N8940E

Service difficulty reports · 62

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 = 'N8940E' 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 REXA201100827Structure · corrodedLT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS PITTING CORROSION APPROX .001"D ON I/B AND O/B ENDS IN NON-CRITICAL REGION AND CHAFING ON THE I/B END APPROX 0.003"D. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 1, 2011 · N8940E · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100826Skin · corrodedLT WING FUEL TANK ACCESS HOLE NR 2 AT WS 12.245 HAS PITTING CORROSION ON I/B AND O/B ENDS IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 1, 2011 · N8940E · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100825Structure · corrodedRT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS PITTING CORROSION APPROX .001"D ON I/B AND O/B ENDS IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.Dec 1, 2011 · N8940E · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA201100824Beam · crackedFS 280 TRANSVERSE BEAM IS CRACKED O/B OF LBL 9.0 AND RBL 9.0. ALSO HAS SIGNS OF CORROSION ACROSS UPPER J-ANGLE AT C/L. REPAIRED IAW BOMBARDIER REO 601R-53-61-926 REV B AND BOMBARDIER SERVICE CORPORATION SR 601R-53-0110.Dec 1, 2011 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100823Bulkhead · chafedFS 621 BULKHEAD FWD FACE HAS CHAFE DAMAGE ON PREVIOUS REPAIR DOUBLERS AT LBL 27, LBL 36, RBL 27 AND RBL 36. DAMAGE MEASURES L= .170", W= .170", DEEPEST IS .006. REPAIRED IAW BOMBARDIER REO 601R-53-61-1285 REV D.Dec 1, 2011 · N8940E · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100838Lever · splitTHRUST LEVERS SPLIT 3/4 TO FULL DURING CLIMB AND MORE THAN 1/2 DURING CRUISE. RT ENG MORE ADVANCED THRUST LEVER BUT SPOOLS SLOWER THAN THE L ENG. PERFORMED ENG RUN-UP IAW AMM 71-00-00. ENG PARAMETERS WITHIN LIMITS. OK FOR SERVICE.Nov 12, 2011 · N8940E · Cndair CL6002B19 · Power LeverSDR REXA201100796Warning System · malfunctionedLT FUEL LO PRESS CAUTION MESSAGE AT ALTITUDE WHEN TRUST LEVERS REDUCED TO IDLE. OPC LT FUEL PRESSURE IAW AMM 73-30-00 OPC NORMAL. OK FOR SERVICE.Oct 31, 2011 · N8940E · Cndair CL6002B19 · Fuel Pressure IndicatingSDR REXA201100645Control Unit · failedFLAPS FAIL DURING CRUISE. TROUBLE SHOT FLAP FAIL IAW 27-052G AND FIM 27-50-00 FECU CODES SHOWED LEFT BPSU, ADC SIGNALS FECU PER FIM 27-50-00 MEGAOHMED LEFT BPSU AND WIRING HARNESS WITH NO DEFECTS NOTED. R & R FECU IAW 27-51-05. OPS CHECKED GOOD. SOct 2, 2011 · N8940E · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100186Landing Gear · malfunctionedGEAR DISAGREE DURING EXTENSION WHILE INBOUND TO JFK. FLIGHT LANDED WITHOUT INCIDENT. FL 4060 AND AIR RETURN TO PVD FOR NOSE GEAR DISAGREE. NOSE GEAR DID NOT COME UP.Mar 14, 2011 · N8940E · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201000125Sill · corrodedSERVICE DOOR LOWER SILL PLATE CORROSION FOUND. REMOVED AND REPLACED SERVICE DOOR LOWER SILL PLATE.Sep 4, 2010 · N8940E · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000072Warning System · malfunctionedA "NOSE GEAR DISAGREE" ON TAKEOFF OUT OF KCLE, FIRST NOSE WHEEL STEERING CAME ON THEN "NOSE GEAR DISAGREE. DIVERTED FROM MSP-DTW. PERFORMED GEAR SWING IAW AMM 32-30-00. OPC GOOD. OK FOR SERVICE.May 5, 2010 · N8940E · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00031Carbon Seal · damaged(REF NR: 05-072) ON DECENT, THE RT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE FLIGHT CREW NOTED THAT THE INDICATED PRESSURE WAS LOW, BUT STILL IN THE GREEN ARC. FLIGHT CREW REVIEWED QRH PROCEDURES FOR A POSSIBLE ENGINE FAILURE. MINUTES LATER THE OIL PRESMay 30, 2005 · N8940E · Cndair CL6002B19 · Turbine Engine Oil System
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