# Service difficulty reports: N59708, cancelled Sep 24, 1999 A list on [N59708, cancelled Sep 24, 1999](https://openairdocs.org/deregistered/N59708-1999-09-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 99ZZZX3196](https://openairdocs.org/sdr/99ZZZX3196.md): Stiffener · cracked · Aug 5, 1999 · N59708 · Emb EMB120RT · Nacelle/Pylon Structure > DURING CONTINENTAL EXPRESS C-CHECK, FOUND LT MLG WHEELWELL AFT BULKHEAD, OUTBOARD STIFFENER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-20-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS. TAC: 27,506. (X) - [SDR 99ZZZX3195](https://openairdocs.org/sdr/99ZZZX3195.md): Skin · chafed · Aug 5, 1999 · N59708 · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING CONTINENTAL EXPRESS 'C' CHECK, FOUND LT FUSELAGE SKIN CHAFED BY A/C HEAT EXCHANGER AT FS 9964.5. BLENDED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS. TAC: 27,506. (X - [SDR C2XA98IA301](https://openairdocs.org/sdr/C2XA98IA301.md): Light · inoperative · Aug 12, 1998 · N59708 · Emb EMB120RT · Emergency Lighting > IAH - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THAT THE LEFT AND RIGHT EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA241](https://openairdocs.org/sdr/C2XA98IA241.md): Bulb · failed · Jun 29, 1998 · N59708 · Emb EMB120RT · Emergency Lighting > IAH - FLT 3901 - DURING POST-FLIGHT INSPECTION, CREW REPORTED RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB, EMERGENCY LIGHTING SYSTEM CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) - [SDR C2XA98IA203](https://openairdocs.org/sdr/C2XA98IA203.md): Fuse · failed · Jun 14, 1998 · N59708 · Emb EMB120RT · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT ROW 6 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FUSE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA043](https://openairdocs.org/sdr/C2XA97IA043.md): Support · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE TOILET FLUSH VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA042](https://openairdocs.org/sdr/C2XA97IA042.md): Stringer · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER USING A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA041](https://openairdocs.org/sdr/C2XA97IA041.md): Seat Track · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA040](https://openairdocs.org/sdr/C2XA97IA040.md): Seat Track · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT 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 C2XA97IA039](https://openairdocs.org/sdr/C2XA97IA039.md): Seat Track · corroded · Jan 28, 1997 · N59708 · 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 C2XA97IA038](https://openairdocs.org/sdr/C2XA97IA038.md): Seat Track · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA037](https://openairdocs.org/sdr/C2XA97IA037.md): Seat Track · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT 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 C2XA97IA036](https://openairdocs.org/sdr/C2XA97IA036.md): Buttstrap · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP BETWEEN FRAMES 40 AND 44, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA035](https://openairdocs.org/sdr/C2XA97IA035.md): Buttstrap · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP BETWEEN FRAMES 39 AND 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA034](https://openairdocs.org/sdr/C2XA97IA034.md): Buttstrap · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP BETWEEN FRAMES 34 AND 38 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA97IA033](https://openairdocs.org/sdr/C2XA97IA033.md): Buttstrap · corroded · Jan 28, 1997 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 13 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA96CL045](https://openairdocs.org/sdr/C2XA96CL045.md): De-Ice Boot · torn · Dec 16, 1996 · N59708 · Emb EMB120RT · Airfoil Anti/De-ice System > CLE - FLT 3176 - CREW REPORTED THAT AFTER TAKEOFF ALL AIRCRAFT DE-ICE BOOTS FAILED. AIRCRAFT RETURN TO STATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT INBOARD WING DE-ICE BOOT IAW EMB-120 MM 30-10-01. OPERATIONAL CHECKS WERE GO - [SDR C2XA96CL014](https://openairdocs.org/sdr/C2XA96CL014.md): Flap Roller · binding · Feb 5, 1996 · N59708 · Emb EMB120RT · Trailing Edge Flaps > CLE - FLIGHT NR 3357 - CREW REPORTED THAT AFTER TAKEOFF WHEN FLAPS WERE SELECTED TO 0 DEGREES, A FLAP DISAGREEMENT OCCURRED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT AND LEFT OUTBOARD FLAP ROLLERS IAW EMB-120 MM 27-50-12. OPERATIONAL - [SDR C2XA96CL011](https://openairdocs.org/sdr/C2XA96CL011.md): Actuator · faulted · Feb 1, 1996 · N59708 · Emb EMB120RT · Trailing Edge Flap Actuator > CLE - FLT NR 3237 - CREW REPORTED THAT AFTER TAKEOFF AND FLAP RETRACTION THEY RECEIVED A FLAP DISAGREEMENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-02. OPERATIONAL CHECKS WERE GOOD IAW EMB- - [SDR C2XA96CL010](https://openairdocs.org/sdr/C2XA96CL010.md): Flap Annunciator · failed · Feb 1, 1996 · N59708 · Emb EMB120RT · Trailing Edge Flap Control System > CLE - FLT 3138 - CREW REPORTED THAT AFTER TAKEOFF AND FLAP RETRACTION, THEY RECEIVED A FLAP DISAGREEMENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP ANNUNCIATOR IAW EMB-120 MM 27-50-05. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50- - [SDR C2XA96CL004](https://openairdocs.org/sdr/C2XA96CL004.md): Actuator · out of adjust · Jan 22, 1996 · N59708 · Emb EMB120RT · Landing Gear Actuator > CLE - FLT NR 3338 - THE CREW REPORTED THAT AFTER TAKEOFF THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT, THE GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULTS. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE LEFT MAIN GEAR ACTUATOR IAW EMB 120MM 32-32-10, ALL O - [SDR C2XA95IA206](https://openairdocs.org/sdr/C2XA95IA206.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 18 LOWER NR 1 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES - 19,430. (X) - [SDR C2XA95IA205](https://openairdocs.org/sdr/C2XA95IA205.md): Stringer · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, FOUND LT WING STR 10 CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE STRINGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. REFERENCE EMBRAER FAXES EST 243/95 AND EST 376/95 FOR REPAIR PROCEDURES - [SDR C2XA95IA204](https://openairdocs.org/sdr/C2XA95IA204.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND THE NR 2 LOWER SKIN SUPPORT FOR LEFT WING RIB 18 CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA202](https://openairdocs.org/sdr/C2XA95IA202.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA201](https://openairdocs.org/sdr/C2XA95IA201.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA200](https://openairdocs.org/sdr/C2XA95IA200.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA199](https://openairdocs.org/sdr/C2XA95IA199.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 5 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA198](https://openairdocs.org/sdr/C2XA95IA198.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA197](https://openairdocs.org/sdr/C2XA95IA197.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, A/C RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA196](https://openairdocs.org/sdr/C2XA95IA196.md): Support · cracked · Aug 23, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, A/C RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) - [SDR C2XA95IA195](https://openairdocs.org/sdr/C2XA95IA195.md): Seat Track · corroded · Aug 23, 1995 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND CABIN RT SIDEWALL SEAT TRACK CORRODED. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95IA194](https://openairdocs.org/sdr/C2XA95IA194.md): Seat Track · corroded · Aug 23, 1995 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND CABIN FLOOR LEFT SEAT TRACK CORRODED. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95IA193](https://openairdocs.org/sdr/C2XA95IA193.md): Seat Track · corroded · Aug 23, 1995 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND CABIN SIDEWALL LEFT SEAT TRACK CORRODED AT FORWARD END. REMOVED AND REPLACED AFFECTED PORTION OF TRACK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95IA192](https://openairdocs.org/sdr/C2XA95IA192.md): Seat Track · corroded · Aug 23, 1995 · N59708 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, FOUND CABIN FLOOR LEFT SEAT TRACK CORRODED FORWARD OF GALLEY. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR C2XA95IA191](https://openairdocs.org/sdr/C2XA95IA191.md): Angle · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT FIN TO FUSELAGE ATTACH (DRAG) ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA190](https://openairdocs.org/sdr/C2XA95IA190.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA189](https://openairdocs.org/sdr/C2XA95IA189.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA188](https://openairdocs.org/sdr/C2XA95IA188.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA187](https://openairdocs.org/sdr/C2XA95IA187.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA186](https://openairdocs.org/sdr/C2XA95IA186.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA185](https://openairdocs.org/sdr/C2XA95IA185.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 5 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA184](https://openairdocs.org/sdr/C2XA95IA184.md): Skin Support · cracked · Aug 22, 1995 · N59708 · 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 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA183](https://openairdocs.org/sdr/C2XA95IA183.md): Skin Support · cracked · Aug 22, 1995 · N59708 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 2, NR 3, NR 4 AND NR 5 SKIN SUPPORTS CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) ## 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 = 'N59708' AND deregistration_id = 'N59708-1999-09-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N59708-1999-09-24/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.