# Service difficulty reports: N16710, cancelled Apr 24, 2015 A list on [N16710, cancelled Apr 24, 2015](https://openairdocs.org/deregistered/N16710-2015-04-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR C2XA99IA620](https://openairdocs.org/sdr/C2XA99IA620.md): Bulb · failed · Nov 23, 1999 · N16710 · Emb EMB120RT · Emergency Lighting > CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA286](https://openairdocs.org/sdr/C2XA99IA286.md): Valve · inoperative · May 19, 1999 · N16710 · Emb EMB120RT · Landing Gear Retraction/Extension System > IAH - FLT 3522 - THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR SHUTOFF VALVE. THE AIRCRAFT WAS TEST FLOWN SATIS - [SDR C2XA99IA283](https://openairdocs.org/sdr/C2XA99IA283.md): Actuator · inoperative · May 14, 1999 · N16710 · Emb EMB120RT · Landing Gear Actuator > IAH - FLT 3438 - THE CREW REPORTED THAT THE LEFT MAIN GEAR WOULD NOT RETRACT AND HAD A RUMBLING VIBRATION UNTIL THE CONTROL LEVER WAS CYCLED MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW EMB120MM, THE LANDING GEAR RELAY BOX I - [SDR C2XA99IA281](https://openairdocs.org/sdr/C2XA99IA281.md): Relay Box · inoperative · May 14, 1999 · N16710 · Emb EMB120RT · Landing Gear Position and Warning > IAH - FLT 3441 - THE CREW REPORTED THAT THE LEFT MAIN GEAR RED INDICATION LIGHT REMAINED ILLUMINATED UNTIL THE CONTROL LEVER WAS CYCLED TWICE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX IAW EM - [SDR C2XA99IA280](https://openairdocs.org/sdr/C2XA99IA280.md): Control Lever · inoperative · May 14, 1999 · N16710 · Emb EMB120RT · Landing Gear Selector > IAH - FLT 3730 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB120MM 32-31-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE - [SDR C2XA99CL022](https://openairdocs.org/sdr/C2XA99CL022.md): Actuator · malfunctioned · Feb 28, 1999 · N16710 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLT 3194 - CREW REPORTED THAT THEY RECEIVED A NACELLE FLAP ASYMMETRY AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT NACELLE FLAP ACTUATOR IAW EMB-120 MM 27-50-08, OPERATIONAL AND LEAK CHE - [SDR C2XA98CL065](https://openairdocs.org/sdr/C2XA98CL065.md): Engine · failed · Sep 8, 1998 · N16710 · Emb EMB120RT · Engine (Turbine/Turboprop) > TOL - FLT 3022 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LEFT ENGINE LOW OIL PRESSURE WARNING, AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE OIL LEVEL TO BE 3 QUARTS LOW. THE ENGINE OIL - [SDR C2XA98IA280](https://openairdocs.org/sdr/C2XA98IA280.md): Seat Track · corroded · Jul 23, 1998 · N16710 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOO SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SEAT TRACK IAW EMB-120 SRM 51-21-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA279](https://openairdocs.org/sdr/C2XA98IA279.md): Skin · cracked · Jul 23, 1998 · N16710 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND TO BE CRACKED AT THE AFT OUTBOARD CORNER OF PANEL 522EB. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB-120 SRM 57-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA278](https://openairdocs.org/sdr/C2XA98IA278.md): Light · inoperative · Jul 23, 1998 · N16710 · Emb EMB120RT · Emergency Lighting > IAH - DURING C-CHECK INSPECTION, THE EMERGENCY AISLE PATH LIGHTING AFT SECTION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA242](https://openairdocs.org/sdr/C2XA98IA242.md): Control Unit · inoperative · Jun 30, 1998 · N16710 · Emb EMB120RT · Landing Gear Retraction/Extension System > IAH - FLT 3684 - THE PILOT REPORTED A SEVERE VIBRATION WAS FELT AFTER THE LANDING GEAR WAS SELECTED TO THE UP POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL BOX, AND THE AI - [SDR C2XA98IA182](https://openairdocs.org/sdr/C2XA98IA182.md): Light · inoperative · May 13, 1998 · N16710 · Emb EMB120RT · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-120 MM 33-50-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97CL050](https://openairdocs.org/sdr/C2XA97CL050.md): Bulb · failed · May 4, 1997 · N16710 · Emb EMB120RT · Emergency Lighting > CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND FORWARD, EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND FORWARD, EXTERIOR EMERGENCY LIGHT BULB IAW EMB-120 MM 33-50-00. OPERATIONAL CHECKS WERE SATISFACTORY, - [SDR C2XA97CL022](https://openairdocs.org/sdr/C2XA97CL022.md): Bulb · failed · Mar 11, 1997 · N16710 · Emb EMB120RT · Emergency Lighting > CLE - DURING A SCHEDULED INSPECTION, THE EXTERIOR EMERGENCY LIGHTS BOTH FORWARD AND AFT ON THE RIGHT SIDE OF THE FUSELAGE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN BOTH FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS IAW EMB - [SDR C2XA97IA018](https://openairdocs.org/sdr/C2XA97IA018.md): Skin · cracked · Jan 2, 1997 · N16710 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED OUTBOARD OF THE NACELLE. MAINTENANCE REPAIRED THE SKIN BY STOP DRILLING THE CRACK, AND APPLYING A DOUBLER. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA017](https://openairdocs.org/sdr/C2XA97IA017.md): Skin · cracked · Jan 2, 1997 · N16710 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING C-CHECK INSPECTION, THE LEFT WING INBOARD SKIN WAS FOUND TO HAVE TWO CRACKS IN ACCESS PANEL CUTOUTS. THE SKIN WAS REPAIRED BY STOP DRILLING THE AFFECTED CRACKS, AND DOUBLERS WERE APPLIED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M - [SDR C2XA97IA016](https://openairdocs.org/sdr/C2XA97IA016.md): Rib · cracked · Jan 2, 1997 · N16710 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB NR 19 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE NOSE RIB USING AND ANGLE DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA015](https://openairdocs.org/sdr/C2XA97IA015.md): T-Profile · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA014](https://openairdocs.org/sdr/C2XA97IA014.md): T-Profile · corroded · Jan 2, 1997 · N16710 · 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 T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA013](https://openairdocs.org/sdr/C2XA97IA013.md): Crease Beam · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM AT FRAME 39 TO 44 WAS FOND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA010](https://openairdocs.org/sdr/C2XA97IA010.md): Seat Track · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT 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 C2XA97IA009](https://openairdocs.org/sdr/C2XA97IA009.md): Seat Track · corroded · Jan 2, 1997 · N16710 · 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 C2XA97IA008](https://openairdocs.org/sdr/C2XA97IA008.md): Seat Track · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA007](https://openairdocs.org/sdr/C2XA97IA007.md): Seat Track · corroded · Jan 2, 1997 · N16710 · 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 C2XA97IA006](https://openairdocs.org/sdr/C2XA97IA006.md): Seat Track · corroded · Jan 2, 1997 · N16710 · 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 C2XA97IA005](https://openairdocs.org/sdr/C2XA97IA005.md): Seat Track · corroded · Jan 2, 1997 · N16710 · 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 C2XA97IA004](https://openairdocs.org/sdr/C2XA97IA004.md): Drag Angle · cracked · Jan 2, 1997 · N16710 · Emb EMB120RT · Vertical Stabilizer > IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE ANGLE USING A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA003](https://openairdocs.org/sdr/C2XA97IA003.md): Drag Angle · cracked · Jan 2, 1997 · N16710 · Emb EMB120RT · Vertical Stabilizer > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE PEFORMED A SPLICE REPAIR OF THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA002](https://openairdocs.org/sdr/C2XA97IA002.md): Support · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Passenger/Crew Doors > IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR FORWARD UPPER SUPPORT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA001](https://openairdocs.org/sdr/C2XA97IA001.md): T-Profile · corroded · Jan 2, 1997 · N16710 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA059](https://openairdocs.org/sdr/C2XA96IA059.md): Sequence Vlv · failed · Feb 24, 1996 · N16710 · Emb EMB120RT · Landing Gear Door Retract Section > IAH - FLT NR 2522 - AFTER TAKEOFF, UPON RETRACTION OF LANDING GEAR A LOUD RUMBLING NOISE WAS HEARD. FLIGHT CREW CYCLED LANDING GEAR, NOISE CONTINUED. AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED SEQUENCE VALVE FOR R - [SDR C2XA95IA363](https://openairdocs.org/sdr/C2XA95IA363.md): Prox Switch · out of adjust · Nov 28, 1995 · N16710 · Emb EMB120RT · Landing Gear Position and Warning > CLL - FLT NR 2627 - PILOT REPORTED THAT AFTER TAKEOFF, THE LEFT MAIN GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD. THE AIRCRAFT WAS THEN FERRIED TO IAH WHERE MAINTENANCE ADJUSTED THE LEFT GEAR UPLOCK PROXIMITY SWITCH. THE AIRCRAFT THEN AIR RET - [SDR C2XA95IA164](https://openairdocs.org/sdr/C2XA95IA164.md): Skin Support · cracked · Aug 3, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING UPPER NR 2 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA163](https://openairdocs.org/sdr/C2XA95IA163.md): Bracket · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND FORWARD BRACKET FOR CARGO DOOR COUNTER BALANCE TORSION RODS CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA162](https://openairdocs.org/sdr/C2XA95IA162.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORTS NR 4 AND NR 5 CRACKED AT RIB NR 25. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA161](https://openairdocs.org/sdr/C2XA95IA161.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT NR 3 CRACKED AT RIB NR 25. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA160](https://openairdocs.org/sdr/C2XA95IA160.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING NR 4 SKIN SUPPORT CRACKED AT RIB NR 21 UPPER. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA159](https://openairdocs.org/sdr/C2XA95IA159.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER FORWARD SKIN SUPPORT CRACKED AT RIB NR 19. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA158](https://openairdocs.org/sdr/C2XA95IA158.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA157](https://openairdocs.org/sdr/C2XA95IA157.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING NR 3 SKIN SUPPORT AT RIB NR 16 CRACKED, LOWER SKIN. MAINTENANCE REMOVED AND REPLACED THE SUPPORT AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA156](https://openairdocs.org/sdr/C2XA95IA156.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA155](https://openairdocs.org/sdr/C2XA95IA155.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 6 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA154](https://openairdocs.org/sdr/C2XA95IA154.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 2, AND NR 3 SKIN SUPPORTS CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA153](https://openairdocs.org/sdr/C2XA95IA153.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA152](https://openairdocs.org/sdr/C2XA95IA152.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA151](https://openairdocs.org/sdr/C2XA95IA151.md): Skin Support · cracked · Aug 2, 1995 · N16710 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA150](https://openairdocs.org/sdr/C2XA95IA150.md): Seat Track · corroded · Jul 31, 1995 · N16710 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT AFT 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 C2XA95IA149](https://openairdocs.org/sdr/C2XA95IA149.md): Seat Track · corroded · Jul 31, 1995 · N16710 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT 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 C2XA95IA086](https://openairdocs.org/sdr/C2XA95IA086.md): Stringer · cracked · May 24, 1995 · N16710 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING A CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 10 CRACKED BETWEEN RIBS NR 8 AND NR 9. MAINTENANCE CUT, REMOVED CRACKED SECTION, AND INSTALLED STRINGER SPLICE USING DER APPROVED EMBRAER FAX NR EST-235/95. (W) - [SDR C2XA95CL001](https://openairdocs.org/sdr/C2XA95CL001.md): Filter · contaminated · Jan 4, 1995 · N16710 · Emb EMB120RT · Engine Fuel Distribution > EWR-EWR - FLT 3698 - ON TAKEOFF ROLL WITH TORQUE THROUGH 55-60 PERCENT, RIGHT ENGINE FUEL FILTER LIGHT ON OVERHEAD AND MASTER CAUTION FUEL LIGHT ON M.A.P. ILLUMINATED. TAKEOFF WAS ABORTED. AS POWER LEVERS WERE RETARDED, WARNING EXTINGUISHED. MAINTENANCE INS ## 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 = 'N16710' AND deregistration_id = 'N16710-2015-04-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16710-2015-04-24/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.