N8886A

Service difficulty reports · 112

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 = 'N8886A' 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 REXA201100470Bulkhead · chafedREAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 2 LOCATIONS ON LT SIDE AT LBL 18 AND LBL 27 ALL LOCATED 30 INCHES ABOVE THE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jul 29, 2011 · N8886A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100469Post · damagedFOUND FS 409.0+128 VERTICAL POST BL 0.00 LT & RT SIDES HAVE INDICATIONS NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS BOTH FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND BOMBARDIER REO 601R-53-41-889.Jul 29, 2011 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100468Post · damagedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT. FLANGE RADIUS FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06, 51-42-22, AND BOMBARDIER REO 601R-53-41-889.Jul 29, 2011 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100467Skin · dentedFUSELAGE SKIN IS DENTED AT FS 642 BETWEEN STR 21L & 22L. DENT MEASURES APPROX .650" DIA X .045"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-4132.Jul 29, 2011 · N8886A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2011004645Floor Support · corrodedCARGO FLOOR SUPPORT BEAM CAP ANGLE HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 589-FS 621, LBL 27. REPAIRED IAW SRM 51-42-34, 51-45-00,51-42-21, 5142-22, AND BOMBARDIER REO 601R53-61-3788 REV A.Jul 27, 2011 · N8886A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100131Engine · malfunctionedCREW REPORTED SMOKE IN THE CABIN EMERGENCY DECLARED. T/S TO THE RIGHT ENGINE CAUSING THE SMOKE IN CABIN WITH EITHER LT OR RT PACKS RUNNING OFF RT ENGINE, A/C WAS FERRIED TO TYS FOR BOROSCOPE AND POSSIBLE ENGINE CHANGE.Feb 21, 2011 · N8886A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA201100080Control Unit · malfunctionedSTAB TRIM RUNAWAY ON DEPARTURE. AIR RETURN TO JFK. QRH COMPLETED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. PERFORMED OPS CHECK ON HSTCU. OPS CHECK GOOD. OK FOR SERVICE.Jan 29, 2011 · N8886A · Cndair CL6002B19 · Stabilizer Control SystemSDR REXA201100041Carbon Seal · leakingON CLIMBOUT OF KDTW THE CAPTAIN SAW SMOKE COMING FROM A VENT. THIS WAS FOLLOWED BY A SMOKE TOILET CAUTION MESSAGE. THE FLIGHT CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO KDTW. AN OTHERWISE UNEVENTFULL APPROACH AND LANDING WAJan 18, 2011 · N8886A · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA201000114Shutoff Valve · inoperativeREFUEL PANEL INOP. NOT READING CORRECTLY. REFUEL SOV INOP. OPERATIONAL CHECK OF FUEL SYSTEM GOOD IAW AMM 28-00-00. THIS CLEARS DM 27692.Aug 24, 2010 · N8886A · Cndair CL6002B19 · Fuel Selector/Shut-Off ValveSDR REX2008F00018Control Panel · malfunctionedRUDDER TRIM RUNAWAY WITH FULL DEFLECTION TO THE LT ON CLIMBOUT. REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. (A)Jul 21, 2008 · N8886A · Cndair CL6002B19 · Rudder Tab Control SystemSDR REXA200500115Control System · malfunctionedFLAP FAIL MESSAGE. INSPECTED PER AD 98-20-01. NO DEFECTS NOTED. RESET FLAPS PER MANUFACTURES FAULT ISOLATION MANUAL (FILM). OPERATIONALLY CHECKS GOOD.Sep 9, 2005 · N8886A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA04040Elt · failedELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.Dec 2, 2004 · N8886A · Cndair CL6002B19 · Emergency Locator Beacon
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