# Service difficulty reports: N12709, cancelled Dec 22, 2014 A list on [N12709, cancelled Dec 22, 2014](https://openairdocs.org/deregistered/N12709-2014-12-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR C2XA99CL091](https://openairdocs.org/sdr/C2XA99CL091.md): Indication · malfunctioned · Aug 20, 1999 · N12709 · Emb EMB120RT · Landing Gear Position and Warning > YYZ-CLE - FLT 3609 - THE CREW REPORTED THAT ON FINAL THEY LOST THE NR 2 T6 INDICATION, TQ INDICATOR, THE GEAR INDICATIONS, COM NR 2 AND THE AURAL WARNING WAS GOING OFF 'TRIM'. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET CB4071, AND JACKED - [SDR C2XA99IA256](https://openairdocs.org/sdr/C2XA99IA256.md): Air Dist · smoking · May 1, 1999 · N12709 · Emb EMB120RT · Air Distribution System > IAH - FLT 3643 ON CLIMB-OUT, THE CREW REPORTED THAT THE CABIN FILLED WITH SMOKE AND THE SMOKE LIGHT ON THE MAP ILLUMINATED AT 10,000 MSL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT WHERE MAINTENANCE GROUND RAN THE COOLING PACKS OFF OF THE A - [SDR C2XA00IA070](https://openairdocs.org/sdr/C2XA00IA070.md): Acm · inoperative · Mar 11, 1999 · N12709 · Emb EMB120RT · Cabin Cooling System > IAH - FLT 3686 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE CAIN. THE AIRCRAFT RETURNED IAH WITHOUT INCIDENT, WHERE MAINTENANCE UNSTUCK THE RIGHT ACM AND OPERATIONLLY CHECKED. THE PROBLEM REPEATED ON FINAL FOR FLIGHT 3686 WHERE THE AIRCRAFT LANDED AT MLU W - [SDR C2XA99IA184](https://openairdocs.org/sdr/C2XA99IA184.md): Acm · inoperative · Mar 11, 1999 · N12709 · Emb EMB120RT · Cabin Cooling System > IAH - FLT 3686 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT, WHERE MAINTENANCE UNSTUCK THE RIGHT ACM AND OPERATIONALLY CHECKED IAW EMB120 SRM 21-60-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA99CL004](https://openairdocs.org/sdr/C2XA99CL004.md): Rod · worn · Jan 11, 1999 · N12709 · Emb EMB120RT · Landing Gear Retraction/Extension System > CLE - FLT 3067 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR LEVER ROD END IAW - [SDR C2XA98CL084](https://openairdocs.org/sdr/C2XA98CL084.md): Actuator · 19681 · Dec 21, 1998 · N12709 · Emb EMB120RT · Trailing Edge Flap Actuator > CLE - FLT 3194 - CREW REPORTED THAT AFTER TAKEOFF, RECEIVED A FLAP ASYMMETRY WITH THE INBOARD FLAPS AT 25 DEGREES AND THE OUTBOARD AND NACELLES AT 15 DEGREES. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT - [SDR C2XA98IA459](https://openairdocs.org/sdr/C2XA98IA459.md): Angle · cracked · Nov 10, 1998 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VERTICAL STIFFENER STABILIZER DRAG ANGEL CRACKED ON FORWARD END. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC - [SDR C2XA98IA458](https://openairdocs.org/sdr/C2XA98IA458.md): Skin · cracked · Nov 10, 1998 · N12709 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD CORNER OF ACCESS 622EB. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC - [SDR C2XA98IA457](https://openairdocs.org/sdr/C2XA98IA457.md): Skin · cracked · Nov 10, 1998 · N12709 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD SIDE OF ACCESS 521AB. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA98CL056](https://openairdocs.org/sdr/C2XA98CL056.md): Hmu · malfunctioned · Jul 27, 1998 · N12709 · Emb EMB120RT · Fuel Controlling System > CLE - FLT 3206 - CREW REPORTED THE RIGHT ENGINE NP WOULD NOT GO BELOW 20.9 PERCENT DURING MANUAL FEATHER CHECK, AND THE NH RUNS AT 64.3 PERCENT. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE HMU IAW - [SDR C2XA97IA214](https://openairdocs.org/sdr/C2XA97IA214.md): Angle · cracked · Jul 19, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING A-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPERSS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5530-01013, AND - [SDR C2XA97CL059](https://openairdocs.org/sdr/C2XA97CL059.md): Handle · inoperative · Jun 20, 1997 · N12709 · Emb EMB120RT · Landing Gear Steering System > CLE - FLT 3057 - CREW REPORTED THAT DURING TAXI THE NOSE WHEEL STEERING WAS SLUGGISH, MAKING THE AIRCRAFT UNSAFE TO TAXI. MAINTENANCE INSPECTED THE STEERING SYSTEM THEN REMOVED AND REPLACED THE STEERING HANDLE IAW EMB120 MM 32-50-01, OPERATIONAL CHECKS WERE S - [SDR C2XA97CL053](https://openairdocs.org/sdr/C2XA97CL053.md): Windshield · shattered · May 12, 1997 · N12709 · Emb EMB120RT · Flight Compartment Windows > DTW - FLT 3294 - CREW REPORTED THAT WHILE EN ROUTE FROM MKE TO CLE, THE FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED. THE AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT MAINTENA - [SDR C2XA97IA133](https://openairdocs.org/sdr/C2XA97IA133.md): T-Profile · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 16 LEFT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA132](https://openairdocs.org/sdr/C2XA97IA132.md): T-Profile · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE ON FRAME 36 LEFT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA131](https://openairdocs.org/sdr/C2XA97IA131.md): Seat Track · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDE WALL 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 C2XA97IA130](https://openairdocs.org/sdr/C2XA97IA130.md): Seat Track · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDE WALL 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 C2XA97IA129](https://openairdocs.org/sdr/C2XA97IA129.md): Seat Track · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD 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 C2XA97IA128](https://openairdocs.org/sdr/C2XA97IA128.md): Seat Track · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD 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 C2XA97IA127](https://openairdocs.org/sdr/C2XA97IA127.md): Stringer · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Main, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 43. MAINTENANCE REMOVED THE DAMAGED SECTION AND PERFORMED A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA126](https://openairdocs.org/sdr/C2XA97IA126.md): T-Profile · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA125](https://openairdocs.org/sdr/C2XA97IA125.md): Seat Track · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT SIDE WALL 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 C2XA97IA124](https://openairdocs.org/sdr/C2XA97IA124.md): Seat Track · corroded · Mar 31, 1997 · N12709 · 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 SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA123](https://openairdocs.org/sdr/C2XA97IA123.md): Seat Track · corroded · Mar 31, 1997 · N12709 · 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 SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA122](https://openairdocs.org/sdr/C2XA97IA122.md): Buttstrap · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGH BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA121](https://openairdocs.org/sdr/C2XA97IA121.md): T-Profile · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA120](https://openairdocs.org/sdr/C2XA97IA120.md): Crease Beam · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 44. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA119](https://openairdocs.org/sdr/C2XA97IA119.md): Buttstrap · corroded · Mar 31, 1997 · N12709 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 41. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA118](https://openairdocs.org/sdr/C2XA97IA118.md): Rib · cracked · Mar 31, 1997 · N12709 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB AT RIB 20 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA117](https://openairdocs.org/sdr/C2XA97IA117.md): Rib · cracked · Mar 31, 1997 · N12709 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97CL003](https://openairdocs.org/sdr/C2XA97CL003.md): Wheel · out of balance · Jan 4, 1997 · N12709 · Emb EMB120RT · Wheel/Ski/Float > CLE - FLT 3061 - CREW REPORTED THAT THEY RECEIVED A STRONG VIBRATION IN THE NOSE AREA AFTER GEAR RETRACTION, THE VIBRATION INCREASED WITH SPEED AND STOP AFTER GEAR WAS EXTENDED. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND AFTER TROUBLESHOOT - [SDR C2XA96CL035](https://openairdocs.org/sdr/C2XA96CL035.md): Eec · failed · Oct 26, 1996 · N12709 · Emb EMB120RT · Fuel Control/Turbine Engines > CLE - FLT 3003 - CREW REPORTED THAT AT 17,500 FEET THEY COULD NOT GET MORE THAN 4 PERCENT TORQUE AND 700 DEGREES EGT WITH POWER LEVER FULL FORWARD. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE ELECTRONIC - [SDR C2XA95IA385](https://openairdocs.org/sdr/C2XA95IA385.md): Stringer · cracked · Dec 10, 1995 · N12709 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING 1A, 3A CHECK, FOUND LEFT WING LOWER SURFACE INTERNAL STRINGER NR 10 CRACKED, FORWARD OF FUEL PANEL NR 522EB. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR SPLICE IN REF TO EMB DER APPROVED FAX NR EST-501/95. AIRCRAFT APPROVED FOR RETURN - [SDR C2XA95IA384](https://openairdocs.org/sdr/C2XA95IA384.md): Skin · cracked · Dec 10, 1995 · N12709 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING 1A, 3A CHECK INSPECTION, FOUND A CRACK IN THE LOWER INBOARD WING SKIN BETWEEN TWO FASTENERS, AT THE AFT OUTBOARD CORNER OF PANEL 522EB. MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IN REFERENCE TO THE EMB 120 SRM 57-20-01. AIRCRAFT APPR - [SDR C2XA95IA269](https://openairdocs.org/sdr/C2XA95IA269.md): Skin · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER SKIN CRACKED AT AFT OUTBOARD CORNER OF FUELING ACCESS DOOR CUT OUT. MAINTENANCE STOP DRILLED, AND INSTALLED REPAIR DOUBLER PER CONTINENTAL EXPRESS ENGINEERING CHANGE, REPAIR AUTHORIZATION EC5730-01031. - [SDR C2XA95IA268](https://openairdocs.org/sdr/C2XA95IA268.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA266](https://openairdocs.org/sdr/C2XA95IA266.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA265](https://openairdocs.org/sdr/C2XA95IA265.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 5 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA264](https://openairdocs.org/sdr/C2XA95IA264.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA263](https://openairdocs.org/sdr/C2XA95IA263.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA262](https://openairdocs.org/sdr/C2XA95IA262.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA261](https://openairdocs.org/sdr/C2XA95IA261.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA260](https://openairdocs.org/sdr/C2XA95IA260.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA259](https://openairdocs.org/sdr/C2XA95IA259.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA258](https://openairdocs.org/sdr/C2XA95IA258.md): Support · cracked · Oct 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA026](https://openairdocs.org/sdr/C2XA95IA026.md): Line · misaligned · Feb 16, 1995 · N12709 · Emb EMB120RT · Ice/Rain Protection System > LRD - FLT NR 2584 - UPON CLIMB, THE RIGHT DUCT LEAK LIGHT ILLUMINATED. THE PILOT REPORTED THAT THE LIGHT WOULD NOT EXTINGUISH UNITL THE RIGHT ENGINE WAS SHUTDOWN. THE CREW RETURNED TO THE FIELD, AFTER SHUTTING THE RIGHT ENGINE DOWN, WITHOUT FURTHER INCIDENT. - [SDR C2XA95IA004](https://openairdocs.org/sdr/C2XA95IA004.md): Control Handle · failed · Jan 16, 1995 · N12709 · Emb EMB120RT · Landing Gear Selector > IAH - FLT 7775 - PRIOR TO FLIGHT, THE CREW REPORTED THE NOSE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. MAINTENANCE INSPECTED AND FOUND THE 'A' SYSTEM UNLOCK LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE GEAR CONTROL HANDLE IAW EMB 120 MM 32-30-0 - [SDR C2XA95IA267](https://openairdocs.org/sdr/C2XA95IA267.md): Support · cracked · Jan 3, 1995 · N12709 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) ## 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 = 'N12709' AND deregistration_id = 'N12709-2014-12-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N12709-2014-12-22/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.