# Service difficulty reports: N12705, cancelled Jul 23, 1999 A list on [N12705, cancelled Jul 23, 1999](https://openairdocs.org/deregistered/N12705-1999-07-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR C2XA98IA027](https://openairdocs.org/sdr/C2XA98IA027.md): Skin · cracked · Feb 13, 1998 · N12705 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL 622DB. MAINTENANCE INSTALLED A DOUBLER REPAIR IAW EMB-120 SRM CHAPTER 57-20-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA026](https://openairdocs.org/sdr/C2XA98IA026.md): Support · cracked · Feb 13, 1998 · N12705 · Emb EMB120RT · Trailing Edge Flaps > IAH - DURING C-CHECK INSPECTION, THE FORWARD MIDDLE SKIN SUPPORT ON THE RIGHT NACELLE FLAP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM CHAPTER 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA025](https://openairdocs.org/sdr/C2XA98IA025.md): Support · cracked · Feb 13, 1998 · N12705 · Emb EMB120RT · Trailing Edge Flaps > IAH - DURING C-CHECK INSPECTION, THE MIDDLE FORWARD SKIN SUPPORT ON THE LEFT NACELLE FLAP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM CHAPTER 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA024](https://openairdocs.org/sdr/C2XA98IA024.md): Trunnion · cracked · Feb 13, 1998 · N12705 · Emb EMB120RT · Nose/Tail Landing Gear Attach Section > IAH - DURING C-CHECK INSPECTION, THE UPPER TRUNNION ON THE NOSE LANDING GEAR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE UPPER TRUNNION IAW EMB-120 MM CHAPTER 32-21-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97CL049](https://openairdocs.org/sdr/C2XA97CL049.md): Control Unit · failed · May 2, 1997 · N12705 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLT 3041 - CREW REPORTED A NACELLE FLAP CONTROL FAULT THAT WOULD NOT RESET IN FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, THEN REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06, OPERATIONAL - [SDR C2XA97CL010](https://openairdocs.org/sdr/C2XA97CL010.md): Transducer · failed · Jan 30, 1997 · N12705 · Emb EMB120RT · Engine Oil Pressure > TYS - FLT 212C - CREW REPORTED, COMPLETED A PRECAUTIONRAY RIGHT ENGINE SHUT DOWN DUE TO OIL PRESSURE INDICATING LESS THEN 20 PSI. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE RIGHT ENGINE AND REMOVED AND REPLACED THE ENGINE OIL PRESSURE TRANSDUCER I - [SDR C2XA96IA253](https://openairdocs.org/sdr/C2XA96IA253.md): Angle · cracked · Oct 2, 1996 · N12705 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA252](https://openairdocs.org/sdr/C2XA96IA252.md): Angle · cracked · Oct 2, 1996 · N12705 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE FRAME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA251](https://openairdocs.org/sdr/C2XA96IA251.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA250](https://openairdocs.org/sdr/C2XA96IA250.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA249](https://openairdocs.org/sdr/C2XA96IA249.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA248](https://openairdocs.org/sdr/C2XA96IA248.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA247](https://openairdocs.org/sdr/C2XA96IA247.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA246](https://openairdocs.org/sdr/C2XA96IA246.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA245](https://openairdocs.org/sdr/C2XA96IA245.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR SERVICE. (M) - [SDR C2XA96IA244](https://openairdocs.org/sdr/C2XA96IA244.md): Seat Track · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA243](https://openairdocs.org/sdr/C2XA96IA243.md): Beam · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA-BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF THE BEAM AT FRAMES 37 TO 39, BY USING A BEAM SPLICE AND DOUBLERS. WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/R - [SDR C2XA96IA242](https://openairdocs.org/sdr/C2XA96IA242.md): T-Profile · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA241](https://openairdocs.org/sdr/C2XA96IA241.md): Buttstrap · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP AT FRAMES 39 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA240](https://openairdocs.org/sdr/C2XA96IA240.md): Buttstrap · corroded · Oct 2, 1996 · N12705 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP AT FRAMES 34 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA029](https://openairdocs.org/sdr/C2XA95IA029.md): Sequence Valve · failed · Feb 24, 1995 · N12705 · Emb EMB120RT · Landing Gear Retraction/Extension System > IAH - FLT 2697 - DURING CLIMB, PILOT REPORTED LT GEAR DID NOT RETRACT WHEN GEAR WAS SELECTED TO THE 'UP' POSITION. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT MLG SEQUENCE VALVE. THE OPERATIONAL CHECK OF ## 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 = 'N12705' AND deregistration_id = 'N12705-1999-07-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N12705-1999-07-23/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.