JASC 3411
Service difficulty reports · 1,588
Reports filed under 3411 · Pitot/Static System, 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 jasc_code = '3411' 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 jasc_code = '3411' 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 COMA0660484Pitot Line · contaminatedFLIGHT 5587 - DURING CLIMBOUT OF AUS WITH AUTO-PILOT ON, THE AIRCRAFT BEGAN PITCHING UP AND DOWN WITH YOKE MOVEMENT FORWARD AND AFT. FLIGHT DIRECTOR NR 1 AND 2 DID NOT MATCH. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE FIELD. PURGED NR 1 AND NR 2 SDR PIDA06084Pitot Tube · obstructedRTO 90 KTS 86000 LBS, NO CAPTAIN'S AIRSPEED, NO STANDBY AIRSPEED, FIRST OFFICER AIRSPEED NORMAL. REMOVED OBSTRUCTION FROM CAPTAINS PITOT TUBE. OPS CHECK NORMAL IAW MM 34-11-0.SDR QXEA200602045Probe · damagedSEA FLIGHT NR 2432: PITOT HEAT STANDBY CAUTION ILLUMINATED DURING TAXI FOR TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE STANDBY PITOT/STATIC PROBE IAW AMM 34-12-11. C/W PITOT/STATIC LEAK CHECK IAW MTC 6341102. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICSDR MASA200601960Pitot Line · obstructedASH 6104 PHX - STALL FAIL CAUTION, RUDDER LIMIT FAULT AND SPOILER STAB FAULT. MX PURGED WATER FROM LINES. OP'S CHECK GOOD.SDR DXTA200601519Pitot System · contaminatedON TAKEOFF ROLL BETWEEN 60 AND 80 KTS, AMBER "MACH TRIM OFF" AND AMBER "YD OFF LOWER" CAS MESSAGES ILLUMINATED. YD AND M TRIM ANNUNCIATORS ON AUTOPILOT CONTROLLER WENT BLANK. AMBER ARROW APPEARED ON PILOTS PFD AND AP MODES DISAPPEARED. V SPEEDS WERE INTERMISDR 06FDEA2663Pitot Tube · dirtyRIGHT AFTER ROTATION BOTH ATS LEVERS DROPPED OFF. ADC FAILED ON CAPT SIDE SWITCHED OVER TO OTHER SYSTEM REENGAGED ATS LEVERS AS PER ECAM THROTTLE RETARDED TO IDLE AS SOON AS ATHR BUTTON PUSHED. NO ECAM FOR ADC. ALSO NR 1 FLT DIRECTOR FAILED. CAPTS ALTIMETESDR DXTA200601502Drain · leakingABORTED TAKEOFF DUE TO AIRSPEED MISMATCH. AT 70 KIAS NR 1 PFD INDICATED 70 KIAS, STANDBY AIRSPEED INDICATED 70 KIAS, NR 2 PFD INDICATED APPROX 83 KIAS. NO DISCREPANCY NOTED ON INITIAL AIRSPEED INDICATIONS AT BEGINNING OF ROLL. WX WAS CLEAR WITH NO PRECIP. CSDR ASMF200607002Cadc · failedAIRCRAFT RETURNED TO PLATFORM, CADC FAIL WINDSHEAR INOP AND F/D FAIL LIGHTS TURNED ON. DURING MAINTENANCE REVISION, WHEN BOTH AIR DATA SYSTEMS WERE SELECTED TO CADC NR 1 POSITION, THE FAIL DISAPPEARED, BUT WHEN SYSTEMS RETURNED TO NORMAL POSITION, FAILURE APPESDR MASA200601711Pitot Line · contaminatedASH 7319 IAD - STALL FAIL AT TAKEOFF. MX FOUND WATER IN THE PITOT LINES AND DRAINED. OPS CHECK NORMAL.SDR DXTA200601459Pitot System · contaminatedDURING T/O ROLL, IAS FLAGGED ON BOTH PILOT AND COPILOT AIRSPEED INDICATOR. T/O WAS ABORTED. PURGED NR 1 AND NR 2 PITOT SYSTEMS IAW CESSNA 560 MM 34-11-10. FOUND WATER IN NR 1 PITOT SYSTEM. PERFORMED PITOT/STATIC LEAK CHECK OF NR 1 AND NR 2 SYSTEMS IAW CESSSDR MASA200601702Pitot Line · contaminatedASH 6127 YEG - THE CREW ABORTED THE TAKEOFF ROLL DUE TO A STALL FAIL CAUTION MESSAGE. MX DRAINED THE PITOT/STATIC LINE TRAPS AND THE CREW PERFORMED A HIGH SPEED TAXI CHECK, SYSTEM OPERATING NORMALLY.SDR DXTA200601455Pitot System · obstructedABORTED TAKEOFF DUE TO SPLIT IN AIRSPEED INDICATIONS. LEFT : HUNG AT 80KTS. RIGHT : READ 100 KTS. INSPECTED LT PITOT PROBE FOR BLACKAGE. NO VISUAL SIGN OF BLOCKAGE NOTED. CONNECTED PITOT TESTER TO LT PITOT TUBE AT ADC. APPLIED PRESSURE AND REMOVED BUG FRSDR F3LA200600068Probe · corrodedDURING C-4 CHECK, INSPECTION REPORTED RT PITOT PROBE SCREW LUGS BENT AND CORRODED. REPLACED RT PITOT PROBE PER AMM 34-11-15-420-050.SDR MASA200601569Pitot System · contaminatedASH 7406 ORD - STALL FAIL CAUTION/RUDDER LIMIT FAULT/SPOILER STAB FAULT. MX DRAINED WATER FROM PITOT SYSTEM AND PERFORMED SPOST. NO FURTHER DEFECTS NOTED.SDR SWIA200616775Tube · contaminatedCLIMBING OUT AT ABOUT 6,000 FEET, GOT AN EFIS COMP MON CAUTION MESSAGE FOLLOWED BY AMBER ALT FLAGS ON BOTH ALTIMETER TAPES. RETURNED TO FIELD. REMOVED CONTAMINATION FROM 1-2 STATIC PARTS ON PITOT/STATIC TUBES, PER MM 34-11-00-100-801. OPERATIONAL CHECKS GOODSDR WRLA2006013Pitot Tube · obstructedON DEPARTURE, FLIGHT DIRECTOR INOP BOTH SIDES AMBER A/P AND ATS BOXES IAS COMPARATOR BOTH SIDES. FA USING AIRSPEED LOST, SUSPECT ERROR. CHECKLIST DETERMINED. DETERMINED CADC NR 1 WAS AT FAULT. DIVERT TO ATL. FOUND FOD NR 1 PITOT TUBE. ALSO TUBE L/E ERODESDR CHQA200600068Relay · burnedFLIGHT 5284 - STL-ATL - DURING CRUISE FLIGHT AT FL330, -PITOT 2 INOP- EICAS MESSAGE APPEARED. TURNED OFF THE PITOT 2 SWITCH AND RAN THE QRH. A SLIGHT ELECTRICAL SMELL IN THE FLIGHT DECK. TALK TO THE F/A, WHO ALSO SMELLED THE ODOR. ALSO NOTED A SLIGHT HAZE SDR MASA200601478Pitot Line · contaminatedASH 5017 EWR - RUDDER LIMIT/SPOILER STAB FAULTS. CONTRACT MX FOUND AND DRAINED WATER FROM STBY PITOT SYSTEM. NO FURTHER DEFECTS NOTED.SDR MASA200601490Pitot System · contaminatedASH 7305 ORD. PILOT ABORTED TAKEOFF, DUE TO STAND BY AIRSPEED IND READING -0- AT THE 80 KNOT CHECK. UNITED MX DRAINED WATER FROM THE PITOT SYSTEM. OP'S NORMAL. NO FURTHER ACTION REQUIRED.SDR ASMF200605018Pitot Tube · dirtyAIRCRAFT REJECTED TAKEOFF AS A CONSEQUENCE OF -IAS DISAGREE- FAIL INDICATION TURNED ON IN FIRST OFFICER DISPLAY AND THE VEL AIRSPEED WINDOW SHOWED 79 KTS. ELECTRICAL POWER WAS REMOVED FROM THE AIRCRAFT AND IT WAS SUPPLIED ONLY WITH THE APU DISAPPEARING THE FASDR DXTA200601413Pitot System · obstructedON TAKEOFF ROLL, COPILOTS AIRSPEED INDICATOR NEVER MOVED OFF OF 40 KTS. CAPTAINS AIRSPEED SHOWED 65 KTS MAX WHEN ABORT WAS INITIATED. STANBY AIRSPEED INDICATOR HAD MOVED FROM ITS MINIMUM 60 KTS. REPEAT WRITEUP. CHECKED PILOT AND COPILOT AIRSPEED INDICATORS WISDR FWT2006F00001Relay · malfunctionedAFTER 00:25 FLYING MINUTES, RETURNED TO GROUND DUE TO 1-30-32-03-01 EICAS MSG L AOA PROBE DISPLAYED. L AOA PROBE HEAT LIGHT ILLUM. 2-30-33-06-00 EICAS MSG TAT PROBE DISPLAYED, TAT PROBE HEAT LIGHT ILLUM. 3-30-31-09-00 EICAS MSG PROBE HEAT DISPLAYED 2 OR MORSDR DXTA200601405Pitot Tube · obstructedON T/O ROLL, L AIRSPEED INDICATOR WAS AT 80 KIAS WHILE R SIDE INDICATED 40 KIAS ( IT NEVER MOVED DURING ROLL). - CLEANED DEBRIS FROM RIGHT PITOT TUBE. OPERATIONAL CHECKS AND LEAK CHECKS OF THE PILOTS AND CO-PILOTS AIRSPEED INDICATOR SATISFACTORY IAW THE HAWKERSDR WRNA200600014Static Line · brokenRUDDER RATIO LIGHT CAME ON IN CLIMB, .84M SPEED 300K ALT 32,000. STAYED -ON- CRUISE 39,000 AT 261K, UPPER RUDDER 2 DEGREES LEFT, LOWER RUDDER 0 DEGREES, LIGHT WENT OUT AT 24,000 AT 300K. RETURNED TO MIA AND MADE A SAFE LANDING. RIGGED UPPER AND LOWER RUDDERSDR DL76L060416Probe · malfunctionedON TAXI OUT, PITOT ANNUNCIATOR LIGHT AND EICAS MSG. REPLACED F/O PITOT PROBE. PART AOG FROM LGW. SYSTEM CKS GOOD CARRIED OUT LEAK CK PER MM 34-11-00.SDR QXEA200601325Pitot Line · contaminatedSEA FLIGHT: DURING CRUISE, CAPTAIN'S AIRSPEED INDICATOR STARTED TO INDICATE ERRONEOUS READINGS. RECEIVED SEVERAL CAUTION LIGHTS ASSOCIATED 'RUD CNTL', 'PITCH TRIM', 'SPOILER OUTBOARD', 'ELEVATOR FEEL' AND 'IAS MISMATCH' MESSAGE ON THE PFD. PER THE EMERG/ABNOSDR KPVA200611Line · contaminatedON TAKEOFF ROLL PITCH TRIM/ELEVATOR FAILED. DRAINED MOISTURE FROM RT PITOT MOISTURE TRAP & CLEARED PITOT STATIC LINE IAW DHC-8 PSM Q400 MM CHAPTER 34-11-06 PG 302 PAR 4A.SDR DXTA200601358Pitot System · contaminatedYAW DAMP, MACH TRIM DISENGAGED TWICE ON TAKEOFF ROLL. PITOT HEAT WAS ON FOR 5 MINUTES PRIOR TO SECOND TAKEOFF ROLL. PERFORMED OPS CHECK OF YAW DAMPNER ON FGC A AND B SIDES, FOUND NO DISCRECPENCIES. DOWNLOAD AFCS FAULTS AND MADC FAULTS AND MAILED TO TEAM X PROSDR CA060419001Pitot Head · obstructedDURING TAKEOFF ROLL, THE CREW OBSERVED A 20 KT DIFFERENTIAL BETWEEN ASIS. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE CLEARED DEBRIS FROM THE CAPT'S PITOT PROBE AND CONDUCTED A SYSTEM LEAK CHECK. THE AIRCRAFT WAS RETURNED TO SERVSDR CA060421016Hose · crackedCREW REPORTED A +- 400FT SPLIT WITH ALTEMETERS. FOUND PITOT/STATIC HOSE CRACKED. NOTE: OUR LEARJET 35 FLEET OF AIRCRAFT WERE RVSM CONVERTED WITH A LEARJET STC, THESE HOSES ARE PART OF THE CONVERSION AND FOUND THIS PROBLEM WITH OTHER LEARJET 35 RVSM CONVERTESDR QXEA200600976Pitot System · contaminatedBZN FLIGHT NR 2350: AUTO PILOT, YAW DAMPER KNOCKED OFF. THEN THE PITCH TRIM, ELEVATOR FEEL, SPOILER OUTBOARD, YUD CONTROL ROLL SPOILER OUTBOARD HYD CAUTION LIGHTS ILLUMINATED. FO'S AIRSPEED STARTED DECREASING. CAPTAIN'S AIR SPEED MATCHED STAND BY. CHECKLISSDR CA060404001Hose · crackedDURING A SCHEDULED INSPECTION, THE AVIONICS TECHNICIAN VISUALLY DISCOVERED SEVERAL HOSES CRACKED IN THE RT PITOT/STATIC CIRCUIT. HOSES WERE FOUND CRACKED AND LEAKING ON THE LT PITOT/STATIC CIRCUIT APPROXIMATELY 1 MONTH AGO. THESE PARTICULAR HOSES WERE INSTALSDR CA060327003Line · contaminatedDURING BIANNUAL ALTIMETER SYSTEM TEST AND INSPECTION PILOTS ALTIMETER AND VSI RESPONDED ERRATICALLY TO INCREASING/DECREASING PRESSURE. WATER DROPLETS WERE FOUND IS PILOTS STATIC SYSTEM BETWEEN NR 1 LEFT STATIC VENT AND Y CONNECTION TO RIGHT VENT.SDR KBM2006F00108Pitot Head · inoperativeUNIT INOPERATIVE, REMOVED AND REPLACED. (K)SDR KBM2006F00114Pitot Tube · inoperativePITOT TUBE, UNIT INOPERATIVE, REMOVED AND REPLACED. (K)SDR CWQR2006003Drain Valve · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE.SDR CWQR2006008Retainer · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAINING RING COMING LOOSE FROM VALVE BASE.SDR CWQR2006007Drain Valve · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE.SDR CWQR2006006Drain Valve · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE.SDR CWQR2006005Drain Valve · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAINING RING COMING LOOSE FROM VALVE BASE.SDR CWQR2006004Drain Valve · looseFOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE.SDR QXEA200600701Pitot Head · erodedYYC C4 , RIGHTHAND PITOT HEAD IS ERRODED. REPAIRED IAW DHC-8-200 TASK 34-11-11-400-801, DHC-8-200 AMM TASK 34-11-00-790-802 AND 30-30-00-710-801.SDR BSY2006F00000Adc · defectiveDURING TAXI OUT, THE OVERSPEED WARNING ACTIVATED AND THE PILOTS ALTIMETER AND ALTITUDE ALERTER FLAGGED. THE CREW ABORTED THE DEPARTURE AND RETURNED TO THE RAMP. THE ADC WAS FOUND TO BE DEFECTIVE AND WAS REPLACED ON 2/27/2006. THE SYSTEM WAS TESTED AND INSPESDR C2XA06IA022Sensor · burnedIAH - FLIGHT 2433, THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE COCKPIT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE THE NUMBER TWO PITOT STATIC CURRENT SENSOR TO BE DISCOLORED. MAINTENANCE REMOVEDSDR COMA0660153Pitot Line · contaminatedFLIGHT 5249 - ABORTED TAKEOFF AT DTW AT 60 KTS DUE TO A COMP MON IAS CAUTION MESSAGE. PURGED WATER FROM THE PITOT SYSTEM P2.SDR C2XA06CL026Sensor · burnedCLE FLIGHT 2269, THE CREW REPORTED A PITOT 3 INOP MESSAGE IN FLIGHT. NOTICED A ELECTRICAL ODOR AFTER THE MESSAGE WAS RECEIVED, DISSIPATED AFTER SEVERAL MINUTES. MAINTENANCE INSPECTED AND REPLACED KOO57 CURRENT SENSOR AND SOCKET. OPERATIONAL CHECKS WERE GOODSDR CA060215001Hose · cracked(CAN) DURING A SCHEDULED PITOT/STATIC CHECK, THE AVIONICS TECHNICIAN DISCOVERED A LEAK ON THE LT PITOT CIRCUIT. AFTER FURTHER TROUBLESHOOTING, THE TECHNICIAN DISCOVERED A HOSE THAT WAS CRACKED (MIL-H-5593-4). THE HOSE WAS REPLACED AND THE SYSTEM WAS SERVICEASDR BSY2006F00001Adc · frozenON FEB 8, 2006 THE PILOTS ALTIMETER FROZE AT 5000 FT AND THE IVSI FROZE AT 3000 FT/MIN CLIMB. THE AIRCRAFT WAS ENROUTE TO FACILITY. UPON TESTING OF THE NR1 SYSTEM, NO DEFECT WAS NOTED. ALL FUNCTIONS OF THE ADC WERE FOUND TO BE OPERATING NORMALLY IAW ICA ANDSDR YENA200605Pitot Head · unknownAIRCRAFT EXPERIENCED LOSS OF ADS SYSTEM NR 3 & NR 4. CMC SHOWED NR 3 & NR 4 (SMART PROBES) PITOT/STATIC AOA SENSOR. REMOVED & REPLACED NR 3 AND NR 4 INTEGRATED PITOT/STATIC AOA SENSOR IAW AMM 34-13-01, OPS CHECK. NO FAULT NOTED.SDR BSY2006F00002Adc · defectiveON FEB 2, 2006, THE PILOTS ALTIMETER, THE ALTITUDE ALERTER, THE PRIMARY TRANSPONDER MODE C ALL FAILED, AND THE OVERSPEED WARNING HORN WAS ACTIVATED CONTINUALLY. THE AZ-252 ADC WAS FOUND TO BE DEFECTIVE AND WAS REPLACED. THE SYSTEM WAS TESTED AND INSPECTED IA
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