N12552

Service difficulty reports · 73

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 = 'N12552' 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 C2XA08SH057Attach Bracket · damagedSHV - DURING C-CHECK LT HORIZONTAL STABILIZER ACTUATOR ATTACHMENT POINT O/B LUG O/B HAT BUSHING HOLE IS ELONGATED. MX REMOVED AND REPLACED LT UPPER HORIZONTAL STAB ACTUATOR ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-04 (DRILLING), 51-20-01 (SEALING), SRM 51-40-Apr 6, 2008 · N12552 · Emb EMB145LR · Stabilizer ActuatorSDR C2XA06BT005Battery · faultyDURING ROUTINE MAINTENANCE FOUND THE AFT OVERWING AND CABIN EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED NR 3 AND NR 4 BATTERY ASSEMBLIES. OPS CHECKED GOOD OF EMERGENCY LIGHTS IAW EMB145 33-50-04.Feb 2, 2006 · N12552 · Emb EMB145LR · Emergency LightingSDR C2XA06CL016Odor · detectedCLE FLIGHT 2266, THE CREW REPORTED THE NR 1 PACK HAD A OIL LIKE SMELL. MAINTENANCE INSPECTED AND PLACED THE NR 1 PACK SYSTEM ON MEL IAW 21-51-00/02. ON 2/2/06 MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE NR 1 PACK SYSTEM. NO DEFECTS WERE FOJan 31, 2006 · N12552 · Emb EMB145LR · Cabin Cooling SystemSDR C2XA06SH002Firewall · crackedSHV - DURING C CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, FIG 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 8, 2006 · N12552 · Emb EMB145LR · APU Cowling/ContainmentSDR C2XA05CL055Battery · dischargedDURING ROUTINE MAINTENANCE THE FIRST OFFICER'S EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY. OPERATIONAL CHECKS WERE GOOD.Jun 29, 2005 · N12552 · Emb EMB145LR · Emergency LightingSDR C2XA04SH139Light · inoperativeSHV - DURING C-CHECK, THE NUMBER FIVE EMERGENCY AISLE PATH LIGHT WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE AISLE PATH LIGHT ASSEMBLY IAW EMB 145 SRM 33-50-12. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEMar 4, 2004 · N12552 · Emb EMB145LR · Emergency LightingSDR C2XA04SH132Panel · crackedSHV- DURING C-CHECK THE RIGHT HAND MAIN LANDING GEAR WHEEL WELL AFT RIB PANEL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PANEL IAW EMB 145 IPC 53-04-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 2, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH128Sill · corrodedSHV-DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AT FRAME 22, STRINGER 15 RIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 29, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH127Structure · chafedSHV- DURING C-CHECK THE RIGHT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Engine Cowling SystemSDR C2XA04SH126Angle · corrodedSHV- DURING 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH125Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH124Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH123Intake · gougedSHV- DURING C-CHECK THE NR 1 ENGINE AIR INTAKE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Engine Air Intake SystemSDR C2XA04SH122Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE AFT FLANGE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Engine Air Intake SystemSDR C2XA04SH121Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT AND RIGHT UPPER APU MOUNTS. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Main, BulkheadSDR C2XA04SH120Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH119Threshold · corrodedSHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED AT FRAME 21. 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH118Bracket · corrodedSHV- DURING C-CHECK THE MAIN DOOR U-BRACKET AT FRAME 17 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH117Bracket · corrodedSHV- DURING C-CHECK THE MAIN DOOR THRESHOLD U-BRACKET AT FRAME 16 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH116Angle · corrodedSHV- DURING 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA04SH115Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH114Stringer · gougedSHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND FRAME 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.Feb 27, 2004 · N12552 · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR C2XA02CL190Fire Loop · chafedCLE FLIGHT NR 3242, CREW REPORTED ENGINE NR 2 FIRE DETECT FAIL MESSAGE. MAINTENANCE INSPECTED AND FOUND THE FIRE LOOP WAS CHAFED. THE NR 2 ENGINE FIRE LOOP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.Sep 30, 2002 · N12552 · Emb EMB145LR · Fire Detection
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