# Service difficulty reports: N16719, cancelled Jan 14, 2000 A list on [N16719, cancelled Jan 14, 2000](https://openairdocs.org/deregistered/N16719-2000-01-14.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 · 53 reports - [SDR C2XA98CL068](https://openairdocs.org/sdr/C2XA98CL068.md): Actuator · failed · Sep 22, 1998 · N16719 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLT 3003 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP CONTROL FAULT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT WING NACELLE FLAP ACTUATOR IAW EMB-120 MM 27-5 - [SDR C2XA98IA346](https://openairdocs.org/sdr/C2XA98IA346.md): Actuator · worn · Sep 3, 1998 · N16719 · Emb EMB120RT · Landing Gear Actuator > IAH - DURING FLIGHT 3778, CREW REPORTED THE LEFT HAND MAIN LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETU - [SDR C2XA98IA396](https://openairdocs.org/sdr/C2XA98IA396.md): Fuse · failed · Aug 27, 1998 · N16719 · Emb EMB120RT · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD RIGHT FUSELAGE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA321](https://openairdocs.org/sdr/C2XA98IA321.md): Actuator · out of adjust · Aug 24, 1998 · N16719 · Emb EMB120RT · Landing Gear Actuator > IAH - DURING FLT 3814, THE PILOT REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THE LEFT MAIN GEAR ACTUATOR TO BE OUT OF ADJUSTMENT. THE ACTUATOR WAS ADJUSTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA102](https://openairdocs.org/sdr/C2XA98IA102.md): Support · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 19 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T SERVICE. (M) - [SDR C2XA98IA068](https://openairdocs.org/sdr/C2XA98IA068.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA067](https://openairdocs.org/sdr/C2XA98IA067.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA066](https://openairdocs.org/sdr/C2XA98IA066.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA065](https://openairdocs.org/sdr/C2XA98IA065.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA064](https://openairdocs.org/sdr/C2XA98IA064.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA063](https://openairdocs.org/sdr/C2XA98IA063.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA062](https://openairdocs.org/sdr/C2XA98IA062.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA061](https://openairdocs.org/sdr/C2XA98IA061.md): Seat Track · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA060](https://openairdocs.org/sdr/C2XA98IA060.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURNG C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 20 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA059](https://openairdocs.org/sdr/C2XA98IA059.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 20 FO THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA058](https://openairdocs.org/sdr/C2XA98IA058.md): T-Profile · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA057](https://openairdocs.org/sdr/C2XA98IA057.md): T-Profile · corroded · Feb 26, 1998 · N16719 · 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 IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA056](https://openairdocs.org/sdr/C2XA98IA056.md): Crease Beam · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA055](https://openairdocs.org/sdr/C2XA98IA055.md): Strap · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA054](https://openairdocs.org/sdr/C2XA98IA054.md): Strap · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA053](https://openairdocs.org/sdr/C2XA98IA053.md): Strap · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA052](https://openairdocs.org/sdr/C2XA98IA052.md): Stringer · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Main, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW EMB120 SRM 53-00-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA051](https://openairdocs.org/sdr/C2XA98IA051.md): Strap · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA050](https://openairdocs.org/sdr/C2XA98IA050.md): T-Profile · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA049](https://openairdocs.org/sdr/C2XA98IA049.md): T-Profile · corroded · Feb 26, 1998 · N16719 · 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 IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA048](https://openairdocs.org/sdr/C2XA98IA048.md): T-Profile · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA047](https://openairdocs.org/sdr/C2XA98IA047.md): Beam · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 40. MAINTENANCE REPAIRED THE AFFECTED AREA IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01043 AND THE AIRCRAFT WAS APPROVED FOR - [SDR C2XA98IA046](https://openairdocs.org/sdr/C2XA98IA046.md): Rib · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01020, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA98IA045](https://openairdocs.org/sdr/C2XA98IA045.md): T-Profile · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER T-PROFILE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA044](https://openairdocs.org/sdr/C2XA98IA044.md): T-Profile · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA043](https://openairdocs.org/sdr/C2XA98IA043.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA042](https://openairdocs.org/sdr/C2XA98IA042.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-4--02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA041](https://openairdocs.org/sdr/C2XA98IA041.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA040](https://openairdocs.org/sdr/C2XA98IA040.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA039](https://openairdocs.org/sdr/C2XA98IA039.md): Bracket · cracked · Feb 26, 1998 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 20 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA038](https://openairdocs.org/sdr/C2XA98IA038.md): Trunnion · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear Attach Section > IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR SPRING BOX LOWER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRUNNION IAW EMB120 CMM ERAM 32-21-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA037](https://openairdocs.org/sdr/C2XA98IA037.md): Trunnion · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear Attach Section > IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR STRUT SPRING BOX UPPER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ALL WORK ACCOMPLISHED IAW ERAM CMM 32-2 - [SDR C2XA98IA036](https://openairdocs.org/sdr/C2XA98IA036.md): Pin · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear > IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK LOWER PIVOT PIN WAS FOUND TO BE CORRODED IN SIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PIVOT PIN IAW ERAC CMM 32-31-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO - [SDR C2XA98IA035](https://openairdocs.org/sdr/C2XA98IA035.md): Pin · corroded · Feb 26, 1998 · N16719 · Emb EMB120RT · Nose/Tail Landing Gear > IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK UPPER PIVOT PIN WAS FOUND TO BE CORRODED INSIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE PIN IAW ERAM CMM 32-31-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA013](https://openairdocs.org/sdr/C2XA98IA013.md): Oil Cooler · cracked · Feb 4, 1998 · N16719 · Emb EMB120RT · Engine Oil Cooler > BTR - FLT 3865 - PILOT REPORTED AFTER DEPARTURE, THE NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY A FLUCTUATING OIL PRESSURE GAUGE WHICH THEN DROPPED TO 0 PSI. THE CREW SHUT DOWN THE NR 2 ENGINE AND LANDED AT BTR WITHOUT INCIDENT. MAINTENANCE FOU - [SDR C2XA97CL080](https://openairdocs.org/sdr/C2XA97CL080.md): Engine · failed · Oct 20, 1997 · N16719 · Emb EMB120RT · Engine (Turbine/Turboprop) > ORF - FLT 3342 - CREW REPORTED THAT THE LEFT PROP RPM WENT TO 115 PERCENT DURING DESCENT, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE IAW CONT EXPRESS MX DIRECTIVES NR 7 AND NR 8, OPERATIONAL - [SDR C2XA97CL028](https://openairdocs.org/sdr/C2XA97CL028.md): Relay Box · failed · Mar 20, 1997 · N16719 · Emb EMB120RT · Landing Gear Retraction/Extension System > CLE - FLT 3092 - CREW REPORTED, THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM THEN REMOVED AND REPLACED THE GEAR RELAY BOX IAW EMB-120MM 32-31-02. THE LANDING GEAR CONTROL HA - [SDR C2XA96CL003](https://openairdocs.org/sdr/C2XA96CL003.md): Relay Box · failed · Jan 19, 1996 · N16719 · Emb EMB120RT · Landing Gear Door Retract Section > CLE - FLT NR 3388 - THE CREW REPORTED THAT UPON GEAR RETRACTION THE MAIN LANDING GEAR FORWARD DOORS REMAINED OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR CONTROL RELAY BOX IAW EMB120MM 32-31-02. ALL OPERATIONAL CHECKS WE - [SDR C2XA96CL002](https://openairdocs.org/sdr/C2XA96CL002.md): Uplock Actuator · out of adjust · Jan 18, 1996 · N16719 · Emb EMB120RT · Landing Gear Retraction/Extension System > ABE - FLT NR 3321 - AFTER TAKEOFF AND GEAR RETRACTION, THE CREW REPORTED THAT THE GEAR DOOR REMAINED OPEN. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE GEAR UPLOCK ACTUATOR, MAINTENANCE ALSO CLEANED THE NOSE AND MAIN GEAR UPLOCK HOOKS. THE OPERATIONA - [SDR C2XA95IA082](https://openairdocs.org/sdr/C2XA95IA082.md): Red Gearbox · corroded · May 18, 1995 · N16719 · Emb EMB120RT · Turbine Engine Reduction Gear > IAH - DURING C-CHECK INSPECTION, FOUND NR 1 ENGINE PROPELLER SHAFT FACE PITTED AND HEAVY RUST ON INSIDE OF PROPELLER SHAFT. MAINTENANCE REMOVED AND REPLACED THE REDUCTION GEARBOX, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) - [SDR C2XA95IA081](https://openairdocs.org/sdr/C2XA95IA081.md): Seat Track · corroded · May 18, 1995 · N16719 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) - [SDR C2XA95IA079](https://openairdocs.org/sdr/C2XA95IA079.md): Angle · cracked · May 11, 1995 · N16719 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN TO FRAME ATTACH ANGLE CRACKED AT BOTH ENDS, FRAME 44 BETWEEN STRINGERS NR 1 LEFT AND NR 1 RIGHT. MAINTENACNE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA078](https://openairdocs.org/sdr/C2XA95IA078.md): Support · cracked · May 11, 1995 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 3RD LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA077](https://openairdocs.org/sdr/C2XA95IA077.md): Support · cracked · May 11, 1995 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 4TH LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA076](https://openairdocs.org/sdr/C2XA95IA076.md): Support · cracked · May 11, 1995 · N16719 · Emb EMB120RT · Wing Miscellaneous Structure > IAH- DURING C-CHECK INSPECTION, FOUND LT WING RIB NR 16, 4TH LOWER SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 11,865.9. CYCLES - 16,738. (X) Next page: https://openairdocs.org/deregistered/N16719-2000-01-14/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 = 'N16719' AND deregistration_id = 'N16719-2000-01-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16719-2000-01-14/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.