# Service difficulty reports: N16702, cancelled Jun 30, 1999 A list on [N16702, cancelled Jun 30, 1999](https://openairdocs.org/deregistered/N16702-1999-06-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR C2XA99IA330](https://openairdocs.org/sdr/C2XA99IA330.md): Angle · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT SIDEWALL/FLOOR ANGLE FROM FRAME 41 TO 44. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA329](https://openairdocs.org/sdr/C2XA99IA329.md): Angle · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT SIDEWALL/FLOOR ANGLE FROM FRAME 31-35. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA328](https://openairdocs.org/sdr/C2XA99IA328.md): Sill · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT OUTBOARD BUTT STRAP FROM FRAME 15 TO FRAME 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA327](https://openairdocs.org/sdr/C2XA99IA327.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD BUTT STRAP FROM FRAME 14 TO FRAME 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA326](https://openairdocs.org/sdr/C2XA99IA326.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 30 TO FRAME 35. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA324](https://openairdocs.org/sdr/C2XA99IA324.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 35 TO FRAME 38. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA323](https://openairdocs.org/sdr/C2XA99IA323.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FRAMES 40, 42 AND 44. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA322](https://openairdocs.org/sdr/C2XA99IA322.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT RBL 19 FROM FRAME 39 TO FRAME 40. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA321](https://openairdocs.org/sdr/C2XA99IA321.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD STRAP FROM STATION 66531.1 TO 87280.0. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA320](https://openairdocs.org/sdr/C2XA99IA320.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CENTER BUTT STRAP FROM STATION 87280.0 TO 99645.0. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA319](https://openairdocs.org/sdr/C2XA99IA319.md): Beam · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON OMEGA BEAM LBL 19 AT FRAMES 40, 42 AND 44. REPAIRED OMEGA BEAM IAW EC5310-01043. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA318](https://openairdocs.org/sdr/C2XA99IA318.md): Crossbeam · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CROSSBEAM FROM RBL 19 TO RBL 31 AT FRAME 38. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA317](https://openairdocs.org/sdr/C2XA99IA317.md): Strap · corroded · Jun 1, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT INBOARD BUTT STRAP FROM FRAME 13 TO 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA99IA325](https://openairdocs.org/sdr/C2XA99IA325.md): Strap · corroded · Jan 6, 1999 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT BL 0 FROM FRAME 35 TO FRAME 39. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98CL009](https://openairdocs.org/sdr/C2XA98CL009.md): Np Gauge · inoperative · Feb 4, 1998 · N16702 · Emb EMB120RT · Propeller Indication System > CLE - FLT 3172 - CREW REPORTED THAT WHILE TAXIING FOR TAKEOFF THE RIGHT ENGINE NP GAUGE WAS INOPERTIVE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT ENGINE NP GAUGE IAW EMB-120 MM 61-40-00. OPERATIONAL CH - [SDR C2XA97IA174](https://openairdocs.org/sdr/C2XA97IA174.md): Power Supply · inoperative · May 23, 1997 · N16702 · Emb EMB120RT · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE PILOT REPORTED THAT THE FORWARD EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97CL045](https://openairdocs.org/sdr/C2XA97CL045.md): Bulb · failed · Apr 19, 1997 · N16702 · Emb EMB120RT · Emergency Lighting > CLE - DURING A SCHEDULED INSPECTION, LEFT HAND AFT FUSELAGE EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND AFT FUSELAGE EXTERIOR EMERGENCY LIGHT BULB IAW EMB-120 MM 33-52-01, OPERATIONAL CHECKS WERE SATISFACTORY - [SDR C2XA97CL044](https://openairdocs.org/sdr/C2XA97CL044.md): Bulb · burned out · Apr 19, 1997 · N16702 · 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 LIGHT BULB IAW EMB-120 MM 33-52-01. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT R - [SDR C2XA97CL024](https://openairdocs.org/sdr/C2XA97CL024.md): Bulb · failed · Mar 19, 1997 · N16702 · Emb EMB120RT · Emergency Lighting > CLE - DURING A SCHEDULED INSPECTINO THE FORWARD CEILING MOUNTED EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY, THEN REMOVED AND REPLACED THE BULB. OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB 120 MM 33-51-01. AIRCRAF - [SDR C2XA97CL013](https://openairdocs.org/sdr/C2XA97CL013.md): De-Ice Boot · ruptured · Feb 5, 1997 · N16702 · Emb EMB120RT · Air Intake Anti/De-Ice System > CLE - FLT 3293 - CREW REPORTED THAT BOTH THE LEFT AND RIGHT ENGINE AIR INLET DE-ICE SYSTEMS FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE AIR INLET DE-ICE BOOT IAW EMB 120 ER MM - [SDR C2XA96CL040](https://openairdocs.org/sdr/C2XA96CL040.md): Garlock Seal · worn · Nov 11, 1996 · N16702 · Emb EMB120RT · Turbine Engine Accessory Drive > CLE - FLT 3121 - CREW REPORTED THAT THEY NOTICED A OIL LEAK ON THE RIGHT ENGINE IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT ENGINE STARTER GENERATOR GARLOCK SEAL AND SHAFT O-RING IAW PW MM 72-01-50 - [SDR C2XA95IA383](https://openairdocs.org/sdr/C2XA95IA383.md): Rib · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 20 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED NOSE RIB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA382](https://openairdocs.org/sdr/C2XA95IA382.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA381](https://openairdocs.org/sdr/C2XA95IA381.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA380](https://openairdocs.org/sdr/C2XA95IA380.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA379](https://openairdocs.org/sdr/C2XA95IA379.md): Support · cracked · Dec 5, 1995 · N16702 · 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 BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA378](https://openairdocs.org/sdr/C2XA95IA378.md): Support · cracked · Dec 5, 1995 · N16702 · 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 BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA377](https://openairdocs.org/sdr/C2XA95IA377.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 19, LOWER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA376](https://openairdocs.org/sdr/C2XA95IA376.md): Support · cracked · Dec 5, 1995 · N16702 · 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 BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA375](https://openairdocs.org/sdr/C2XA95IA375.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA374](https://openairdocs.org/sdr/C2XA95IA374.md): Support · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 23, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA372](https://openairdocs.org/sdr/C2XA95IA372.md): Mount · cracked · Dec 5, 1995 · N16702 · Emb EMB120RT · Cargo/Baggage Doors > IAH - DURING C-CHECK INSPECTION, FOUND THE CARGO DOOR TORSION BAR FORWARD MOUNT TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA371](https://openairdocs.org/sdr/C2XA95IA371.md): Profile · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA370](https://openairdocs.org/sdr/C2XA95IA370.md): Seat Track · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT FORWARD LOWER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA369](https://openairdocs.org/sdr/C2XA95IA369.md): Seat Track · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA368](https://openairdocs.org/sdr/C2XA95IA368.md): Seat Track · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT LOWER FORWARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA367](https://openairdocs.org/sdr/C2XA95IA367.md): Seat Track · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA366](https://openairdocs.org/sdr/C2XA95IA366.md): Floor Support · corroded · Dec 5, 1995 · N16702 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SUPPORT CORRODED FROM FRAME 38.5 TO 40. MAINTENANCE REMOVED AND REPLACED THE SECTION OF FLOOR SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA365](https://openairdocs.org/sdr/C2XA95IA365.md): Seat Track · corroded · Dec 5, 1995 · N16702 · 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. (M) - [SDR C2XA95IA364](https://openairdocs.org/sdr/C2XA95IA364.md): Angle · cracked · Dec 4, 1995 · N16702 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF.EMB FAX EST435/95. (M) - [SDR C2XA95CL108](https://openairdocs.org/sdr/C2XA95CL108.md): Control Panel · malfunctioned · Aug 3, 1995 · N16702 · Emb EMB120RT · Weather Radar System > FLT NR 3265 - CLE-CVG - RADAR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD IAW EMB MM 34-41-00, 34-41-01, 34-41-02. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95CL107](https://openairdocs.org/sdr/C2XA95CL107.md): Rt Unit · failed · Aug 3, 1995 · N16702 · Emb EMB120RT · Weather Radar System > FLT NR 3265 - CLE-CVG - RADR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD IAW EMB MM 34-41-00, 34-41-01, 34-41-02. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95CL052](https://openairdocs.org/sdr/C2XA95CL052.md): Clip · sheared · Mar 26, 1995 · N16702 · Emb EMB120RT · Brake Anti-Skid Section > FLT 3232 - DAY-CLE - BRAKES FAILED WITH ANTI-SKID ON. MAINTENANCE REMOVED AND REPLACED NR 3 WHEEL SPEED TRANSDUCER CLIP. OPS CHECK GOOD IAW EMB-120 MM 32-42-00. AIRCRAFT RETURNED TO SERVICE. (W) - [SDR C2XA95CL025](https://openairdocs.org/sdr/C2XA95CL025.md): Rollers · binding · Feb 11, 1995 · N16702 · Emb EMB120RT · Trailing Edge Flaps > FLT NR 3337 - PIT-CLE - FLAP DISAGREEMENT AFTER TAKEOFF, 1 MINUTE LATER CLEARED ITSELF. AFTER LANDING IN CLE MAINTENANCE CLEANED FLAP TRACKS AND ROLLERS. AIRCRAFT WAS SENT ON A TEST FLIGHT. TEST FLIGHT WAS UNSATISFACTORY. MAINTENANCE REMOVED AND REPLACED L - [SDR C2XA95CL018](https://openairdocs.org/sdr/C2XA95CL018.md): Hyd Pump · failed · Feb 7, 1995 · N16702 · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main > CLE-DAY - FLT 3223 - THE LT MAIN HYDRAULIC PUMP FAILED IN FLIGHT. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW EMB MM 29-10-03. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) - [SDR C2XA95CL006](https://openairdocs.org/sdr/C2XA95CL006.md): Prox Sensor · failed · Jan 19, 1995 · N16702 · Emb EMB120RT · Landing Gear Retraction/Extension System > DAY\CLE - FLT 3285 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT AIR RETURNED TO DAY. MAINTENANCE SWAPPED LEFT UPLOCK 'A' AND 'B' SYSTEM CANNON PLUGS IAW SNL 120-032-0015. OPS CHECK GOOD. PLACED 'B' SYSTEM INDICATION ON MEL 32-60-01, CONTROL NR 769924. - [SDR C2XA95CL004](https://openairdocs.org/sdr/C2XA95CL004.md): Control Box · failed · Jan 16, 1995 · N16702 · Emb EMB120RT · Landing Gear Retraction/Extension System > CORRECTED SDR. DTW\CLE - FLT 3142 - ON CLIMB-OUT, SELECTED GEAR RETRACTION. SIX GREEN LIGHTS REMAIN ILLUMINATED ALONG WITH FIVE RED GEAR LIGHTS. LEFT 'B' RED GEAR LIGHT ONLY ONE NOT ILLUMINATED. GEAR DID NOT MOVE. MAINTENANCE SWAPPED LEFT GEAR 'A' AND 'B' ## 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 = 'N16702' AND deregistration_id = 'N16702-1999-06-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N16702-1999-06-30/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.