N624AE

Service difficulty reports · 147

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 = 'N624AE' 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 SIMA200935801Hydraulic Line · crackedON FLIGHT 3283 DURING THE CLIMBOUT THE CREW REPORTED A HYDRAULIC SYSTEM FAIL. THE CREW PERFORMED AIRCRAFT OPERATING PROCEDURES CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED A CRACDec 23, 2009 · N624AE · Emb EMB145LR · Hydraulic System, MainSDR SIMA200912002Relay · failedON FLIGHT 4512 CREW REPORTED ON CLIMB-OUT THEY RECEIVED A ENGINE 2 REV FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND PERFORMED ENGINE NUMBER 2 SHUTDOWN. AIRCRAFT LANDED UNEVENTFULLY IN ORD. AIRCRAFT REMOVED FROM SERVICE. REOPENED MEL 78-1 AUTH NR 040319M-C.Apr 17, 2009 · N624AE · Emb EMB145LR · Engine Thrust ReverserSDR SIMA200910304SUPRelay · malfunctionedON FLIGHT 4323, CREW REPORTED DURING APPROACH ENGINE 2 THRUST REVERSER FAIL MSG ON EICAS. CREW DECLARED AN EMERGENCY. APPLIED MEL 7801. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RELAYS IAW EMB 145 AMM 20-13-02-000-801-A AND 20-13-02-400-801-A. DApr 10, 2009 · N624AE · Emb EMB145LR · Engine Thrust ReverserSDR SIMA200910304Warning Light · illuminatedON FLIGHT 4323, CREW REPORTED DURING APPROACH ENGINE 2 THRUST REVERSER FAIL MSG ON EICAS. CREW DECLARED A EMERGENCY. APPLIED MEL 7801.Apr 10, 2009 · N624AE · Emb EMB145LR · Engine Thrust ReverserSDR SIMA200903301Connector · contaminatedON FLIGHT 3550 DURING CLIMB CREW REPORTED GEAR RETRACTION RIGHT MAIN GEAR INDICATION REMAINED UNSAFE. DID NOT INDICATE UP FOR SEVERAL SECONDS. CREW RECEIVED LG/LEVER DISAGREE MSG ON EICAS. CREW RETURNED TO GSP AND LANDED WITHOUT INCIDENT. NO OTHER PROBLEMSJan 31, 2009 · N624AE · Emb EMB145LR · Landing Gear System WiringSDR SIMA200803103Floor Support · corrodedDURING A MBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. AIRCRAFT WAS OUT OF SERVICE. REMOVED AND REPLACED SILL WITH NEW SILL IAW EMB SAR 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.Jan 26, 2008 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200727702Actuator · malfunctionedUPON LANDING, GEAR EXTENSION AT MEM RIGHT MAIN LANDING GEAR DID NOT INITIALLY COME DOWN. AIRCRAFT NATURALLY YAWED THEN GEAR CAME DOWN APPROX 5 SECONDS. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. AIRCRAFT RETURNED TO SERVICE.Oct 3, 2007 · N624AE · Emb EMB145LR · Landing Gear ActuatorSDR SIMA200727603Transceiver · inoperativeEN ROUTE WEATHER RADAR TESTED GOOD BUT WEATHER RADAR WOULD NOT PAINT. REMOVED AND REPLACED WEATHER RADAR RT UNIT IAW AMM TASK 34-42-01-000- AND TASK 34-42-01-1100-801-A. PERFORMED OPS CK OF WEATHER RADAR IAW AMM 34-42-00-700-801. AIRCRAFT RETURNED TO SERVIOct 2, 2007 · N624AE · Emb EMB145LR · Weather Radar SystemSDR SIMA200706701Engine · odor"SUP" FOUL ODOR IN CABIN AND COCKPIT. REMOVED AND REPLACED NR 1 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.Mar 7, 2007 · N624AE · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200705802Battery Pack · failedFOUND EMERGENCY PATH LIGHTS AT ROW 8 THROUGH 12 INOPERATIVE, ALL 4 EMERGENCY OVERWING EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY PACK IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.Feb 26, 2007 · N624AE · Emb EMB145LR · Emergency LightingSDR SIMA200629202Structure · vibrationRUDDER PEDALS AND CONTROL COLUMN VIBRATION FELT AFTER A CLUNK NOISE ON RIGHT SIDE OF THE AIRCRAFT. VIBRATION FELT MOSTLY ON RIGHT CONTROL COLUMN AND ON FLOORBOARD ALONG THE AIRCRAFT. WALK AROUND REVEALED NO VISIBLE DAMAGE. FLIGHT DIVERTED TO BNA. COMPLIED Oct 10, 2006 · N624AE · Emb EMB145LR · Fuselage Structure (General)SDR SIMA200606905Seat Track · corrodedRT OB SEAT TRACK NR 5 CORRODED. REPLACED SEAT TRACK IAW MM. (K)Mar 3, 2006 · N624AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200606904Seat Track · corrodedRT OB SEAT TRACK NR 4 CORRODED. REPLACED SEAT TRACK IAW MM. (K)Mar 3, 2006 · N624AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200606902Seat Track · corrodedRT OB SEAT TRACK NR 2 CORRODED. REPLACED SEAT TRACK IAW AIRCRAFT MM. (K)Mar 3, 2006 · N624AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200427903Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING CENTER SILL AND CLEANED AREA. INSTALLED NEW CENTER SILL IAW SRM (SRM EMB-145/1142 REV 27) CHAPTER 51-20-01, 03,04 AND 51-40-06. (SW212005280)Sep 24, 2004 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200427902Floor Support · corrodedA PREVIOUS REPAIR OF THE FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR OF THE FORWARD DIGITAL AND CLEANED ATHE AREA. PREPARED SECTION FROM A NEW DIGITAL. FABRICATED SHIMS AND 2 DOUBLERS. REPAIR DONE IAW SRM (SRM EMB 145/1142 REV 27) CHAPTSep 24, 2004 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200424303Warning Light · illuminatedSGF - FLT 3940 - AIRCRAFT HAD A FLAP FAIL MESSAGE ON LANDING. EMERGENCY DECLARED. MAINTENANCE FOUND ASSOCIATED FLAP DRIVE TS FAIL MESSAGE ON CENTRAL MAINTENANCE COMPUTER. COMPLIED WITH FAULT ISOLATION MANUAL 27-51-00-810-804A. RESET FLAP SYSTEM WHILE RESETAug 29, 2004 · N624AE · Emb EMB145LR · Trailing Flap Position Indicating SystemSDR SIMA200417701Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND IN THE LEFT WING LOWER TRAILING EDGE SKIN. A DOUBLER REPAIR WAS COMPLETED IAW ENGINEERING ORDER EM 57MR-123R6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 22, 2004 · N624AE · Emb EMB145LR · Wing, Plate/SkinSDR SIMA200417201Yoke · vibrationDURING CLIMB AND MOST OF FLIGHT INTO MQT, CREW NOTED A SLIGHT VIBRATION ON BOTH YOKES. NOTE: VIBRATION WAS AT AIRSPEEDS OF 230-310. AUTO PILOT ON/OR OFF HAD NO AFFECT. REPLACED LEFT AILERON BUSHING AND HARDWARE. PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETJun 19, 2004 · N624AE · Emb EMB145LR · Control Column SectionSDR SIMA200307602Light · failedCMH - FLT 3213 - CREW REPORTED THE MOST AFT SECTIONS OF FLOOR PROXIMITY EMERGENCY LIGHTS DO NOT ILLUMINATED. MAINTENANCE REPLACED THE AFT FLOOR PROXIMITY STRIP LIGHTS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 16, 2003 · N624AE · Emb EMB145LR · Emergency LightingSDR SIMA200227918Frame · corrodedDURING AN MFG INSPECTION, MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR ONLY). FABRICATED A DOUBLER ANGLE, FILLER, PLATE, AND TWO SHIMS. REPAIR DONE IAW MFG SRM ANSep 15, 2002 · N624AE · Emb EMB145LR · Fuselage Main, FrameSDR SIMA200226102Floorbeam · corrodedABI - DURING IMBV INSPECTION, THE FORWARD DIGITAL IN THE GALLEY WAS FOUND TO BE CORRODED. CUT OUT DAMAGED PORTION ON THE DIGITAL, 16.5 BY 21, AND FABRICATED TWO DOUBLERS, ONE SHIM. REPAIR DONE IAW EMB 145, SRM 145/1142, REV 18 SRM 53-21-10, AND STANDARD SRM Sep 13, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200226103Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON GALLEY RIGHT FLOOR BEAM. REMOVED CORRODED GALLEY RIGHT BEAM. INSTALLED NEW BEAM IAW EMB-145, SRM 145/1142, CHAPTER 51, RV 19, 51-40-02, AMERICAN EAGLE AIRLINES INC ETN NR EM-53-028 AND STANDARD SRM PRACTICESep 12, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200225501Floorbeam · corrodedABI - FOUND GALLEY CENTER HAT BEAM CORRODED BEYOND LIMITS. INSTALLED NEW CENTER HAT BEAM IAW EMB145 SRM 145/1142 CHAPTER 51, REV 19, 51-40-02, 51-40-04, 51-20-01, 51-20-03 AND EMB GST-2758/02. (M)Sep 11, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200225502Floorbeam · corrodedABI - FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. FABRICATED AND INSTALLED A DOUBLER ANGLE FILLER PLATE AND TWO SHIMS IAW EMB-145 SRM 145/1142, CHAPTER 53, REV 19 53-21-10, FIG 201 AND STANDARD SRM PRACTICES. (M)Sep 10, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200225403Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, MAINTENANCE FOUND AN AREA OF THE FORWARD DIGITAL CORRODED. BLENDED CORRODED AREA. FABRICATED A DOUBLER AND INSTALLED IAW EMB GST-2721.02 PARA 1 DATED SEP 5, 2002 AND STANDARD SRM PRACTICES. (M)Sep 9, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200226117Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, GALLEY CENTER HAT BEAM IS CORRODED ADJACENT TO PREVIOUS REPAIR. MAINTENANCE REMOVED AND INSTALLED NEW GALLEY HAT BEAM IAW EMB 145 SRM 51-20-01, 51-40-02 AND GST 2758/02. (M)Sep 8, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200226104Sill · corrodedABI - DURING AN IMBV INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. BLENDED CORRODED AREAS AND FILLED WITH EPOXY RESIN. FABRICATED TWO L PROFILE DIFFERENT SIZES AND REINFORCEMENT DOUBLER. REPAIR DONE IAW EMB GST-2721/02 PARA 3 AND AMERICAN EAGLE ENGINSep 7, 2002 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200225402Skin · corrodedABI - DURING AN IMBV INSPECTION A SCRATCH WAS DISCOVERED ON LEFT FUSELAGE FORWARD OF FRAME 26 AND BELOW STRINGER 18L. BLENDED OUT SCRATCH AND PERFORMED AN EDDY CURRENT INSPECTION AND THICKNESS INSPECTION. THICKNESS WAS DETERMINED TO BE BELOW SRM LIMITS. FABSep 5, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SIMA200225401Sill · corrodedABI - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE CARGO DOOR LOWER CENTER SILL TO BE CORRODED BEYOND SRM LIMITS. MAINTENANCE REMOVED THE CORRODED SILL AND INSTALLED NEW CENTER SILL IAW EMB 145 SRM 145/1142, CHAPTER 51, REV 17, 51-40-02 AND STANDARD SRM PSep 5, 2002 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200226116Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200226115Seat Track · corrodedABI - THIS IS A LEVEL 2 FINDING, LEFT NR 2 SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED LEFT NR 2 SEAT TRACK IAW EMB 145 AMM 53-60-00. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200226114Seat Track · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT INBOARD NR 1 SEAT TRACK CORRODED. MAINTENANCE REMOVED AND INSTALLED RIGHT INBOARD NR 1 SEAT TRACK IAW EMB 145 AMM 53-01-00. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200226113Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, CENTER OMEGA BEAM RAMP REQUIRES REPLACEMENT. MAINTENANCE REMOVED AND REPLACED NEW CENTER OMEGA BEAM IAW EMB 145 SRM 51-20-01, 51-20-05, 51-40-02. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200226112Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, PREVIOUS REPAIR ON LEFT OMEGA BEAM FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 53-21-10 AND 51-40-02. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA200226111Floor Support · corrodedTHIS IS A LEVEL 2 ITEM, LEFT CABIN FLOOR SILL CORRODED BETWEEN FRAME 19-23. MAINTENANCE REPLACED FLOOR SILL IAW EMB 145 SRM 51-40-02. (M)Sep 1, 2002 · N624AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR E4G2001F00001Bushing · out of positionBUSHINGS ARE MIGRATING CAUSING EXCESSIVE WEAR TO ELEVATOR CONTROL QUADRANT SUPPORT FITTINGS.Oct 10, 2001 · N624AE · Emb EMB145LR · Elevator Control SystemSDR SIMA200124301Fuel Line · chafedXNA - MAINTENANCE REPORTED APU WOULD NOT START. MAINTENANCE TROUBLESHOT AND FOUND APU FUEL LINE WHICH RUNS TO THE START FUEL NOZZLES CHAFFED. REMOVED AND REPLACED APU FUEL LINE IAW HAMILTON SUNSTRAND CMM. (M)Aug 31, 2001 · N624AE · Emb EMB145LR · APU Engine Fuel and ControlSDR SIMA200115701O-Ring · leakingCMH - FLT 4160 - AIRCRAFT RETURNED TO FIELD FOR NR 1 BLEED LEAK. REMOVED AND REPLACED CARGO COMPARTMENT BLEED LINE O-RING IAW AMM 36-11-801-A AND 36-11-00-400-801-A. OPS CHECK GOOD. (M)Jun 6, 2001 · N624AE · Emb EMB145LR · Pneumatic Distribution SystemSDR SIMA200115622Warning Light · false indicationCMH - FLT 4093 - NR 2 BLEED LEAK IN FLIGHT. COULD NOT DUPLICATE PROBLEM. PERFORMED CHECKS IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M)Jun 5, 2001 · N624AE · Emb EMB145LR · Bleed Air Indicating SystemSDR SIMA200108002Engine · shutdownORD - FLT 4309 - ON CLIMB-OUT, CREW HEARD LOUD NOISE AND ENGINE SHUTDOWN ON ITS OWN. CREW DECLARED EMERGENCY AND LANDED SAFELY IN ORD. CREW TRIED TO RESTART ENGINE, COULD NOT RESTART. (M)Mar 21, 2001 · N624AE · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200103503O-Ring · leakingORD - FLT 4047 - AFTER DEPARTURE FROM ORD RT/ENG BLEED LEAK LIGHT ILLUMINATED. CREW ELECTED TO RETURN TO ORD. REMOVED AND REPLACED O-RING AT RIGHT OVERWING BLEED IAW AMM. OPS CHECK GOOD. (M)Feb 4, 2001 · N624AE · Emb EMB145LR · Pneumatic Distribution SystemSDR SIMA3411Inverter · inoperativeHOU - FLT 3618 - CREW REPORTED THAT REAR EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ENTRY DOOR TO AFT CABIN SEATS. FERRIED AIRCRAFT TO DFW AND REPLACED EMERGENCY LIGHT INVERTER. (M)Dec 6, 2000 · N624AE · Emb EMB145LR · Emergency LightingSDR SIMA2905Warning Light · illuminatedDFW - FLT 3827 - FLIGHT CREW REPORTED NR 2 BLEED LEAK WARNING DURING CLIMB. EPC AND AOM PROCEDURES C/W. BLEED LEAK CLEARED AFTER 2 MINUTES. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. GROUND ENGINE RUN OF BOTH ENGINES AND BOTH AIR CONDTIONING SYSTEMS WITHOct 16, 2000 · N624AE · Emb EMB145LR · Pneumatic Indicating SystemSDR SIMA1772Sensor · failedORD - FLT 4123 - ENGINE NR 1 LOW N1 ON TAKEOFF, WARNING MESSAGE ON EICAS. ABORTED TAKEOFF. MAINTENANCE FOUND THE ENGINE FAN SPEED SENSOR INOPERATIVE. BOTH ENGINE SENSORS REMOVED AND REPLACED. OPERATIONAL CHECK SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE.Jun 25, 2000 · N624AE · Emb EMB145LR · Engine RPM Indicating SystemSDR 20000821SH012Sensor · inoperativeORD - FLT 4123 - ENGINE NR 1 LOW N1 ON TAKEOFF, WARNING MESSAGE ON EICAS. ABORTED TAKEOFF. MAINTENANCE FOUND THE ENGINE FAN SPEED SENSOR INOPERATIVE. BOTH ENGINE SENSORS REMOVED AND REPLACED. OPERATIONAL CHECK SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE.Jun 25, 2000 · N624AE · Emb EMB145LR · Engine RPM Indicating SystemSDR SIMA993201Control Lever · failedDFW - FLT 3619 - AFTER TAKEOFF, THE LANDING GEAR CONTROL LEVER COULD NOT BE MOVED TO THE UP POSITION. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. FUNCTIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)Nov 16, 1999 · N624AE · Emb EMB145LR · Landing Gear Selector
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