# Service difficulty reports: N12924, cancelled Apr 3, 2017 A list on [N12924, cancelled Apr 3, 2017](https://openairdocs.org/deregistered/N12924-2017-04-03.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 · 55 reports - [SDR ASOA201610270625](https://openairdocs.org/sdr/ASOA201610270625.md): Control Module · odor · Oct 27, 2016 · N12924 · Emb EMB145LR · Passenger Compartment Lighting > F/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. - [SDR ASOA20160510022R](https://openairdocs.org/sdr/ASOA20160510022R.md): Control Module · shorted · May 10, 2016 · N12924 · Emb EMB145LR · Passenger Compartment Lighting > CREW 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. - [SDR ASOA20150609057](https://openairdocs.org/sdr/ASOA20150609057.md): Packing · torn · Jun 9, 2015 · N12924 · Emb EMB145LR · Turbine Engine Oil System > THE 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 SE - [SDR ASOA20150602125](https://openairdocs.org/sdr/ASOA20150602125.md): Door Frame · corroded · Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Structure > DURING 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. - [SDR ASOA20150602124](https://openairdocs.org/sdr/ASOA20150602124.md): Stringer · corroded · Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > DURING 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. - [SDR ASOA20150602123V](https://openairdocs.org/sdr/ASOA20150602123V.md): Skin · cracked · Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING 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. - [SDR ASOA20150602122V](https://openairdocs.org/sdr/ASOA20150602122V.md): Skin · cracked · Jun 2, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING 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. - [SDR ASOA20150528121](https://openairdocs.org/sdr/ASOA20150528121.md): Firewall · canning · May 28, 2015 · N12924 · Emb EMB145LR · APU Cowling/Containment > DURING 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. - [SDR ASOA20150528120](https://openairdocs.org/sdr/ASOA20150528120.md): Floor Support · corroded · May 28, 2015 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR ASOA20150528119](https://openairdocs.org/sdr/ASOA20150528119.md): Skin · cracked · May 28, 2015 · N12924 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING 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. - [SDR ASOA20130917109](https://openairdocs.org/sdr/ASOA20130917109.md): Light · inoperative · Sep 17, 2013 · N12924 · Emb EMB145LR · Emergency Lighting > DURING 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. - [SDR ASOA20130703071](https://openairdocs.org/sdr/ASOA20130703071.md): Acm · seized · Jul 3, 2013 · N12924 · Emb EMB145LR · Cabin Cooling System > CREW 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. - [SDR ASOA20130616090](https://openairdocs.org/sdr/ASOA20130616090.md): Flapper Bearing · leaking · Jun 16, 2013 · N12924 · Emb EMB145LR · Fuel Storage > DURING 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. - [SDR ASOA20121025084](https://openairdocs.org/sdr/ASOA20121025084.md): Charger · faulty · Oct 25, 2012 · N12924 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MX, AFT ASILE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MX REPLACED THE BATTERY POWER SUPPLY CHARGER. OPS CHECKED GOOD. - [SDR ASOA20121012082](https://openairdocs.org/sdr/ASOA20121012082.md): Battery Pack · inoperative · Oct 12, 2012 · N12924 · Emb EMB145LR · Emergency Lighting > DURING 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. - [SDR ASOA20120923084R](https://openairdocs.org/sdr/ASOA20120923084R.md): Battery Pack · inoperative · Sep 23, 2012 · N12924 · Emb EMB145LR · Emergency Lighting > DURING 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. - [SDR ASOA20120824064](https://openairdocs.org/sdr/ASOA20120824064.md): Charger · inoperative · Aug 24, 2012 · N12924 · Emb EMB145LR · Emergency Lighting > DURING 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. - [SDR C2XA11RI091](https://openairdocs.org/sdr/C2XA11RI091.md): Controller · defective · May 24, 2011 · N12924 · Emb EMB145LR · Cabin Pressure Controller > FLIGHT 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 OPERATIONA - [SDR C2XA11RI090](https://openairdocs.org/sdr/C2XA11RI090.md): Controller · defective · May 24, 2011 · N12924 · Emb EMB145LR · Cabin Pressure Controller > FLIGHT 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 C - [SDR C2XA11IA088](https://openairdocs.org/sdr/C2XA11IA088.md): Flow Divider · leaking · May 8, 2011 · N12924 · Emb EMB145LR · APU Engine Fuel and Control > FLIGHT 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 SERVI - [SDR C2XA10CL112](https://openairdocs.org/sdr/C2XA10CL112.md): O-Ring · deteriorated · Jul 12, 2010 · N12924 · Emb EMB145LR · Pneumatic Distribution System > THE 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. - [SDR C2XA10TY058](https://openairdocs.org/sdr/C2XA10TY058.md): Light · inoperative · Apr 18, 2010 · N12924 · Emb EMB145LR · Emergency Lighting > TYS - EMERGENCY LIGHT ABOVE RT PACK PANEL INOP. REMOVED AND REPLACED BULB. - [SDR C2XA10RI036](https://openairdocs.org/sdr/C2XA10RI036.md): Unknown · odor · Mar 12, 2010 · N12924 · Emb EMB145LR · Air Distribution System > FLIGHT 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 TO - [SDR C2XA09TY249](https://openairdocs.org/sdr/C2XA09TY249.md): Attach Bracket · corroded · Sep 29, 2009 · N12924 · Emb EMB145LR · Fuselage, Stabilizer Attach Fittings > FRETTING 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. - [SDR C2XA09TY248](https://openairdocs.org/sdr/C2XA09TY248.md): Fitting · damaged · Sep 29, 2009 · N12924 · Emb EMB145LR · Vertical Stabilizer > FRM 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. - [SDR C2XA09TY237](https://openairdocs.org/sdr/C2XA09TY237.md): Structure · corroded · Sep 17, 2009 · N12924 · Emb EMB145LR · Nacelle/Pylon Miscellaneous Structure > TYS - 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 THE - [SDR C2XA09RI158](https://openairdocs.org/sdr/C2XA09RI158.md): Tube · leaking · Sep 7, 2009 · N12924 · Emb EMB145LR · Pneumatic Distribution System > FLIGHT 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. - [SDR C2XA09IA193](https://openairdocs.org/sdr/C2XA09IA193.md): O-Ring · blown · Jul 29, 2009 · N12924 · Emb EMB145LR · Pneumatic Distribution System > IAH - 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 LE - [SDR C2XA09IA105](https://openairdocs.org/sdr/C2XA09IA105.md): Ahrs · inoperative · Apr 22, 2009 · N12924 · Emb EMB145LR · Integrated Flight System > IAH - 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 - [SDR C2XA08CL021](https://openairdocs.org/sdr/C2XA08CL021.md): Relay · faulty · Feb 18, 2008 · N12924 · Emb EMB145LR · Electrical Power System > CLE 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 W - [SDR C2XA07IA252](https://openairdocs.org/sdr/C2XA07IA252.md): Landing Gear · malfunctioned · Dec 20, 2007 · N12924 · Emb EMB145LR · Landing Gear Retraction/Extension System > FLIGHT 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 RETR - [SDR C2XA07BT012](https://openairdocs.org/sdr/C2XA07BT012.md): Unknown · odor · Jan 26, 2007 · N12924 · Emb EMB145LR · Air Distribution System > FLT 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 BLE - [SDR C2XA06IA068](https://openairdocs.org/sdr/C2XA06IA068.md): Battery Pack · loose · May 2, 2006 · N12924 · Emb EMB145LR · Emergency Lighting > STL - 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 SERVI - [SDR C2XA06IA041](https://openairdocs.org/sdr/C2XA06IA041.md): Ballast · malfunctioned · Mar 12, 2006 · N12924 · Emb EMB145LR · Passenger Compartment Lighting > IAH - 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 SERVICE - [SDR C2XA03SH510](https://openairdocs.org/sdr/C2XA03SH510.md): Strip · inoperative · Dec 22, 2003 · N12924 · Emb EMB145LR · Emergency Lighting > SHV- 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 - [SDR C2XA03SH507](https://openairdocs.org/sdr/C2XA03SH507.md): Sill · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH502](https://openairdocs.org/sdr/C2XA03SH502.md): Buttstrap · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH508](https://openairdocs.org/sdr/C2XA03SH508.md): Angle · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH506](https://openairdocs.org/sdr/C2XA03SH506.md): Floorbeam · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV- 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. - [SDR C2XA03SH505](https://openairdocs.org/sdr/C2XA03SH505.md): Floorbeam · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV- 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. - [SDR C2XA03SH504](https://openairdocs.org/sdr/C2XA03SH504.md): Floorbeam · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV- 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. - [SDR C2XA03SH503](https://openairdocs.org/sdr/C2XA03SH503.md): Sill · corroded · Dec 18, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH501](https://openairdocs.org/sdr/C2XA03SH501.md): Angle · corroded · Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH500](https://openairdocs.org/sdr/C2XA03SH500.md): Buttstrap · corroded · Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV-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. - [SDR C2XA03SH499](https://openairdocs.org/sdr/C2XA03SH499.md): Buttstrap · corroded · Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH498](https://openairdocs.org/sdr/C2XA03SH498.md): Floorbeam · corroded · Dec 17, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV-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. - [SDR C2XA03SH497](https://openairdocs.org/sdr/C2XA03SH497.md): Buttstrap · corroded · Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV- 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. - [SDR C2XA03SH496](https://openairdocs.org/sdr/C2XA03SH496.md): Buttstrap · corroded · Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH494](https://openairdocs.org/sdr/C2XA03SH494.md): Sill · corroded · Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. - [SDR C2XA03SH493](https://openairdocs.org/sdr/C2XA03SH493.md): Support · corroded · Dec 13, 2003 · N12924 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV- 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. Next page: https://openairdocs.org/deregistered/N12924-2017-04-03/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 = 'N12924' AND deregistration_id = 'N12924-2017-04-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N12924-2017-04-03/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.