# Service difficulty reports: N31711, cancelled Jan 14, 2000 A list on [N31711, cancelled Jan 14, 2000](https://openairdocs.org/deregistered/N31711-2000-01-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR C2XA99IA224](https://openairdocs.org/sdr/C2XA99IA224.md): Selector · inoperative · Apr 19, 1999 · N31711 · Emb EMB120RT · Landing Gear Selector > IAH - DURING TAKEOFF ON FLIGHT 3660, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE GEAR RETRACTION HANDLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA164](https://openairdocs.org/sdr/C2XA99IA164.md): Stiffener · chafed · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon Structure > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP WELL STIFFENER CHAFED. REPLACED STIFFENER IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA163](https://openairdocs.org/sdr/C2XA99IA163.md): Stringer · cracked · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE PANEL 425 IMPROPERLY REPAIRED AT FORWARD INBOARD END. REMOVED RIVETS FROM EXISTING REPAIR AND FOUND EXTENSIVE DAMAGE TO STRINGER. REPLACED STRINGER IAW SRM 51-40-02 AND 51-70-04. AIRCRAFT APPR - [SDR C2XA99IA162](https://openairdocs.org/sdr/C2XA99IA162.md): Skin · worn · Feb 16, 1999 · N31711 · Emb EMB120RT · Trailing Edge Flaps > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP RIVETS PULLING THROUGH LOWER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-20-01 AND INSTALLED IAW SRM 51-40-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA161](https://openairdocs.org/sdr/C2XA99IA161.md): Frame · cracked · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED AT OUTBOARD COWL STAY FITTING. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 51-70-05 AND SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA160](https://openairdocs.org/sdr/C2XA99IA160.md): Frame · cracked · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED ON COWL FLANGE FOR PANEL 414. WELDED CRACKED AREA IAW MIL-STD-2219, NDT PENETRANT REVEALS NO CRACK EXISTS AFTER REPAIR. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA159](https://openairdocs.org/sdr/C2XA99IA159.md): Skin · gouged · Feb 16, 1999 · N31711 · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED BELOW GPU RECEPTACLE DOOR. REMOVED DAMAGED, FABRICATED FILLER AND DOUBLER REPAIR AND INSTALLED IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA158](https://openairdocs.org/sdr/C2XA99IA158.md): Frame · cracked · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FORWARD FRAME CRACKED AT INBOARD COWL STAY FITTING. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA157](https://openairdocs.org/sdr/C2XA99IA157.md): Angle · cracked · Feb 16, 1999 · N31711 · Emb EMB120RT · Nacelle/Pylon Structure > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE BYPASS DUCT SUPPORT ANGLE CRACKED. FABRICATED REPLACEMENT ANGLE IAW SRM 51-70-05 AND INSTALLED IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA156](https://openairdocs.org/sdr/C2XA99IA156.md): Skin · chafed · Feb 16, 1999 · N31711 · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN CHAFED BY HEAT EXCHANGER. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBLER REPAIR AND INSTALLED IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA550](https://openairdocs.org/sdr/C2XA98IA550.md): Latch · unlatched · Dec 29, 1998 · N31711 · Emb EMB120RT · Landing Gear Door Retract Section > IAH - FLT 3795 - THE CREW REPORTED A VIBRATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LANDING GEAR DOORS TO BE UNLATCHED. MAINTENANCE LATCHED THE GEAR DOORS, AND THE AIR - [SDR C2XA98CL022](https://openairdocs.org/sdr/C2XA98CL022.md): Water Separator · faulted · Mar 1, 1998 · N31711 · Emb EMB120RT · Humidity Control System > CLE - FLT 3116 - CREW REPORTED A DUCT LEAK LIGHT ON THE RIGHT ENGINE DURING DEPARTURE, CREW PERFORMED QRH ITEMS AND LIGHT EXTINGUISHED AT THE 3 MINUTE MARK. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 WATER - [SDR C2XA98CL007](https://openairdocs.org/sdr/C2XA98CL007.md): Actuator · out of adjust · Jan 25, 1998 · N31711 · Emb EMB120RT · Landing Gear Actuator > CLE - FLT 3114 - CREW REPORTED THAT WHEN GEAR WAS CYCLED UP THEY FELT A STRONG VIBRATION FROM THE LEFT MAIN GEAR WITH THE 'A' INDICATION REMAINING ILLUMINATED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE THE LEFT MAIN GEAR A - [SDR C2XA97IA264](https://openairdocs.org/sdr/C2XA97IA264.md): Engine · seized · Sep 10, 1997 · N31711 · Emb EMB120RT · Engine (Turbine/Turboprop) > VCT - FLT 3792 - THE PILOT NOTED 4 TO 5 LOUD BANGS EMITTED FROM THE RIGHT ENGINE WITH A NOTED RISE IN T-6 TEMPERATURE. THE CREW ELECTED TO SHUTDOWN THE ENGINE AND DIVERTED TO VCT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGINE SEIZED, AND REMOVED AN - [SDR C2XA97IA225](https://openairdocs.org/sdr/C2XA97IA225.md): Fitting · chafed · Aug 6, 1997 · N31711 · Emb EMB120RT · Trailing Edge Flaps > IAH - INSPECTION CHECK 1C, 2C, DURING ROUTINE INSPECTION, THE RIGHT OUTBOARD FLAP WAS FOUND TO BE CHAFED BEYOND LIMITS AT INBOARD ROLLER ATTACHMENT AREA. MAINTENANCE REPLACED THE INBOARD END CLOSURE FITTING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA97IA224](https://openairdocs.org/sdr/C2XA97IA224.md): Connect Section · cracked · Aug 6, 1997 · N31711 · Emb EMB120RT · Portable Oxygen System > IAH - INSPECTION CHECK 1C, 2C, DURING ROUTINE INSPECTION, THE VERTICAL STABILIZER TO HORIZONTAL STABILIZER LEFT FORWARD CONNECTING SECTION WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A REPAIR PER COEX EX NR 5530-01013, AND THE AIRCRAFT WAS LATER APPROVED F - [SDR C2XA97IA213](https://openairdocs.org/sdr/C2XA97IA213.md): Prox Switch · faulting · Jul 14, 1997 · N31711 · Emb EMB120RT · Landing Gear Position and Warning > IAH - FLT 3791 - THE PILOT REPORTED THAT AFTER TAKEOFF THE GEAR SELECTOR WAS PUT IN THE UP POSITION AND THE NOSE GEAR HAD AN UPLOCK AND AN INTRANSITION INDICATION AT THE SAME TIME. CREW CYCLED THE GEAR SELECTOR AND COULD NOT CLEAR THE INDICATION PROBLEM. THE - [SDR C2XA97CL058](https://openairdocs.org/sdr/C2XA97CL058.md): Hyd Pump · failed · Jun 15, 1997 · N31711 · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main > CLE - FLT 4054 - CREW REPORTED THAT DURING CRUISE FLIGHT AT 21,000 FEET THE GREEN SYSTEM HYDRAULIC MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY AND THE ELECTRIC PUMP CAME ON INTERMITTENTLY. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE - [SDR C2XA96CL042](https://openairdocs.org/sdr/C2XA96CL042.md): Actuator · failed · Nov 18, 1996 · N31711 · Emb EMB120RT · Landing Gear Actuator > SDF - FLT 4244 - CREW REPORTED THAT AFTER TAKEOFF, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT WAS FERRIED TO CLE, MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NOSE LANDING GEAR ACTUATOR IAW EMB 120 MM 32-32-11. ALL OPERATIONAL - [SDR C2XA96IA090](https://openairdocs.org/sdr/C2XA96IA090.md): Skin · cracked · Apr 11, 1996 · N31711 · Emb EMB120RT · Wing, Plate/Skin > IAH - DURING A 20,000 CYCLE INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND CRACKED AT THE OUTBOARD NACELLE CHORDWISE ATTACHMENT FLANGE FASTENER HOLE. MAINTENANCE OVERSIZED THE FASTENER HOLE, INSERTED A NEW FASTENER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO - [SDR C2XA96IA013](https://openairdocs.org/sdr/C2XA96IA013.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 16. THE SKIN SUPPORT IS LOCATED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA012](https://openairdocs.org/sdr/C2XA96IA012.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 2ND AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA011](https://openairdocs.org/sdr/C2XA96IA011.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA010](https://openairdocs.org/sdr/C2XA96IA010.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA009](https://openairdocs.org/sdr/C2XA96IA009.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 5TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA008](https://openairdocs.org/sdr/C2XA96IA008.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA007](https://openairdocs.org/sdr/C2XA96IA007.md): Support · cracked · Jan 5, 1996 · N31711 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA004](https://openairdocs.org/sdr/C2XA96IA004.md): Seat Track · corroded · Jan 4, 1996 · N31711 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING 1C INSPECTION, FOUND LEFT AFT LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA003](https://openairdocs.org/sdr/C2XA96IA003.md): Seat Track · corroded · Jan 4, 1996 · N31711 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING 1C INSPECTION, FOUND LEFT FORWARD LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA002](https://openairdocs.org/sdr/C2XA96IA002.md): Seat Track · corroded · Jan 4, 1996 · N31711 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING 1C INSPECTION, FOUND LEFT FORWRAD UPPER SEAT TRACK CORRODED AT FWD END. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA001](https://openairdocs.org/sdr/C2XA96IA001.md): Seat Track · corroded · Jan 4, 1996 · N31711 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING 1C INSPECTION, FOUND RIGHT FORWARD UPPER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA006](https://openairdocs.org/sdr/C2XA96IA006.md): Angle · cracked · Dec 24, 1995 · N31711 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE NACELLE FRAME 2 ATTACH ANGLE INBOARD SIDE CRACKED AT RIVETS. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96IA005](https://openairdocs.org/sdr/C2XA96IA005.md): Angle · cracked · Dec 24, 1995 · N31711 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME 2 ATTACH ANGLE CRACKED ON OUTBOARD END. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95CL126](https://openairdocs.org/sdr/C2XA95CL126.md): Uplock Actuator · out of adjust · Dec 12, 1995 · N31711 · Emb EMB120RT · Landing Gear Retraction/Extension System > GRR - FLT NR 3378 - AFTER TAKEOFF AND GEAR RETRACTION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE AN UP AND LOCKED CONDITION. THE LANDING GEAR WAS RECYCLED WITH THE SAME RESULTS. THE AIRCRAFT AIR RETURNED TO GRR. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJU - [SDR C2XA95CL105](https://openairdocs.org/sdr/C2XA95CL105.md): Oil Press Reg · out of adjust · Jul 27, 1995 · N31711 · Emb EMB120RT · Engine Oil Pressure > FLT NR 3357 - CLE - CRUISE FLIGHT LEFT ENGINE OIL PRESSURE ROSE TO 68/69 PSID, AS PER QRH REDUCED POWER TO 40 PERCENT, OIL PRESSURE REMAINED AT 66/68 PSID FOR REMAINDER OF FLIGHT. MAINTENANCE REMOVED TWO WASHERS FROM OIL PRESSURE REGULATOR IAW PWA 72-01-50 AN - [SDR C2XA95CL035](https://openairdocs.org/sdr/C2XA95CL035.md): Rollers · binding · Feb 11, 1995 · N31711 · Emb EMB120RT · Trailing Edge Flaps > FLT NR 3183 - CLE-CLE - AFTER TAKEOFF, UPON FLAP RETRACTION, GOT DISAGREEMENT WARNING. OUTBOARD AND INBOARD FLAPS STAYED DOWN TWO LIGHT BARS. MAINTENANCE CLEANED ALL FLAP TRACK AND INSPECTED THE ROLLERS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED ## 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 = 'N31711' AND deregistration_id = 'N31711-2000-01-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N31711-2000-01-14/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.