N846AE
Service difficulty reports · 91
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 = 'N846AE' 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 = 'N846AE' 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 SIMA20130216003Flashlight · inoperativeDURING MAINTENANCE INSPECTION FOUND THE FLASHLIGHT AT THE FLIGHT ATTENDANT SEAT POSITION INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT AT THE FLIGHT ATTENDANT SEAT POSITION IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECKSDR SIMA20130209003Roller · lack of lubeON FLIGHT 4158 THE FLIGHT ATTENDANT REPORTED THE FORWARD ENTRY DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATE MAIN DOOR FRAME ROLLERS IAW EMB-140 M/M 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130207004Flashlight · defectiveON FLIGHT 4187 THE CREW REPORTED THE COCKPIT BULKHEAD FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS EMERGENCY FLASHLIGHT IAW EMB-140 A 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURSDR SIMA20130121002Fastener · looseON FLIGHT 4404 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT HOLDER WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED LOOSE HARDWARE IAW AMM 33-50-16 ON FLIGHT ATTENDANT’S FLASHLIGHT CRADLE. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121123003Door · lack of lubeON FLIGHT 4121 THE FLIGHT ATTENDANT REPORTED THE CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED LUBRICATION OF DOOR IAW EMB-140 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD, NO FURTHER DEFECTS NOTED. THE AIRCRAFSDR SIMA20121120002Light · inoperativeDURING B INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WASDR SIMA20121014005Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT IN CEILING FORWARD INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IN CABIN FORWARD IAW EMB 140 AMM 23-22-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRSDR SIMA20120928014Floor Support · corrodedCENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 57-59. REPAIRED CENTER OMEGA BEAM IAW AE EOEM-53MR-1518.SDR SIMA20120928013Floor Support · corrodedLEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 57-59. REPAIRED OMEGA BEAM IAW AE EO EM-53MR-1518.SDR SIMA20120928012Gusset · corrodedDURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120928011Gusset · corrodedDURING B INSPECTION FOUND THE LEFT BEAM GUSSET CORRODED BETWEEN FRAMES 60-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT BEAM GUSSET BETWEEN FRAMES 60-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120928010Gusset · corrodedDURING B INSPECTION FOUND THE CENTER BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER BEAM GUSSET BETWEEN FRAMES 59-61. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120726008Connector · brokenDURING MAINTENANCE INSPECTION, FOUND THE BATTERY CONNECTOR BROKEN ON THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT BATTERY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT THE FLIGHT ATTENDANT’S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS SDR SIMA20120726007Connector · brokenDURING MAINTENANCE INSPECTION, FOUND BATTERY CONNECTOR BROKEN ON THE FIRST OFFICER’S EMERGENCY FLASHLIGHT BATTERY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRSDR SIMA20120715007Switch · failedFLIGHT 2766, CREW REPORTED THAT AT ROTATION THEY RECEIVED A LANDING GEAR AIR/GND/FAIL MESSAGE ON EICAS. DID NOT ATTEMPT TO RETRACT GEAR AS THEY CONTINUED THE CLIMB-OUT. FOLLOWED THE AOM VOL 1 PROCEDURES. LANDING GEAR INDICATORS REMAINED GREEN DURING ENTIRE SDR SIMA20120620013Light · defectiveDURING B INSPECTION FOUND THE READING LIGHT ASSEMBLY ABOVE SEAT 11A IS EMITTING A BURNING ODOR AS SMOKE IS VISIBLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LIGHT BULB REMOVED. ENTIRE LIGHT ASSY NEEDS REPLACEMENT. PARTS NOT AVAILABLE. DEFERRED AS NEF 25-21CSDR SIMA20120617001Control Unit · inoperativeON FLIGHT 4228 THE CREW REPORTED THAT WHILE IN FLIGHT WHEN THE SPEED BRAKE LEVER WAS SELECT TO OPEN THE CREW RECEIVED A SPOILER FAIL MESSAGE ON THE EICAS AND THE SPLRS INDICATION INDICATED CLOSED ON THE EICAS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO ORSDR SIMA2012053002Flashlight · inoperativeFLIGHT 3058, THE CREW REPORTED THE CAPTAIN`S FLASHLIGHT NOT WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN`S FLASHLIGHT ASSY IAW AMM 33-50-16 AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA201101104Indication Sys · defectiveON FLIGHT 3045 THE CREW REPORTED THE NR 1 FUEL QUANTITY INDICATION ON EICAS AS UNREADABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT HAND NR 4 TANK UNIT IAW EMB140 AMM 28-41-2. THE OPERATIONAL CHECK WAS GOOD IAW EMB140 AMM 28-41-0SDR SIMA201028802Trim System · malfunctionedON FLIGHT 4508 THE CAPTAIN ACTIVATED THE PITCH TRIM ON SHORT FINAL AND RECEIVED MASTER A WARNING MICAS "PTRIM MAIN INOP". BOTH CAPTAIN’S AND FIRST OFFICER’S TRIM INOPERATIVE BUT BACKUP SYSTEM WORKED PROPERLY. THE CAPTAIN DECLARED AND EMERGENCY. THE AIRCRAFTSDR SIMA201020004Seal · lack of lubeON FLIGHT 4307 THE CREW REPORTED THAT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE FIRST OFFICER HAD TO ASSIST THE FLIGHT ATTENDANT TO OPEN AND CLOSE THE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ADJUSTED THE MAIN DOOR STOPS IAW EMB 140 AMSDR SIMA201015202Ballast · malfunctionedON FLIGHT 4340 DURING TAXI THE CREW REPORTED NOTICING ELECTRICAL FUME ODORS IN GALLEY ROW AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BALLASTS (BOTH) IN GALLEY IAW EMB-140 CMM 25-28-24. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WASSDR SIMA201014801Ballast · malfunctionedFOR FLIGHT 4053 UPON ENTERING THE AIRCRAFT THE FLIGHT CREW REPORTED, SMELLED A STRONG ELECTRICAL ODOR AROUND ROW 3. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SIDEWALL 3BC BALLAST IAW EMB 140 AMM 33-21-04. NO DEFECTS NOTED. THE ASDR SIMA201013404Trim System · malfunctionedON FLIGHT 4394 THE CREW DETERMINED THE MAIN PITCH TRIM WAS INOPERABLE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED HORIZONTAL STABILIZER AND PITCH TRIM SYSTEM PER FIM IAW EMB 140 AMM 27-40-00. SDR SIMA201011102Switch · out of adjustFLIGHT 3445 THE CREW REPORTED THE CABIN MAIN DOOR SENSOR KEPT GIVING A MAIN DOOR OPEN WARNING ON THE GROUND. THE FLIGHT ATTENDANT HAD TO OPEN AND CLOSE THE DOOR TO RESET IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ADJUSTED SWITCH ON THE MAIN CABIN DOOR IASDR SIMA201010910Mechanism · lack of lubeON FLIGHT 2865 THE CREW REPORTED THAT THE MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN CABIN DOOR LOCKING MECHANISM, THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-18-00. NO PARTS REMOVED OR REPLACESDR SIMA200930903Skin · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND STRUCTURAL DAMAGE FROM A BIRD STRIKE BELOW THE CAPTAIN’S WINDSHIELD AND FORWARD TO RADOME. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AMERICAN EAGLE AIRLINES EO EM-53MR-1414, WORK ORDER 36849. THE AIRCSDR SIMA200930901Skin · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE SKIN SPLICE PLATE AT FRAME 6 AND STRINGER 11L MISS DRILLED DURING TEMPORARY REPAIR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SKIN SPLICE PART NUMBER 120-27430-003 IAW EMB SRM 51-40-02. THSDR SIMA200930902Skin · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE SKIN SPLICE PLATE PART NUMBER 123-10953-001 DAMAGED FROM A BIRD STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SKIN SPLICE PLATE PART NUMBER 123-10953-001 IAW EMB SRM 51-40-02. THE AIRCSDR SIMA200930904Profile · bentDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 9L IAW EMB SRM 51-40-02. THE AIRCRAFTSDR SIMA200931002Profile · bentDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FUSELAGE 1 BULKHEAD PROFILE AT STRINGER 4L IAW EMB SRM 51-40-02. THE AIRCRSDR SIMA200826802Light · burnedON FLIGHT 4354 CREW REPORTED ON ARRIVAL THAT THE FLIGHT ATTENDANT SMELLED SMOKE COMING FROM LAV AREA NEAR THE ELT. CREW CONFIRMED SMELL BUT NO VISIBLE SMOKE. ACFT REMOVED FROM SERVICE. C/A FOUND FLUORESCENT BULB ABOVE TOILET WITH BURNT SOCKET. REMOVED BULBSDR SIMA200721102Battery Pack · failedEMERGENCY LIGHTS NO TEST. REMOVED AND REPLACED ALL FOUR BATTEY PACKS IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR SIMA200710604Engine · leakingRECEIVED LAVATORY SMOKE INDICATION ON CLIMB-OUT, NO VISUAL INDICATION OF SMOKE, FAINT SMELL NOTED. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORKCARD 72-000-00. OPERATIONAL AND LEAK CHECK GOOD WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.SDR SIMA200621305Smoke Detector · malfunctionedCREW REPORTED CARGO SMOKE WARNING AT 31,000 FEET, DECLARED EMERGENCY, DISCHARGED FIRE BOTTLES, DIVERTED TO ALB. RAI BAGGAGE COMPARTMENT HIGH RATE AND LOW RATE FIRE BOTTLES, IAW EMB AMM 26-23-01, RAI FORWARD BAGGAGE SMOKE DETECTOR IAW EMB 140 AMM 26-15-01. RASDR SIMA200621304Warning System · activatedJAX - FLT 4497 - BAGGAGE SMOKE INDICATION IN FLIGHT. CREW DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT FIRE EXTINGUISHER BOTTLES. PART NR FOR FIRE BOTTLE, IAW EMB140, AMM 26-23-01. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (SDR SIMA200619807Connector · unsecureFOUND EMERGENCY EXIT LIGHT STRIP AT EXIT ROW INOP. RESECURED CONNECTOR ON THE STRIP, OPS CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)SDR SIMA200501205Floor Support · corrodedDURING AN INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)SDR SIMA200501204Floor Support · corrodedDURING AN INSPECTION OF AIRCRAFT THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)SDR SIMA200501201Floor Support · corrodedDURING AN MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)SDR SIMA200428703Flashlight · odorSTRONG ELECTRICAL ODOR IN FORWARD CABIN. ODOR ISOLATED TO FLIGHT ATTENDANTS FORWARD FLASHLIGHT. REPLACED FLIGHT ATTENDANTS FORWARD FLASHLIGHT IAW EMB 145 MM 25-60-00, OPS CHECK GOOD. (M)
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