EXIT ROWS WOULD NOT LIGHT, DURING TEST. MX INSPECTED AND PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. OPS CHECKED GOOD. - [SDR ASOA20130725081](https://openairdocs.org/sdr/ASOA20130725081.md): Light · unknown · Jul 25, 2013 · N12922 · Emb EMB145LR · Emergency Lighting > PILOT REPORTED THE EMERGENCY EXIT LIGHT IN THE CEILING FACING THE FLIGHT DECK WAS DISCOVERED INOPERATIVE. MX PERFORMED AN OPS CHECK OF THE CABIN EMERGENCY LIGHTS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120821133](https://openairdocs.org/sdr/ASOA20120821133.md): Skin · damaged · Aug 19, 2012 · N12922 · Emb EMB145LR · Fuselage Main, Plate/Skin > DENT BETWEEN FRM 15 & 16 AND BETWEEN STRINGER 17L & 18L. REPAIRED DAMAGE, INSTALLED PATCH AND REPLACED SHEAR CLIP IAW ETD2012-145-011674 REV B. ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20120312031](https://openairdocs.org/sdr/ASOA20120312031.md): Beam · corroded · Mar 12, 2012 · N12922 · Emb EMB145LR · Cargo/Baggage Doors > ACFT IN FOR A C-CHECK, BAGGAGE DOOR LATERAL L SHAPE BEAM AT FRAME 68 CORRODED. MX REMOVED THE CORROSION IAW THE SRM 51-10-03. ACFT WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA20120307023](https://openairdocs.org/sdr/ASOA20120307023.md): Floor Support · corroded · Mar 3, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > CENTER OMEGA BEAM BETWEEN FRM 59 TO 61 CORRODED AT FORWARD NUT PLATE. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLERS. - [SDR ASOA20120307022](https://openairdocs.org/sdr/ASOA20120307022.md): Crossbeam · corroded · Mar 3, 2012 · N12922 · Emb EMB145LR · Fuselage Main, Floor Beam > CROSS MEMBER AT FRM 25 CORRODED. BLENDED CORROSION MATERIAL REMOVED IS WITHIN LIMITS. - [SDR ASOA20120307021](https://openairdocs.org/sdr/ASOA20120307021.md): Floor Support · corroded · Mar 3, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > CAP ON CENTER OMEGA BEAM AT FRAME 18 - FRAME 20 CORRODED. BLENDED CORROSION MATERIAL REMOVED IS WITHIN LIMITS. - [SDR ASOA20120319035](https://openairdocs.org/sdr/ASOA20120319035.md): Floor Support · corroded · Mar 2, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > CARGO COMPARTMENT DIGITAL Y-479 HAS CORROSION FROM FRM59 TO FRM61. R & R DIGITAL. - [SDR ASOA20120307020](https://openairdocs.org/sdr/ASOA20120307020.md): Floor Support · corroded · Mar 2, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > RT OMEGA BEAM CORRODED JUST AFT OF FRM 18. BLENDED CORROSION, MATERIAL REMOVED IS WITHIN LIMITS. - [SDR ASOA20120307019](https://openairdocs.org/sdr/ASOA20120307019.md): Floor Support · corroded · Mar 2, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > CENTER OMEGA BEAM CAP FROM FRM 59 TO FRM 61 CORRODED. REPLACED CENTER OMEGA BEAM CAP. - [SDR ASOA20120319039](https://openairdocs.org/sdr/ASOA20120319039.md): Sill · corroded · Feb 23, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > REAR GALLEY RT AFT SILL CORRODED. R & R SILL. - [SDR ASOA20120319038](https://openairdocs.org/sdr/ASOA20120319038.md): Sill · corroded · Feb 23, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > FWD GALLEY SILL CORRODED. R & R SILL. - [SDR ASOA20120319036](https://openairdocs.org/sdr/ASOA20120319036.md): Support · corroded · Feb 23, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > CROSS MEMBER FOR POTABLE WATER LT SIDE CORRODED. R & R CROSS MEMBER. - [SDR ASOA20120302018T](https://openairdocs.org/sdr/ASOA20120302018T.md): Structure · corroded · Feb 23, 2012 · N12922 · Emb EMB145LR · Fuselage Main, Structure > MAIN DOOR CUT-OUT REAR DIGITAL HAS CORROSION. R & R DIGITAL. - [SDR ASOA201203020009](https://openairdocs.org/sdr/ASOA201203020009.md): Sill · corroded · Feb 23, 2012 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > RT SILL FROM FRAME 59 TO FRAME 61 CORRODED. R & R SILL. - [SDR ASOA201111261007](https://openairdocs.org/sdr/ASOA201111261007.md): Inverter · inoperative · Nov 26, 2011 · N12922 · Emb EMB145LR · Emergency Lighting > SEAT 12BC TOP EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE - [SDR C2XA10CL144](https://openairdocs.org/sdr/C2XA10CL144.md): Controller · faulty · Sep 6, 2010 · N12922 · Emb EMB145LR · Cabin Pressure Controller > CLE FLT 2611 AIR RETURN CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED PRESSURIZATION DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10RI075](https://openairdocs.org/sdr/C2XA10RI075.md): Unknown · odor · Jun 6, 2010 · N12922 · Emb EMB145LR · Air Distribution System > FLIGHT 2217 - EWR - FLIGHT CREW REPORTED ELECTRICAL SMELL AT ROWS 1-4. EWR MX RAN ELECTRICAL SYSTEMS BUT COULD NOT DUPLICATE ELECTRICAL SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10IA129](https://openairdocs.org/sdr/C2XA10IA129.md): Altimeter · sticking · Apr 24, 2010 · N12922 · Emb EMB145LR · Altimeter, Barometric/Encoder > IAH - FLIGHT 2433, ON TAKEOFF THE CREW REPORTED THE STANDBY ALTIMETER TO BE STICKING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE STANDBY ALTIMETER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT W - [SDR C2XA10RI013](https://openairdocs.org/sdr/C2XA10RI013.md): Relay · inoperative · Jan 19, 2010 · N12922 · Emb EMB145LR · Extinguishing System > FLIGHT 2391 - EWR - FLIGHT CREW REPORTED BAGG EXTINGUISHER LIGHT NOT ILLUMINATED DURING TEST. EWR MX REMOVED AND REPLACED RELAY K0629 AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10SH027](https://openairdocs.org/sdr/C2XA10SH027.md): Support · cracked · Jan 13, 2010 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LAV WASTE DRAIN SUPPORT CRACKED. REMOVED AND REPLACED LAV WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH023](https://openairdocs.org/sdr/C2XA10SH023.md): Bushing · migrated · Jan 10, 2010 · N12922 · Emb EMB145LR · Horizontal Stabilizer Structure > SHV - DURING C-CHECK RT I/B HORIZ STAB HINGE PIN BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RIGHT I/B HORIZ STAB HINGE PIN BUSHING IAW EC5510-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH022](https://openairdocs.org/sdr/C2XA10SH022.md): Bushing · migrated · Jan 10, 2010 · N12922 · Emb EMB145LR · Horizontal Stabilizer Structure > SHV - DURING C-CHECK RIGHT O/B HORIZ STAB HINGE PIN BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RIGHT O/B HORIZ STAB HINGE PIN BUSHING IAW EC 5510-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH021](https://openairdocs.org/sdr/C2XA10SH021.md): Bushing · migrated · Jan 10, 2010 · N12922 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK RT GROUND SPOILER O/B HINGE FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND RE-INSTALLED RT GROUND SPOILER O/B HINGE FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152, CHECKED AND FOUND TO BE WITHIN LIMITS. THE AIRCRAFT WAS A - [SDR C2XA10SH020](https://openairdocs.org/sdr/C2XA10SH020.md): Sill · corroded · Jan 10, 2010 · N12922 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CORROSION (LEVEL 3 LOCAL) AROUND SCREW HOLES FOR SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR CENTER SILL (THRESHOLD) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH019](https://openairdocs.org/sdr/C2XA10SH019.md): Bushing · migrated · Jan 10, 2010 · N12922 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK RT SPEED BRAKE ACTUATOR FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REINSTALLED RT SPEED BRAKE ACTUATOR FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152, WITHIN LIMITS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH018](https://openairdocs.org/sdr/C2XA10SH018.md): Bushing · migrated · Jan 10, 2010 · N12922 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK RT GROUND SPOILER ACTUATOR FITTING I/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REINSTALLED RT GROUND SPOILER ACTUATOR FITTING I/B HAT BUSHING IAW EMB-145 EC5740-01152 CHECKED AND FOUND TO BE WITHIN LIMITS. THE AIRCRAFT WAS APPRO - [SDR C2XA10SH017](https://openairdocs.org/sdr/C2XA10SH017.md): Structure · corroded · Jan 10, 2010 · N12922 · Emb EMB145LR · Passenger/Crew Doors > SHV - DURING C-CHECK MAIN DOOR HAS CORROSION (LEVEL 2 LOCAL) AROUND NUT PLATE HOLE AT BOTTOM SECTION OF DOOR. MAINTENANCE PERFORMED REPAIR AT MAIN DOOR LOWER NUT PLATE HOLES IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA253](https://openairdocs.org/sdr/C2XA09IA253.md): Ballast · defective · Oct 12, 2009 · N12922 · Emb EMB145LR · Passenger Compartment Lighting > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING ODOR AT THE SEAT 6-10 AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST AT ROW 8, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED F - [SDR C2XA09RI136](https://openairdocs.org/sdr/C2XA09RI136.md): Fuse · blown · Aug 10, 2009 · N12922 · Emb EMB145LR · Trailing Edge Flap Control System > FLIGHT 2580 - EWR - DURING LANDING, FLIGHT CREW REPORTED FLAP FAIL WARNING ON EICAS AND FLAP STUCK TO 0. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FECU (SDR C2XA09RI134), FDMU (SDR C2XA09RI135) AND FUSE 0098. MX PERFORMED OPERATIONAL CHECK Next page: https://openairdocs.org/deregistered/N12922-2019-01-10/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 = 'N12922' AND deregistration_id = 'N12922-2019-01-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N12922-2019-01-10/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.