# Service difficulty reports: N12996, cancelled Dec 17, 2018 A list on [N12996, cancelled Dec 17, 2018](https://openairdocs.org/deregistered/N12996-2018-12-17.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 · 59 reports - [SDR ASOA20150828165](https://openairdocs.org/sdr/ASOA20150828165.md): Frame · corroded · Aug 28, 2015 · N12996 · Emb EMB145LR · Service Doors > DURING C-CHECK THE SERVICE DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5240-01102. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150828164V](https://openairdocs.org/sdr/ASOA20150828164V.md): Frame · corroded · Aug 28, 2015 · N12996 · Emb EMB145LR · Passenger/Crew Doors > DURING C-CHECK THE MAIN CABIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01036. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150828163](https://openairdocs.org/sdr/ASOA20150828163.md): Skin · cracked · Aug 28, 2015 · N12996 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND 5 FASTENER LOCATIONS BETWEEN FRAMES 77-78, STR 3R-6R. MAINTENANCE PERFORMED BUSHING REPAIRS IAW EC5330-03049. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150828162](https://openairdocs.org/sdr/ASOA20150828162.md): Fitting · cracked · Aug 28, 2015 · N12996 · Emb EMB145LR · Trailing Edge Flaps > DURING C-CHECK THE RT OTBD FLAP INBD ROLLER FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5750-01708. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150219014](https://openairdocs.org/sdr/ASOA20150219014.md): Engine · leaking · Feb 19, 2015 · N12996 · Emb EMB145LR · Engine (Turbine/Turboprop) > THE CREW REPORTED LAVATORY SMOKE WARNING MESSAGE AND SMOKE IN THE CABIN. MAINTENANCE REPLACED THE NR 2 ENGINE. OPS CHECKED WERE GOOD. - [SDR ASOA20150207009](https://openairdocs.org/sdr/ASOA20150207009.md): Smoke Detector · false indication · Feb 7, 2015 · N12996 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED A LAVATORY SMOKE WARNING INDICATION ON THE EICAS ON CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY SMOKE SENSOR. OPS CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE. - [SDR ASOA20141111091](https://openairdocs.org/sdr/ASOA20141111091.md): Smoke Detector · false activation · Nov 11, 2014 · N12996 · Emb EMB145LR · Smoke Detection > THE CREW REPORTED A MOMENTARY LAVATORY SMOKE MESSAGE DURING FLIGHT. MAINTENANCE INSPECTED AND R & R SMOKE DETECTOR. OPS CHECKS WERE GOOD. - [SDR ASOA20141021118](https://openairdocs.org/sdr/ASOA20141021118.md): Smoke Detector · false indication · Oct 21, 2014 · N12996 · Emb EMB145LR · Smoke Detection > PILOT REPORTED A LAVATORY SMOKE WARNING INDICATION ON EICAS WITH NO INDICATION OF SMOKE OR FIRE. MAINTENANCE INSPECTED LAVATORY FOR SMOKE AND EVIDENCE OF FIRE WITH NOTHING FOUND. MAINTENANCE ALSO PERFORMED OPS CHECK OF LAVATORY SMOKE DETECTOR SYS GOOD. ACFT - [SDR ASOA20140930121](https://openairdocs.org/sdr/ASOA20140930121.md): Smoke Warning · false activation · Sep 30, 2014 · N12996 · Emb EMB145LR · Smoke Detection > CREW REPORTED A LAVATORY SMOKE MESSAGE ON EICAS AFTER TAKE OFF. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, LAV WIRING WITH NO DEFECTS NOTED, R & R FOUR FLUORESCENT LIGHT BULBS AS A PRECAUTION AND THE ACFT WAS APPROVED FOR RETURN TO - [SDR ASOA20140916113](https://openairdocs.org/sdr/ASOA20140916113.md): Structure · damaged · Sep 16, 2014 · N12996 · Emb EMB145LR · Cargo/Baggage Doors > DURING 1A INSPECTION, A SMALL HOLE WAS FOUND IN THE CARGO DOOR LOWER FWD CORNER. MAINTENANCE PERFORMED AN INTERNAL DOUBLER REPAIR TO THE CARGO DOOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140608066](https://openairdocs.org/sdr/ASOA20140608066.md): Brake Assy · slipped · Jun 8, 2014 · N12996 · Emb EMB145LR · Landing Gear Brake System > PILOT REPORTED THE BRAKES SLIPPING ON LANDING AND VERY NOISE DURING SLOW TAXI. MX R & R 1 BRAKE ASSY OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE - [SDR ASOA20131114127](https://openairdocs.org/sdr/ASOA20131114127.md): Display · shorted · Nov 14, 2013 · N12996 · Emb EMB145LR · Attitude and Direction Data System > NR 2 PFD CIRCUIT BREAKER TRIPPED WITH BURNING ODOR IN COCKPIT. MAINTENANCE R & R THE NR 2 PFD, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130901218V](https://openairdocs.org/sdr/ASOA20130901218V.md): Bushing · migrated · Sep 1, 2013 · N12996 · Emb EMB145LR · Wing Main, Frame Structure > DURING C-CHECK, LT AILERON OTBD PCA ATTACHMENT FITTING OTBD LUG, OTBD HAT BUSHING MIGRATED. MX R & R THE LT AILERON OTBD PCA ATTACHMENT FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130622062R](https://openairdocs.org/sdr/ASOA20130622062R.md): Light · inoperative · Jun 22, 2013 · N12996 · Emb EMB145LR · Emergency Lighting > DURING SCHEDULED MX INSPECTION, THE CABIN FLOOR EMERGENCY LIGHTS AT ROW 6 AND 7 WERE INOPERATIVE. MX R & R THE FLOOR STRIP LIGHT WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH162](https://openairdocs.org/sdr/C2XA11SH162.md): Door Frame · corroded · Oct 25, 2011 · N12996 · Emb EMB145LR · Passenger/Crew Doors > SHV - DURING C-CHECK PAX DOOR FRAME LOWER SECTION HAS CORRODED NUT PLATE HOLES (NEAR DOOR SEAL). MAINTENANCE PERFORMED REPAIR AT PAX DOOR LOWER NUT PLATE AREAS IAW EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH161](https://openairdocs.org/sdr/C2XA11SH161.md): Skin · gouged · Oct 25, 2011 · N12996 · Emb EMB145LR · Cargo/Baggage Doors > SHV - DURING C-CHECK BAGGAGE DOOR INNER FRAME SKIN GOUGED AT LOWER, FWD AND CENTER AREAS. MAINTENANCE PERFORMED REPAIR ON BAGGAGE DOOR INNER SKIN IAW EC5230-01208. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH160](https://openairdocs.org/sdr/C2XA11SH160.md): Frame · corroded · Oct 25, 2011 · N12996 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK CORROSION PRESENT IN AREA WHERE THE SHUNT CONNECTION BAR COMES IN CONTACT WITH STRUCTURE. MAINTENANCE PERFORMED REPAIR AT APU SHUNT FRAME 80 IAW EC5310-01544 REV C, BONDING CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH159](https://openairdocs.org/sdr/C2XA11SH159.md): Floor Support · corroded · Oct 25, 2011 · N12996 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM SUPPORT FLANGE AT FRAME 21-25 NUT PLATE CORRODED. MAINTENANCE PERFORMED REPAIR AND INSTALLED FABRICATED DOUBLER AT LT OMEGA BEAM FLANGE BETWEEN FRAME 21-22 IAW EC5320-01257 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER - [SDR C2XA11SH158](https://openairdocs.org/sdr/C2XA11SH158.md): Skin · canning · Oct 25, 2011 · N12996 · Emb EMB145LR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK STRINGER 11 EXTERNAL FUSELAGE PATCH JUST AFT OF PAX DOOR IS OIL CANNING. MAINTENANCE PERFORMED REPAIR AT STRINGER 11L JUST AFT OF PAX DOOR IAW EC5330-02500, NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11IA085](https://openairdocs.org/sdr/C2XA11IA085.md): Computer · failed · May 7, 2011 · N12996 · Emb EMB145LR · Integrated Flight System > IAH - FLIGHT 2695, DURING TAKEOFF THE CREW REPORTED THAT THE NUMBER ONE AHRS COMPUTER FAILED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, - [SDR C2XA10CL107](https://openairdocs.org/sdr/C2XA10CL107.md): Electronic Unit · faulty · Jul 8, 2010 · N12996 · Emb EMB145 · Landing Gear Position and Warning > CLE FLT 2209 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LGEU. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10IA163](https://openairdocs.org/sdr/C2XA10IA163.md): O-Ring · leaking · May 28, 2010 · N12996 · Emb EMB145LR · Pneumatic Distribution System > IAH - FLIGHT 2948, THE CREW REPORTED A BLEED ONE LEAK IN CLIMB OUT THAT CLEARED UPON CLOSING BLEED ONE WITH NO APU. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED BLEED DUCT O-RING AT J - [SDR C2XA09SH503](https://openairdocs.org/sdr/C2XA09SH503.md): Floor Skin · corroded · Dec 17, 2009 · N12996 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK FUSELAGE FLOOR SKIN CORRODED (LEVEL 2 LOCAL) BETWEEN FRAMES 61-62 STRINGERS 21L-21R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN FRAMES 61-62 STRINGERS 21L-21R IAW EMB-145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO S - [SDR C2XA09SH490](https://openairdocs.org/sdr/C2XA09SH490.md): Frame · cracked · Dec 11, 2009 · N12996 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK, FR 10 CRACKED AT STR 10L. REMOVED AND REPLACED FRAME IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH473](https://openairdocs.org/sdr/C2XA09SH473.md): Frame · cracked · Dec 7, 2009 · N12996 · Emb EMB145LR · Fuselage Main, Frame > SHV - DURING C-CHECK RT HALF FRAME AT FRAME 10 IS CRACKED AT DV WINDOW. MAINTENANCE REMOVED AND REPLACED RT HALF FRAME AT FRAME 10 AT DV WINDOW. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH469](https://openairdocs.org/sdr/C2XA09SH469.md): Support · corroded · Dec 7, 2009 · N12996 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 46 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH468](https://openairdocs.org/sdr/C2XA09SH468.md): Support · corroded · Dec 7, 2009 · N12996 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 3 LOCAL) AT FRAME 50 ATTACHMENT. MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH467](https://openairdocs.org/sdr/C2XA09SH467.md): Support · corroded · Dec 7, 2009 · N12996 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 50 IAW EC5320-01512. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH466](https://openairdocs.org/sdr/C2XA09SH466.md): Support · corroded · Dec 7, 2009 · N12996 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT CORRODED (LEVEL 2 LOCAL) AT FRAME 46. MAINTENANCE REPAIRED RT UPPER SEAT TRACK SUPPORT AT FRAME 46 IAW EC5320-01512. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09RI187](https://openairdocs.org/sdr/C2XA09RI187.md): Sign · inoperative · Oct 30, 2009 · N12996 · Emb EMB145LR · Emergency Lighting > RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. MX REMOVED AND REPLACED EXIT SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09RI133](https://openairdocs.org/sdr/C2XA09RI133.md): Power Supply · not seated · Aug 3, 2009 · N12996 · Emb EMB145LR · Emergency Lighting > RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT WING AFTERWARD EMERGENCY LIGHT AND EMERGENCY LIGHT IN FRONT OF SEAT 3B INOPERATIVE. MX RESEATED NR 3 EMERGENCY LIGHT POWER PACK AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETUR - [SDR C2XA09RI054](https://openairdocs.org/sdr/C2XA09RI054.md): Battery · discharged · Mar 24, 2009 · N12996 · Emb EMB145LR · Emergency Lighting > EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT AT OVERWING CEILING INOPERATIVE. MX REMOVED AND REPLACED NR 3 BATTERY AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09RI053](https://openairdocs.org/sdr/C2XA09RI053.md): Battery · discharged · Mar 24, 2009 · N12996 · Emb EMB145LR · Emergency Lighting > EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY EXIT LIGHT ON AFT GALLEY WALL INOPERATIVE. MX REMOVED AND REPLACED NR 2 BATTERY AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09CL028](https://openairdocs.org/sdr/C2XA09CL028.md): Trim Switch · intermittent · Mar 12, 2009 · N12996 · Emb EMB145LR · Stabilizer Control System > CLE FLIGHT 2080 - THE CREW REPORTED THE PITCH TRIM WAS INOPERATIVE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS PITCH TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA09IA028](https://openairdocs.org/sdr/C2XA09IA028.md): Windshield · cracked · Jan 31, 2009 · N12996 · Emb EMB145LR · Flight Compartment Windows > OKC - FLIGHT 2205 - THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD CRACKED ON CLIMBOUT BLOCKING VISIBILITY. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD, OPERATIONALLY AND - [SDR C2XA09IA031](https://openairdocs.org/sdr/C2XA09IA031.md): Inverter · inoperative · Jan 24, 2009 · N12996 · Emb EMB145LR · Emergency Lighting > MCI - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING EMERGENCY EXIT MARKER LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC - [SDR C2XA08IA038](https://openairdocs.org/sdr/C2XA08IA038.md): Inverter · inoperative · Jan 23, 2008 · N12996 · Emb EMB145LR · Emergency Lighting > MCI - DURING MAINTENANCE INSPECTION THE FORWARD OVERWING CEILING EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RE - [SDR C2XA07BT024](https://openairdocs.org/sdr/C2XA07BT024.md): Connector · dirty · Mar 5, 2007 · N12996 · Emb EMB145LR · Light System Wiring > EWR LOG SQUAWK FLT 2347 FORWARD OVERHEAD EMERGENCY EXIT LOCATER SIGN AT ROW 11 OUT. CLEANED CONNECTOR AND RESECURED FORWARD EMERGENCY EXIT LOCATER AT ROW 11 IAW EMB145 AMM 33-50-13. OPS CHECK GOOD. CLOSED - [SDR C2XA05BT071](https://openairdocs.org/sdr/C2XA05BT071.md): Sign · faulty · Oct 7, 2005 · N12996 · Emb EMB145LR · Emergency Lighting > DURING SERVICE ROUTINE CHECK ON OVERNIGHT, MAINTENANCE FOUND ROW 12 OVERHEAD EMERGENCY EXIT SIGN NOT WORKING. REMOVED AND REPLACED ROW 12 OVERHEAD EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15, OPS CHECKED GOOD. - [SDR C2XA05CL046](https://openairdocs.org/sdr/C2XA05CL046.md): Warning Light · false activation · Jun 15, 2005 · N12996 · Emb EMB145LR · Smoke Detection > MHT FLIGHT 3054, THE CREW REPORTED A BAGGAGE COMPARTMENT SMOKE INDICATION ON THE EICAS THAT WOULD NOT CLEAR. MAINTENANCE INSPECTED AND RESET AIRCRAFT POWER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA04RI016](https://openairdocs.org/sdr/C2XA04RI016.md): Amplifier · failed · Nov 28, 2004 · N12996 · Emb EMB145LR · Interphone/Passenger Announcement (PA) System > ORF - FLT 2017, DURING PREFLIGHT CHECK THE CREW FOUND CABIN AND CABIN EMERGENCY LIGHTS IN OVERHEAD PANEL ILLUMINATED AND CABIN INTERPHONE AND PA INOP. MAINTENANCE REMOVED AND REPLACED PA AMP. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED - [SDR C2XA04CL061](https://openairdocs.org/sdr/C2XA04CL061.md): Light · inoperative · Jun 4, 2004 · N12996 · Emb EMB145LR · Emergency Lighting > CLE FLIGHT 2266, THE CREW REPORTED THAT THE SECOND TO AFT EMERGENCY LIGHT STRIP WAS INOP WHEN TESTED. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LIGHT STRIP. ALL OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA04CL018](https://openairdocs.org/sdr/C2XA04CL018.md): Trim System · malfunctioned · Mar 7, 2004 · N12996 · Emb EMB145LR · Aileron Tab Control System > IAH FLIGHT 2390 CREW REPORTED, ROLL TRIM RUN-AWAY AFTER TAKEOFF FROM IAH. CREW FOLLOWED QRH AND RESET CIRCUIT BREAKER FOR AILERON TRIM. SYSTEM OPS CHECKED GOOD. CREW CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM WITH NO DEFECTS - [SDR CX2A04SH012](https://openairdocs.org/sdr/CX2A04SH012.md): Angle · chafed · Jan 9, 2004 · N12996 · Emb EMB145LR · Engine Cowling System > SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH006](https://openairdocs.org/sdr/C2XA04SH006.md): Buttstrap · corroded · Jan 4, 2004 · N12996 · Emb EMB145LR · Fuselage Main, Structure > SHV- DURING C-CHECK THE FWD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH005](https://openairdocs.org/sdr/C2XA04SH005.md): Buttstrap · corroded · Jan 4, 2004 · N12996 · Emb EMB145LR · Fuselage Main, Structure > SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 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 C2XA04SH004](https://openairdocs.org/sdr/C2XA04SH004.md): Stiffener · chafed · Jan 4, 2004 · N12996 · Emb EMB145LR · Nacelle/Pylon Miscellaneous Structure > SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH526](https://openairdocs.org/sdr/C2XA03SH526.md): Rib · gouged · Dec 31, 2003 · N12996 · Emb EMB145LR · Nacelle/Pylon, Frame/Spar/Rib > DURING C CHECK THE AFT EDGE MEMBER WAS FOUND TO BE GOUGED AT THE SIX O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03SH524](https://openairdocs.org/sdr/C2XA03SH524.md): Beam · corroded · Dec 30, 2003 · N12996 · Emb EMB145LR · Fuselage Main, Structure > SHV-DURING C-CHECK THE LOWER CARGO DOOR CUT OUT 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 C2XA03SH523](https://openairdocs.org/sdr/C2XA03SH523.md): Floorbeam · corroded · Dec 30, 2003 · N12996 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Next page: https://openairdocs.org/deregistered/N12996-2018-12-17/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 = 'N12996' AND deregistration_id = 'N12996-2018-12-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N12996-2018-12-17/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.