# Service difficulty reports: N16944, cancelled Dec 16, 2015 A list on [N16944, cancelled Dec 16, 2015](https://openairdocs.org/deregistered/N16944-2015-12-16.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 · 99 reports - [SDR ASOA20140122013](https://openairdocs.org/sdr/ASOA20140122013.md): Fan · failed · Jan 22, 2014 · N16944 · Emb EMB145EP · Air Distribution Fan > THE CREW REPORTED A STRONG ELECTRICAL ODOR AT TURNED TO FINAL. LANDED WITHOUT INCIDENT, MAINTENANCE R & R THE NR 1 RECIRCULATION FAN, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131001182](https://openairdocs.org/sdr/ASOA20131001182.md): Light · shorted · Oct 1, 2013 · N16944 · Emb EMB145EP · Flight Compartment Lighting > CREW REPORTED COCKPIT READING LIGHT CIRCUIT BREAKER TRIPPED WITH A BURNING ODOR. MX INSPECTED AND R & R F/O'S READING LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130615089](https://openairdocs.org/sdr/ASOA20130615089.md): Control Module · overheated · Jun 15, 2013 · N16944 · Emb EMB145EP · Passenger Compartment Lighting > THE CREW REPORTED A PLASTIC ODOR FROM THE CABIN DOOR ENTRYWAY. MX VERIFIED THE ODOR TO BE COMING FROM THE F/A CABIN LIGHT CONTROL MODULE, DEACTIVATED THE MODULE AND PLACED ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MX R & R THE AFFECTED CABIN L - [SDR ASOA20130423156](https://openairdocs.org/sdr/ASOA20130423156.md): Skin · corroded · May 12, 2013 · N16944 · Emb EMB145ER · Fuselage Main, Plate/Skin > DURING C-CHECK, THE CENTER FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-15 AND STRINGERS 19R-20L. MX R & R THE SKIN IAW EC5330-02761. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130423153](https://openairdocs.org/sdr/ASOA20130423153.md): Frame · cracked · May 11, 2013 · N16944 · Emb EMB145ER · Fuselage Main, Frame > DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE PILOTS DV WINDOW AT STRINGER 9L. MX R & R THE CRACKED FRAME SECTION IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20121017133](https://openairdocs.org/sdr/ASOA20121017133.md): Seal · loose · Oct 17, 2012 · N16944 · Emb EMB145EP · Cargo/Baggage Doors > THE CREW REPORTED A RAPID DEPRESSURIZATION (>3000FPM) WHILE CLIMBING THROUGH 21,000' AND THAT THEY COULD NOT RECOVER PRESSURIZATION. THE CREW PERFORMED AN EMERGENCY DECENT AND LEVELED OFF AT 10,000'. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCI - [SDR C2XA11IA254](https://openairdocs.org/sdr/C2XA11IA254.md): Battery Pack · loose · Nov 8, 2011 · N16944 · Emb EMB145EP · Emergency Lighting > FLIGHT 4641, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 8-12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE EMERGENCY LIGHT BATTERY AT ROW 12A, OPERATIONALLY TESTED WITH NO DEFECT - [SDR C2XA11IA200](https://openairdocs.org/sdr/C2XA11IA200.md): Unknown · odor · Sep 4, 2011 · N16944 · Emb EMB145EP · Air Distribution System > IAH - THE CREW REPORTED A BURNING SMELL IN THE LAV THAT SEEMED TO BE AROUND THE LIGHT. MAINTENANCE INSPECTED THE LAV ARE, AND COULD NOT DUPLICATE THE SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH020](https://openairdocs.org/sdr/C2XA11SH020.md): Skin · cracked · Jan 13, 2011 · N16944 · Emb EMB145EP · Wing, Plate/Skin > SHV - DURING C-CHECK LT WING SKIN HAS CRACK JUST FWD OF GROUND SPOILER CTR HINGE POINT. REPAIRED SKIN IAW EC5740-01276. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH021](https://openairdocs.org/sdr/C2XA11SH021.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH019](https://openairdocs.org/sdr/C2XA11SH019.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 30-35. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH018](https://openairdocs.org/sdr/C2XA11SH018.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · 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 C2XA11SH017](https://openairdocs.org/sdr/C2XA11SH017.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH016](https://openairdocs.org/sdr/C2XA11SH016.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - LT 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 C2XA11SH015](https://openairdocs.org/sdr/C2XA11SH015.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · 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 C2XA11SH014](https://openairdocs.org/sdr/C2XA11SH014.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 24-29. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH013](https://openairdocs.org/sdr/C2XA11SH013.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH012](https://openairdocs.org/sdr/C2XA11SH012.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · 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 C2XA11SH011](https://openairdocs.org/sdr/C2XA11SH011.md): Floor Support · corroded · Jan 13, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH010](https://openairdocs.org/sdr/C2XA11SH010.md): Floor Support · corroded · Jan 12, 2011 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 58. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH009](https://openairdocs.org/sdr/C2XA11SH009.md): Skin · cracked · Jan 11, 2011 · N16944 · Emb EMB145EP · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK RT SKIN CRACKED AT FR 75 STR 2R. REPAIRED SKIN IAW EC5330-02340. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH008](https://openairdocs.org/sdr/C2XA11SH008.md): Skin · cracked · Jan 11, 2011 · N16944 · Emb EMB145EP · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 4R TO 7R. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH007](https://openairdocs.org/sdr/C2XA11SH007.md): Skin · cracked · Jan 11, 2011 · N16944 · Emb EMB145EP · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 3L TO 6L. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH445](https://openairdocs.org/sdr/C2XA10SH445.md): Floor Support · corroded · Dec 29, 2010 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA338](https://openairdocs.org/sdr/C2XA10IA338.md): Jack · disconnected · Dec 19, 2010 · N16944 · Emb EMB145EP · Audio Integrating System > IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS BOOM MIC JACK, HAND MIC JACK, RECONNECTE - [SDR C2XA10IA337](https://openairdocs.org/sdr/C2XA10IA337.md): Jack · inoperative · Dec 19, 2010 · N16944 · Emb EMB145EP · Audio Integrating System > IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS BOOM MIC JACK, HAND MIC JACK, RECONNECTE - [SDR C2XA10IA335](https://openairdocs.org/sdr/C2XA10IA335.md): Light · overheated · Dec 18, 2010 · N16944 · Emb EMB145EP · Passenger Compartment Lighting > IAH - FLIGHT 2304 A BURNING SMELL WAS NOTICED IN THE CABIN AT ROW 5. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY AT ROW 5A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA240](https://openairdocs.org/sdr/C2XA10IA240.md): Battery Pack · discharged · Aug 30, 2010 · N16944 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2935, DURING POST-FLIGHT INSPECTION THE CREW REPORTED SOME EXIT ROW FLOOR LIGHTING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO - [SDR C2XA10IA220](https://openairdocs.org/sdr/C2XA10IA220.md): Display · malfunctioned · Aug 9, 2010 · N16944 · Emb EMB145EP · Central Display > CRP - FLIGHT 2096, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE NR 2 PFD WENT BLANK AND SMOKED. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AN - [SDR C2XA10IA108](https://openairdocs.org/sdr/C2XA10IA108.md): Skin · cracked · Mar 25, 2010 · N16944 · Emb EMB145EP · Fuselage Main, Plate/Skin > CRP - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RET - [SDR C2XA10IA039](https://openairdocs.org/sdr/C2XA10IA039.md): Duct · defective · Jan 25, 2010 · N16944 · Emb EMB145EP · Air Distribution System > IAH - FLIGHT 2569, THE CREW REPORTED THAT THE PACK TWO VALVE CLOSED ON CLIMBOUT WITH NO PRESSURIZATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE PACK 2 EXHAUST DUCT, OPERAT - [SDR C2XA10IA034](https://openairdocs.org/sdr/C2XA10IA034.md): Clamp · loose · Jan 22, 2010 · N16944 · Emb EMB145EP · Pneumatic Distribution System > IAH - FLIGHT 2165, THE CREW REPORTED THAT THE BLEED 1 VALVE CLOSED FROM T/O TO 10'000 FEET. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED SEVERAL CLAMPS, OPERATIONAL AND LEAK CHECKS WERE ACC - [SDR C2XA10IA033](https://openairdocs.org/sdr/C2XA10IA033.md): Clamp · loose · Jan 22, 2010 · N16944 · Emb EMB145EP · Air Distribution System > IAH - FLIGHT 2165, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED TWICE DURING CLIMB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, RE-SECURED SEVERAL CLAMPS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP - [SDR C2XA10IA018](https://openairdocs.org/sdr/C2XA10IA018.md): Precooler · leaking · Jan 15, 2010 · N16944 · Emb EMB145EP · Pneumatic Distribution System > IAH - FLIGHT 2617, THE CREW REPORTED A BLEED ONE LEAK MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PRECOOLER, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT - [SDR C2XA10IA013](https://openairdocs.org/sdr/C2XA10IA013.md): Landing Gear · low · Jan 11, 2010 · N16944 · Emb EMB145EP · Nose/Tail Landing Gear Strut/Axle > IAH - FLIGHT 2413, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE AFTER TAKEOFF WITH A THRUST REVERSER DISAGREE EICAS MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NOSE - [SDR C2XA09IA185](https://openairdocs.org/sdr/C2XA09IA185.md): Metering Unit · malfunctioned · Jul 20, 2009 · N16944 · Emb EMB145EP · Fuel Controlling System > MFE - FLIGHT 2627, THE CREW REPORTED THAT E2 WOULD NOT ADVANCE 85 PERCENT N2 OR 90 PERCENT N1 AND ITT WAS SPIKING ERRONEOUSLY BETWEEN 300-500 DEGREES, WITH AN EICAS CHECK MESSAGE ON MFD WITH BOTH IGNITERS ON FOR E2. THE ISSUE RESOLVED ITSELF AFTER TWO MINUTES - [SDR C2XA08IA225](https://openairdocs.org/sdr/C2XA08IA225.md): Battery · discharged · Oct 13, 2008 · N16944 · Emb EMB145EP · Emergency Lighting > IAH DURING A CHECK INSPECTION THE AFT 3 AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2X2008F00002](https://openairdocs.org/sdr/C2X2008F00002.md): Battery · discharged · Jun 8, 2008 · N16944 · Emb EMB145EP · Emergency Lighting > EMERGENCY LIGHTING OVERHEAD AND FLOOR BY EMERGENCY EXITS ARE DIM. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. (S) - [SDR C2XA07TY034](https://openairdocs.org/sdr/C2XA07TY034.md): Skin · crushed · Jul 5, 2007 · N16944 · Emb EMB145EP · Fuselage Main, Plate/Skin > TYS - AIRCRAFT SUFFERED GROUND DAMAGE FROM A BAGGAGE CART TO THE FUSELAGE UNDER WINDOWS 4 AND 5. MAINTENANCE REMOVED AND REPLACED STRINGERS 11L, 12L AND FRAME 27 AND 2 SHEAR CLIPS ON FRAME 29 AND 30. REPLACED SKIN PANEL FROM FRAME 23 TO FRAME 36. ALSO, REPL - [SDR C2XA06BT048](https://openairdocs.org/sdr/C2XA06BT048.md): Lamp · failed · Nov 1, 2006 · N16944 · Emb EMB145EP · Passenger Compartment Lighting > EWR LOG SQUAWK ELECTRICAL SMOKE ODOR IN THE CABIN. FOUND TO BE FORWARD SIDEWALL LIGHT ON SEAT 1A. MEL'D. LATER RE-LAMPED LIGHT AT SEAT 1A 2A IAW EMB145 AMM 33-21-01. OPS CHECK GOOD. - [SDR C2XA06TY011](https://openairdocs.org/sdr/C2XA06TY011.md): Floor Support · corroded · Feb 22, 2006 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > TYS - DURING A ROUTINE C-CHECK INSPECTION THE RIGHT SIDE OMEGA BEAM IN THE GALLEY WAS CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGE AREA AND FABRICATED A NEW PART AND INSTALL DOUBLER IAW EC5320-01291. ALL WORK WAS ACCOMPLISHED AND A/C WILL BE RELEASED - [SDR C2XA06TY010](https://openairdocs.org/sdr/C2XA06TY010.md): Shear Plate · corroded · Feb 21, 2006 · N16944 · Emb EMB145EP · Fuselage Miscellaneous Structure > TYS - DURING A SCHEDULE 2C INSPECTION CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT ON LOWER SILL AT STR 16L AT FR 65. MAINTENANCE BLENDED ALL SIGNS OF CORROSION, CUT OUT DAMAGE SECTION, FABRICATED A SPLICE AND CUT A NEW SECTION OF SHEAR CLIP. INSTALLED SPLIC - [SDR C2XA05TY007](https://openairdocs.org/sdr/C2XA05TY007.md): Bearing · worn · Jan 24, 2005 · N16944 · Emb EMB145ER · Vertical Stabilizer > TYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VERTICAL BEARING HOUSING AND INSTALL NEW BUSHINGS IAW EC5510-01108. ALL WORK WAS ACCOMPLISHED AND O - [SDR C2XA03SH474](https://openairdocs.org/sdr/C2XA03SH474.md): Angle · corroded · Nov 23, 2003 · N16944 · Emb EMB145ER · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 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 C2XA03SH473](https://openairdocs.org/sdr/C2XA03SH473.md): Threshold · corroded · Nov 23, 2003 · N16944 · Emb EMB145ER · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH472](https://openairdocs.org/sdr/C2XA03SH472.md): Buttstrap · corroded · Nov 23, 2003 · N16944 · Emb EMB145ER · Fuselage Miscellaneous Structure > SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 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 C2XA03SH467](https://openairdocs.org/sdr/C2XA03SH467.md): Structure · gouged · Nov 19, 2003 · N16944 · Emb EMB145ER · Engine Cowling System > SHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH466](https://openairdocs.org/sdr/C2XA03SH466.md): Structure · gouged · Nov 19, 2003 · N16944 · Emb EMB145ER · Engine Cowling System > SHV-DURING C-CHECK THE RIGHT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH465](https://openairdocs.org/sdr/C2XA03SH465.md): Buttstrap · corroded · Nov 19, 2003 · N16944 · Emb EMB145ER · Fuselage Miscellaneous Structure > SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE LEFT OMEGA BEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH464](https://openairdocs.org/sdr/C2XA03SH464.md): Floorbeam · corroded · Nov 19, 2003 · N16944 · Emb EMB145ER · Fuselage Main, Floor Beam > SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Next page: https://openairdocs.org/deregistered/N16944-2015-12-16/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 = 'N16944' AND deregistration_id = 'N16944-2015-12-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16944-2015-12-16/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.