N132QS
Service difficulty reports not matched to an aircraft · 17
They name N132QS, 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 = 'N132QS' 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 = 'N132QS' 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 DXTA2013053105406Evaporator · unknownWHITE SMOKE OBSERVED COMING FROM THE AFT CABIN WALL WITH THE FREON AIR CONDITIONER OPERATING. THE SMOKE APPEARED TO BE COMING FROM THE COAT CLOSET SIDE OF THE LAV AREA. REMOVED THE FREON AIR CONDITIONING AFT EVAPORATOR MODULE AND INSTALLED NEW EVAPORATOR MODUSDR DXTA2012122605215Line · misinstalledON TAXI OUT, WENT TO MAKE A LEFT TURN AND PUSHED ON THE LEFT BRAKE TO HELP AND THE PLANE TURNED RIGHT. THEN PUSHED ON THE RIGHT BRAKE AND THE PLANE TURNED LEFT. THEN TRANSFERED CONTROL TO MY PARTNER IN THE RIGHT SEAT AND HE HAD THE SAME PROBLEM. FOUND LT ASDR DXTR20121217003Angle · crackedLEFT ENG THRUST REVERSER, LOWER DOOR, INBD & OTBD STIFFENERS CRACKED. R & R INBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN OFF 202-0001-29 AND PN ON 202-0001-29 IAW SRM 51-42-00. R & R OTBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN OSDR DXTA2012110705174Unknown · odorWHEN PERFORMING OCF: RAN ACFT ON GROUND FOR 10 MINS AT VARIOUS HIGH AND LOW POWER SETTINGS (BLEEDS ON) NO ABNORMAL ODORS PRESENT. ON TAKEOFF JUST AFTER BECOMING AIRBORNE, A STRONG ENVIORMENTAL BURNING ODOR WAS PRESENT. NO VISABLE SMOKE BUT FUMES WERE VERY STRSDR DXTA2012110205164Unknown · odorA STRONG ODOR OF HOT (NOT QUITE BURNING) PLASTIC OR RUBBER COMING FROM THE COCKPIT WEMAC VENTS DURING TAKEOFF, A FEW SECONDS AFTER APPLYING FULL TAKEOFF POWER. THE ODOR DISSIPATES SUBSTANTIALLY A FEW MINUTES AFTER TAKEOFF. PERFORMED TAKEOFF POWER SEVERAL TISDR DXTA2011120204811Windshield · unknownON CLIMBOUT PASSING FL 370 SUDDEN, LOUD, CONTINUOUS HIGH PITCHED NOISE EMANATING FROM SOMEWHERE IN THE FWD PEDESTAL/CENTER INSTRUMENT PANEL AREA. LEVELED AT FL 380, DECLARED EMERGENCY AND BEGAN DESCENT WITH NOISE CONSTANT. PASSING FL330, NOISE BEGAN TO GRADUASDR DXTA2010071504154Ahrs · inoperativeNR 2 AHRS INOPERATIVE IN FLIGHT. TSS COULD NOT DUPLICATE ON GROUND. REPOSITIONED NR1 FCC IN NR 2 POSITION & REPOSITIONED NR 2 FCC IN NR 1 POSITION FOR CONVENIENCE PURPOSES IAW MCC.SDR DXTA2010030804019Fuel Control · malfunctionedRT ENG EFC FAIL LIGHT ILLUMINATED SEVERAL TIMES IN FLIGHT WITH RPM ROLLBACK ON THE RT ENGINE. EFC RESET SUCCESSFULLY TWICE, THEN WOULD NOT RESET THEREAFTER. TROUBLESHOT IAW MM 76-10 & 73-20, ASSISTED BY MFG TECH SUPPORT. REMOVED THE LT & RT EEC & T/O PROBES SDR DXTA200803026Computer · inoperative1 HOUR INTO FLIGHT, AT FL380, THE RUDDER BOOST FAIL LIGHT CAME ON. REMOVED AND REPLACED WITH OVERHAULED FGC COMPUTER. RUDDER BOOST OPS CHECKED GOOD IAW MM 27-21.SDR DXTA20082911Squat Switch · defectiveSPEED BRAKES WORK INTERMITTENTLY IN FLIGHT. TROUBLE SHOT SPEED BRAKE SYSTEM & FOUND LH WOW SWITCH DEFECTIVE AND LT THROTTLE LEVER 85 PERCENT SWITCH OPERATING ARM OUT OF ADJUSTMENT. REMOVED UNSERVICEABLE LT WOW SWITCH & INSTALLED A NEW SWITCH. ADJUSTED LT THSDR DXTA200702563Transducer · inoperativeON CLIMB OUT AFTER FLAP RETRACTION, ACCELERATING THROUGH 160 KIS, (RDR BST FAIL) YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH DISENGAGEMENT OF THE YAW DAMPER. REMOVED NR 1 ENGINE TRANSDUCER PN APTE233A-1750300A SN 7064-16-116, 7064-16-129 AND NR 2 ENGINE TRANSDSDR DXTA200702549Downlock Switch · malfunctionedON FINAL APPROACH THE RT MAIN GEAR (GREEN) LIGHT FAILED TO ILLUMINATE. ACCESSED CONNECTOR P272 IN RT WW. OHMED OUT DOWN LOCK SWITCH FOUND 2 OHMS RESISTANCE THROUGH CLOSED CONTACTS OF SWITCH, REMOVED SWITCH AND INSTALLED NEW CUSTOMER SUPPLIED SWITCH. REINSTALSDR DXTA200702448Adapter · failedRDR BST FAIL LIGHT FLASHED INTERMITTENTLY DURING TAKEOFF, THEN CAME ON STEADY 1 MIN AFTER TAKEOFF. 09-27-07 INTERROGATED AVIONICS STATUS ON THE MFD & FOUND NO CODES FOR RUDDER BOOST FAIL MESSAGE. PER THE RUDDER BOOST T/S CHART INTERROGATED THE LRU FAULT SDR DXTA200702284Unknown · unknownAT 13,000 FT, WITH THE AUTOPILOT ENGAGED, THE AIRCRAFT BEGAN AN UNCOMMANDED ROLL TO THE RT. THE ALTITUDE REMAINED LEVEL. [07-12-07] INSPECTED AUTOPILOT SYSTEM NO FAULT CODES WERE RECORDED IN THE FCC COMPUTER. FOUND CIRCUIT BOARD CARD A194 LOOSE. RESECURESDR 2007FA0000507Nut · looseCREW REPORTED PRESSURIZATION CONTROL INEFFECTIVE, CABIN RATE CLIMBING AND DESCENDING, WHILE DESCENDING IN AUTOMATIC MODE. STABILIZED BRIEFLY WHILE IN MANUAL MODE. TROUBLESHOT IAW FIM 21-30-00, EXCESSIVE LEAK RATE NOTED AT TEST PORT 2. FOUND LOOSE (B) NUT ONSDR DXTA200601761Control Cable · out of adjustLOUD BUZZ HEARD AND VIBRATION FELT THROUGH OUT AIRPLANE APPROX. 10 MINUTES AFTER TAKEOFF. BUZZ AND VIBRATION INTENSIFIED AS AIRSPEED INCREASED WENT AWAY WHEN FLAPS EXTENDED FOR LANDING. ON POSTFLIGHT. FOUND FLAPS NOT FULLY RETRACTED WITH FLAP INDICATOR SHOWINSDR DXTA200601256Landing Gear · malfunctionedLOWERED LANDING GEAR AND GOT THREE GREEN LIGHTS AND 2 RED LIGHTS. RETRACTED LANDING GEAR AND GOT NO GREEN LIGHTS AND 2 RED LIGHTS CYCLED GEAR SEVERAL TIMES AND GOT SOME INDICATIONS, DID EMERGENCY GEAR EXTENSION GOT NORMAL GEAR INDICATION 3 GREEN. VERIFIED AD
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