N8877A

Service difficulty reports · 117

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 = 'N8877A' 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 REXA201100765Transmitter · defectiveAT FLIGHT LEVEL 270, AT 300 KNOTS, AIRCRAFT HAD A UNCOMMANDED FLAP MOVEMENT UP AND DOWN THREE TIMES CAUSING AIRCRAFT TO PITCH DOWN. EMERGENCY WAS DECLARED, DIVERTED TO GRB. AFTER REVIEWING THE DFDR DATA WE COULD SEE A FAULTY INDICATION COMING FROM THE LT SIOct 20, 2011 · N8877A · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR REXA201100279Sill · damagedFLOOR SILL LBL 36 BETWEEN FS 409+80 AND FS 409+96, TRANSVERSE BEAM 409+96N AND STRINGER 17L BETWEEN FS 409+80 AND FS 409+96 HAVE TOOL MARKS. REPAIRED IAW BOMBARDIER REO 601R-53-31-725A.May 14, 2011 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100278Skin · damagedTEMP REPAIR ON FUSELAGE SKIN AT FS 409+96 STRINGER 18L REQUIRES PERMANENT REPAIR. REPAIRED IAW BOMBARDIER REO 601R53-31-723.May 14, 2011 · N8877A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100271Angle · crackedFUSELAGE STATION 280 FLOOR ANGLE WEB CRACKED OUTBOARD OF LBL 9 AND OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B,BOMBARDIER SERVICE CORPORATION SR 601R-53-0110, BOMBARDIER SERVICE CORPORATION EO 601R-53-21301A, AND BOMBARDIER SERVICE CORMay 9, 2011 · N8877A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100270Skin · dentedFUSELAGE SKIN IS CREASED AT FS 409.00+16 BETWEEN STRINGERS 15L AND 16L. REPAIRED IAW BOMBARDIER REO 601R-53-31-724.May 9, 2011 · N8877A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100269Rib · crackedBATT RIB CRACKED AT WS 53.60 IN THE LT MAIN LANDING GEAR BAY, INBOARD OF MAIN LANDING GEAR TRUNNION. REPAIRED IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 2.May 7, 2011 · N8877A · Cndair CL6002B19 · Wing, Rib/BulkheadSDR REXA201100266Support · corrodedLEFT O/B ENGINE MOUNT SUPPORT P/N 601-37010-1 ON PYLON IS CORRODED. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.May 5, 2011 · N8877A · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR REXA201100267Support · corrodedRIGHT O/B ENGINE MOUNT SUPPORT P/N 601-37010-1 ON PYLON IS CORRODED. REPAIRED IAW BOMBARDIER REO 601R-54-50-036.May 4, 2011 · N8877A · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR REXA201100265Rib · crackedBATT RIB CRACKED AT WS 53.60 IN THE LT MAIN LANDING GEAR BAY INBOARD OF MAIN LANDING GEAR TRUNNION. REPAIRED IAW BOMBARDIER REO 601R-57-51-046 REV B.May 4, 2011 · N8877A · Cndair CL6002B19 · Wing, Rib/BulkheadSDR REXA201100264Bulkhead · crackedFS 202.75 BULKHEAD LBL 23.75 AT THE PARKING BRAKE CABLE CUTOUT HOLE FAILED NDT INSPECTION. REPAIRED IAW BOMBARDIER REO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0101A.May 4, 2011 · N8877A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000331Sensor · out of adjustON CLIMBOUT OF KCID FOR KMSP THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING INOP WARNING. THE FLIGHT CREW COMPLETED THE QRH AND DECLARED AN EMERGENCY. THE FLIGHT WAS VECTORED TO KMSP WERE AN OTHERWISE NORMAL APPROACH AND LANDING WERE MADE. MAINTENANCE FOUNDDec 26, 2010 · N8877A · Cndair CL6002B19 · Landing Gear Steering SystemSDR REXA201000153Hinge · damagedDAMAGE WAS FOUND ON THE RIGHT WING INBOARD FLAP HINGE ARM ASSEMBLY ON THE UPPER SURFACE OF THE INBOARD LUG AT WS=127. DAMAGE TO THE P/N 601R10917-2 HINGE ARM ASSEMBLY CONSISTS OF A GOUGE MEASURING 0.020 INCH LONG BY 0.090 INCH WIDE WITH A MAXIMUM DEPTH OF 0.0Sep 21, 2010 · N8877A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201000087Connector · looseON CLIMBOUT OF KTYS TO KDTW ON A PART 91 REPOSITIONING FLIGHT, THE RT REV UNLOCKED WARNING ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND ELECTED TO RETURN TO KTYS. CENTER WAS NOTIFIED AND THE FLIGHT WAS VECTORED TO KNOXVILLE. AN OTHERWISE NORMAL APPROAMay 21, 2010 · N8877A · Cndair CL6002B19 · Engine Exhaust System WiringSDR REXA201000081Oil System · fluctuatesAFTER REACHING CRUISE ALTITUDE OF FL330 ENROUTE, CAPTAIN OBSERVED RT ENGINE OIL PRESSURE FLUCTUATING FROM 42 TO 27 PSI. FLT CREW PERFORMED QRH & REDUCED THRUST ON RT ENGINE. JUST AS THE THRUST REDUCED, RT ENG LOW OIL PRESSURE MESSAGE ILLUMINATED FOR ABOUT 2May 18, 2010 · N8877A · Cndair CL6002B19 · Engine Oil Indicating SystemSDR REXA200900135Proximity Switch · faultyAFTER T/O IN DTW RECEIVED STEERING INOP, WOW INPUT CAUTION MSG, AND WOW OUTPUT STATUS MSG. CONTINUE TO TYS AND LANDED ON RWY 23L SAFELY. AFTER LANDING TOWED TO THE GATE. MTX REMOVED AND REPLACED PROX SWITCH PS13GA (NLG WOW NR 1).Dec 11, 2009 · N8877A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2008F00052Apu · failedON TAXI OUT, APU FAILED WHICH RESULTED IN SMOKE IN THE CABIN. FLIGHT CREW DECLARED AN EMERGENCY AND CALLED. NO EVIDENCE OF FIRE WAS FOUND AND THE SMOKE CLEARED. CFR CLEARED AIRCRAFT TO TAXI BACK TO THE GATE. MAINT DEFERRED THE APU AND THE AIRCRAFT WAS RELEOct 7, 2008 · N8877A · Cndair CL6002B19 · APU Core EngineSDR REXA04039Elt · failedELT FAILS G-SWITCH TEST DURING 12-MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.Dec 2, 2004 · N8877A · Cndair CL6002B19 · Emergency Locator Beacon
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