N11565

Service difficulty reports · 76

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N11565' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA06SH041Floor Support · corrodedSHV - DURING C CHECK, THE CENTER OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, STEP 4, FIG 203, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TOMar 28, 2006 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA06SH035Firewall · chafedSHV - DURING C CHECK, THE APU FIREWALL WAS FOUND TO BE CHAFED. DAMAGE WAS FOUND TO BE GREATER THAN 50 PERCENT OF MATERIAL THICKNESS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER AND FILLER REPAIR IAW EC 5330-01359, SEC 1.3. THE AIRCRAFT WAS Mar 22, 2006 · N11565 · Emb EMB145LR · APU Cowling/ContainmentSDR C2XA05IA089Sign · malfunctionedORF - DURING PREFLIGHT INSPECTION, THE FLIGHT CREW REPORTED THE SERVICE DOOR EXIT SIGN NOT ILLUMINATING WHEN TESTED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY EXIT LIGHTING SYSTEM AND THE SERVICE DOOR EXIT SIGN OPERATED NORMALLY WITHOUT ANY Jul 14, 2005 · N11565 · Emb EMB145LR · Emergency LightingSDR C2XA04SH341Doubler · corrodedDURING C CHECK THE RT OMEGA BEAM AFT DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 1, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH340Angle · corrodedDURING C CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 1, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH339Sill · corrodedSHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 7 FIG 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 1, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH334Sill · corrodedDURING C-CHECK, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH333Sill · corrodedDURING C-CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH332Skin · dentedSHV-DURING C CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 19A AND STRINGER 12L. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-22-01 STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR C2XA04SH331Stiffener · chafedDURING C CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH330Floorbeam · corrodedDURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH328Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Passenger/Crew DoorsSDR C2XA04SH327Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Passenger/Crew DoorsSDR C2XA04SH326Floorbeam · corrodedSHV-DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH325Floorbeam · corrodedSHV-DURING C CHECK THE SHELL PLATE ON TOP OF THE CENTER OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH324Firewall · crackedDURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13 SECTION 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · APU Cowling/ContainmentSDR C2XA04SH323Stiffener · gougedSHV-DURING C CHECK THE T REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH322Intake · gougedDURING C-CHECK THE NR 2 INTAKE WAS FOUND TO BE GOUGED AT 12 O'CLOCK. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 26, 2004 · N11565 · Emb EMB145LR · Engine Air Intake SystemSDR C2XA04SH321Intake · gougedSHV - DURING C-CHECK THE NR 1 ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 26, 2004 · N11565 · Emb EMB145LR · Engine Air Intake SystemSDR C2XA04SH320Sill · corrodedSHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 26, 2004 · N11565 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03CL176Inverter · inoperativeCLE FLIGHT 2317 THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE INVERTER. OPERATIONAL CHECKS WERE GOOD.Oct 22, 2003 · N11565 · Emb EMB145LR · Emergency LightingSDR C2XA03CL162Inverter · inoperativeCLE FLIGHT 2058 THE CREW REPORTED 2 EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Sep 10, 2003 · N11565 · Emb EMB145LR · Emergency LightingSDR C2XA03CL137Inverter · inoperativeCLT FLIGHT NR 2223 THE CREW REPORTED NR 1 FLOOR PROXIMITY STRIP INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER,OPERATIONAL CHECKS WERE GOOD.Aug 5, 2003 · N11565 · Emb EMB145LR · Emergency LightingSDR C2XA03CL124Wire · looseTHE CREW REPORTED THE FIRST ROW OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE RESECURED WIRE, OPERATIONAL CHECKS WERE GOOD.Jul 14, 2003 · N11565 · Emb EMB145LR · Light System WiringSDR C2XA03CL103Inverter · inoperativeCLE FLIGHT 2104 THE CREW REPORTED THE FIRST SECTION OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.May 24, 2003 · N11565 · Emb EMB145LR · Emergency LightingSDR C2XA02IA155Brake · failedCREW REPORTED THAT ON DESCENT THE FLAPS WOULD NOT EXTEND. THE AIRCRAFT ACCOMPLISHED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FLAP TRANSMISSION BRAKE TO HAVE FAILED. THE AFFECTED FLAP BRAKE WAS REMOVED AND REPLACED,Aug 3, 2002 · N11565 · Emb EMB145LR · Trailing Edge Flap Control System
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