N842AE

Service difficulty reports · 84

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 = 'N842AE' 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 SIMA20130304007Acm · malfunctionedON FLIGHT 3226 THE CREW REPORTED THAT AT CRUISE THE FLIGHT CREW DETECTED TOXIC FUMES IN THE COCKPIT. THE FLIGHT ATTENDANT SMELLD FUMES IN THE FORWARD CABIN. THE FLIGHT ATTENDANT SAID THAT FUMES WERE CONCENTRATED IN THE FORWARD PART OF CABIN. THE CREW PERFORMar 4, 2013 · N842AE · Emb EMB135KL · Cabin Cooling SystemSDR SIMA20130216002Light · looseDURING MAINTENANCE INSPECTION FOUND THE LEFT REAR WING/FUSELAGE FAIRING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED EXISTING LAMP IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 16, 2013 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA20130131011Engine · bird ingestionFOR FLIGHT 3582 THE CREW REPORTED THAT ON TAKEOFF AFTER V1 MANY SUSPECTED BIRD STRIKES. THE SMELL ENTERED THE CABIN OF COOKED BIRD. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED THOROUGH INSPECTION OF A/C IAW EMB WORKCARD 05-200-07 BIRD STRIKE INSPECTIONJan 31, 2013 · N842AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA20130104006Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW ERJ 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WASJan 4, 2013 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA20121227002Switch · missingCAPTAINS FLASHLIGHT IS MISSING PLASTIC ON/OFF SWITCH. REMOVED BROKEN FLASHLIGHT BEHIND PILOT SEAT AND INSTALLED SERVICEABLE FLASHLIGHT IN REFERENCE WITH EMB 140 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A.Dec 27, 2012 · N842AE · Emb EMB135KL · Emergency EquipmentSDR SIMA20120919002Flashlight · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IN FORWARD CABIN IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-5Sep 19, 2012 · N842AE · Emb EMB135KL · Emergency EquipmentSDR SIMA20120910002Engine · malfunctionedFOR FLIGHT 3259 - THE RAMP PERSONNEL REPORTED ON TAXI IN SMOKE WAS COMING FROM NR 1 ENGINE. SMOKE SMELLED SOMETHING LIKE BURNING ELECTRIC WIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF LEFT ENGINE IAW AE3007A MM 72-00-00. SMOSep 10, 2012 · N842AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA20120820009Oil System · overservicedDURING MAINTENANCE INSPECTION, NOTICED A STRONG ODOR IN COCKPIT WHILE APU BLEED WAS RUNNING. AIRCRAFT REMOVED FROM SERVICE. RAN APU IAW AMM 49-13-00. SUPPLIED APU BLEED AND FOUND NO ODOR NOTED. OPS CHECKED GOOD. FOUND APU OIL OVER SERVICED REF NRWC NR 842Aug 20, 2012 · N842AE · Emb EMB135KL · APU Oil SystemSDR SIMA20120801002Lamp · inoperativeDURING B INSPECTION, FOUND THE RIGHT FORWARD OVERWING EMERGENCY LIGHT OUT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.Aug 1, 2012 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA20120723004Beam · crackedDURING MAINTENANCE, FOUND BEAM 3 IN THE RIGHT OVERWING EMERGENCY EXIT CRACKED .250 INCHES IN LENGTH NEAR THE AFT CORNER. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BEAM IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.Jul 23, 2012 · N842AE · Emb EMB135KL · Emergency ExitsSDR SIMA20120704007Wire · brokenDURING B INSPECTION, FOUND THE LEFT NR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH CONNECTORS ON THE LEFT NR 1 EMERGENCY LIGHT IAW SWPM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.Jul 4, 2012 · N842AE · Emb EMB135KL · Light System WiringSDR SIMA20120504003Light · looseDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDENTS SEAT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK IAW EMB 140 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. THE OPERMay 4, 2012 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA20120229004Light · inoperativeDURING MAINTENANCE INSPECTION FOUND RIGHT EXTERIOR OVERWING FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT IAW EMB 140 AMM 33-50-10, OPERATIONAL WAS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.Feb 29, 2012 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA201134801Oxygen Bottle · defectiveON FLIGHT 4387 THE CREW REPORTED A PASSENGER’S PORTABLE OXYGEN BOTTLE WAS OPERATING AT AT 1100 PSI. THE CREW ELECTED TO DECLARE AN EMERGECNY AND DIVERT TO CRW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACEDec 11, 2011 · N842AE · Emb EMB135KL · Portable Oxygen SystemSDR SIMA2011318008Holder · defectiveON FLIGHT 4003 THE CREW REPORTED THE FLASHLIGHT HOLDER BEHIND THE CAPTAIN DOES NOT HOLD THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER ASSEMBLY IAW EMB-140AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE Nov 12, 2011 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA2011294022Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT OVER THE WING EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVER THE WING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS REOct 21, 2011 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA201119201Brake Assy · malfunctionedON FLIGHT 2900 THE CREW REPORTED UPON LANDING AND TAXIING, RECEIVED A MESSAGE ABOUT THE LEFT INBOARD BRAKE OVERHEATING. THE CREW DECLARED AND EMERGENCY AND CRASH, FIRE AND RESCUE WERE DISPATCHED. FIRE DEPT TOOK A READING OF 1200. THEY ALSO HAD A NR 1 TIRE FJul 8, 2011 · N842AE · Emb EMB135KL · BrakeSDR SIMA201115104Light · inoperativeFOR FLIGHT 2721 DURING THE PREFLIGHT INSPECTION FOUND THE MAIN DOOR LINER EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR LINER EMERGENCY ASSEMBLY IAW EMB 140 AMM 33-50-06. THE OPERATIONAL CHECK WAS GOODMay 30, 2011 · N842AE · Emb EMB135KL · Emergency LightingSDR SIMA201020301Control Unit · malfunctionedON FLIGHT 3707 DURING THE CLIMBOUT THE CREW REPORTED, RECEIVED AN AIR/GROUND FAIL MESSAGE ON EICAS THAT REMAINED ON FOR DURATION OF FLIGHT. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOJul 21, 2010 · N842AE · Emb EMB135KL · Landing Gear Retraction/Extension SystemSDR SIMA201014407Pressure Switch · faultyON FLIGHT 3275 DURING CLIMB THE CREW REPORTED THE RUDDER SEEMED TO BE HALFWAY INOPERABLE IN FLIGHT. THE CREW COMPLIED WITH THE AIRCRAFT OPERATING MANUAL. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROMMay 23, 2010 · N842AE · Emb EMB135KL · Rudder Control SystemSDR SIM2008F00017Floor Support · corrodedDURING MBV A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THAT EXISTING REPAIR DOUBLER AND CLEANED THE AREA. POSITIONED, MARKED, DRILLED, TREATED AND INSTALLED NEW REPAIR DOUBLER PN EPNEM53EP54701. REPAIRS PERFORMED IAW SRM 53Jul 21, 2008 · N842AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200820305Sill · corrodedDURING MBV THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A)Jul 21, 2008 · N842AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200736001Pressure Switch · malfunctionedON FLIGHT 3485, FLIGHT CREW NOTICED BRAKE ON LIGHT. CREW DECLARED EMERGENCY AND LANDED SAFELY IN SJT. REMOVED AND REPLACED PARK BRAKE PRESS SWITCH AND CLEANED CONNECTOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Dec 24, 2007 · N842AE · Emb EMB135KL · BrakeSDR SIMA200725003Control Panel · failedRECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE, RETURNED TO ORD. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL IAW EMB 24-00-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.Sep 5, 2007 · N842AE · Emb EMB135KL · DC Power Distribution SystemSDR SIMA200716201Actuator · failedPITCH TRIM INOP MESSAGE ON TAKEOFF, BACKUP SYSTEMS FUNCTIONED NORMAL. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB AMM 27-40-02. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.Jun 7, 2007 · N842AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200632402Warning System · activatedRECEIVED ELECTRICAL ABNORMAL MESSAGE, DIVERT TO BDL.Nov 17, 2006 · N842AE · Emb EMB135KL · AC Indicating SystemSDR SIMA200631704Sensor · faultyFLAP FAIL MESSAGE ON DESCENT THROUGH 16,000 WITH VMC-ICING CONDITIONS. NO EMERGENCY DECLARED. THE FLAPS DID NOT MOVE WHEN 9 DEGREES POSITION WAS SELECTED. RMU AND EICAS BOTH INDICATED ZERO, ONLY MESSAGE WAS FLAP FAIL. COMPLIED WITH AMERICAN EAGLE DOCUMENT Nov 11, 2006 · N842AE · Emb EMB135KL · Trailing Flap Position Indicating SystemSDR SIMA200626803Line · looseAFTER TAKEOFF FROM LGA HYDRAULIC SYSTEM 2 FLUID DROPPED TO `0` QUANTITY FOLLOWED BY ENGINE 2 HYDRAULIC PUMP FAILURE AND HYDRAULIC 2 LOW QUANTITY MESSAGE. FOUND LOOSE ENGINE 2 HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE. TIGHTEN NUT AND PERFORMED ENGINE DRIVEN PSep 23, 2006 · N842AE · Emb EMB135KL · Hydraulic System, MainSDR SIMA200627704Stringer · chafedSAW - DURING IMBV INSPECTION, FOUND STRINGER 19 LEFT BETWEEN FRAMES 52-53 IS CHAFED. REPAIRED STRINGER IAW EMB SRM 53-24-00 BY CUTTING OUT DAMAGED PORTION OF STRINGER AND INSTALLING A DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)Sep 13, 2006 · N842AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200627703Floorbeam · corrodedSAW - DURING IMBV INSPECTION, FOUND RIGHT UPPER FLOORBEAM AT FRAME 23 IS CORRODED. REMOVED AND REPLACED FLOORBEAM, IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)Sep 11, 2006 · N842AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200627702Gusset · corrodedDURING IMBV INSPECTION, FOUND GUSSET CONNECTING RIGHT HAT BEAM TO FLOORBEAM 20 CORRODED. REMOVED AND REPLACED GUSSET, IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)Sep 11, 2006 · N842AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200513607Terminal · burnedLAX - FLT 3121 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE CABIN. NO VISIBLE SMOKE NOTED. CREW ELECTED TO RETURN TO LAX AND DECLARED EMERGENCY. MAINTENANCE FOUND THE CAUSE TO BE THE NR 1 WINDSHIELD HEAT CONTROLLER TERMINALS WERE BURNEDMay 13, 2005 · N842AE · Emb EMB135KL · Ice/Rain Protection System WiringSDR SIMA200502401Windshield · crackedON CLIMB OUT AT 11,000 FL CAPTAINS WINDSCREEN SHATTERED RETURNED TO AIRPORT, LANDED SAFELY. NO LOSS OF CABIN PRESSURIZATION. REPLACED CAPTAIN WINDSHIELD. AC RETURNED TO SERVICE. (SW21200503048) (K)Jan 21, 2005 · N842AE · Emb EMB135KL · Flight Compartment WindowsSDR SIMA200435201Floor Support · corrodedDURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGED OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FILLER. REPAIR DONE IADec 9, 2004 · N842AE · Emb EMB135KL · Fuselage Miscellaneous Structure
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