# Service difficulty reports: N15713, cancelled Sep 13, 2013 A list on [N15713, cancelled Sep 13, 2013](https://openairdocs.org/deregistered/N15713-2013-09-13.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 · 52 reports - [SDR C2XA01IA252](https://openairdocs.org/sdr/C2XA01IA252.md): Light · inoperative · May 26, 2001 · N15713 · Emb EMB120ER · Emergency Lighting > IAH - FLIGHT 3034, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA01IA193](https://openairdocs.org/sdr/C2XA01IA193.md): Power Supply · discharged · Apr 3, 2001 · N15713 · Emb EMB120ER · Emergency Lighting > IAH - FLIGHT 3471, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA00IA370](https://openairdocs.org/sdr/C2XA00IA370.md): Battery Pack · discharged · Oct 4, 2000 · N15713 · Emb EMB120RT · Emergency Lighting > IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00IA252](https://openairdocs.org/sdr/C2XA00IA252.md): Apu · leaking · Aug 10, 2000 · N15713 · Emb EMB120RT · APU Oil System > SHV - THE CREW REPORTED THAT THE APU EMITS A FUEL SMELL IN THE COCKPIT AND CABIN ON THE GROUND. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB120 MM 49-00-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00IA255](https://openairdocs.org/sdr/C2XA00IA255.md): Seat Track · corroded · Jul 6, 2000 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 31 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW WITH EMB120 SRM 53-01-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA00IA254](https://openairdocs.org/sdr/C2XA00IA254.md): Frame · cracked · Jul 6, 2000 · N15713 · Emb EMB120RT · Nacelle/Pylon, Main Frame > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE RIGHT NACELLE NR 1 FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00IA253](https://openairdocs.org/sdr/C2XA00IA253.md): Frame · cracked · Jul 6, 2000 · N15713 · Emb EMB120RT · Nacelle/Pylon, Main Frame > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE LEFT NAELLE NUMBER ONE FRAME. MAINTENANCE REMOVED AND REPLACED HE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00CL008](https://openairdocs.org/sdr/C2XA00CL008.md): Accumulator · failed · Jan 21, 2000 · N15713 · Emb EMB120RT · Landing Gear Retraction/Extension System > SYR - FLT 3182 - ON APPROACH INTO SYRACUSE, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED WITH NORMAL GEAR EXTENSION, ELECTRIC OVERRIDE, OR FREEFALL. NOSE GEAR EVENTUALLY SHOWED DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REP - [SDR C2XA00CL007](https://openairdocs.org/sdr/C2XA00CL007.md): Handle · failed · Jan 21, 2000 · N15713 · Emb EMB120RT · Landing Gear Selector > CLE - FLT 3214 - ON APPROACH TO CLEVELAND, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED WITH NORMAL GEAR EXTENSION. THE GEAR WAS LOWERED WITH THE ELECTRIC OVERRIDE SWITCH. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE - [SDR C2XA00CL006](https://openairdocs.org/sdr/C2XA00CL006.md): Harness · failed · Jan 20, 2000 · N15713 · Emb EMB120RT · Landing Gear Position and Warning > CLE - FLT 3139 - ON APPROACH TO CLEVELAND, THE NOSE GEAR DID NOT INDICATE A DOWN AND LOCKED LIGHT UNTIL AFTER EMERGENCY FREE FALL EXTENSION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR - [SDR C2XA99CL092](https://openairdocs.org/sdr/C2XA99CL092.md): Selector · failed · Aug 21, 1999 · N15713 · Emb EMB120RT · Landing Gear Selector > CAK - FLT 3008 - THE CREW REPORTED THAT THE LEFT MAIN GEAR DISAGREEMENT LIGHT AFTER SELECTING THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR HANDLE AND PERFORMED OPERATIONAL CHECKS IAW EMB12 - [SDR C2XA98IA415](https://openairdocs.org/sdr/C2XA98IA415.md): Switch · failed · Oct 9, 1998 · N15713 · Emb EMB120RT · Landing Gear Position and Warning > FLT 3722 - EFD-IAH - DURING FLT, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON THE INITIAL TRY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWNLOCK SYSTEM A PROX SWITCH T - [SDR C2XA98IA411](https://openairdocs.org/sdr/C2XA98IA411.md): Bracket · cracked · Oct 8, 1998 · N15713 · Emb EMB120RT · Landing Gear Doors > IAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FORWARD OUTBOARD DOOR ACTUATOR ATTACH BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA410](https://openairdocs.org/sdr/C2XA98IA410.md): Bearing · corroded · Oct 8, 1998 · N15713 · Emb EMB120RT · Passenger/Crew Doors > IAH - DURING C-CHECK INSPECTION, THE AFT OPENING/LOCKING BEARING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING IAW EMB120 MM CH 52-10-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA409](https://openairdocs.org/sdr/C2XA98IA409.md): Stringer · cracked · Oct 8, 1998 · N15713 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 10 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPR - [SDR C2XA98IA408](https://openairdocs.org/sdr/C2XA98IA408.md): Stringer · cracked · Oct 8, 1998 · N15713 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPRO - [SDR C2XA98IA407](https://openairdocs.org/sdr/C2XA98IA407.md): Stringer · cracked · Oct 8, 1998 · N15713 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPR - [SDR C2XA98IA406](https://openairdocs.org/sdr/C2XA98IA406.md): Stringer · cracked · Oct 8, 1998 · N15713 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS APPR - [SDR C2XA98CL045](https://openairdocs.org/sdr/C2XA98CL045.md): Hose · ruptured · Jun 8, 1998 · N15713 · Emb EMB120RT · Cabin Cooling System > CLE - FLT 3079 - CREW REPORTED THAT THE COCKPIT AND CABIN FILLED WITH SMOKE DURING TAXI OUT, AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED A BLOWN HOSE AND CLEANED OIL FROM THE RIGHT ACM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-12 - [SDR C2XA97CL099](https://openairdocs.org/sdr/C2XA97CL099.md): Prop Bulkhead · grooved · Dec 11, 1997 · N15713 · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System > CLE - FLT 3073 - CREW REPORTED THAT THE LEFT PROPELLER DE-ICE WAS INOPERATIVE. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE PROPELLER BULKHEAD IAW HAMILTON STANDARD MM 61-10-00, OPS CHE - [SDR C2XA97CL043](https://openairdocs.org/sdr/C2XA97CL043.md): Fuse · failed · Apr 17, 1997 · N15713 · Emb EMB120RT · Emergency Lighting > CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND EXTERIOR FORWARD EMERENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE EMERGENCY LIGHTS, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120 MM E33-50-00. AIRCRAFT RELEASED FOR - [SDR C2XA97IA099](https://openairdocs.org/sdr/C2XA97IA099.md): Buttstrap · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP AT FRAME 38 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 C2XA97IA098](https://openairdocs.org/sdr/C2XA97IA098.md): Buttstrap · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT BUTTSTRAP FROM FRAME 38 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 C2XA97IA097](https://openairdocs.org/sdr/C2XA97IA097.md): T-Profile · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA096](https://openairdocs.org/sdr/C2XA97IA096.md): Seat Track · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT 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 C2XA97IA095](https://openairdocs.org/sdr/C2XA97IA095.md): Seat Track · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA094](https://openairdocs.org/sdr/C2XA97IA094.md): Seat Track · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT 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 C2XA97IA093](https://openairdocs.org/sdr/C2XA97IA093.md): Buttstrap · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAMES 38 TO 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA092](https://openairdocs.org/sdr/C2XA97IA092.md): Buttstrap · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAMES 34-38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA091](https://openairdocs.org/sdr/C2XA97IA091.md): T-Profile · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA090](https://openairdocs.org/sdr/C2XA97IA090.md): Floorbeam · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Main, Floor Beam > IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE FLOORBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA089](https://openairdocs.org/sdr/C2XA97IA089.md): T-Profile · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER 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 C2XA97IA088](https://openairdocs.org/sdr/C2XA97IA088.md): Buttstrap · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT BUTTSTRAP FROM FRAME 34 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA087](https://openairdocs.org/sdr/C2XA97IA087.md): Crease Beam · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CREASE BEAM AT FRAME 38 TO 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA086](https://openairdocs.org/sdr/C2XA97IA086.md): Crease Beam · corroded · Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WALL 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 C2XA97CL008](https://openairdocs.org/sdr/C2XA97CL008.md): Pcu · faulty · Jan 20, 1997 · N15713 · Emb EMB120RT · Propeller Controlling System > CLE - FLT 3283 - CREW REPORTED THAT DURING CLIMB THE RIGHT PROP NP FLUCTUATES BETWEEN 1 PERCENT AND 2 PERCENT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT PROPELLER CONTROL UNIT IAW EMB-120 MM 61-21-00. - [SDR C2XA96IA239](https://openairdocs.org/sdr/C2XA96IA239.md): Wheel · failed · Sep 28, 1996 · N15713 · Emb EMB120RT · Wheel/Ski/Float > IAH - FLT 3797 - PILOT REPORTED THAT DURING TAKEOFF, THE NR 1 MAIN GEAR TIRE BLEW OUT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MAIN TIRE, AND BRAKE ASSEMBLY WHICH WAS DAMAGED FROM THE TIRE. THE - [SDR C2XA96CL013](https://openairdocs.org/sdr/C2XA96CL013.md): Control Unit · failed · Feb 5, 1996 · N15713 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLIGHT NR 3933 - CREW REPORTED THAT ON APPROACH WHEN THE FLAPS WERE SELECTED TO 15 DEGREES A FLAP DISAGREEMENT OCCURRED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD - [SDR C2XA95IA257](https://openairdocs.org/sdr/C2XA95IA257.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, 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) - [SDR C2XA95IA256](https://openairdocs.org/sdr/C2XA95IA256.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, 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 C2XA95IA255](https://openairdocs.org/sdr/C2XA95IA255.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 20, 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) - [SDR C2XA95IA254](https://openairdocs.org/sdr/C2XA95IA254.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, 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 C2XA95IA253](https://openairdocs.org/sdr/C2XA95IA253.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, 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 C2XA95IA252](https://openairdocs.org/sdr/C2XA95IA252.md): Skin Support · cracked · Sep 22, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, UPPER 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 C2XA95IA251](https://openairdocs.org/sdr/C2XA95IA251.md): Support · cracked · Sep 20, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA95IA250](https://openairdocs.org/sdr/C2XA95IA250.md): Support · cracked · Sep 20, 1995 · N15713 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA95CL056](https://openairdocs.org/sdr/C2XA95CL056.md): Connector · dirty · Apr 3, 1995 · N15713 · Emb EMB120RT · Landing Gear Position and Warning > CLE-BUF - FLT 3216 - CREW HEARD CLICK, THEN NOTICED STRONG ELECTRICAL SMELL FOLLOWED BY STICK SHAKER/PUSHER ACTUATION WHILE PARKED AT GATE. MAINTENANCE CLEANED AND RESEATED PROX SENSOR CANNON PLUGS ON LEFT AND RIGHT MAIN GEARS. OP'S CHECKED STALL WARNING SYS - [SDR C2XA95CL033](https://openairdocs.org/sdr/C2XA95CL033.md): Engine · failed · Feb 13, 1995 · N15713 · Emb EMB120RT · Engine (Turbine/Turboprop) > FLT NR 3183 - CLE-CLE - SHORTLY AFTER TAKEOFF THE LEFT ENGINE OIL PRESSURE DROPPED TO ZERO FOLLOWED BY A LOUD BANG. THE FLIGHT CREW SECURED THE LEFT ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-120 MM MAINTENAN - [SDR C2XA95CL015](https://openairdocs.org/sdr/C2XA95CL015.md): Actuator · out of adjust · Feb 2, 1995 · N15713 · Emb EMB120RT · Landing Gear Retraction/Extension System > SYR-CLE - FLT 3189 - THE RT MAIN GEAR WOULD NOT RETRACT. FERRIED ACFT TO CLE. MAINTENANCE ADJUSTED RT MAIN GEAR ACTUATOR AND OPS CHECK GOOD. IAW EMB MM 32-30-00. ACFT RETURNED TO SERVICE. (W) - [SDR C2XA95CL011](https://openairdocs.org/sdr/C2XA95CL011.md): Roller'S · binding · Jan 29, 1995 · N15713 · Emb EMB120RT · Trailing Edge Flaps > PIT-CLE - FLT 3331 - FLAP ASSYMETRY O/B LT SIDE. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ROLLERS WITH NEW STYLE IAW EMB MM 27-50-12 AND EA275001007. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) Next page: https://openairdocs.org/deregistered/N15713-2013-09-13/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 = 'N15713' AND deregistration_id = 'N15713-2013-09-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15713-2013-09-13/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.