# Service difficulty reports: N15725, cancelled Oct 24, 2007 A list on [N15725, cancelled Oct 24, 2007](https://openairdocs.org/deregistered/N15725-2007-10-24.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 C2XA01IA377](https://openairdocs.org/sdr/C2XA01IA377.md): Clamp · loose · Oct 16, 2001 · N15725 · Emb EMB120ER · Cabin Cooling System > IAH- FLIGHT 3442 NOTED SMOKE WARNING ON MAP, FOLLOWED BY #2 PACK FAIL IN FLIGHT. RAN QRH ON BOTHWARNINGS, AND, RETURNED TO IAH. BOTH WARNINGS CLEARED ON RETURN TO IAH. IAH- MAINTENANCE TIGHTENED CLAMPS ON NUMBER 2 HEAT EXCHANGER,PERFORMED A OPERATIONAL CH - [SDR C2XA01IA356](https://openairdocs.org/sdr/C2XA01IA356.md): Connector · loose · Sep 5, 2001 · N15725 · Emb EMB120ER · Emergency Lighting > IAH- DURING PERFLIGHT THE CREW NOTED THAT THE LAST ROW OF EMERGENCY LIGHTING ON THE FLOOR DID NOT ILLUMINATE. IAH- MAINTENANCE RESECURED THE EMERGENCY LIGHT CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED,AND, THE A - [SDR C2XA01IA287](https://openairdocs.org/sdr/C2XA01IA287.md): Frame · cracked · Jun 22, 2001 · N15725 · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib > IAH - DURING 2A INSPECTION, THE LEFT HAND NACELLE LOWER HALF FRAME FOR THE OUTBOARD AFT GEAR DOOR WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED FRAME IN ACCORDANCE WITH EMB120-SRM 54-20-04, AND THE AIRCRAFT WAS APPROVED FOR R - [SDR C2XA01IA263](https://openairdocs.org/sdr/C2XA01IA263.md): Smoke · detected · Jun 4, 2001 · N15725 · Emb EMB120ER · Air Distribution System > SHV - THE CREW REPORTED SMOKE IN THE CABIN, MAINTENANCE RESET THE RIGHT MAIN LANDING GEAR AIR/GROUND CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA01IA251](https://openairdocs.org/sdr/C2XA01IA251.md): Door · unlatched · May 21, 2001 · N15725 · Emb EMB120ER · Landing Gear Door Retract Section > IAH - FLIGHT 2913, THE CREW REPORTED A NOSE GEAR UNSAFE LIGHT DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RELATCHED THE LEFT HAND FORWARD MAIN LANDING GEAR DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN - [SDR C2XA01IA249](https://openairdocs.org/sdr/C2XA01IA249.md): Power Supply · inoperative · May 18, 2001 · N15725 · Emb EMB120ER · Emergency Lighting > IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA01IA196](https://openairdocs.org/sdr/C2XA01IA196.md): Hose · loose · Apr 4, 2001 · N15725 · Emb EMB120ER · Air Distribution System > IAH - FLIGHT 3454, THE CREW REPORTED SMOKE IN THE CABIN SHORTLY AFTER DEPARTURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED A LOOSE HOSE ON THE LEFT HAND AIR CYCLE MACHINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO - [SDR C2XA01IA127](https://openairdocs.org/sdr/C2XA01IA127.md): Sensor · out of adj · Feb 22, 2001 · N15725 · Emb EMB120ER · Landing Gear Position and Warning > SHV - FLIGHT 3443, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN GEAR UPLOCK PROXIMITY SENSOR IN ACCORDANCE WITH EMB-12 - [SDR C2XA01IA020](https://openairdocs.org/sdr/C2XA01IA020.md): Battery Pack · discharged · Jan 31, 2001 · N15725 · Emb EMB120RT · Emergency Lighting > IAH - FLT 2926 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHTS WOULD NOT OPERATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POSITION EMERGENCY LIGHT BATTERY PACK IAW EMB-120 MM 33-50-02. THE AIRCRAFT WAS APPROVED FOR RE - [SDR C2XA00IA102](https://openairdocs.org/sdr/C2XA00IA102.md): Strap · corroded · Apr 10, 2000 · N15725 · Emb EMB120RT · Fuselage Main, Structure > DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CARGO BAY CENTER FLOOR SUPPORT CORRODED. REMOVED AND REPLACED CENTER FLOOR SUPPORT IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00IA101](https://openairdocs.org/sdr/C2XA00IA101.md): Frame · cracked · Apr 10, 2000 · N15725 · Emb EMB120RT · Nacelle/Pylon, Main Frame > DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND RIGHT ENGINE NACELLE, FRAME NR 1 CRACKED. REMOVED AND REPLACED RIGHT ENGINE NACELLE FRAME NR 1 IAW CONTINENTAL EXPRESS EC 5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA00IA100](https://openairdocs.org/sdr/C2XA00IA100.md): Wire · chafed · Apr 10, 2000 · N15725 · Emb EMB120RT · Fuel System Wiring > RIGHT FUEL QTY INDICATOR FLUCTUATES IN FLIGHT. FOUND RIGHT NR 3 FUEL PROBE WIRING CHAFING AND SHORTING ON FUEL LINE INSIDE RIGHT FUEL TANK. INSULATED WIRE WITH HEAT SHRINK AND SECURED WIRING TO PREVENT FURTHER CHAFING IAW AWM 20-21-00. FUNCTIONAL CHECK OF F - [SDR C2XA99CL058](https://openairdocs.org/sdr/C2XA99CL058.md): Relay Box · failed · Jul 21, 1999 · N15725 · Emb EMB120RT · Landing Gear Retraction/Extension System > CLE - FLT 3180 - THE CREW REPORTED THAT DURING GEAR RETRACTION, THEY FELT A STRONG VIBRATION AND HEARD A LOUD RUMBLING NOISE FROM THE NOSE GEAR AREA. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GE - [SDR C2XA99IA316](https://openairdocs.org/sdr/C2XA99IA316.md): Battery Pack · discharged · Jun 16, 1999 · N15725 · Emb EMB120RT · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION, THE AFT FIVE AISLE PATH EMERGNECY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA98IA449](https://openairdocs.org/sdr/C2XA98IA449.md): Angle · cracked · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5530-01013. THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR C2XA98IA448](https://openairdocs.org/sdr/C2XA98IA448.md): Angle · cracked · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REPAIRED THE ANGLE IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR EC5530-01013. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA447](https://openairdocs.org/sdr/C2XA98IA447.md): Skin · damaged · Oct 27, 1998 · N15725 · Emb EMB120RT · Elevator, Plate/Skin > IAH - DURING C-CHECK INSPECTION, THE LEFT ELEVATOR WAS FOUND TO HAVE LIGHTENING STRIKE DAMAGE. MAINTENANCE REPAIRED THE AFFECTED AREAS OF THE ELEVATOR IAW EMB 120 SRM 55-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA446](https://openairdocs.org/sdr/C2XA98IA446.md): Seat Track · corroded · Oct 27, 1998 · N15725 · 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 PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA445](https://openairdocs.org/sdr/C2XA98IA445.md): Seat Track · corroded · Oct 27, 1998 · N15725 · 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 PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA444](https://openairdocs.org/sdr/C2XA98IA444.md): Support · cracked · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTIONS, THE SUPPORTS FOR THE COCKPIT ENTRY STEP WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS IAW THE EMB120 SRM. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA443](https://openairdocs.org/sdr/C2XA98IA443.md): Beam · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. REFERENCE EMB120 SRM 51-40-02. (M) - [SDR C2XA98IA442](https://openairdocs.org/sdr/C2XA98IA442.md): Beam · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CEHCK INSPECTION, THE CREASE BEAM AT FRAME 44 TO FRAME 47 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM IAW THE EMB 120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA441](https://openairdocs.org/sdr/C2XA98IA441.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP AT FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA440](https://openairdocs.org/sdr/C2XA98IA440.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. - [SDR C2XA98IA439](https://openairdocs.org/sdr/C2XA98IA439.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SER - [SDR C2XA98IA438](https://openairdocs.org/sdr/C2XA98IA438.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER BUTTSTRAP AT FRAME 28 TO FRAME 33 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA437](https://openairdocs.org/sdr/C2XA98IA437.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 33 TO FRAME 38, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA436](https://openairdocs.org/sdr/C2XA98IA436.md): Seat Track · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB 120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA435](https://openairdocs.org/sdr/C2XA98IA435.md): Strap · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT SIDE BUTTSTRAP AT FRAME 13A WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA434](https://openairdocs.org/sdr/C2XA98IA434.md): Stringer · cracked · Oct 27, 1998 · N15725 · Emb EMB120RT · Wing, Longeron/Stringer > IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE AFFECTED PORTION OF STRINGER AND INSTALLED A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010. THE AIRCRA - [SDR C2XA98IA433](https://openairdocs.org/sdr/C2XA98IA433.md): Trunnion · corroded · Oct 27, 1998 · N15725 · Emb EMB120RT · Nose/Tail Landing Gear Attach Section > IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR LOWER TRUNNION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA98IA362](https://openairdocs.org/sdr/C2XA98IA362.md): Harness · failed · Sep 12, 1998 · N15725 · Emb EMB120RT · Landing Gear Retraction/Extension System > IAH - FLT 3893 - THE CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE 'A' SYSTEM DOWNLOCK PROXIMITY SWITCH WIRING HARNESS, AND THE AIRCRAFT WAS APPROVED FOR RETURN - [SDR C2XA96CL047](https://openairdocs.org/sdr/C2XA96CL047.md): Roller Assembly · lack of lube · Dec 19, 1996 · N15725 · Emb EMB120RT · Landing Gear Retraction/Extension System > CLE - FLT 3199 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION THE NOSE GEAR A/B RED LIGHTS STAYED ILLUMINATED ASSOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED AND LUBRICATED THE UPLOCK HOOK R - [SDR C2XA96CL046](https://openairdocs.org/sdr/C2XA96CL046.md): Prox Switch · dirty · Dec 19, 1996 · N15725 · Emb EMB120RT · Landing Gear Position and Warning > CLE - FLT 3283 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE NOSE LANDING GEAR A/B RED LIGHTS STAYED ILLUMINATED ASSOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED THE NOSE LANDING GEAR P - [SDR C2XA96CL017](https://openairdocs.org/sdr/C2XA96CL017.md): Flap Contl Unit · failed · Feb 12, 1996 · N15725 · Emb EMB120RT · Trailing Edge Flap Control System > LAN - FLIGHT NR 3120 - CREW REPORTED, THAT AFTER TAKEOFF THEY HAD AN OUTBOARD FLAP DISAGREEMENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIR - [SDR C2XA95IA284](https://openairdocs.org/sdr/C2XA95IA284.md): Skin Support · cracked · Oct 7, 1995 · N15725 · 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 SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA283](https://openairdocs.org/sdr/C2XA95IA283.md): Skin Support · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA282](https://openairdocs.org/sdr/C2XA95IA282.md): Skin Support · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 5 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA281](https://openairdocs.org/sdr/C2XA95IA281.md): Drag Angle · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Horizontal Stabilizer Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA280](https://openairdocs.org/sdr/C2XA95IA280.md): Skin Support · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA279](https://openairdocs.org/sdr/C2XA95IA279.md): Nose Rib · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing, Rib/Bulkhead > IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 17 WAS FOUND TO BE CRACKED ALONG THE UPPER EDGE. MAINTENANCE REPAIRED THE RIB BY REMOVING THE CRACKED PORTION AND INSERTING A SPLICE ANGLE. ALL WORK WAS ACCOMPLISHED IN REFERENCE TO EMBRAER DER FAX E - [SDR C2XA95IA278](https://openairdocs.org/sdr/C2XA95IA278.md): T-Cap · corroded · Oct 7, 1995 · N15725 · Emb EMB120RT · Fuselage Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT T-CAP, AT FRAME 36, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-CAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA277](https://openairdocs.org/sdr/C2XA95IA277.md): Skin Support · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA276](https://openairdocs.org/sdr/C2XA95IA276.md): Skin Support · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Wing Miscellaneous Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 22, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA275](https://openairdocs.org/sdr/C2XA95IA275.md): Angle · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA274](https://openairdocs.org/sdr/C2XA95IA274.md): Angle · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Nacelle/Pylon Structure > IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA273](https://openairdocs.org/sdr/C2XA95IA273.md): Mount · cracked · Oct 7, 1995 · N15725 · Emb EMB120RT · Cargo/Baggage Doors > IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR FORWARD TORSION BAR MOUNT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95IA272](https://openairdocs.org/sdr/C2XA95IA272.md): Seat Track · corroded · Oct 7, 1995 · N15725 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE LEFT 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 C2XA95IA271](https://openairdocs.org/sdr/C2XA95IA271.md): Seat Track · corroded · Oct 7, 1995 · N15725 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings > IAH - DURING C-CHECK INSPECTION, THE RIGHT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) - [SDR C2XA95CL104](https://openairdocs.org/sdr/C2XA95CL104.md): Control · intermittent · Jul 26, 1995 · N15725 · Emb EMB120RT · Inertial Guidance System > FLT NR 3363 - IND-CLE - CAPTAINS BRAKES FAILED DURING TAXI, FIRST OFFICERS WORKED NORMAL. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW EMB MM 32-42-03. OPS CHECKED GOOD. (M) Next page: https://openairdocs.org/deregistered/N15725-2007-10-24/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 = 'N15725' AND deregistration_id = 'N15725-2007-10-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15725-2007-10-24/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.