N606AE
Service difficulty reports · 180
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 = 'N606AE' 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 = 'N606AE' 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 SIMA20140330013Skin · damagedMULTIPLE HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER INBD SKIN. R & R RT ELEVATOR UPPER INBD SKIN IAW SRM 51-40-02, AEA ETN-EM-55-076 & ETN-EM-55-073.SDR SIMA20140328016Connector · brokenSERVICE DOOR FRAME FWD LOWER TRIM PANEL EMERGENCY LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR ON SERVICE DOOR FRAME FWD LOWER TRIM PANEL EMERGENCY LIGHT IAW SWPM 20-21-00 STEP 5. LIGHT OPERATIONS CHECK GOOD.SDR SIMA20140324006Trim System · malfunctionedDURING CLIMB FROM DFW, RECEIVED PTRIM MAIN INOPERATIVE EICAS WARNING AFTER PASSING ACCELERATION ALTITUDE. BOTH CAPTAIN & FIRST OFFICER SWITCHES INOPERATIVE, BACKUP SWITCH NORMAL. CONTINUED TO SDF FOR CONTRACT MX. RESET IAW FIM 27-43-00 & OPERATIONS CHECK IASDR SIMA20140324002Battery · dischargedFOUND LT WING TO FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE & COCKPIT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD, NO FURTHER FAULTS FOUND.SDR SIMA20140319003Light · inoperativeEMERGENCY LIGHT FWD OF WING INOPERATIVE. R & R FWD EMERGENCY LIGHT IAW AMM 33-50-10, LIGHT OPERATIONS CHECKED GOOD.SDR SIMA20131211002Holder · brokenON FLIGHT 3226 THE CREW REPORTED CAPTAIN`S FLASHLIGHT HOLDER BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R 7 R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16 & OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130904002Flashlight Assy · inoperativeF/A FLASHLIGHT WILL NOT CHARGE. R & R FLASHLIGHT ASSY IAW EAMM 33-50-16, OPS CHECKED GOOD AT THIS TIME.SDR SIMA20130821003Flashlight Assy · inoperativeFWD F/A EMERGENCY FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-55-16. OPS CHECKED GOOD.SDR SIMA20130715005Pump · inoperativeNR 1 HYD QTY LOW, "EMPTY". HYD SYS 1-FAIL AND GEAR ELECTRICAL OVERIDE DID NOT ACTUATE. FREE FALL LEVER WAS USED TO LOWER GEAR IAW AOM-1. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R NR 1 HYD ENGSDR SIMA20130522003Fadec · malfunctionedTHE CREW REPORTED THAT DURING CRUISE FLIGHT, NR 2 ENGINE (N1) SMOOTHLY ROLLED BACK ABOUT 25-30 PERCENT AND THEN SMOOTHLY CAME BACK UP, IT DID THIS 3 TIMES IN ABOUT 15 MINUTES AND THEN RETURNED TO NORMAL. ON LANDING, GOT E1 EXCEEDANCE ON EICAS. THE ACFT WAS RSDR SIMA20130519005Light · inoperativeDURING B INSPECTION, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, STEPS 2M(1)(A-F) AND 3IL(1)(A-G). OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR SIMA20130430002Light · inoperativeDURING B INSPECTION FOUND THE MAIN PASSENGER DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THSDR SIMA20130410002Inverter · inoperativeDURING B INSPECTION FOUND THE MID CABIN OVER HEAD FORWARD FACING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 AC/DC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUSDR SIMA20130228002Skin · dentedDURING MAINTENANCE INSPECTION FOUND THE FORWARD FUSELAGE I UPPER SKIN DENTED DUE TO BIRD STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED DOUBLER IAW AEA EO EM-53MR-1887. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130131018Wire Harness · chafedDURING MAINTENANCE INSPECTION FOUND THE WIRE HARNESS (AIRCRAFT SIDE) FOR THE EMERGENCY LIGHT STRIP NR 1 CHAFED ON BOTH WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE WIRE HARNESS (AIRCRAFT SIDE) FOR THE EMERGENCY LIGHT STRIP NR 1 IAW EMB 145 AMM SDR SIMA20130131017Light · inoperativeDURING B INSPECTION FOUND THE NR 1 AND 8 EMERGENCY LIGHT STRIPS NEED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 AND 8 EMERGENCY LIGHT STRIPS AND FLOOR SIDEWALL BASE ASSEMBLIES IAW EMB 145 AMM 33-50-12.SDR SIMA20130131016Wire Harness · detachedDURING B INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP 3 WIRE HARNESS DETACHED FROM THE LIGHT STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP #3 IAW EMB145 AMM 33-50-12. THE OPERATIONSDR SIMA20130131015Wire · cutDURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 8 CONNECTOR WIRES ON AIRCRAFT SIDE CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP NR 8 WIRES IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUSDR SIMA20130131014Door Seal · tornDURING B INSPECTION FOUND THE MAIN DOOR SEAL TORN ALONG THE UPPER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR SEAL IAW EMB145 AMM 52-18-04. THE FUNCTIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130131013Connector · brokenDURING MAINTENANCE INSPECTION FOUND THE NR 3 AND 6 EMERGENCY LIGHT STRIP CONNECTORS ON THE FLOOR BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE NR 3 AND 6 EMERGENCY LIGHT STRIP CONNECTORS IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOSDR SIMA20130127004Hydraulic System · contaminatedFOR FLIGHT 2759 THE CREW REPORTED THAT DURING THE HYDRAULIC FLIGHT CONTROL CHECK NR 2 HYD RIGHT RUDDER DIFFICULT TO PUSH FORWARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLED RUDDER SYSTEM NR 1 AND SYSTEM NR 2 IAW EMB 145 AMM 27-22-00. THE OPERATIONAL CHECK SDR SIMA20130127003Guide · obstructedON FLIGHT 2759 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED EXCESSIVE MOLYKOTE FROM MAIN DOOR GUIDES IAW EMB 145 AMM 20-30-04. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW EMB 145SDR SIMA20130116003Door · dirtyON FLIGHT 4092 THE CREW REPORTED THE MAIN PASSENGER CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED THE PASSENGER DOOR. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-00-00. THE AIRCRAFT WAS RETUSDR SIMA20121224008Skin · dentedNOSE SKIN DENTED. C/W PART B OF EO EM-53MR-1887, NO FURTHER DEFECTS NOTED AT THIS TIME.SDR SIMA20121128005Wire · looseDURING B INSPECTION FOUND THE EMERGENCY SIGN ON CEILING (FORWARD FACING) INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED EMERGENCY SIGN IN CEILING (FORWARD FACING) FOUND LOOSE WIRE AND REPAIRED AS NEEDED IAW EMB 145 AMM TASK 33-50-15-000-801-A ASDR SIMA20121123004Retaining Ring · missingON FLIGHT 4092 THE FLIGHT ATTENDANT REPORTED THE CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MISSING RETAINING RING ON FOLDING FLAP ACTUATING ROD. INSTALLED NEW RETAINING RING PER STANDARD MAINTENANCE PRACTICES. SDR SIMA20121118009Fuel Sys · leakingON FLIGHT 4284 THE CREW REPORTED VISUAL FUEL LEAK STREAMING FROM LEFT WING NEAR ROOT FROM HINGES OF THE SPOILER (UPPER SIDE OF WING) AND FROM INBOARD AND OUTBOARD FLAPS. VISUAL CONFIRMATION OF 1800 LBS IMBALANCE IN FLIGHT. REPORTS OF FUEL STREAMING HEAVIER DSDR SIMA20121112003Roller · lack of lubeON FLIGHT 4103 THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED ROLLERS IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121018003Inverter · inoperativeDURING B INSPECTION FOUND SEAT 12A FORWARD EMERGENCY SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER PER EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TSDR SIMA20121008001Light · inoperativeDURING B INSPECTION FOUND THE CENTER AISLE EMERGENCY LIGHT NR 4 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LIGHT NR 4 IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVISDR SIMA20120921002Hinge · lack of lubeON FLIGHT 2724 - THE CREW REPORTED THE MAIN PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. CREW REPORTED IT FELT ABNORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED THE MAIN DOOR HINGE AND ROLLERS. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-10-0SDR SIMA20120805006Lamp · inoperativeDURING B INSPECTION, FOUND THE EMERGENCY LIGHT INOPERATIVE AT 12C. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT 12C IAW AMM TASK: 33-50-08-000-801-A, AND 33-50-08-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120630003Flashlight · defectiveON FLIGHT 3248 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT CATCH IS NOT HOLDING LIGHT IN THE HOLDER & KEEPS FALLING OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN EMERGENCY FLASHLIGHT AND CRADLE IN ACCORDANCE WITH EMB 145 AMM 33-SDR SIMA20120523002Lamp · inoperativeDURING B INSPECTION, FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 12 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERHEAD AISLE EMERGENCY LIGHT LAMP IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120521003Unknown · odorFOR FLIGHT 2952 THE CREW REPORTED AN AMBER EICAS MESSAGE "PACK 1 OVLD" PRECEEDED BY A ODOR LIKE COOKING FOOD. TRIPPED OFF ON APU AND ENGINE BLEEDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PACK COOLING SYSTEM NR 1 WAS VERIFIED AND OPERATED NORMAL. BLEED TEMPSDR SIMA20120429009Hinge · lack of lubeON FLIGHT 2845 THE CREW REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN, THE ROLLER PIN CATCHES ON LATCH AND METAL IS WORN SHARP. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR HINGES IAW AMM 52-18-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFTSDR SIMA20120410015Lamp · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT AFT OVER WING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVER WING EMERGENCY LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120407006Lamp · inoperativeDURING B-INSPECTION, FOUND CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 12. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 12 CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVISDR SIMA20120401002Light · inoperativeDURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT HAND OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUSDR SIMA20120323003Light · inoperativeDURING B-INSPECTION FOUND THE CEILING EMERGENCY LIGHT AT 12A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT AT 12A IAW EMB 145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SSDR SIMA2012058013Flashlight · missingON FLIGHT 2786 FLIGHT ATTENDANT REPORTED FLASHLIGHT MISSING ABOVE FLIGHT ATTENDANT JUMPSEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMPSEAT AS PER EMB MM 25-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201205102Coupling · inoperativeON FLIGHT 2040 THE CREW REPORTED A BLEED LEAK NR 1. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FWA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH BLEED LEAK OPERATIONAL CHECK IAW AMM 36-00-00. BLEED NR 1 LEAK STAYS EXSDR SIMA2012010010Light · inoperativeDURING MAINTENANCE BASE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT INOPERABLE AT SEATS 14-16 A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED PROXIMITY LIGHT AT SEATS 14-16 A IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201134303Handle · out of adjustFLIGHT ATTENDANT REPORTS MAIN CABIN DOOR HARD TO OPEN. ADJUSTED AND SET MAIN CABIN DOOR HANDLE IAW EMB AMM 52-18-00.SDR SIMA201130404Shutoff Valve · leakingON FLIGHT 3314 THE CREW REPORTED A FUEL SEAP ON THE LEFT WING INFLIGHT. THE CREW ELECTED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT SHUTOFF VALVE IAW EMB AMM 28-23-02. THE LEAK CHESDR SIMA201113604Controller · inoperativeON FLIGHT 2702 THE CREW REPORTED THAT AT 37,000 FLIGHT LEVEL IN CRUISE THE AUTO CABIN PRESSURIZATION FAILED CABIN. THE PRESSURIZATION WAS AT 11,000. NO MASK DROP. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED INTO MTY. THE CREW DID NOT USE MANUAL MODE. TSDR SIMA201113002Outflow Valve · failedON FLIGHT 3565 THE CREW REPORTED THAT CLIMBING THROUGH FLIGHT LEVEL 270-280 THEY LOST CONTROL OF AUTO PRESSURIZATION. THE CAPTAIN DECLARED AN EMERGENCY DESCENT AND WENT TO MANUAL MODE. THE PANEL WENT TO DASHES IN MANUAL MODE. THE AIRCRAFT DIVERTED TO RDU ANSDR SIMA201111203Floor Support · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED AT FRAME 25 WHERE CARBON BEAM ATTACHES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201111202Floor Support · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND CENTER OMEGA BEAM CORRODED AT FRAME 25 WHERE CARBON BEAM ATTACHES. THE AIRCRAFT WAS REMOVED FROM SERCVICE. REPAIRED CENTER OMEGA BEAM AT FRAME 25 WITH DOUBLER REPAIR IAW SRM 53-00-10. THE AIRCRAFT WAS RETURNED SDR SIMA201109401Floor Support · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 20 CROSS MEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW SRM 53-00-10 FIGURE 201. THE AIRCRAFT WAS RETURNED TO SERVICE.
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