N322QS
Service difficulty reports not matched to an aircraft · 18
They name N322QS, 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 = 'N322QS' 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.
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 = 'N322QS' AND registry_match IS NULL 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 DXTA2014091905888Brake Sys · malfunctionedLOSS OF BRAKING DURING LANDING ROLLOUT.SDR DXTA2010031004023Brake Sys · weakBOTH COPILOT BRAKE PEDAL ARE SOFT, TRAVEL 75 PERCENT THEN BRAKES GRAB; ALSO PULLS LT. PILOT SIDE BRAKE PRESSURES SEEM OK BUT HAVE A SLIGHT DELAY FOR BRAKING. FOUND LT BRAKE GRABBING AND CHATTERING. REPLACED IAW AMM 32-92-01. BLED BOTH SIDES RT/LT IAW AMM 3SDR DXTA2010011403944Landing Gear · malfunctionedWHILE ATTEMPTING TO EXTEND THE LANDING GEAR, THE RED UNLOCK CAME ON FOR 3 SECONDS WITH NO AUDIBLE GEAR EXTENSION SOUNDS. THE AFTER 3 SECONDS THE GEAR EXTENDED NORMALLY.SDR DXTA2010011103942Rod End · out of adjustBOTH THROTTLE LEVERS AT ALTITUDE BECOME EXTREMELY DIFFICULT TO MOVE. THE LT THROTTLE LEVER TAKES 2 HANDS AND EXCESSIVE FORCE TO MAKE ANY TYPE OF POWER CHANGE. AT LOWER ALTITUDES (10,000 AND BELOW) THROTTLE LEVERS SEEM NORMAL. REMOVED BOTH ENGINE THROTTLE CABLSDR DXTA2010011103936Brake Assy · malfunctionedBOTH PILOT AND CO-PILOT LT BRAKE PEDAL REQUIRES EXCESSIVE TRAVEL/FORCE. BLED BRAKES AND AFTER BLEEDING BRAKES SYS NOTED A PUDDLE OF HYD FLUID UNDER PILOTS LT BRAKE PEDAL. REPLACED PILOTS LT BRAKE MASTER CYL BLED BRAKES OPERATED BRAKE SYS AND BOTH BRAKE PEDASDR DXTA2009051403650Cam · looseLT ENGINE T/R ARM LIGHT CAME ON IN FLIGHT AND ON THE GROUND. THE T/R'S WOULD NOT STOW IMMEDIATLY-ONCE STOWED, THE LT T/R WOULD DEPLOY EVERYTIME THE POWER LEVER WAS ADVANCED. FOUND LT THRUST REVERSER SEQUENCING CAM LOOSE IN PEDESTAL, ALLOWING OPERATION OF T/R SDR DXTA2009042003607Display · burnedSTRONG SYNTHETIC BURNING ODOR FROM COCKPIT WAS FOLLOWED MINUTES LATER BY FMS SCREEN GOING BLANK. FMS UNIT STILL DISPLAYED DATA ON MFD. BURNING ODOR FILLED ACFT. REMOVED AND INSTALLED A SERVICEABLE FMS, OPS CHECKS GOOD AT THIS TIME ALL WORK DONE IAW MM 34-61-0SDR DXTA200802962Throttle Cable · frozenLT (NR 1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02.SDR DXTA20082962Throttle Cable · frozenLT (NR1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02.SDR DXTA20082873Brake · weakBOTH LT BRAKES REQUIRE MORE PRESSURE THAN THE RT. REMOVED AND REPLACED LT AND RT BRAKE ASSY'S IAW MM CH. 32-42-00. BLED BRAKES IAW MM CH 32-42-00. TAXI CHECK GOOD. LEAK CHECK GOOD.SDR DXTA200702706Gyro · inoperativeNR 1 HEADING INDICATOR FAILED. 1 PFD, STANDBY HEADING INDICATOR AND MFD HEADING INDICATOR FAILED. REMOVED & REPLACED NR 1 DG IAW CE560 MM CHAPTER 34-21-05. OPS CHECKS GOODSDR DXTA200702402Reservoir · overservicedDURING ROLL OUT, THE BRAKES FAILED MOMENTARILY BUT HAD PRESSURE AT THE PEDALS. TROUBLESHOT SYSTEM AND FOUND BRAKE RESERVOIR TO BE OVERSERVICED. REMOVED SOME OF THE FLUID FROM THE RESERVOIR. RAN AIRCRAFT AND PERFORMED BRAKE SYSTEM FUNCTIONAL CHECK WITH NO DEFSDR DXTA200702379Pedal · stiffRT SEAT BRAKE PEDALS REQUIRE LARGE AMOUNT OF MOVEMENT TO WORK. RT PEDAL TRAVELS HALFWAY TO THE FLOOR BEFORE ANY PRESSURE IS FELT. BLED BRAKE SYSTEM IAW 560 MM 32-42-00. OPS CHECK GOOD ON TAXI CHECK.SDR DXTA200601662Brake · malfunctionedCO-PILOTS BRAKE PEDALS (LT AND RT) ARE SPONGY. IT TAKES APPROXIMATLEY 2 INCHES OF TRAVEL TO GET ANY BRAKING ACTION. VERIFIED DISCREPANCY FOUND BLEEDER SCREW LOOSE ON LT BRAKE AND RESERVOIR LEVEL AT MIDDLE OF UPPER SIGHT GLASS. ACCOMPLISHED BRAKE BLEEDING IAW SDR DXTA200601558Link · out of adjustUPON APPLYING STATIC TAKEOFF POWER, NR1 ENGINE (LT SIDE) ONLY MADE 95.1 N1. THE BOOK CALLED FOR 96.7 PERCENT N1. OAT WAS 28 DEGREES C. CHECKED NR 1 ENGINE THROTTLE LINKAGE AND ADJUSTED NR1 ENG MAX N2 STOP. OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY. ACCSDR DXTA200601475Transducer · inoperativeLEFT SIDE BRAKES FEEL VERY HARD ON LANDING. CONSTANT PRESSURE FELT THEN GRADUAL SOFT PRESSURE (DIFFERENT FROM ANTI-SKID RELEASE) HIGH SPEED TEST: SOFTER W/ANTI-SKID OFF. CHECK ANTI-SKID BITE INDICATORS, NO FAULTS. REPLACED BOTH ANTI-SKID TRANDUCERS. REPLACSDR DXTA200500600Switch · failedAT FL 410 RECEIVED THE EMERGENCY PRESS LIGHT. RAN THE CHECKLIST AND RESET THE SYSTEM BACK TO NORMAL. THE CABIN ALTITUDE WENT TO 9000 FEET. THE RATE CONTROLLER SEEMED TO HAVE NO AFFECT AND COULD NOT GET THE CABIN ALTITUDE TO COME DOWN TO THE PROPER ALTITUDE.SDR DXTA200400414Engine · shutdownWHILE BEING VECTORED FOR A VISUAL APPROACH, THE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED, FOLLOWED BY THE LEFT ENGINE UNCOMMANDED SHUT DOWN. DECLARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.
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