N363QS

Service difficulty reports not matched to an aircraft · 28

They name N363QS, 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 = 'N363QS' 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.

SDR DXTA2011060704607Master Cylinder · leakingCO-PILOT SIDE RT BRAKE IS FREE MOVING HALF WAY THROUGH THE BRAKES. WHEN APPLIED IT CAUSES UNEVEN BRAKING. R & R LT & RT CO-PILOTS BRAKE MASTER CYLINDER. PERFORMED BRAKE SYS BLEED, AND OPS, AND LEAK CHECKED SATISFACTORY. ALL WORK DONE IAW MM 32-42-02 AND Jun 6, 2011 · N363QS · Cessna 560CESSNA · Master Cylinder/Brake ValveSDR DXTA2011060604605Brake Sys · weakCOPILOTS LT AND RT BRAKE PEDALS ARE SPONGY. RT SIDE PEDAL GOES ALMOST TO THE FLOOR ON BRAKE APPLICATION. PERFORMED BLEED PROCEDURE ON RT BRAKE SYS. PERFORMED TAXI CHECK, BOTH PILOT AND COPILOTS BRAKES GOOD. WORK PERFORMED IAW MM 32-42-00.Jun 4, 2011 · N363QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA2011052004585Brake · unknownAIRPLANE PULLS HARD TO THE LEFT WHEN BRAKING FROM PILOTS AND COPILOTS SIDE. COMPLIED WITH BRAKE SYS BLEED IAW MM 32-42-00. LEAK AND TAXI CHECKED GOOD.May 20, 2011 · N363QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR CWQR201102Angle · crackedDURING A SCHEDULED PHASE INSP, FOUND MINOR CORRISION ON THE RT ENGINE BOX BEAM. THE ENGINE WAS REMOVED AND WHEN THE CLOSE OUT PANEL WAS REMOVED FOR CORRISION INSP THE TECH FOUND ANGLE PN 6654002-14, -12 CRACKED, THEY ARE LOCATED ON THE RT ENGINE BOX BEAM LOWERJan 20, 2011 · N363QS · Cessna 560CESSNA · Nacelle/Pylon, Main FrameSDR CWQR201101Channel · damagedDURING A SCHEDULED PHASE INS, THE TECH FOUND MINOR CORROISION ON THE RT ENGINE BOX BEAM. THE ENGINE WAS REMOVED AND WHEN THE CLOSE OUT PANEL WAS REMOVED FOR CORROSION INSP, THE TECH FOUND THAT SOME FASTENERS WERE NOT INSTALLED DURING MFG. THE 4 ANGLES PN 665Jan 20, 2011 · N363QS · Cessna 560CESSNA · Nacelle/Pylon, Main FrameSDR 2008FA0000832Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000831Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000830Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000829Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000828Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000827Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000826Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000825Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000824Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000823Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000822Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000821Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000820Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000819Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000818Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000817Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000816Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000815Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000814Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000813Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000812Rib · crackedWHILE PERFORMING PHASE 1-4 INSPECTIONS, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STAB. AFTER REMOVAL OF THE TOP SKINS ON BOTH STAB, 10 CRACKED RIBS ON THE RT SIDE AND 11 CRACKS ON THE LT SIDE WERE FOUND. ALL OF THE CRACKS WAS FOOct 29, 2008 · N363QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR DXTA200702079Brake Assy · faultedF/O BRAKES LITTLE TO NO EFFECT DURING FIRST 80 PERCENT OF TRAVEL WORKED DURING LAST PART BUT SOFT. NEEDED TO BE PUMPED AT LEAST TWICE TO GET RESISTANCE BUT FADED FAST CAPT SIDE FELT NORMAL. NO LEAKS NOTED.Apr 4, 2007 · N363QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR CWQ2003F00001Duct · crackedDURING ROUTINE INSPECTION, LOOKED INTO DORSAL NACA SCOOPS AND SAW THE LOWER AIR VANE WITH A 3 IN CRACK STARTING FROM CENTER OF (V) CUT TO OUTBOARD EDGE. GAINED ACCESS FROM THE TAILCONE BAGGAGE AREA AND REMOVED CRACKED VANE. REMOVED EA 9309 WHICH SECURES VANFeb 12, 2003 · N363QS · Cessna 560CESSNA · Air Distribution System
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