N629AE
Service difficulty reports · 150
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 = 'N629AE' 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.
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 = 'N629AE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA201131304Skin · crackedDURING MAINTENANCE BASE VISIT FOUND FORWARD FUSELAGE II SKIN CRACKED AT LEFT WINDSHIELD SIDE POST UPPER END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1890. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201129702Fcu · inoperativeON FLIGHT 4154 THE CREW REPORTED THAT WHILE REACHING CRUISE ALT SELECTED CRZ TRUST RATING APPROX 20 SEC LATER EICAS WARNING FUEL 1 LO LEVEL CAUTION FUEL IMBALANCE. EICAS INDICATED NR 1 ENG 0 PPH 0 LBS FUEL. MFD FUEL PG INDICATED TANK 1 0LBS. FMS FUEL PAGE ISDR SIMA201115705Holder · brokenFOR FLIGHT 2769 DURING THE PREFLIGHT INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT CHARGER HOUSING BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT HOLDER ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16.SDR SIMA201115203Light · inoperativeFOR FLIGHT 2969 DURING THE PREFLIGHT INSPECTION FOUND THE LEFT FUSELAGE AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FUSELAGE AFT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATISDR SIMA201030505Connector · looseON FLIGHT 2915 DURING CRUISE THE CREW REPORTED FLAP INDICATOR INDICATED SEVERAL DIFFERENT DEGREE POSITION FROM 1 DEGREE TO 43 INTERMITTENTLY. EN ROUTE FLAPS DID NOT MOVE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVESDR SIMA201021507Light · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICSDR SIMA201014502Power Supply · inoperativeDURING THE MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201013801Mechanism · lack of lubeFOR FLIGHT 3243 PRIOR TO FLIGHT MAINTENANCE DISCOVERED THE SERVICE DOOR (CABIN) NEEDS TO BE LUBRICATED DUE TO IT WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SERVICE DOOR LINING PANEL PERFORMED SERVICE DOOR ACTUATING AND LOCKING MECHANISSDR SIMA201012705Battery · dischargedDURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD EXIT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY & CHARGER IAW EMB145 AMM TASK 33-50-04-000-801-A & 37--50-04-400-801-A. THE AIRCRAFT WASSDR SIMA201012704Light · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT OVERHEAD EMERGENCY LIGHT LAMP IAW AMM EMB 145 TASK33-50-08000-801A & 33-50-08-400-801A. THE AISDR SIMA201003905Skin · gougedDURING MAINTENANCE INSPECTION FOUND TWO GOUGES IN THE LOWER FORWARD FUSELAGE SKIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE TWO GOUGES IN THE LOWER FORWARD FUSELAGE SKIN IAW EO EM-53MR-1150 R2 PT C. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201003402Floor Support · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE CENTER CROSS BEAM CORRODED UNDER CROSS BEAM BETWEEN FRAME 24 AND FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CROSS BEAM IAW EMB 145 SRM 53-00-10 FIGURE 203, SHEET 2. THE AIRCRAFT WAS RETURNED TOSDR SIMA201003401Wire · brokenDURING MAINTENANCE BASE INSPECTION FOUND THAT THE LEFT NR 1 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH CONNECTORS IAW EMB 145 SWPM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201002901Skin · damagedDURING MAINTENANCE BASE VISIT FOUND THE SKIN ABOVE CENTER MOUNT ON LEFT ELEVATOR CRACKED / BENT. THE CRACK LENGTH IS APPROXIMATELY .9 / .7 INCHES. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE, INSTALLED DOUBLER IAW EMB SRM 55-20-01. THE AIRCRAFT WSDR SIMA200908202Ballast · failedON FLIGHT 4209 CREW REPORTED ELECTRICAL BURNING ODOR IN THE FWD CABIN GALLEY AREA. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED CEILING AND SIDE WALL BALLAST IAW AMM 33-21-03, IAW AMM 33-21-05 OPS CHECKED GOOD NO MORE BURNING SMELLS DETECTED. ACFT RETURNESDR SIMA200816801Light · malfunctionedON FLIGHT 3411 DURING PREFLIGHT THE CREW FOUND THE EMERGENCY EXIT IDENTIFIER OVER GALLEY AND THE OVERHEAD CENTER AISLE AT EMERGENCY EXIT ROW DOES NO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. WHEN MAINTENANCE ARRIVED ALL THE EMERGENCY LIGHTS WERE OPERATING ASDR SIMA200813403Inverter · inoperativeON FLIGHT 4036, CREW REPORTED EMERGENCY EXIT LIGHT IS INOPERATIVE OVER GALLEY SERVICE DOOR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER 2 (PS 8501-234) IAW EMB 145 33-50-11. OPERATIONAL CHECKED GOOD OF EMERGENCY LIGHT SYSTEM IAW EMB 145 ASDR SIMA200808107Sill · corrodedDURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND REPLACED WITH NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200808110Floor Support · corrodedDURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND CORRODED. REWORKED AREA IAW SRM 53-21-10, FIG 206. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200808112Floor Support · corrodedDURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 53-00-10, 53-20-03, 51-21-04 AND 51-21-05. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200808111Sill · corrodedDURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200712005Inverter · burnedSTRONG ELECTRICAL ODOR FOR ONE MINUTE AND THEN DISSIPATED. REMOVED AND REPLACED NR 1, NR 2 RECIRCULAR FANS AND NR 1 RECIRCULAR FAN INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR SIMA200602330Ecu · failedFLAP FAIL MESSAGE FLAP STUCK BETWEEN 0-8 DEGREES. REPLACED FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)SDR SIMA200228224Sill · corrodedDURING AN MBV INSPECTION, CORROSION WAS FOUND ON SERVICE DOOR CENTER SILL THAT WAS BEYOND SRM LIMITS. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE BLENDED AREAS. NO DEFECTS NOTED. FABRICATED THREE REPAIR DOUBLERS. REPAIR DONE IAW SRM.SDR SIMA200228217Floorbeam · corrodedDURING A IMBV INSPECTION LEFT HAND BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED BEAM. FABRICATED A FILLER, TWO SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM.SDR SIMA200228207Floorbeam · corrodedDURING AN IMBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM. REMOVED CORRODED GALLEY CENTER FLOORBEAM INSTALLED NEW BEAM IAW SRM.SDR SIMA200228220Floorbeam · corrodedDURING AN IMBV INSPECTION, THE DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUT OUT. FABRICATED A REPLACEMENT STRAP AND TWO DOUBLERS, SHIMS. REPAIR DONE IAW SRM.SDR SIMA200228222Doubler · corrodedDURING AN IMBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LEFT HAND OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM. NO ADDITIONAL DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS, PLATE. REPASDR SIMA200228223Floorbeam · corrodedDURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 29. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS. REPAIR DONE IAW SRM.SDR SIMA200228208Stringer · chafedDURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED. BLENDED CHAFE. PERFORMED AND NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIR DONE IAW SRM.SDR SIMA200228216Floorbeam · corrodedDURING AN IMBV INSPECTION THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 23. BLENDED THE DAMAGED AREA TO COMPLETELY REMOVED THE CORROSION. FABRICATED A U SHAPED DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200228226Sill · corrodedDURING AN IMBV INSPECTION OF AIRCRAFT, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED SERVICEABLE SILL IAW SRM.SDR SIMA200228218Frame · chafedDURING A IMBV INSPECTION FOUND LOWER FRAME 81 CHAFED BEYOND SRM LIMITS. REMOVED EXISTING LOWER FRAME 81. INSTALLED NEW FRAME IAW SRM.SDR SIMA200228225Sill · corrodedRIGHT SILL CORRODED BETWEEN FRAME 24 AND 29. PERFORMED EDDY CURRENT AND THICKNESS INSPECTION WITH NO DEFECTS FOUND. REPLACED SILL IAW GST.SDR SIMA200228Frame · corrodedSTRINGER 19L HAS CORROSION BETWEEN FRAMES 23 AND 24 UNDER FLOOR. PERFORMED EDDY CURRENT AND THICKNESS, NO DEFECTS. REPAIR DONE IAW GST.SDR SIMA200228205Sill · corrodedRIGHT HAND SILL IS CORRODED BETWEEN FRAME 29 AND 35. PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. REPAIRED RIGHT HAND SILL BETWEEN FR 29-35 IAW GST.SDR SIMA200228214Sill · corrodedCARGO DOOR SILL IS CORRODED. REMOVED AND INSTALLED NEW CARGO DOOR SILL IAW CPM.SDR SIMA200228206Floorbeam · corrodedLEFT HAND FLOOR BEAM GUSSET IS CORRODED BETWEEN FRAME 65-68. INSTALLED SERVICEABLE GUSSET IAW SRM.SDR SIMA200228221Floor Support · corrodedCENTER BEAM RAMP IS CORRODED. REMOVED AND INSTALLED NEW CENTER BEAM GUSSET IAW SRM.SDR SIMA200228215Floorbeam · corrodedPREVIOUS REPAIR AT FRAME 20 ON LEFT FLOORBEAM IS CORRODED. REPAIRED IAW SRM.SDR SIMA200228213Floorbeam · corrodedRIGHT FLOORBEAM CORRODED AT FRAME 23. REPAIRED IAW SRM.SDR SIMA200228212Angle · corrodedPROFILE AT FRAME 23 IS CORRODED. REMOVED AND REPAIRED PROFILE AND DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200228211Seat Track · corrodedSEAT TRACK CORRODED BETWEEN FRAMES 18 AND 23 ON LEFT FLOORBEAM. REMOVED AND REPLACED SEAT TRACK IAW AMM.SDR SIMA200228210Crossbeam · corrodedCROSSMEMBER AT FRAME 23 IS CORRODED. REMOVED CROSSMEMBER AND REPAIRED IAW SRM.SDR SIMA200228209Floor Support · corrodedPASSENGER DOOR FLOOR SUPPORT CORRODED. REMOVED AND INSTALLED SERVICEABLE SUPPORT IAW SRM.SDR SIMA200226802Stringer · chafedABI - DURING AN IMBV INSPECTION MAINTENANCE FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFED AREA. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB-145SDR SIMA200217301Engine · flamed outDISC - NR 2 ENGINE FLAME OUT DURING CRUISE. WOULD NOT RESTART. C/A REPLACED NR 2 ENGINE.SDR SIMA1713Drain Line · odorHSV - FLT 4403 - FLIGHT CREW DETECTED A STRONG SMELL OF JET FUEL/EXHAUST SMELL WHEN THE APU WAS ON. THE PACKS WERE ON AT THE TIME. APU PUT ON MEL. MAINTENANCE REMOVED AND REPLACED DRAIN HOSE FROM THE COLLECTOR TUBE TO THE APU DRAIN SYSTEM OUTLET IAW EMBRAERSDR SIMA0184Light · inoperativeDFW - FLT 3700 - FOUND EMERGENCY LIGHTS INOPERATIVE AT ROW 12. REMOVED AND REPLACED EMERGENCY LIGHTS AT ROW 12. OPS CHECK GOOD. (M)SDR SIMA993274Unknown · odorORD - FLT 4162 - STRONG FUEL ODOR IN CABIN NEAR PASSENGER SEAT ROWS 14 AND 15. INSPECTED AIRCRAFT EXTERNAL DRAINS AND PANELS. OPENED CABIN FLOOR PANELS AND PERFORMED ENGINE GROUND RUNS, BUT NO EVIDENCE OF LEAKS OR VAPORS WAS DETECTED OF ANY KIND. AIRCRAFT R
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