# Service difficulty reports: N16927, cancelled Sep 6, 2019 A list on [N16927, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N16927-2019-09-06.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 · 118 reports - [SDR V0XD2014062192732](https://openairdocs.org/sdr/V0XD2014062192732.md): Seal · deteriorated · Jun 20, 2014 · N16927 · Emb EMB145EP · Fluid Service Doors > AFT MAINTENANCE DOOR PANEL 312AR SEAL DETERIORATED. R & R WITH SERVICEABLE SEAL IAW AMM 52-44-02, - [SDR V0XD2014062192731](https://openairdocs.org/sdr/V0XD2014062192731.md): Tube · damaged · Jun 20, 2014 · N16927 · Emb EMB145EP · Cabin Cooling System > TUBE ASSY FORWARD OF RT PACK VALVE MISSING PART IF INSULATION. REPLACED DAMAGED TUBE ASSY WITH INSULATION WITH SERVICEABLE TUBE ASSY WITH INSULATION PN: 145-27547-409, IAW AMM 36-11-09 AND 21-51-01, WO 80232, WC 1265. - [SDR V0XD2014062192730](https://openairdocs.org/sdr/V0XD2014062192730.md): Gasket · damaged · Jun 20, 2014 · N16927 · Emb EMB145EP · Wing Main, Frame Structure > RT UNDERWING FUEL PANEL 631CB HAS DAMAGED MESH GASKET. REPLACED MESH GASKET WITH SERVICEABLE GASKET PN:15-20060 IAW AMM28-11-01, WO 80232, WC 6018. - [SDR V0XD2014062192729](https://openairdocs.org/sdr/V0XD2014062192729.md): Tank · cracked · Jun 20, 2014 · N16927 · Emb EMB145EP · Aircraft Fuel System > FUEL PROBE HAS CRACKED HOUSING. R & R TANK UNITS - [SDR V0XD2014062192733](https://openairdocs.org/sdr/V0XD2014062192733.md): Attach Bracket · worn · Jun 19, 2014 · N16927 · Emb EMB145EP · APU Cowling/Containment > LOWER RT APU COWLING MOUNTING ATTACH POINT WILL NOT ACCEPT FASTENER. R & R APU COWLING MOUNTING, BRACKET, ATTACH POINTS IAW SRM 51-40-00. - [SDR V0XD2014062192728](https://openairdocs.org/sdr/V0XD2014062192728.md): Pushrod · corroded · Jun 19, 2014 · N16927 · Emb EMB145EP · Elevator Control System > SPRING TAB PUSH ROD CORRODED. R & R PUSH ROD IAW AMM27-31-08. - [SDR V0XD2014061492727](https://openairdocs.org/sdr/V0XD2014061492727.md): Floor Support · corroded · Jun 12, 2014 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > LEFT OMEGA BEAM AT FRAME 54 UNDERNEATH CENTER AISLE CROSSBEAM HAS A CORROSION HOLE. REPAIRED OMEGA BEAM IAW SRM 53-00-10. - [SDR V0XD2014061492726](https://openairdocs.org/sdr/V0XD2014061492726.md): Floorbeam · cracked · Jun 12, 2014 · N16927 · Emb EMB145EP · Fuselage Main, Floor Beam > FLOORBEAM TEE CRACKED AT RT SIDE JUST AFT OF LAV. R & R FLOORBEAM TEE IAW SRM 51-40-02. - [SDR V0XD2014061492725](https://openairdocs.org/sdr/V0XD2014061492725.md): Floor Support · corroded · Jun 12, 2014 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > RIGHT FLOOR SUPPORT AT FRAME 24 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02. - [SDR V0XD2014061092724](https://openairdocs.org/sdr/V0XD2014061092724.md): Floor Support · corroded · Jun 6, 2014 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > LT OMEGA BEAM AT FRAME 20 UNDERNEATH CENTER AISLE CROSSBEAM HAS HEAVY CORROSION. REPAIRED OMEGA BEAM IAW SRM 53-00-10 & CPM 51-21-04. - [SDR V0XD2014061092723](https://openairdocs.org/sdr/V0XD2014061092723.md): Floor Support · corroded · Jun 6, 2014 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > RT FLOOR SUPPORT CORRODED OUT OF LIMIT AT FRAMES 35 TO 38. R & R FLOOR SUPPORT IAW SRM 51-40-02. - [SDR ASOA20140401055](https://openairdocs.org/sdr/ASOA20140401055.md): Sign · inoperative · Apr 1, 2014 · N16927 · Emb EMB145EP · Emergency Lighting > DURING 4A INSPECTION THE EMERGENCY EXIT SIGN AT SEAT 18A WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140330052](https://openairdocs.org/sdr/ASOA20140330052.md): Skin · cracked · Mar 30, 2014 · N16927 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING MAINTENANCE INSPECTION, THE TEE POST BETWEEN THE F/O'S WINDSHIELD AND DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER/FILLER REPAIR IAW DISPOSITION ETD2014-145-026772 AND THE ACFT WAS APPROVED FOR RETURN TO SER - [SDR ASOA20130701095](https://openairdocs.org/sdr/ASOA20130701095.md): Sign · inoperative · Jul 1, 2013 · N16927 · Emb EMB145EP · Emergency Lighting > DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT (SIGN) WAS NOT ILLUMINATING. MX INSPECTED THE ACFT, R & R THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130518079](https://openairdocs.org/sdr/ASOA20130518079.md): Skin · cracked · May 18, 2013 · N16927 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED BELOW STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETUR - [SDR ASOA20130518078](https://openairdocs.org/sdr/ASOA20130518078.md): Skin · cracked · May 18, 2013 · N16927 · Emb EMB145EP · Fuselage Main, Plate/Skin > DURING 5A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED ABOVE STR 2R AT FR 75. MX REMOVED THE DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RE - [SDR ASOA20130327044](https://openairdocs.org/sdr/ASOA20130327044.md): Light · unknown · Mar 27, 2013 · N16927 · Emb EMB145EP · Emergency Lighting > DURING `A` CHECK INSPECTION, EMERGENCY LIGHT AT 12C WAS FOUND TO BE INOPERATIVE. MX PERFORMED OPS CHECKS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130327043](https://openairdocs.org/sdr/ASOA20130327043.md): Light · inoperative · Mar 27, 2013 · N16927 · Emb EMB145EP · Emergency Lighting > DURING `A` CHECK INSPECTION, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130211014H](https://openairdocs.org/sdr/ASOA20130211014H.md): Lamp · burned · Feb 11, 2013 · N16927 · Emb EMB145EP · Emergency Lighting > THE CREW REPORTED THAT DURING LANDING, A BURNING ODOR AND LIGHT LAYER OF SMOKE WAS NOTED IN THE CABIN. THE SMOKE DISSIPATED AFTER LANDING, HOWEVER THE ODOR REMAINED. THE ACFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT WHERE MX FOUND 2 LATERAL LIGHTS TO BE B - [SDR ASOA201212226001](https://openairdocs.org/sdr/ASOA201212226001.md): Pressure Switch · inoperative · Dec 26, 2012 · N16927 · Emb EMB145EP · Landing Gear Brake System > THE CREW REPORTED BRAKE DEGRADE ON LANDING WITH VERY LITTLE BRAKE PRESSURE, ALSO HAD CMC MESSAGE BRAKE WHEEL SPEED TRANSDUCER 3 FAIL OCCURRED 3 TIMES. THE ACFT LANDED WITHOUT INCIDENT AND MX INSPECTED THE ACFT AND PLACED IT ON MEL 32-41-08, AND THE ACFT WAS A - [SDR ASOA20120921124](https://openairdocs.org/sdr/ASOA20120921124.md): Inverter · inoperative · Sep 21, 2012 · N16927 · Emb EMB145EP · Emergency Lighting > DURING MX INSPECTION THE AISLE PATH LIGHT AT ROWS 3 THRU 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120914121H](https://openairdocs.org/sdr/ASOA20120914121H.md): Wire · broken · Sep 14, 2012 · N16927 · Emb EMB145EP · Light System Wiring > DURING MX INSPECTION, THE AISLE PATH LIGHT STRIP AT ROW 10-11 WAS FOUND INOPERATIVE. MX INSPECTED THE ACFT AND REPAIRED THE WIRE ON THE LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120809107](https://openairdocs.org/sdr/ASOA20120809107.md): Light · broken · Aug 9, 2012 · N16927 · Emb EMB145EP · Emergency Lighting > DURING MX INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND TO HAVE THE BULB OUT OF ITS SOCKET. MX R & R THE LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120406057](https://openairdocs.org/sdr/ASOA20120406057.md): Inverter · inoperative · Apr 6, 2012 · N16927 · Emb EMB145EP · Emergency Lighting > DURING MX INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120401052](https://openairdocs.org/sdr/ASOA20120401052.md): Solenoid Valve · inoperative · Apr 1, 2012 · N16927 · Emb EMB145EP · Landing Gear Retraction/Extension System > AFTER TAKEOFF, CREW REPORTED THAT AFTER RETRACTING THE LANDING GEAR, HEARD SEVERAL LOUD BANGS FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. INSPECTED ACFT AND FOUND THE NLG DOORS HAD CLOSED WHILE N - [SDR ASOA20120318039](https://openairdocs.org/sdr/ASOA20120318039.md): Control Lever · inoperative · Mar 18, 2012 · N16927 · Emb EMB145EP · Landing Gear Selector > THE CREW REPORTED THAT THE NLG DOOR OPENED IN FLIGHT. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE LANDING GEAR CONTROL LEVER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20111214015](https://openairdocs.org/sdr/ASOA20111214015.md): Relay · faulted · Dec 14, 2011 · N16927 · Emb EMB145EP · Engine (Turbine/Turboprop) > CREW REPORTED DURING CLIMB OUT AT 3000 FT, THERE WAS A TEMPORARY LOSS OF POWER ON NR 1 ENGINE, N1 APPROX 70 PERCENT. A FEW MINUTES LATER, A SECOND LOSS OF POWER ON NR 1 ENGINE, THIS TIME TO APPROX 60 PERCENT N1. BOTH TIMES THRUST LEVERS WERE IN CLIMB DETENT - [SDR ASOA201112141001](https://openairdocs.org/sdr/ASOA201112141001.md): Relay · faulted · Dec 14, 2011 · N16927 · Emb EMB145EP · Engine (Turbine/Turboprop) > THE CREW REPORTED THAT DURING CLIMB OUT AT 3000 FEET THERE WAS A TEMPORARY LOSS OF POWER ON ENG NR 1, N1 APPROX 70%. A FEW MINUTES LATER, A SECOND LOSS OF POWER ON ENGINE NR 1, THIS TIME TO APPROX 60% N1. BOTH TIMES THRUST LEVERS WERE IN THE DETENT / CLIMB SET - [SDR ASOA201111231005](https://openairdocs.org/sdr/ASOA201111231005.md): Fadec · failed · Nov 23, 2011 · N16927 · Emb EMB145EP · Fuel Controlling System > THE CREW REPORTED THAT AFTER ROTATION THE ACFT YAWED AND THE F/O CALLED POWER LOSS. THE POWER LEVERS WERE PUSHED FULL FORWARD AND THE N1 ON THE LT ENGINE WAS AROUND REMAINED AROUND 24 PERCENT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT WHERE M - [SDR C2XA11IA081](https://openairdocs.org/sdr/C2XA11IA081.md): Acm · seized · May 3, 2011 · N16927 · Emb EMB145EP · Cabin Cooling System > XNA - FLIGHT 3099, THE CREW REPORTED A BURNING SMELL AND SMOKE FROM THE LEFT COCKPIT VENT AT THE WINDOW WITH A PACK 1 OVERHEAT MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WHERE PACK TWO WAS CHECKED USING BOTH ENGINES WITH NO DEFECTS, AND PACK ONE WAS PLACED ON - [SDR C2XA10IA341](https://openairdocs.org/sdr/C2XA10IA341.md): Power Supply · inoperative · Dec 22, 2010 · N16927 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRC - [SDR C2XA10IA340](https://openairdocs.org/sdr/C2XA10IA340.md): Battery Pack · discharged · Dec 22, 2010 · N16927 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 2779, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHTING BEHIND ROW 12 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRC - [SDR C2XA10IA323](https://openairdocs.org/sdr/C2XA10IA323.md): Ballast · overheated · Dec 6, 2010 · N16927 · Emb EMB145EP · Passenger Compartment Lighting > FLIGHT 2634, A PASSENGER AND F/A NOTICED AN ELECTRICAL BURNING ODOR IN MID CABIN DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT BALLAST AT ROW 10 ON MEL, AND THE AIRCRAFT WAS A - [SDR C2XA10IA322](https://openairdocs.org/sdr/C2XA10IA322.md): Ballast · overheated · Dec 6, 2010 · N16927 · Emb EMB145EP · Passenger Compartment Lighting > DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR AT SEAT 6A. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT AT SEAT 6A ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE CABIN L - [SDR C2XA10IA317](https://openairdocs.org/sdr/C2XA10IA317.md): Light · overheated · Nov 30, 2010 · N16927 · Emb EMB145EP · Passenger Compartment Lighting > TUL - FLIGHT 2972, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A SMOKE SMELL AND FLICKERING CABIN LIGHTING. MAINTENANCE INSPECTED THE LIGHTING AND PLACED THE LIGHT AT SEAT 7A ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 12/01/10 IAH MAI - [SDR C2XA10SH249](https://openairdocs.org/sdr/C2XA10SH249.md): Battery · overtemp · Jul 25, 2010 · N16927 · Emb EMB145EP · Battery/Charger System > LEFT BATTERY NR 2 OVERTEMP. REMOVED AND REPLACED NR 2 BATTERY IAW EMB 145 AMM 24-36-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA135](https://openairdocs.org/sdr/C2XA10IA135.md): Skin Panel · cracked · Apr 26, 2010 · N16927 · Emb EMB145EP · Fuselage Main, Plate/Skin > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BETWEEN THE CAPTAINS DV WINDOW AND WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO S - [SDR C2XA10IA090](https://openairdocs.org/sdr/C2XA10IA090.md): Unknown · odor · Mar 7, 2010 · N16927 · Emb EMB145EP · Air Distribution System > IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, GROUND RAN BOTH - [SDR C2XA100IA088](https://openairdocs.org/sdr/C2XA100IA088.md): Unknown · odor · Mar 7, 2010 · N16927 · Emb EMB145EP · Air Distribution System > IAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, AND GROUND RAN B - [SDR C2XA09IA284](https://openairdocs.org/sdr/C2XA09IA284.md): Light · inoperative · Nov 6, 2009 · N16927 · Emb EMB145EP · Emergency Lighting > IAH - FLIGHT 3020, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE NUMBER FIVE AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETUR - [SDR C2XA09SH280](https://openairdocs.org/sdr/C2XA09SH280.md): Floor Support · corroded · Aug 5, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM IAW EC 5320-01467. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH261](https://openairdocs.org/sdr/C2XA09SH261.md): Battery · discharged · Aug 3, 2009 · N16927 · Emb EMB145EP · Emergency Lighting > SHV - DURING C-CHECK PROXIMITY LIGHT 3 AND 4 FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY IAW EMB-145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH260](https://openairdocs.org/sdr/C2XA09SH260.md): Hinge · worn · Aug 3, 2009 · N16927 · Emb EMB145EP · Passenger/Crew Doors > SHV - DURING C-CHECK MAIN DOOR LOWER HINGE LOCK PIN HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED MAIN DOOR LOWER HINGE IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH259](https://openairdocs.org/sdr/C2XA09SH259.md): Hinge · worn · Aug 3, 2009 · N16927 · Emb EMB145EP · Ailerons > SHV - DURING C-CHECK LT AILERON OUTBOARD HINGE POINT HAS MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE POINT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH258](https://openairdocs.org/sdr/C2XA09SH258.md): Floor Support · corroded · Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAME 17-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH257](https://openairdocs.org/sdr/C2XA09SH257.md): Support Bracket · cracked · Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK FRAME 10 SUPPORT BRACKET CRACKED JUST UNDER LEFT DV WINDOW LOWER CUTOUT FRAME. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAME 10 LT IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH256](https://openairdocs.org/sdr/C2XA09SH256.md): Channel · cracked · Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK FRAME 10 CRACKED AT STRINGER 13L. MAINTENANCE REMOVED AND REPLACED CHANNEL AT FRAME 10 STRINGER 13L IAW EMB-145 SRM 51-40-02 AND CPM 51-21-05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH255](https://openairdocs.org/sdr/C2XA09SH255.md): Doubler · corroded · Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK RT DOUBLER AT FRAME 61 CORRODED (LEVEL 2 LOCAL) AT RIVET HOLES (BEHIND CARBON CROSS BEAM). MAINTENANCE REMOVED AND REPLACED RT DOUBLER AT FRAME 61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH254](https://openairdocs.org/sdr/C2XA09SH254.md): Buttstrap · corroded · Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) FRAME 46-53. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM BUTTSTRAP FRAME 46-53 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH253](https://openairdocs.org/sdr/C2XA09SH253.md): Fitting · cracked · Aug 3, 2009 · N16927 · Emb EMB145EP · Wing Miscellaneous Structure > SHV - DURING C-CHECK LEFT O/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT O/B LEADING EDGE SPLICE SHEAR CLIP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Next page: https://openairdocs.org/deregistered/N16927-2019-09-06/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 = 'N16927' AND deregistration_id = 'N16927-2019-09-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16927-2019-09-06/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.