# Service difficulty reports: N15973, cancelled Jan 5, 2017 A list on [N15973, cancelled Jan 5, 2017](https://openairdocs.org/deregistered/N15973-2017-01-05.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 · 92 reports - [SDR ASOA20150104001](https://openairdocs.org/sdr/ASOA20150104001.md): Battery Pack · inoperative · Jan 4, 2015 · N15973 · Emb EMB145LR · Emergency Lighting > DURING MAINTENANCE INSPECTION THE NR 1 EMERGENCY LIGHT SYS BATTERY WOULD NOT HOLD A CHARGE. MAINTENANCE R & R NR 1 EMERGENCY LIGHT SYSTEM BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140106009](https://openairdocs.org/sdr/ASOA20140106009.md): Shear Tie · cracked · Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting Structure > C-CHECK, A CRACKED SHEAR TIE WAS FOUND AT FRAME 24 BETWEEN S15-16R. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02. - [SDR ASOA20140106008](https://openairdocs.org/sdr/ASOA20140106008.md): Shear Tie · cracked · Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting Structure > C-CHECK, A CRACK WAS FOUND IN A SHEAR TIE AT FRAME 73 BETWEEN STR8L AND 9L. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02. - [SDR ASOA20140106007](https://openairdocs.org/sdr/ASOA20140106007.md): Floor Support · cracked · Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > C-CHECK, A CRACK WAS FOUND IN THE RT OMEGA BEAM INBD SUPPORT BETWEEN FRAMES 47 AND 48. MAINTENANCE R & R THE OMEGA BEAM SUPPORT IAW SRM 53-23-02 AND SRM 51-40-02. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA20140106006](https://openairdocs.org/sdr/ASOA20140106006.md): Shear Tie · cracked · Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting Structure > C-CHECK, A SHEAR TIE AT FRAME 26 BETWEEN STR 15R AND 16R WAS FOUND CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-20--01 AND 51-40-02. - [SDR ASOA20140106005](https://openairdocs.org/sdr/ASOA20140106005.md): Floor Support · cracked · Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > CRACK IN RT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT. - [SDR ASOA20140106004](https://openairdocs.org/sdr/ASOA20140106004.md): Floor Support · cracked · Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > CRACK IN LT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT. - [SDR ASOA20140106002](https://openairdocs.org/sdr/ASOA20140106002.md): Beam · corroded · Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Main, Structure > CARGO DOOR CUTOUT THRESHOLD BEAM CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R THRESHOLD BEAM. - [SDR ASOA20140106001](https://openairdocs.org/sdr/ASOA20140106001.md): Floor Support · corroded · Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > RT OTBD FLOOR SUPPORT AT FRAME 50 CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT. - [SDR ASOA20120301018](https://openairdocs.org/sdr/ASOA20120301018.md): Mount · cracked · Mar 1, 2012 · N15973 · Emb EMB145LR · Engine Mount Section > DURING C-CHECK, NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REPAIRED YOKE IAW EC5450-01047. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA145](https://openairdocs.org/sdr/C2XA11IA145.md): Unknown · odor · Jul 4, 2011 · N15973 · Emb EMB145LR · Air Distribution System > IAH - FLIGHT 2818, THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN AFTER LANDING. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN THE ENGINES, PACKS, AND APU ALL WITH NO DEFECTS - [SDR C2XA11RI111](https://openairdocs.org/sdr/C2XA11RI111.md): Fastener · loose · Jun 17, 2011 · N15973 · Emb EMB145LR · Flight Compartment Windows > FLIGHT 6061 - IAD - FLIGHT CREW REPORTED LOUD NOISE COMING FROM F/O WINDSHIELD. IAD MX RETORQUED F/O WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA11RI110](https://openairdocs.org/sdr/C2XA11RI110.md): Conditioner · defective · Jun 12, 2011 · N15973 · Emb EMB145LR · Landing Gear Brake System > FLIGHT 2041 - EWR - FLIGHT CREW REPORTED RT O/B BRAKE OVERTEMP MSG ON EICAS DURING T/O. UPON LANDING MESSAGE CLEARED AND BRAKE INDICATED NORMAL TEMP. EWR MX REMOVED AND REPLACED O/B TEMP SIGNAL CONDITIONER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT - [SDR C2XA10CL031](https://openairdocs.org/sdr/C2XA10CL031.md): Bleed Valve · failed · Feb 20, 2010 · N15973 · Emb EMB145LR · Compressor Bleed Valve > CLE FLT 2513 THE CREW REPORTED A NR 1 HIGH STAGE BLEED VALVE FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HIGH STAGE VALVE AND THE NR 1 ENGINE INDICATING HARNESS. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10SH057](https://openairdocs.org/sdr/C2XA10SH057.md): Trunnion · corroded · Feb 10, 2010 · N15973 · Emb EMB145LR · Main Landing Gear Attach Section > SHV - DURING C-CHECK RIGHT MLG AFT UPPER TRUNNION HAS PITTING CORROSION AND IS OUT OF LIMITS. REPAIRED RIGHT MLG AFT UPPER TRUNNION IAW EC57350-01406. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH056](https://openairdocs.org/sdr/C2XA10SH056.md): Wire · broken · Feb 10, 2010 · N15973 · Emb EMB145LR · Landing Gear System Wiring > SHV - DURING C-CHECK LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPAIRED BROKEN WIRE IAW EMB 145 WM 20-21-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH051](https://openairdocs.org/sdr/C2XA10SH051.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH050](https://openairdocs.org/sdr/C2XA10SH050.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH049](https://openairdocs.org/sdr/C2XA10SH049.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH048](https://openairdocs.org/sdr/C2XA10SH048.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH047](https://openairdocs.org/sdr/C2XA10SH047.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH046](https://openairdocs.org/sdr/C2XA10SH046.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH045](https://openairdocs.org/sdr/C2XA10SH045.md): Floor Support · corroded · Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH042](https://openairdocs.org/sdr/C2XA10SH042.md): Floor Support · corroded · Feb 1, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED LT OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH041](https://openairdocs.org/sdr/C2XA10SH041.md): Structure · corroded · Jan 31, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH038](https://openairdocs.org/sdr/C2XA10SH038.md): Floor Support · corroded · Jan 31, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09IA051](https://openairdocs.org/sdr/C2XA09IA051.md): Unknown · odor · Feb 17, 2009 · N15973 · Emb EMB145LR · Air Distribution System > IAH - FLIGHT 2875 THE FLIGHT ATTENDANT REPORTED A BURNING SMELL WHEN THE HEATER WAS ON. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUEN - [SDR C2XA09CL012](https://openairdocs.org/sdr/C2XA09CL012.md): Strut · underserviced · Jan 27, 2009 · N15973 · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle > CLE FLIGHT NR 2847 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG AND A THRUST REVERSE 1&2 DISAGREE MSG ON THE EICAS ON CLIMBOUT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND SERVICED THE NOSE GEAR STRUT. OPS CHECK WA - [SDR C2XA08IA269](https://openairdocs.org/sdr/C2XA08IA269.md): Muffler · loose · Dec 28, 2008 · N15973 · Emb EMB145LR · Air Distribution System > IAH - FLIGHT 2434, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED IN FLIGHT, AND WERE UNABLE TO RESET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE PACK 2 DISTRIBUTION MUFFLER, OPERATIO - [SDR C2XA08IA268](https://openairdocs.org/sdr/C2XA08IA268.md): Wire · broken · Dec 28, 2008 · N15973 · Emb EMB145LR · Air Conditioning System Wiring > IAH - FLIGHT 2434, THE CREW REPORTED A PACK 1 VALVE CLOSED ADVISORY MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE W101-2447-22 AT THE BUSHBUTTON FOR PACK ONE, OPERATIONALLY TESTED WITH NO DEFECTS, - [SDR C2XA08SH019](https://openairdocs.org/sdr/C2XA08SH019.md): Floor Support · cracked · Feb 2, 2008 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LEFT OMEGA BEAM AT FR 22 HAS A CRACK IN WEB THROUGH RIVET. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19 AND 23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA08SH018](https://openairdocs.org/sdr/C2XA08SH018.md): Floor Support · corroded · Feb 2, 2008 · N15973 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LEFT OMEGA BEAM WEB AND FLANGE AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19-23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA07IA222](https://openairdocs.org/sdr/C2XA07IA222.md): Lock · defective · Oct 10, 2007 · N15973 · Emb EMB145LR · Flight Compartment Windows > IAH - FLIGHT 2711, THE CREW REPORTED THAT THE CAPTAINS DV WINDOW POPPED OPEN DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE CAPTAINS DV WINDOW LOCK BAR AND ADJUSTED IAW EMB-145 M - [SDR C2XA07IA192](https://openairdocs.org/sdr/C2XA07IA192.md): Ballast · defective · Sep 2, 2007 · N15973 · Emb EMB145LR · Passenger Compartment Lighting > IAH - FLIGHT 2857, THE CREW REPORTED THAT THE BALLAST ABOVE SEAT 4A SMELLED BURNT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHTING IN MEL 33-210-00/1 CAT C CONTROL 128447, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED - [SDR C2XA07CL073](https://openairdocs.org/sdr/C2XA07CL073.md): Sign · inoperative · Aug 28, 2007 · N15973 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE EXIT SIGN AT THE RIGHT AFT DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA07CL064](https://openairdocs.org/sdr/C2XA07CL064.md): Sensor · shorted · Jul 31, 2007 · N15973 · Emb EMB145LR · Ice/Rain Protection System Wiring > FLIGHT NR 2666 THE CREW REPORTED A TAT 1 HEAT INOP MESSAGE ON THE EICAS WITH A FAINT ELECTRICAL BURNING ODOR THAT LASTED FOR 1 TO 2 MINUTES.MAINTENANCE INSPECTED AND REPLACED THE NR 1 TAT CURRENT SENSOR KO064. OPERATIONAL CHECKS OF THE SYSTEM WERE GOOD. - [SDR C2XA07RI018](https://openairdocs.org/sdr/C2XA07RI018.md): Smoke Detector · inoperative · Apr 19, 2007 · N15973 · Emb EMB145LR · Smoke Detection > FLIGHT 2882 - EWR - CREW REPORTED NR 2 CARGO SMOKE DETECTOR INOP. EWR MX REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW EMB AMM 26-23-00. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07IA079](https://openairdocs.org/sdr/C2XA07IA079.md): Unknown · odor · Apr 4, 2007 · N15973 · Emb EMB145LR · Air Distribution System > IAH - FLIGHT 2151, DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA07CL030](https://openairdocs.org/sdr/C2XA07CL030.md): Carbon Seal · leaking · Mar 12, 2007 · N15973 · Emb EMB145LR · Turbine Engine Oil System > EWR FLIGHT 3068 THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES. THE NR 1 ENGINE WAS FOUND TO BE THE CAUSE OF THE LAV INDICATION AND SMOKEY - [SDR C2XA07BT020](https://openairdocs.org/sdr/C2XA07BT020.md): Unknown · smoke · Feb 23, 2007 · N15973 · Emb EMB145LR · Air Distribution System > EWR LOG SQUAWK FLT NR 2292 ON CLIMB AT 8000 FT. WE GOT LAV SMOKE WARNING. THE FA CONFIRMED SMOKE IN THE CABIN. INSPECTED ALL OVERHEAD LIGHTS IN CABIN AND LAV. NO DEFECTS NOTED. PERFORMED RR FIM TASK 72-00-00-810-814. RAN BOTH ENGINES INDIVIDUALLY WITH BL - [SDR C2XA06TY017](https://openairdocs.org/sdr/C2XA06TY017.md): Frame · cracked · Mar 28, 2006 · N15973 · Emb EMB145LR · Fuselage Main, Frame > PAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER OUTBOARD HOLE HAS A CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310- 01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOOD - [SDR C2XA06TY015](https://openairdocs.org/sdr/C2XA06TY015.md): Frame · cracked · Mar 17, 2006 · N15973 · Emb EMB145LR · Fuselage Main, Frame > PAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER INBOARD HOLE HAS CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310-01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOOD. - [SDR C2XA06TY016](https://openairdocs.org/sdr/C2XA06TY016.md): Bracket · cracked · Mar 17, 2006 · N15973 · Emb EMB145LR · Fuselage Main, Structure > PAX DOOR FRAME CUT-OUT, FWD LOWER STOP STRUCTURE, LOWER INBOARD HOLE HAS TWO CRACKS, ONE ON THE FRAME AND ONE IN THE BACK CASTING. REMOVED CRACKED BRACKET, DRILLED CRACKED HOLE ON SKIN SIDE TO 10MM. DRILLED NEW BRACKET AND INSTALLED. REAMED AND COLD WORKED - [SDR C2XA05BT077](https://openairdocs.org/sdr/C2XA05BT077.md): Power Supply · faulty · Oct 30, 2005 · N15973 · Emb EMB145LR · Emergency Lighting > BNA - CREW REPORTED, ON HEAD START, EXIT ROW OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB145 AMM NR 33-50-04, OPS CHECK GOOD. - [SDR C2XA05IA106](https://openairdocs.org/sdr/C2XA05IA106.md): Inverter · inoperative · Sep 13, 2005 · N15973 · Emb EMB145 · Emergency Lighting > STL - DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LOCATOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO - [SDR C2XA04CL120](https://openairdocs.org/sdr/C2XA04CL120.md): Motor · failed · Nov 28, 2004 · N15973 · Emb EMB145 · Trailing Edge Flap Actuator > CREW REPORTED FLAP FAILED IN FLIGHT. REPLACED THE NR 1 FLAP DRIVE MOTOR. AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA04SH309](https://openairdocs.org/sdr/C2XA04SH309.md): Cowling · chafed · May 22, 2004 · N15973 · Emb EMB145 · Engine Cowling System > DURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH296](https://openairdocs.org/sdr/C2XA04SH296.md): Beam · corroded · May 18, 2004 · N15973 · Emb EMB145 · Fuselage Main, Structure > SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER 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 C2XA04SH295](https://openairdocs.org/sdr/C2XA04SH295.md): Stiffener · chafed · May 18, 2004 · N15973 · Emb EMB145 · Nacelle/Pylon, Frame/Spar/Rib > SHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH294](https://openairdocs.org/sdr/C2XA04SH294.md): Skin · dented · May 18, 2004 · N15973 · Emb EMB145 · Engine Air Intake System > DURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Next page: https://openairdocs.org/deregistered/N15973-2017-01-05/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 = 'N15973' AND deregistration_id = 'N15973-2017-01-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15973-2017-01-05/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.