N908QS
Service difficulty reports not matched to an aircraft · 24
They name N908QS, 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 = 'N908QS' 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 = 'N908QS' 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 DXTA2012032604431A/C Pack · smokeWHILE IN FLIGHT, A FAINT POP WAS HEARD, FOLLOWED BY A SLIGHT SMOKE ODOR. CABIN WAS INSPECTED AND NO SOURCE FOUND. UPON ARRIVAL AT RAMP AFTER ENGINE SHUTDOWN, CABIN RAPIDLY FILLED WITH SMOKE. APU RUNNING, BOTH PAC'S ON. ACFT SHUTDOWN AND SMOKE CLEARED. R &SDR DXTA2010040104056Strut · underserviced"BUMP IN THE NIGHT" NOSE GEAR BUMP OCCURRED SEVERAL TIMES IN FLIGHT. FOUND LOWER STRUT AT 38 PSI. SERVICED LOWER STRUT AS REQ'D. READS 50 PSI AT THIS TIME. OPS CHECK GOOD.SDR 2010F00034Warning Light · illuminatedFUEL FILTER BYPASS R ILLUMINATED IN FLIGHT.SDR DXTA2009091103782Metering Valve · weakBRAKES DO NOT WORK PROPERLY. HAVE TO PUSH DOWN BRAKE PEDALS VERY HARD AND STILL DOES NOT SLOW DOWN AIRPLANE PROPERLY. NEED MORE RUNWAY THEN USUAL TO STOP. REMOVED AND REPLACED BRAKE METERING VALVE IAW CE750 M/M CHAPTER 32-42-03. OPS AND LEAK CHECK GOOD. TAXI SDR DXTA2009041303594Wheel · vibrationYAW DAMPER OFF LOWER AMBER CAS MESSAGE ILLUMINATED DURING INITIAL T/O ROLL. ASSOCIATED WITH MODERATE SHIMMY FELT IN NOSE WHEEL. INSPECTED NOSE GEAR TORQUE LINKS AND FOUND SATISFACTORY DO TO NOSE SHIMMING REMOVED AND REPLACED LT AND RT NOSE WHEELS WITH OVER HASDR DXTA200702669Irs · unknownDURING CRUISE FLT AT FL410, NR2 IRS FAILED. WE WERE ABLE TO REVERT AND USE NR1 IRS INFO. CHECKED FAULTS AND FAULTS FOR PREVIOUS LEG CALL FOR RETURN TO SERVICE & MONITOR PER HONEYWELL FAULT ISOLATION MANUAL. NO PREVIOUS HISTORY OF IRS FAULTS. SYSTEM OPERATIONSDR DXTA200702476Unknown · malfunctionedTHE APU WAS RUNNING NORMAL WHEN IT SHUTDOWN BY ITSELF FOR NO REASON. TRIED TO RESTART THE APU BUT IT WOULD NOT GO PAST 23 PERCENT. DID A COMPLETE RESET OF THE AIRPLANE AND SYSTEMS. TRIED TO START THE APU AGAIN AND WOULD NOT PASS 23 PERCENT. THE APU WILL NOT STSDR DXTA200702455Cable · stickingBRAKES REQUIRE EXCESSIVE FORCE FOR LANDING AND TAXIING. AFTER LANDING, BRAKES SEEMED AT TIMES AS IF THEY WERE DRAGGING AND HAD TO APPLY 50+ N2 TO TAXI. VERIFIED SQUAWK. RT BRAKES LOCK UP WHEN HYDRAULIC POWER IS ON. TROUBLESHOT STICKY CABLE, C/P SEAT. LUBED SDR DXTA200702449Brake · noisyAFTER LANDING THE RT BRAKE MADE A LOUD GRINDING NOISE. WE REQUIRED 50 PERCENT N1 TO TAXI THE AIRCRAFT.SDR DXTA200702440Brake Assy · noneRT BRAKE REQUIRES EXCESSIVE FORCE FOR NORMAL BRAKING. SAME FOR LT AND RT SEAT PEDALS. PERFORMED HIGH SPEED TAXI CHECK AND APPLIED BRAKES NUMEROUS TIMES. NO EXCESSIVE FORCE WAS NEEDED TO APPLY RT BRAKE. INSPECTED NR 3 & 4 BRAKE ASSY. NO DEFECTS FOUND.SDR DXTA200702415Bypass Valve · inoperativeAN EXCESSIVE ODOR OF BURNING OIL IS PRESENT THROUGHOUT CABIN. FOUND APU OIL OVER SERVICED. REMOVED 0.5 CAPS OIL TO BRING APU OIL TO SERVICEABLE LEVEL. INSPECTED AND CLEANED AIR DELIVERY LINES FROM WATER SEPERATOR LEFT SIDE TO THE PERSSURE BULKHEAD. REPLACED FWSDR DXTA200702297Hydraulic System · failedDURING CRUISE AT FL480, THE B SIDE HYDRAULIC SYSTEM FAILED. AMBER CAS MESSAGE B PUMP FAIL, THE B QTY LOW, B PRESSURE DROPPED TO 0 PSI, QTY DROPPED TO 2 PERCENT, BTEMP AT 60 DEGREES. [07-13-07] FOUND RT ENGINE DRIVEN HYD PUMP FAILED INTERNALLY. REMOVED PUMSDR DXTA200702189Acm · frozenAFTER LANDING, COCKPIT TEMP INDICATOR ROSE TO 250 DEGREES AND BLACK SMOKE FILLED THE COCKPIT. COCKPIT TEMP WAS UNCONTROLLABLE THE LAST 30 MINUTES OF THE FLT WITH COCKPIT TEMP AT 150*, REST FLT, LEFT PAC VERY HOT. KPWM TO KSFO. ON GROUND AT KSFO, REPLACED ACSDR DXTA200701898Unknown · odorBURNING SMELL COMING FROM OUTSIDE THE LT AFT FUSELAGE. (NEAR TAILCONE AND NR 1 ENGINE). ACRID AND OILY CONSISTENCY. RAN APU & BOTH ENGINES FOR A PERIOD OF 30 MINS. INSPECTED LEFT AFT FUSELAGE, NR 1 AND 2 ENGINES FOR ANY LEAKS AND NONE WERE NOTED. OPENED TAISDR DXTA200601604Reservoir · unknownBRAKES ARE SPONGY ON LANDING, DURING A STATIC TAKEOFF THE BRAKES WOULD NOT HOLD THE AIRCRAFT ABOVE 75% N1 FROM EITHER PILOT SEAT. BLED ALL BRAKES. TAXIED ACFT TO RUN-UP AREA AND RAN BOTH ENG'S TO 85 PERCENT N1 AT SAME TIME. BRAKES HELD AND NOT SPONGY. OPS SDR DXTA200601351Nut · looseAFTER TAKEOFF CLIMBING THROUGH FL 250 NOTICE A BUMP OR THUMP APPARENTLY COMING FROM NOSE GEAR AREA FOLLOWED BE GEAR UNLOCKED RED LIGHT. CYCLED GEAR ON APP & LIGHT WENT OUT. LOWER GEAR & NORMAL LAND. FOUND STRUT EXTENSION EXCEEDING MAX. LIMITS. FOUND RETAININSDR DXTA200601177Sensor · malfunctionedYAW DAMPER FAIL UPPER A - B FAIL ILLUMINATED IN FLIGHT UPPER RUDDER WOULD NOT MOVE. REMOVED AND REPLACED RT UPPER RUDDER POSITION SENSOR. COMPLIED WITH RIG & OPS CHECK ALL WORK ACCOMPLISHED IAW 750 M/M 27-40-01.SDR DXTA200500827Actuator · failedAMBER "RUB LIMIT FAIL B" CAS MESSAGE WITH A AMBER "RUDDER LIMIT 18%" MESSAGE IN EICAS CNTRL POSITION PAGE. EVENT MARKER PUSHED. COULD NOT DUP FLT CREWS DISCREPANCY ON ARRIVAL. RANG OUT WIRING FROM LOGIC MODULE TO LWR RUDDER LIMIT ACT WITH NO DISCREPANCYS FOUNSDR DXTA200500817Brake · malfunctionedDURING LANDING ROLLOUT BRAKES WERE SOFT AND FELT UNRESPONSIVE WHEN HARD BRAKING WAS APPLIED. ON TAXI IN BRAKES WERE CHECKED BY BOTH PILOTS AND BOTH PILOTS HAD THE SAME PROBLEM AT SLOW SPEEDS AS WELL. ITEM IS UNDER INVESTIGATION.SDR DXTA200500834Actuator · failedRUD LIMIT FAIL B AMBER CAS MESSAGE IN CRUISE FLIGHT, FAILED AT 18%. INSTALLED OVERHAULED LWR RUDDER TRAVEL LIMITER ACTUATOR IAW 750 M/M 27-23-00, AND 27-20-00-720. OPS CHECK GOOD.SDR DXTA200500653Sensor · failedON TAKEOFF ROLL, FULL POWER, ABOUT 70-80 KTS THE RED STAB BLD LEAK L CAS MESSAGE ILLUMINATED. INSTALLED NEW STABILIZER TEMP SENSOR. OPS CHECKED GOOD IAW 750 MM CHAPTER 30-14-00.SDR DXTA200500605Acm · disintegratedDESCENDING FROM FL 410, LOAD POP HEARD FROM REAR OF AIRPLANE AND SMOKE SMELL FILLED THE COCKPIT. PER CHECKLIST ISOLATED THE COCKPIT PAC AND THE SMOKE DISSIPATED. TROUBLESHOT TO COCKPIT ACM TURBINE (COMING APART). REMOVED & REPLACED COCKPIT ACM IAW CE 750 MMSDR DXTA200300117Filter · cloggedFUEL FILTER BYPASS L CAS MESSAGE CAME ON ABOUT 5 SECONDS AFTER TAKEOFF POWER APPLIED. TAKEOFF ABORTED. INSTALLED NEW FUEL FILTER & RESET BYPASS INDICATOR IAW AE3007C MM CHAPTER 73-30-00, LEAK AND OPS CHECKED GOOD.SDR DXTA200300104Circuit Breaker · trippedDURING CLIMB THRU 7000 FEET " REMOTE CB TRIPPED" CYAN CAS MESSAGE ILLUMINATED AND ELECTRICAL FIRE SMELL WAS NOTED IN COCKPIT, NO SMOKE SEEN IN AIRCRAFT. FOUND PASSENGER SAFETY SIGN ON ESCAPE HATCH SHORTED. REMOVED AND REPLACED PASSENGER SAFETY SIGN WITH NEW
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