N811AA, cancelled Apr 8, 2026
Service difficulty reports · 21
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 = 'N811AA' AND deregistration_id = 'N811AA-2026-04-08' 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 = 'N811AA' AND deregistration_id = 'N811AA-2026-04-08' 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 Y2PA2023100523050Actuator · leakingCREW STATED THAT WHILE ON FINAL FOR RUNWAY 19L, THE GEAR DID NOT COME DOWN. THEY REQUESTED DELAY VECTORS TO RUN PROCEDURE. THEY PERFORMED PROCEDURE A SUCCESSFULLY, GEAR EXTENDED. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. FOUND THE RH MAISDR Y2PA2023082223045Valve · bindingDISCREPANCY: CREW REPORTED THAT THE CABIN ALTITUDE LIGHT AND HORN WENT OFF UPON REACHING CRUISE ALTITUDE. THEY DONNED MASKS AND RAN POH PROCEDURE. THEY COULD NOT REDUCE CABIN ALTITUDE WITH AUTO OR MANUAL SYSTEMS. THEY EXECUTED EMERGENCY DESCENT. THEY EXECUTED SDR Y2PA2022090622048Engine · flamed outDISCREPANCY: CREW REPORTED THAT WHILE CONDUCTING ENGINE ACCELERATION CHECKS ON THE #1 ENGINE, THE #1 ENGINE FLAMED OUT AT FL290. THE CREW DECLARED AN EMERGENCY WITH CLEVELAND CENTER TO OBTAIN LOWER ALTITUDE, THEY DESCENDED AND PERFORMED A SUCCESSFUL RELIGHT ATSDR Y2PA2019121719050Switch · out of adjustDISCREPANCY: CREW REPORTED RIGHT GEAR “GREEN” DOWN AND LOCKED FAILED TO ILLUMINATE, LANDING GEAR WARNING HORN COULD NOT
BE SILENCED, CREW PERFORMED LANDING GEAR EXTENSION EMERGENCY CHECKLIST “PROCEDURE A”, COMPLETED UNSUCCESSFULLY,
“PROCEDURE C” ALSO UNSUCCSDR Y2PA201911265046Skin · crackedDISCREPANCY: DURING C-CHECK AT KBVO, CRACK WAS FOUND ON NLG SKIN AND DOUBLER AT AFT LH CORNER OF WHEEL WELL. CRACK
DIMENSIONS HAVE BEEN SENT TO DFJ
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CRACK AT NOSE WHEEL WELL LF AFT CORNER FRAME 7 AT STRINGER 22 IAW SDR Y2PA201911265045Skin · corrodedDISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON
BOTH LH AND RH SIDES OF THE FUSELAGE
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-SDR Y2PA2019112600025Skin · corrodedDISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON
BOTH LH AND RH SIDES OF THE FUSELAGE
CORRECTIVE ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-SDR Y2PA201911265044Skin · corrodedDISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON LH SIDE OF FUSELAGE DURING SPOT WELD NDT
INSPECTION.2 SPOTS ARE OUT OF LIMITS, AREAS ARE LOCATED FROM FRAME 18 TO FRAME 19, BETWEEN STRINGER 10 TO STRINGER 13
CORRECTIVE ACTION: PHSDR Y2PA201911265043Skin · corrodedDISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON RH SIDE OF FUSELAGE DURING SPOT WELD NDT
INSPECTION.12 SPOTS ARE OUT OF LIMITS, AREAS ARE LOCATED FROM FRAME 5 TO FRAME 19, BETWEEN STRINGER 15 TO STRINGER 20
CORRECTIVE ACTION: PHOENSDR Y2PA2018112170040Blade · failedCREW REPORTED – AT 34,000 FT LEFT ENGINE EXPERIENCED A LOUD BANG, LOST THRUST, EPR=1.2, EGT=695°, N1=70% AND DEVELOPED A LOUD WHIRRING SOUND. DECLARED EMERGENCY, SOUND AS THOUGH ENGINE WAS OVERSPEEDING. WAS ABLE TO USE ENGINE TO LANDING @ KONT, WITHOUT INCIDESDR Y2PA2018100100034Selector Switch · unserviceableCREW REPORTED – FO'S LEG. NORMAL TAKEOFF ROLL @V1 (122) JUST BEFORE ROTATION TWO (2) JACKRABBITS RAN IN FRONT OF THE AIRCRAFT. AT LEAST ONE WAS STRUCK BY THE LEFT MAIN LANDING GEAR STRUT. THE LEFT (NO. 1 ENGINE) ROLLED BACK BUT RECOVERED IMMEDIATELY. AT POSITISDR Y2PA2018052960020Pressure Sensor · failedCREW REPORTED THEY WERE UNABLE TO EXTINGUISH NR 2 HYDRAULIC LIGHT ON STANDBY GAUGE. RAN CHECKLIST. NO GUIDANCE IN CHECKLIST FOR IF LIGHT DOES NOT EXTINGUISH. USED SYSTEMS DIAGRAM AND KNOWLEDGE TO ASSESS THE SITUATION. MAINTENANCE CONTROL ADVISED TO RETURN TSDR Y2PA2015043000021Control Panel · shortedCREW REPORTED LANDING GEAR EXTENSION FAILURE, E27. LT GEAR UNSAFE, NO GREEN LIGHT. CYCLED GEAR ONCE, NO GREEN LIGHT. PERFORMED MISSED APPROACH AND ENTERED LANDING PATTERN. DECLARED EMERGENCY AND FLEW EXTENDED PATTERN TO LOWER GEAR WITH PROCEDURE A, 3 GREEN SDR Y2PA20130316015Trim Panel · malfunctionedCREW REPORTED, ON HAND FLOWN AT 2500' IN IMC, PILOT FLYING ENCOUNTERED AN UNCOMMANDED ROLL TO THE LEFT. PF IMMEDIATELY PULLED "ROLL" CIRCUIT BREAKER TO STOP RUNAWAY TRIM CONDITION. TRIM INDICATED APPROX. .5 TO .666 DEFLECTION TO THE LT OF CENTER. PM DECLARESDR Y2PA20130120004Turbine Blades · fodCREW REPORTED ENGINE FLAMEOUT AT FL346 AND REQUESTED DESCENT TO FL290. CREW DECLARED AN EMERGENCY AND WERE VECTORED. CREW RAN ENGINE FAILURE AND RELIGHT CHECKLIST. ENGINE RELIGHT WAS SUCCESSFUL AT FL280. ACFT CONTINUED AND USING NORMAL PROCEDURES, LANDED USDR Y2PA20120618032Governor · bypassingIN CRUISE AT .66 MACH AND FL 350, ADJUSTED EPR FROM 1.44 TO 1.60, AFTER 30 SECONDS FURTHER INCREASED EPR TO 1.75. APPROX 1 MINUTE LATER THE NR 1 ENGINE FLAMED OUT. DECLARED AN EMERGENCY WITH INTENT TO LAND. RAN ENGINE FLAME OUT CHECKLIST, RELIGHT SUCCESSFULSDR Y2PA20120428021Governor · bypassingNR 1 ENGINE FLAMED OUT AT FL350, NO INDICATION FOR REASON WHY. INSPECTED FUEL FILTERS, BOROSCOPED AND VISUALLY INSPECTED ENGINE, NO DEFECTS FOUND. R & R FUEL PRESSURE VALVE, OPS AND LEAK CHECKED GOOD. PERFORMED GROUND RUN, NO DEFECTS NOTED. TEST FLIGHT OF ASDR Y2PA20120417013Turbine Case · rupturedAT 14000 FT, NR 1 ENGINE FIRE INDICATION AND HORN ACTUATED. REDUCED THRUST IAW EMERGENCY CHECKLIST, LIGHT EXTINGUISHED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTION DISCOVERED A HOLE ON PYLON SIDE OF THE ENGINE TURBINE CASING, CAUSING FIRE INDSDR Y2PA05008Pump · intermittentDURING CLIMB OUT NR 1 ENG STARTED TO SURGE. NR 1 FUEL PRESSURE DROPPED TO ZERO. OPENED CROSSFEED THEN NR 2 ENG LOST 50 PERCENT POWER, FUEL PRESSURE DROPPED TO NEAR ZERO AND NR 2 FUEL PRESSURE LIGHT CAME ON. CREW DECLARED EMERGENCY, TURNED BACK TOWARDS FIELDSDR Y2PA04008Wheel · vibrationON TAKEOFF, CREW DETECTED VIBRATION ON RT MAIN GEAR. CREW HAD TOWER INSPECT RUNWAY TO FIND TIRE CAP AS SUSPECTED. AC DIVERTED, TO BURN FUEL AND OBTAIN EMERGENCY FACILITIES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. EMERGENCY WAS CANCELLED BY SDR Y2PA96050Jet Pump · cloggedELP - WHEN FUEL WAS NOT ABLE TO TRANSFER PROPERLY FROM RIGHT TO LEFT WING, THE CREW RETURNED TO POINT OF DEPARTURE AT ELP. NO EMERGENCY PROCEDURES WERE REQUIRED. MAINTENANCE FOUND THAT THE LEFT WING INTERCONNECT JET PUMP WAS CLOGGED. THE OBSTRUCTION WAS REM
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