N802EA
Service difficulty reports not matched to an aircraft · 62
They name N802EA, 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 = 'N802EA' 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.
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 = 'N802EA' AND registry_match IS NULL 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 20000609AP002Actuator · leakingON TAKEOFF ROLL, A SYSTEM QUANTITY RAPIDLY DECREASED AND HELD STEADY AT 1.8 GALLONS HYD SYSTEM B CONTINUOUSLY DECREASED TO O QUANTITY WHEN B SYSTEM HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. AOM PROCEDURES ACCOMPLISHED, DIVERTED TO MIAMI, NO FUEL DUMPED. FOUNDSDR 20000425SH022Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 344 WALL-TO-WALL HAS SPOTS OF CORROSION. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000425SH021Beam · misrepairedFOUND DURING SCHEDULED C-CHECK, J-BEAM HAS ROUTED OUT SECTION AT TOP OF CUT OUT WITH PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. (X)SDR 20000425SH020Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 360 BL 24 TO 24 CORROSION AT ANCHOR NUT HOLES. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000425SH019Beam · misrepairedFOUND DURING SCHEDULED C-CHECK, J-BEAM HAS ROUTED OUT SECTION AT TOP OF CUT-OUT WITH PREVIOUS REPAIR ABOVE RT WING NR 8 SPOILER ACTUATOR AREA.SDR 20000425SH018Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 314 BL ZERO HAS CORROSION. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000609AP010Angle · crackedDURING C-CHECK, FOUND NR 1 ENGINE PYLON T/E RIB ATTACH ANGLE CRACKED AND RIB HOLES ELONGATED. REMOVED CRACKED ANGLE, FABRICATED NEW REPAIR PARTS PER SRM 51-40-2. INSTALLED NEW REPAIR PARTS AND SEALED AREA PER SRM 51-10-1 AND SRM 51-40-2. (M)SDR 20000613AP007Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH PREVIOUS REPAIR ABOVE RIGHT WING NR 8 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)SDR 20000522AP004Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 314 BL 0 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6, FOUND OUT OF LIMITS PER SRM 53-10-8, CUT OUT DAMGED FLOORBEAM IAW SRM 53-10-8, PERFORMED HFEC INSPECTION. NO CRACKS NOTED PER SRM 51-10-00. FABRICATED NSDR 20000522AP003Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 344 WALL TO WALL HAS SPOTS OF CORROSION. REMOVED AND FABRICATED NEW FLOORBEAM PER SRM 51-10-1 PAGE 14. TREATED AND PRIMED PER SRM 51-10-6 PAGE 2. INSTALLED FLOORBEAM PER SRM 53-10-1 PAGE 14. (M)SDR 20000522AP002Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 360 BL 24 TO 24 CORROSION AT ANCHOR NUT HOLES. NOTED 1 INCH CRACK AT RBL 5 UNDER FORWARD FLANGE. REMOVED CORROSION TO AFFECTED AREA IN ANCHOR NUT HOLES, WITHIN LIMITS IAW SRM 51-10-6. AT 1 INCH CRACK REMOVED CORSDR 20000615AP004Bracket · crackedDURNIG C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL 9503 LEFT AND RIGHT LOWER SECTION BRACKETS CRACKED. REMOVED BRACKETS, FABRICATED, TREATED AND INSTALLED PER SRM 51-30-3 APGE 14A. (M)SDR 20000615AP003Panel · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M)SDR 20000615AP014Angle · crackedDURING C-CHECK, FOUND TWO RIVETS PULLING, AND .375 INCH CRACK AT DOUBLER AT LT WING LOWER FAIRING SUPPORT ANGLE AFT FALSE SPAR AREA, OUTBOARD OF NR 3 FLAP TRACK. REMOVED DOUBLER FOR CRACK AND TWO RIVETS PULLING AS PER SRM 51-30-2 PAGE 1. FABRICATED NEW DOUBLSDR 20000615AP013Channel · crackedDURING C-CHECK, FOUND 1.5 INCH CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT CHANNEL. INSTALLED NEW CHANNEL IAW SRM 51-30-2 PAGE 1. (M)SDR 20000613AP010Rib · crackedDURING C-CHECK, FOUND NR 3 ENGINE PYLON T/E INNER COMPARTMENT, AFT OF AFT ENGINE MOUNT SUPPORT RIB CRACKED. FABRICATED NEW MOUNT SUPPORT RIB PER SRM 51-10-2 PAGE 1 AND INSTALLED PER SRM 51-30-2 PAGE 1. (M)SDR 20000615AP012Rib · crackedDURING C-CHECK, FOUND TWO EACH 1 INCH CRACKS INSIDE LEFT WING FIXED L/E AT TOP AFT END OF NOSE RIB-SLAT STATION 0, SEEN FROM OUTBOARD SIDE. FABRICATED NEW RIB AND INSTALLED IAW 51-10-1, PAGE 4. (M)SDR 20000615AP011Rib · crackedDURING C-CHECK, FOUND RIGHT WING FIXED L/E RIB AFT END HAS TWO .75 INCH CRACKS THROUGH BOLT HOLES WHERE IT MOUNTS TO FRONT SPAR. CUT OUT CRACK AREAS AT R/W L/E INTERIOR WEB STATION 130-599 IAW SRM 51-40-2 FIG 1. FABRICATED FILLER AND REPAIR DOUBLER AND INSTASDR 20000615AP010Bracket · crackedDURING C-CHECK, FOUND BRACKET HAS 1 INCH CRACK WHERE RT WING NR 8 SLAT LOWER SKIN EXTENSION ATTACHES TO BOTTOM OF INBOARD TRACK. REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2 PAGE 1 AND PAGE 4. (M)SDR 20000615AP009Channel · crackedDURING C-CHECK, FOUND RIGHT WING LOWER TRAILING EDGE SUPPORT INBOARD CHANNEL CRACKED APPROX 1 INCH. REPLACED CHANNEL IAW SRM 51-10-1 PAGE 4. (M)SDR 20000615AP008Angle · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT ANGLE ON BOTTOM OF RIGHT WING UPPER T/E PANEL AT WEB 5 INCHES FORWARD OF INBOARD AILERON L/B LEADING EDGE. FABRICATED NEW ANGLE PER SRM 51-10-1 PAGE 4. INSTALLED ANGLE PER SRM 51-30-2 PAGE 1. (M)SDR 20000615AP007Slat Track · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT LT WING FIXED L/E CUTOUT ABOVE NR 4 SLAT OUTBOARD TRACK. TRIMMED OUT DAMAGED SKIN AND FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PER SRM 57-30-4, PAGE 6. (M)SDR 20000615AP006Rib · crackedDURING C-CHECK, FOUND RIGHT WING L/E RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)SDR 20000615AP005Angle · crackedDURING C-CHECK, FOUND RIGHT WING RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)SDR 20000613AP008Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH IMPROPER PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)SDR 20000613AP009Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACK STATION 680 TO 740 LBL 24 HAS CORROSION OUT OF LIMITS PER SRM 53-10-1, PAGE 16. REMOVED AND FABRICATED SEAT TRACK, INSTALLED PER SRM 51-30-2 PAGE 1. (M)SDR 9805602705Longeron · corrodedDURING H CHECK, FOUND CORROSION ON STR 27L AT FS 1168. REPAIRED PER EA 27-156099.SDR 9805622705Floorbeam · corrodedDURING H CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT FS 1130, RBL 16-27, WL 208. REPAIRED PER EA 27-154488.SDR 9805612705Longeron · corrodedDURING H CHECK, FOUND CORROSION ON STR 29R AT FS 950. REPAIRED PER EA 27-154490.SDR 9724422705Batteries · dischargedDURING PREFLIGHT, FOUND EMERGENCY LIGHT ABOVE REAR EXIT INOPERATIVE. REPLACED BATTERIES AND CLEANED CONTACTS, OPERATIONAL CHECK OK.SDR 9722162705Connectors · corrodedDURING PREFLIGHT, FOUND CEILING EMERGENCY LIGHT ROW 8 INOPERATIVE. CLEANED CORRODED TERMINALS AND INSTALLED SERVICEABLE BATTERIES. OPERATIONAL CHECK OK.SDR 9715512705Batteries · dischargedAFT FLIGHT ATTENDANT SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK.SDR 9715502705Light · inoperativeVENTRAL STAIR EMERGENCY LIGHT INOPERATIVE. CLEANED BATTERY CONTACTS, OPERATIONAL CHECK OK.SDR 9715412705Battery Pack · dischargedDURING SERVICE CHECK, FOUND THAT THE FORWARD GALLEY DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK.SDR 971541Battery Pack · dischargedDURING SERVICE CHECK, FOUND THAT THE FORWARD GALLEY DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK.SDR 9711312705Battery · dischargedDURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK OK.SDR 9702392705Sensor · failedON APPROACH WITH GEAR SELECTED TO THE DOWN POSITION, THE RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND LOCKED. GEAR WAS RECYCLED AND ALL THREE GREEN GEAR INDICATION LIGHTS INDICATED NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT THE RIGHT GEAR INDICATISDR 9700982705Position Switch · failedDURING CLIMB ON FLAP RETRACTION, AMBER LEADING EDGE LIGHT WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 LEADING EDGE FLAP POSITION SWITCH. LEADING EDGE INDICATING SYSTEM OPERATIONALLY CHECKED OK.SDR 9626052705Anti-Ice Duct · failedDURING CLIMB SHORTLY AFTER WING ANTI-ICE WAS TURNED ON, A THUMP WAS HEARD IN THE TAIL COMPARTMENT FOLLOWED BY A LOWER AFT BODY OVERHEAT INDICATION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED BLOWN ANTI-ICE DUCT ON LEFT SIDE OF AFT VENTRALSDR 9624882705Switch · failedDURING TAKEOFF, THE NR 4 LEADING EDGE SLAT INDICATED STILL DOWN ON SLAT/FLAP RETRACTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 LEADING EDGE SWITCH S-205. PERFORMED OPERATIONAL CHECK OF SLAT/FLAP INDICATION SYSTEM, OPERATIONSDR 9624342705Compressor · stalledUPON APPLICATION OF TAKEOFF POWER, AN ENGINE STALL OCCURRED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. CREW WAS NOT ABLE TO DETERMINE WHICH ENGINE CAUSED THE STALL. WINDS WERE REPORTED GUSTING AT 24 KNOTS. MAINTENANCE INSPECTED INLETS AND OUTLETS ON ALL TSDR 9623112705Battery · dischargedDURING LINE CHECK, FOUND THAT THE EXTERIOR LOWER LEFT AFT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK, CHECKED OK.SDR 9615512705Position Switch · failedDURING CLIMB ON FLAP/SLAT RETRACTION, THE NR 4 LEADING EDGE SLAT STILL INDICATED IN TRANSIT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 4 LEADING EDGE FLAP/SLAT POSITION SWITCH AND FLAP/SLAT ANNUNCIATOR INDICATION PANEL, SYSTEM CHECKEDSDR 9610392705Battery Pack · dischargedDURING PREFLIGHT, FOUND AFT FLASHLIGHT WOULD NOT TEST. REPLACED BATTERY PACK, CHECKED OK.SDR 9609342705T/O Warning · activatedDURING TAKEOFF ROLL, THE AIRCRAFT EXPERIENCED TAKEOFF WARNING INDICATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETURNED TO THE GATE. SRQ MAINTENANCE PERFORMED FLIGHT CONTROL AND TAKEOFF WARNING CHECK, SYSTEM CHECKED OK.SDR 9606292705Rmi · malfunctionedDURING CRUISE FLIGHT, THE INSTRUMENT COMPARATOR LIGHT CAME ON IN FLIGHT WITH A 10 DEGREE SPLIT BETWEEN RMI'S. WHEN SWITCHING TO CAPTAIN'S OR FIRST OFFICER'S RMI HAD A 90 DEGREE SPLIT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE INSTRUSDR 9604192705Dn Lock Sensor · failedDURING GEAR EXTENSION, THE LEFT MAIN LANDING GEAR HAD NO INDICATION WARNING LIGHTS. ON THIRD GEAR EXTENSION, GEAR WARNING OPERATED NORMALLY, THREE GREEN LIGHTS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED DAMAGED GEAR DOWNLOCK SENSOR. OPERATIONAL CHECK OF WSDR 9602622705Battery Pack · dischargedDURING PREFLIGHT, FOUND AFT ENTRY EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OK.SDR 9520312705Fcu Water Trap · contaminatedNR 3 ENGINE WAS SLOW TO ACCELERATE DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE FCU MOISTURE TRAP. SUBSEQUENT ENGINE RUN-UP WAS SATISFACTORY.SDR 9518542705Compressor · stalledTHE NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS DURING CLIMB-OUT FROM MSP. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT.
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