N12924, cancelled Apr 3, 2017

Service difficulty reports · 55

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N12924' AND deregistration_id = 'N12924-2017-04-03'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA201610270625Control Module · odorF/A REPORTS A BURNING SMELL COMING FROM BEHIND SPEAKER IN GALLEY. MX REMOVED AND REPLACED GALLEY LIGHTING CONTROL MODULE POWERED A/C WITH NO BURNING SMELL FOUND REF 145 33-29-01. A/C WAS APPROVED FOR RETURN TO SERVICE.Oct 27, 2016 · N12924 · Emb EMB145LR · Passenger Compartment LightingSDR ASOA20160510022RControl Module · shortedCREW REPORTED THE RIGHT SIDEWALL PASSENGER LIGHTS WOULD NOT TURN ON AND PRODUCED A BURNING ODOR. MAINTENANCE R & R THE LIGHTS CONTROL MODULE WITH OPS CHECK GOOD AND NO BURNING ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.May 10, 2016 · N12924 · Emb EMB145LR · Passenger Compartment LightingSDR ASOA20150609057Packing · tornTHE CREW REPORTED THAT THE ACFT HAD A VERY STRONG ODOR ASSOCIATED WITH THE PACKS. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, R & R THE NR 1 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SEJun 9, 2015 · N12924 · Emb EMB145LR · Turbine Engine Oil SystemSDR ASOA20150602125Door Frame · corrodedDURING C-CHECK THE MAIN CABIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01348. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20150602124Stringer · corrodedDURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-00-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR ASOA20150602123VSkin · crackedDURING C-CHECK, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 3 FASTENERS BETWEEN FRAMES 78-79, STRINGERS 2R-5R. MAINTENANCE PERFORMED 3 BUSHING REPAIRS TO THE SKIN IAW EC 5330-03018. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20150602122VSkin · crackedDURING C-CHECK, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND 4 FASTENERS BETWEEN FRAMES 77-78, STRINGERS 3L-4L. MAINTENANCE PERFORMED 4 BUSHING REPAIRS TO THE SKIN IAW EC5330-03018. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20150528121Firewall · canningDURING C-CHECK THE APU FIREWALL AT FRAME 81 WAS FOUND TO BE OIL-CANNING BY THE LT SIDE STIFFENER BELOW THE BLEED DUCT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 28, 2015 · N12924 · Emb EMB145LR · APU Cowling/ContainmentSDR ASOA20150528120Floor Support · corrodedDURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-02044. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 28, 2015 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20150528119Skin · crackedDURING C-CHECK THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGERS 1R-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03019. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 28, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20130917109Light · inoperativeDURING MX INSPECTION THE AISLE FLOOR EMERGENCY LIGHT AT ROW 16 WAS DISCOVERED INOPERATIVE. MX R & R LIGHT, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.Sep 17, 2013 · N12924 · Emb EMB145LR · Emergency LightingSDR ASOA20130703071Acm · seizedCREW REPORTED SMOKE IN COCKPIT AND CABIN IN FLIGHT. MX PERFORMED ABNORMAL SMOKE INSPECTION OF CABIN & COCKPIT AND FOUND NR 1 ACM DAMAGED. R & R NR 1 ACM WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 3, 2013 · N12924 · Emb EMB145LR · Cabin Cooling SystemSDR ASOA20130616090Flapper Bearing · leakingDURING CLIMB, THE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE ACFT RETURNED TO AIRPORT WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE OTBD FLAPPER VALVE IN THE RT WING AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 16, 2013 · N12924 · Emb EMB145LR · Fuel StorageSDR ASOA20121025084Charger · faultyDURING ROUTINE MX, AFT ASILE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE BATTERY POWER SUPPLY CHARGER. OPS CHECKED GOOD.Oct 25, 2012 · N12924 · Emb EMB145LR · Emergency LightingSDR ASOA20121012082Battery Pack · inoperativeDURING ROUTINE MX, THE REAR INTERIOR AND EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE GOOD.Oct 12, 2012 · N12924 · Emb EMB145LR · Emergency LightingSDR ASOA20120923084RBattery Pack · inoperativeDURING MX INSPECTION, FOUND NR 4 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. MX R & R NR 4 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 23, 2012 · N12924 · Emb EMB145LR · Emergency LightingSDR ASOA20120824064Charger · inoperativeDURING MX INSPECTION, THE LT AND RT EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 BATTERY CHARGING TRAY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 24, 2012 · N12924 · Emb EMB145LR · Emergency LightingSDR C2XA11RI091Controller · defectiveFLIGHT 6165 - IAD - FLIGHT CREW REPORTED AUTO PRESS ERRACTIC. IAD MX MEL`ED THE SYSTEM. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT DUPLICATE FAIL. MX REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAMay 24, 2011 · N12924 · Emb EMB145LR · Cabin Pressure ControllerSDR C2XA11RI090Controller · defectiveFLIGHT 5790 - ORF - FLIGHT CREW REPORTED PRESSURIZATION FAIL IN AUTO AND MANUAL MODE. RIC MX PERFORMED OPERATIONAL CHECK OF AUTO PRESSURIZATION AND COULD NOT DUPLICATE FAIL. MX REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CMay 24, 2011 · N12924 · Emb EMB145LR · Cabin Pressure ControllerSDR C2XA11IA088Flow Divider · leakingFLIGHT 2557 FROM IND THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT DURING TAKEOFF. THE AIRCRAFT CONTINUED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIMay 8, 2011 · N12924 · Emb EMB145LR · APU Engine Fuel and ControlSDR C2XA10CL112O-Ring · deterioratedTHE CREW REPORTED A "BLEED 1 LEAK" MESSAGE ON CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT O-RINGS AT JOINT 17 AND 25 OF THE BLEED SYSTEM. OPERATIONAL CHECKS WERE GOOD.Jul 12, 2010 · N12924 · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA10TY058Light · inoperativeTYS - EMERGENCY LIGHT ABOVE RT PACK PANEL INOP. REMOVED AND REPLACED BULB.Apr 18, 2010 · N12924 · Emb EMB145LR · Emergency LightingSDR C2XA10RI036Unknown · odorFLIGHT 3073 - EWR - FLIGHT CREW REPORTED STRONG SMELL NOTICEABLE IN PAST HALF OF ACFT CABIN. EWR MX PERFORMED OPERATIONAL CHECK OF THE PACKS AND PERFORMED CABIN CONTAMINATION TROUBLESHOOTING CHART SUCCESSFULLY - NO SMELL NOTED. ACFT WAS APPROVED TO RETURN TOMar 12, 2010 · N12924 · Emb EMB145LR · Air Distribution SystemSDR C2XA09TY249Attach Bracket · corrodedFRETTING AT FRM 75 STR 1R AT FUSELAGE TO STAB ATTACH BRACKET AS MARKED. REMOVED FITTING AT FRM 75, BLENDED CORROSION, PERFORMED DYE-PEN, REPAIRED FITTING AND INSTALLED IAW EC5310-01480, EMB 145 SRM 51-40-02 AND EC5310-01317.Sep 29, 2009 · N12924 · Emb EMB145LR · Fuselage, Stabilizer Attach FittingsSDR C2XA09TY248Fitting · damagedFRM 75 UPPER FITTING HAS OVERSIZED HOLE ON RT O/B HOLE. REMOVED, REPAIRED AND INSTALLED FITTING IAW EC5530-01187, EMB 145 SRM 51-40-02 AND EC5310-01317.Sep 29, 2009 · N12924 · Emb EMB145LR · Vertical StabilizerSDR C2XA09TY237Structure · corrodedTYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION IN TWO HOLES ON THE NR 2 ENGINE INLET. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHINGS TO REMOVE THE CORROSION. ALL WORK WAS ACCOMPLISHED IAW EC5420-01158 AND WILL BE RELEASED AT THE END OF THESep 17, 2009 · N12924 · Emb EMB145LR · Nacelle/Pylon Miscellaneous StructureSDR C2XA09RI158Tube · leakingFLIGHT CREW REPORTED ENGINE BLEED NR 2 LEAK AFTER TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 BLEED SYSTEM TUBE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Sep 7, 2009 · N12924 · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA09IA193O-Ring · blownIAH - FLIGHT 2695, THE CREW REPORTED A BLD 2 LK INDICATION ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BLEED DUCT O-RINGS UNDER THE CARGO FLOOR. OPERATIONAL AND LEJul 29, 2009 · N12924 · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA09IA105Ahrs · inoperativeIAH - FLIGHT 2027, THE CREW REPORTED AN AHRS1 FAIL / ATT FAIL 1, AND SPS ADVANCE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ONE AHRS COMPUTER, OPERATIONALLY Apr 22, 2009 · N12924 · Emb EMB145LR · Integrated Flight SystemSDR C2XA08CL021Relay · faultyCLE FLIGHT 2793 - THE CREW REPORTED MULTIPLE WARNINGS DURING CLIMB E1 FUEL LO LEVEL, AMBER DASHES ON FUEL TOTAL + TANK 2 FUEL LEVELS, RMU NR 2 BLANK, APU SHUTOFF VALVE CLOSED, AURAL WARNING FLAP FAIL, AUTO PILOT FAIL. THE AIRCRAFT RETURNED TO CLE AND LANDED WFeb 18, 2008 · N12924 · Emb EMB145LR · Electrical Power SystemSDR C2XA07IA252Landing Gear · malfunctionedFLIGHT 2412 - DGO - IAH, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO DGO AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE LANDING GEAR EXTENSION AND RETRACTION TESTS WERE PERFORMED. THE GEAR RETRDec 20, 2007 · N12924 · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR C2XA07BT012Unknown · odorFLT NR 2312 - SMELLED BURNING ODOR 20 MINUTES AND 5 MINUTES BEFORE LANDING. NO SMOKE OBSERVED. FLT ATTENDANT SMELLED IT FIRST IN FWD CABIN. INSP COCKPIT AREA OVERHEAD PANELS, SIDE WALL PANELS UNDER COCKPIT FOORS RAN BOTH ENGINES AT MAX POWER WITH ENGINE BLEJan 26, 2007 · N12924 · Emb EMB145LR · Air Distribution SystemSDR C2XA06IA068Battery Pack · looseSTL - DURING MAINTENANCE INSPECTION BOTH OVERWING EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIMay 2, 2006 · N12924 · Emb EMB145LR · Emergency LightingSDR C2XA06IA041Ballast · malfunctionedIAH - FLIGHT 2732, A BURNING SMELL WAS NOTICED IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED TWO LIGHT BALLASTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEMar 12, 2006 · N12924 · Emb EMB145LR · Passenger Compartment LightingSDR C2XA03SH510Strip · inoperativeSHV- DURING C-CHECK THE NR 4 AND NR 5 EMERGENCY PROXIMITY AISLE LIGHTS WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 5 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. MAINTENANCE OPERATIONALLY CHECKED ALL LIGHT STRIPS Dec 22, 2003 · N12924 · Emb EMB145LR · Emergency LightingSDR C2XA03SH507Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH502Buttstrap · corrodedSHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 15. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR EMB IC2003-145/4250. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH508Angle · corrodedSHV- DURING C-CHECK THE LEFT HAND RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH506Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA03SH505Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA03SH504Floorbeam · corrodedSHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA03SH503Sill · corrodedSHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAME 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH501Angle · corrodedSHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH500Buttstrap · corrodedSHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH499Buttstrap · corrodedSHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH498Floorbeam · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 16 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA03SH497Buttstrap · corrodedSHV- DURUNG C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA03SH496Buttstrap · corrodedSHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH494Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03SH493Support · corrodedSHV- DURING C-CHECK THE MAIN PASSENGER DOOR SILL SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE MAIN PASSENGER DOOR SILL SUPPORT IAW EMB 145 IPC 53-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure
Back to N12924, cancelled Apr 3, 2017