N837QS
Service difficulty reports not matched to an aircraft · 27
They name N837QS, 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 = 'N837QS' 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 = 'N837QS' 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 DXTA2017073106431Engine · overheatedDURING TAKE OFF, RIGHT ITT WENT TO APPROXIMATELY 740 DEGREES FOR ABOUT 2 SECONDS SOON AFTER LIFT OFF. IMMEDIATELY REDUCED THRUST ON RIGHT ENGINE AND ITT RETURNED TO NORMAL.SDR EBVR20170608001Wire · burnedWHEN PRESSURIZATION, THE KNOB WAS SELECTED TO ANY POSITION OTHER THAN NORMAL, THE NORMAL AND EMERGENCY PRESSURIZATION CIRCUIT BREAKERS TRIPPED. FOUND DURING POST RUN CHECKS. VERIFIED THE DAMAGED AREA ON WIRE APT022-JPA002(20) AT CONNECTOR PT022, RT BLEED AIR SDR EBVR20170606001Bracket · corrodedCORRODED AILERON QUADRANT BRACKET. REPLACED THE CORRODED AILERON QUADRANT BRACKET IAW EO ERO-896682. REV IR.SDR DXTA2016121706343Unknown · odorTHE WINDSHIELD AIR OVERHEAT LIGHT ILLUMINATED DURING DESCENT IN ICING CONDITIONS. THE RAT WAS 5 DEGREES. COULD ALSO SMELL A BURNING ODOR. PERFORMED MULTIBLE OPS CHECKS TO WINDSHIELD ANTI-ICE. NO DEFECTS NOTED. PERFORMED RE RIGGING OF MANUAL CONTROL VALVES. SDR DXTR2016111301Block · wornLT & RT RUDDER PHENOLIC RUB BLOCKS ARE WORN OUT OF LIMITS ALLOWING THE CABLES TO CONTACT THE ALUMINUM AIRCRAFT STRUCTURE. REPAIRED IAW ERO-870610.SDR DXTR2016110701Doubler · damagedAFT VERTICAL STABILIZER DOUBLER AT WL 160.00 DAMAGED. REPAIRED IAW ERO-868612.SDR DXTR2016110401Skin · dentedLT WING LOWER LEADING EDGE SKIN HAS A 5" LONG DENT CENTERED AT APPROXIMATELY WS 139.07. ACCOMPLISHED REPAIR IAW REPORT S-560-0685/04RD.SDR DXTR2016103102Skin · gougedLT FUSELAGE SKIN AT WING FAIRING SCRATCHED (GOUGED) APPROXIMATE LOCATION FS 254.00 WL.100. SKIN THICKNESS IN THIS AREA IS 0.040". REPAIRED IAW ENGINEERING ORDER ERO-868481.SDR DXTR2016103101Drag Angle · crackedLEFT WING FWD UPPER DRAG ANGLE HAS A CRACK APPROXIMATELY 0.20" LONG. COMPLIED WITH ERO-867731 REVISION 1R.SDR CWQR20160307011Rheostat · burnedREPLACED FLIGHT COMPARTMENT FLOOD LIGHT RHEOSTAT DUE TO DEAD SPOTS ON RHEOSTAT. DURING OPERATIONAL CHECK OF NEW RHEOSTAT, WHEN SELECTING DIM, THE RHEOSTAT HEATED UP, EMITTED SPARKS, SMOKE & NR 2 TERMINAL MELTED & FELL OFF RHEOSTAT. AFTER TROUBLESHOOTING FLOOSDR DXTA2016010806159Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT. HANDLE IN THE UP POSITION INDICATIONS WERE, 3 GREEN, 1 RED UNSAFE & HYD PRESS ALL ILLUMINATED. NO GEAR MOVEMENT NOTED. CYCLED HANDLE SEVERAL TIMES WITH SAME INDICATIONS EACH TIME. FOUND GEAR BLOW DOWN BOTTLE LOCKED IN EMERGSDR DXTA2015072306046Compressor · shutdownAIR CONDITIONING COMPRESSOR SHUT ITSELF OFF WHILE ON THE GROUND WITH GROUND POWER UNIT, IMMEDIATELY CREATED A SMOKY ODOR INSIDE THE CABIN. BLACK SMOKE WAS VISIBLE COMING OUT OF THE AFT EQUIP COMPARTMENT, TURNED OFF THE POWER & OPENED THE AFT BAGGAGE DOOR. R SDR DXTR2014061002Skin · dentedFOUND DENT NEAR NOSE JACK PAD, FWD PRESSURE BULKHEAD AREA. ACCOMPLISHED NDT EDDY CURRENT & ULTRASONIC INSPECTION AT LT LOWER FORWARD PRESSURE BULKHEAD AREA AROUND JACK POINT FOR CRACKS & TO VERIFY REMAINING THICKNESS. NO CRACKS NOTED IN THE AREA OF INSPECTIONSDR DXTR2014011701Wire Harness · chafedFOUND SEVERAL FUEL PROBE WIRES CHAFING IN SEVERAL SPOTS IN LT WING FUEL TANK FROM WHAT APPEARS TO BE THE RESULT OF TIE RAP RUBBING. R & R CHAFED WIRES & INSTALLED AND ROUTED LT WING FUEL HARNESS REF DWG 6528110, PROVIDED BY MFG ENGINEERING, WIRING DIAGRAM 28-4SDR DXTR2013120201Door · unknownDURING PREPARATION FOR A PHASE 5 INSPECTION, TECHNICIANS WERE UNABLE TO FREELY OPEN THE EMERGENCY EXIT DOOR WITHOUT EXERTING EXTREME FORCE. THIS IS THE SECOND EVENT THIS YEAR FOR THIS EMERGENCY EXIT; THE FIRST OCCURED ON 06/21/13.SDR DXTR2013062101Door · stuckDURING COMPLIANCE OF INSPECTION TASK 041008 CHAPTER 4 EMERGENCY EXIT DOOR FRAME "INSPECTION TIME LIMITS" TASK 53-10-09-212, TECHNICIANS WERE UNABLE TO FREELY OPEN THE EMERGENCY EXIT DOOR WITHOUT EXERTING EXTREME FORCE WHICH RESULTED IN DAMAGE TO THE DOOR SEAL.SDR DXTA2013012405259Valve · inoperativeIN CRUISE AT 45,000, ACM O'HEAT AND EMERGENCY PRESSURE ANNUNCIATORS ILLUMINATED. THE EMERGENCY PRESSURE VALVE DID NOT OPEN AUTOMATICALLY. CABIN STARTED RISING AT 3300 FPM. FOLLOWED ACM OVERHEAT AND EMERGENCY PRESSURE CHECKLISTS AND SELECTED A WARMER TEMP. NSDR DXTA2011071804659Module · failedON GROUND WITH GPU, AVOINICS AND AIR CONDITIONING ON, CABIN BEGAN TO FILL WITH AN ACIDIC WHITE SMOKE. AIR CON COMPRESSOR LIGHT WAS STILL ON. SHUT OFF ENTIRE ELECTRICAL SYS. AFT EGUIPMENT BAY ALSO FILLED WITH THE SAME SMOKE. REMOVED AND REPLACED AIR CON COSDR DXTA20101104333Warning Light · malfunctionedNOSE GEAR RED UPLOCK LIGHT FAILED TO EXTINGUISH DURING TAKEOFF GEAR RETRACTION.SDR DXTA2010011103941Rudder Pedal · obstructedWHILE TAXIING TO A RT TURN, THERE WAS A LOUD BANG FROM THE RUDDER PEDAL AREA. THERE WAS ALSO REDUCED RUDDER PEDAL TRAVEL AND FREEDOM OF MOVEMENT. INSPECTED RUDDER STEPS, CALBE & PULLEYS ASLO NOSE STEERING MECHANISM. ALL CHECK NORMAL. FOUND CAPT'S LT RUDDER SDR DXTA200803129Tire · failedRT MAIN TIRE BLEW ON TAKEOFF ROLL, ABORTED T/O. REMOVED AND REPLACED RT MLG WHEEL AND TIRE ASSY WITH REPAIRED ASSY. SERVICED TIRE TO 163 PSI WITH NITROGEN. WORK DONE IAW MM 32-42-01.SDR DXTA200802757Landing Gear · inoperativeLANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. PLACED AIRCRAFT ON JACKS. INSTALLED ROBO MULE TO RIGHT ENGINE TO PERFORMED LANDING GEAR OPERATIONAL CHECKS. INSPECTED ALL LANDING GEAR ELECTRICAL CONNECTORS AND LANDING GEAR CONTROL VALVE. SYSTEM CHECKED GOODSDR DXTA200702636Lamp · inoperativeYAW DAMPNER WOULD NOT ENGAGE ON DEPARTURE. PERFORMED AND CHECK AND FOUND BOTH LAMP IN THE SWITCH/IND BURNED. RELALMPED AND PERFORMED A GOOD OPERATIONAL CHECK REF CESSNA 560 MM 22-11-00 AND 33-10-00
SDR DXTA200701984Connector · dirtyWHEN GEAR SELECTED DOWN WE HAS A NOSE AND LT MAIN DOWN INDICATION BUT NO RT AND A GEAR UNLOCK LIGHT STAYED ON. GEAR RETRACTED ON GO AROUND. WHEN RETRACTED ON GO AROUND. WHEN SELECTING GEAR DOWN AGAIN TO RUN CHECKLIST WE STILL GET NO RIGHT INDICATION AND GEASDR DXTA200501027Warning Light · illuminatedUPON GEAR EXTENSION GOING INTO SUN, THE GEAR LIGHTS INDICATED 2 GREEN 1 RED. THE LT MAIN WAS NOT INDICATING GREEN. TURNED OUT OF THE VALLEY TO RUN THE EMERGENCY CHECKLIST ABOUT ONE MINUTE AFTER THE INITIAL GEAR EXTENSION THE LEFT MAIN INDICATED GREEN. ITEM SDR DXTA200501000Static Port · contaminatedDURING TAKEOFF ROLL THE RIGHT AIRSPEED TAPE ADVANCED PRIOR TO THE LEFT, AFTER LEFT TAPE BEGAN TO ADVANCE IAW ANNUNCIATOR APPEARED ON BOTH PFD'S. TAKEOFF ABORTED AT 65 KNOTS. COULD NOT DUPLICATE DISCREPANCY. FOUND BOTH ALTIMETERS WERE IN AGREEMENT. RAN BOTHSDR DXTA200500759Landing Gear · malfunctionedNOSE GEAR WILL NOT RETRACT. PERFORMED LANDING GEAR HYDRO SYSTEMS ADJUSTMENT TEST IAW 560 MM 32-01-00. OPS CHECK GOOD. INSPECTED NOSE GEAR, NO DEFECTS FOUND.
Back to N837QS