N715AE

Service difficulty reports not matched to an aircraft · 18

They name N715AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N715AE' AND registry_match IS NULL
  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 SIMA200812109Controller · odorON FLIGHT 4684, CREW REPORTED A ACRID SMELL IN COCKPIT ON APPROACH TURNED OFF WINDSHIELD HEAT 1 AND 2 SMELL DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FO'S WINDSHIELD TEMP CONTROLLER IAW EMB 135 AMM 30-42-01. OPERATION CHECK GOOD. AIRCApr 28, 2008 · N715AE · Emb EMB135LR · Windshield/Door Rain/Ice RemovalSDR SIMA200807901Electronic Unit · malfunctionedON FLIGHT 4557, CREW REPORTED THAT AFTER TAKEOFF LANDING GEAR AIR/GND FAIL CAUTION MESSAGE ILLUMINATED. RETURNED FOR NORMAL LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LGEU IAW EMB 135 32-32-01. PERFORMED OPERATIONAL CHECK NO DEFECTS OR MEMar 17, 2008 · N715AE · Emb EMB135LR · Landing Gear Retraction/Extension SystemSDR SIMA200732502Module · malfunctionedAIRCRAFT DIVERTED TO JFK, ON TAKEOFF FROM DCA HEADING TO BOS RECEIVED LANDING GEAR AIR/GROUND FAIL MSG AND GEAR HANDLE WOULD NOT GO TO THE UP POSITION. FLEW WITH GEAR DOWN INTO JFK FOR REPAIR. DID DECLARE EMERGENCY. LANDED WITHOUT INCIDENT. REMOVED AND REPNov 5, 2007 · N715AE · Emb EMB135LR · Landing Gear Retraction/Extension SystemSDR SIMA200612802Control System · failedON LANDING, THE AIRCRAFT SWERVED RIGHT UNCONTROLLABLY, NOSE WHEEL STEERING DISCONNECTED. AIRCRAFT DEPARTED THE SIDE OF THE RUNWAY AND THEN RETURNED BACK ON TO THE RUNWAY. REPLACED FEED BACK POTENTIOMETER, P0054 PLUG, STEERING MANIFOLD AND ALL 6 TIRES. PERFOMay 4, 2006 · N715AE · Emb EMB135LR · Landing Gear Steering SystemSDR SIMA2005232403Floor Support · corrodedSAW - FOUND DURING CPCP INSPECTION, DIGITAL CORRODED AT FRAME 14 COCKPIT ENTRY. REMOVED CORROSION AND FOUND DIGITAL TO BE CRACKED. REPLACED DIGITAL IAW SRM 51-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 16, 2005 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200523405Rod · damagedFOUND DURING MBV, FORWARD END OF LOWER NR 2 RUDDER ROD HAS PLAY WHERE FORWARD FITTING SCREWS INTO ROD. REPLACED LOWER NR 2 RUDDER ROD IAW EMB AMM 27-21-08. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 16, 2005 · N715AE · Emb EMB135LR · Rudder StructureSDR SIMA200523404Skin · crackedFOUND DURING MBV, RUDDER NR 2 SKIN CRACKED ON RIGHT LOWER TRAILING EDGE. REPAIRED DAMAGED SKIN ON RUDDER NR 2 IAW IC2005-145/4198A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 12, 2005 · N715AE · Emb EMB135LR · Rudder, Plate/SkinSDR SIMA200523401Support · corrodedSAW - FOUND DURING CPCP INSPECTION, INBOARD RAMP AT FRAME 20 CORRODED. REPLACED INBOARD RAMP AT FRAME 20 IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 10, 2005 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200523402Floor Support · corrodedFOUND DURING CPCP INSPECTION, GALLEY FLOOR SUPPORT CORRODED AT FRAME 22. INSTALLED NEW GALLEY FLOOR SUPPORT AT FRAME 22 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 10, 2005 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200321005Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRJul 27, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200321001Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142, REV 22, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M)Jul 25, 2003 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200321004Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. APPLIED TREATMENT TO THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW EMB REPAIR STATJul 23, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200320805Skin · gougedABI - DURING AN IMBV INSPECTOIN, SEVEN GOUGES WERE FOUND JUST AFT OF FRAME 24 AND BELOW STRINGER 18L. COMPLETELY REMOVED DAMATE BY PERFORMING A CUTOUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMBL 145 SRM, SRM 145/1142 REV 22, 53-22-01, CPM 51-21-0Jul 22, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200320802Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, CORROSION FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CREATIN A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND A PLATE. REPAIR DONE IAW EMB 145 SRM, 145-1142 REV 22, 53-21-10 PARA 2 FIG 201 SHJul 22, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200321806Beam · corrodedABI - THIS LEVEL TWO ITEM FOUND DURING AN IMBV INSPECTION, THE CENTER BEAM WEB EXTENSION CORRODED AT FRAMES 22-23. REMOVED CORRODED CENTER BEAM WEB EXTENSION AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-20-03, 51-40-06, 51-40-02. (M)Jul 18, 2003 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200229402Windshield · crackedCREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.Oct 16, 2002 · N715AE · Emb EMB135LR · Flight Compartment WindowsSDR SIMA200206507Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. FABRICATED A DOUBLER, FILLER, PLATE, AND TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1172 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M)Jan 22, 2002 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA2876Switch · out of adjCLE - FLT 4384 - DURING TAKEOFF CREW NOTED E2 THRUST/REVERSER DISAGREE MESSAGE. RETURNED TO CLE WITH NO FURTHER INCIDENTS REPORTED. PUT ON MEL AT THIS TIME. MAINTENANCE PERFORMED STOW/TRANSIT MICROSWITCH ADJUSTMENT IAW EMB MM 78-34-01. OPERATIONAL CHECK GOct 13, 2000 · N715AE · Emb EMB135LR · Engine Thrust Reverser
Back to N715AE