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 C2XA08IA128Pitot Line · contaminatedIAH - FLIGHT 2546, DURING FLIGHT IN IMC DESCENDING THROUGH FL320 THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT FOLLOWED BY AN SPS ADVANCED MESSAGE ON EICAS, IAS AND ALT ON BOTH PFD'S, CAPT AIRSPEED DOWN TO 147KTS, AND FO'S TO 157KTS, FOLLOWED BY LOSSSDR C2XA08CL056Sensor · burnedFLIGHT NR 2706 THE CREW REPORTED A ELECTRICAL ODOR IN THE COCKPIT. MAINT INSPECTED AND REPLACED THE NR 1 PITOT CURRENT SENSOR AND SOCKET. OPERATIONAL CHECKS WERE GOOD.SDR WGEA200800053Pitot Tube · defectiveDURING T/O, RECEIVED AIRSPEED DISAGREE AND STICK PUSHER FAIL MESSAGE. CPT AIRSPEED INDICATED 74 KTS ON TAXI IN AND 63 KTS STOPPED ON THE RAMP. RESOLVED ON W/O:1834 TASKCARD: NR-00001. REPLACED LT PITOT/AOA PROBE WITH NEW PROBE IAW AMM 34-10-10. PERFORMED ASDR Q2SA746006Pitot Tube · defectiveON DEPARTURE, CAPTAIN AND FIRST OFFICER'S ALTIMETER SPLIT 500 FEET, AIRSPEED SPLIT 30 KTS. WHEN ALTERNATE STATIC SELECTED ON CAPTAIN'S SIDE, ALL INSTRUMENTS MATCHED UP. DURING ILS FLIGHT, ALTITUDE SHOWED 1800 FEET AT 6.3 DME (SHOULD HAVE BEEN 1600 FEET). RESDR SIMA200808117Pitot Line · contaminatedON FLIGHT 4125, CREW REPORTED DURING APPROACH THAT THEY COULD NOT TELL WHAT ATTITUDE THEY WERE AT. ALL THREE ALTIMETERS SHOWING DIFFERENT READINGS. CREW DECLARED EMERGENCY, FMS MESSAGE UNRELIABLE ALTIMETER DO NOT USE FOR NAV. AFTER LANDING CREW NOTICED THE SDR DXTA20082950Pitot System · contaminatedON TAKEOFF ROLL F/O AIRSPEED MISCOMPAIRED WITH CAPT A/S, TAKEOFF WAS ABORTED. DRAINED OUT EXCESS WATER FROM THE PITOT PROBES AND STATIC PROBES, AND PERFORMED AN AIR DATA SYSTEMS - INSPECTION/ CHECK. SYSTEMS CHECKED NORMAL IAW MM REV. 23, 34-11-10 & 34-11-26.SDR FDKA200803095Pitot Head · inoperativeFDM 6201 FLL (0629 PHX LCL) - DECLARED EMERGENCY CAPTAIN AIRSPEED AND ALTITUDE INDICATION INACCURATE AND SUSPECT PITOT HEAT SYSTEM INOP. MX DRAINED WATER FROM PITOT STATIC SYSTEM AND RESET PITOT HEAT SYSTEM, SYSTEM OPS CHECKED GOOD.SDR CA080303006Static Port · obstructed(CAN) WHILE DOING A PRE-PURCHASE INSP, DISCOVERED A PIECE OF TAPE COVERING THE RT STATIC PORT.SDR 2008FA0000238Bushing · incorrectSTATIC SYSTEM FAILED LEAK CHECK DURING 2 YEAR STATIC SYS IFR CERTIFICATION, LEAKS WERE CAUSED BY REDUCED BUSHING FAILING TO SEAL STATIC LINE SUMP. (ON BOTH SIDES, PILOT AND COPILOT). TO REPAIR THE LEAKAGE, PIPE THREAD TAPE (TEFLON TAPE) WAS USED ON THE REDUCSDR VQMA02132008001Static Port · leakingFOUND RT SIDE LOWER STATIC PORT SLIGHTLY LOOSE. REMOVED BOTH RT SIDE STATIC PORTS, CLEANED AREA ON INSIDE AND OUTSIDE OF AC. APPLIED PRIMER TO AFFECTED AREAS. INSTALLED (2) STATIC PORTS P/N-CM2933-7 ON RT SIDE OF AC WITH (8) CM3827AD-4 RIVETS.SDR Y2LA200800008Static Port · scratchedCAPTAINS STATIC PORT ON RIGHT HAND SIDE HAS SCRATCH IN RVSM CRITICAL AREA. REPAIRED SCRATCH ON CAPTAINS STATIC PORT ON RIGHT HAND SIDE OF AIRCRAFT PER SRM 53-11-11. FOUND SCRATCH TO BE IN LIMITS PER SRM 53-00-11. RVSM NOT AUTHORIZED MAINTENANCE CONTROL NOTISDR C2XA08IA058Relay · inoperativeMCI - FLIGHT 2212, THE CREW REPORTED A PITOT2 INOP MESSAGE APPEARED DURING APPROACH WITH A BURNING SMELL. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY FOR PITOT TWO, OPERATIONALLY CHECKED WITH NOSDR WGEA200800019Probe · malfunctionedCENTER AIRSPEED AND ALTIMETER READS 200 FEET LOW AND 20 KNOTS RESPECTIVELY UP TO CRUISE ALTITUDE OF 2200 FEET. REMOVED AND REPLACED STANDBY PITOT/STATIC PROBE WITH SERVICEABLE PROBE IAW EA500 AMM 34-10-12. PERFORMED STANDBY PITOT/STATIC VERIFICATION TEST. OPSDR A6WA200840048Pitot System · contaminatedON TAKEOFF ROLL STANDBY IAS READS -0- KNOTS, REJECTED TAKEOFF AT ABOUT 85 KNOTS, MAX BTMS = 8,7,6,6. NOTE: NO HES/RTO INSPECTION REQUIRED. FOUND WATER IN THE STANDBY PITOT/STATIC SYSTEM. PERFORMED CONTAMINATION REMOVAL OF THE STANDBY PITOT/ STATIC SYSTEM. SDR 2008FA0000066Fitting · failedPRIOR TO COMPLIANCE WITH FAR 91.411, A STATIC SYSTEM CHECK WAS CONDUCTED. UNDER TEST SYSTEM SHOWED APPROXIMATELY 100 FPM DESCENT RATE. INSPECTION REVEALED THE 90 DEGREE PLASTIC FITTINGS (ONE ON EACH SIDE OF THE FORWARD FUSELAGE) FOR STATIC SYSTEM PLUMBING WERESDR 2008UALA0043Static Line · out of positionFOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL.SDR SIMA200736202Pitot Head · contaminatedON FLIGHT 3378, AFTER TAKEOFF STANDBY ATTITUDE INDICATED (OUT OF ORDER). CAPT DECIDED TO RETURN TO GPT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLUID IN PITOT STATIC PORT DRAINED FLUID FROM PITOT STATIC LINES IAW AMM 34-13-00 AND COMPLETED OPS CHECK IAW AMM 34SDR DXTA200702690Pitot Tube · contaminatedABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON PILOTS SIDE. DRAINED MOISTURE FROM LT PITOT TUBE. PERFORMED PURGE TO PILOTS SYSTEM. TESTED LT PITOT SYSTEM. OPERATIONAL CHECK SATISFACTORY IAW MANUAL 34-11-08.SDR CA071214007Pitot Tube · corroded(CAN) FOLLOWING A FAILED PITOT STATIC TEST, AN INSPECTION OF THE PITOT STATIC TUBING WAS CARRIED OUT AND MAINT FOUND THAT ONE OF THE TUBES (P/N 25-7SF209-9) HAD A PIN HOLE, WHICH APPEARS TO HAVE BEEN CAUSED BY INTERGRANULAR CORROSION. THE LINE WAS REPAIRED ANDSDR YENA2007113Pitot Tube · pluggedFLT 411, BOS-SAN, RETURNED TO BOS DUE ON TAKEOFF F/O AIR SPEED, AUTO THRUST WENT AWAY, ALSO RUDDER TRAVEL LIM ECAM AND LOSS OF AUTOPILOTS. REMOVED AND REPLACED F/O PITOT PROBE IAW MM 34-11-15. OPS CHECK OK. PRECAUTIONARY REMOVED AND REPLACED ADIRU 2 IAW 34-SDR QXEA200701777Pitot Head · damagedSEA - NR 2 AIRSPEED INDICATION FAILED FOR ABOUT 3 MINUTES DURING A SEVERE ICING ENCOUNTER. MAINTENANCE REPLACED THE RT PITOT HEAD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0734063Pitot Head · obstructedNON-ETOPS FLIGHT 275 HNL-LIH. DURING TAKEOFF, THE NR 2 AIRSPEED INDICATOR AND THE NR 2 ALTIMETER FAILED TO OPERATE PROPERLY. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CLEARED DEBRIS FROM THE FIRST OFFICER’S PITOT/STATIC SYSTEM. AS A PRSDR AMTA200700651Relay · malfunctionedAFTER ENGINE START, "CAPT PITOT" WARNING ON EICAS AND OVERHEAD ILLUMINATED. T/S PER FIM 30-31-00 FIG 103. REMOVED AND REPLACED K243 RELAY, RAN ENGINES, OPS CHECK NORMAL. (M)SDR CA071130014Seal · debonded(CAN) STATIC DISCHARGE SEAL DEBONDED WHILE ENGINE (SN 295-291) WAS BEING RUN. OUR INTERNAL SQID REPORT NR 07-06724 REFERS. (TC NR 20071130014)SDR COEA0702819Pitot Head · obstructedFLT 8080 - ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOT NOTICED NR 2 AIRSPEED INDICATOR READ ZERO, FOLLOWED BY (DACD DATA INVALID) ON AFCS CONTROL PANEL. PILOT RETURNED TO RAMP AT OAK. MAINTENANCE FOUND AND REMOVED DEBRIS IN PITOT PROBE, TWO INSECTS. AIRCRAFTSDR ASMF200710006Pitot Head · warning messageAIRCRAFT RETURNED TO PLATFORM, THE RT ELEVATOR PITOT LIGHT TURNED ON. MAINTENANCE PERSONNEL REPLACED THE PITOT PROBE RT ELEVATOR IAW MM 27-31-94 AND TESTED CORRECT IAW MM 27-31-17 AND FIM PROCEDURE 30-31 TASKS 808-809.SDR A6WA200740592Drain · contaminatedABORTED TAKEOFF BELOW 80 KNOTS DUE TO FAILED STANDBY AIRSPEED INDICATOR 0 KNOTS. ALL BRAKE TEMPERATURES INDICATE NORMAL. FOUND WATER IN P3 DRAIN. PERFORMED P3 CONTAMINATION REMOVAL PER AMM 34-11-00. PERFORMED LEAK TEST OF P3 PER AMM 34-11-00-790-803 TEST OSDR 2007UALA04083Static Inverter · smokeFOUND COCKPIT AND CABIN FILLED WITH SMOKE. OBSERVED SMOKE COMING FROM STATIC INVERTER. CB'S DID NOT POP.SDR DHLA200700048Pitot Tube · obstructedON TAKEOFF ACCELERATION AT 80 KTS NO AIRSPEED INDICATION ON F/O AIRSPEED. A/C WT 131.7 AS 90KTS 27 DEGREES C ALT 0 FT COMPLETE RTO FLOW CHART BRAKE ENERGY NORMAL RANGE RWY 18R MCO. FOUND FOREIGN OBJECT IN F/O PITOT TUBE REMOVED OBJECT PERFORMED PITOT STATICSDR IXXA070048OPitot Tube · damagedDURING CLIMB-OUT FROM PHIK, THE CREW NOTICED THE PITOT HEATER INOP LIGHT ILLUMINATED, ZERO AMPS INDICATED ON THE FIRST OFFICER'S PITOT TUBE POSITION. THE CREW RETURNED TO PHIK, MADE 50 DEGREES FLAP EMERGENCY OVERWEIGHT LANDING AND LANDED WITH OUT INCIDENT. MSDR CA070907002Hose · cracked(CAN) DURING PITOT STATIC CHECKS IT WAS FOUND THE SYSTEM WAS SLIGHTLY LEAKING. FURTHER VISUAL INSPECTION FOUND THE STATIC HOSE GOING TO THE ADC WAS WEATHER CRACKED AND LEAKING NEAR THE FITTING. THE HOSE WAS MFG THE FIRST QUARTER OF 2001.(1Q01).(25W752005-063H)SDR DL75E071170Probe · inoperativeAFTER ENGINE START F/O PITOT EICAS MESSAGE WILL NOT EXTINGUISH. F/O PITOT PROBE REPLACED PER M/M.SDR WGEA200700003Probe · obstructedON INITIAL LEVEL OFF AT 4000 FT ACCELERATING TO 220 KEAS HAD AIRSPEED DISAGREE, YAW DAMP FAIL AND AUTO PILOT FAIL CAS MESSAGE. AUTO PILOT DISENGAGE, AIRSPEED 224 LEFT 216 RIGHT. SUP CLEANED PILOTS AND COPILOTS PITOT PROBES. PERFORMED PITOT/STATIC VERIFICATISDR M000999Static Port · leakingSPLIT IN ALTIMETERS (RT ALTIMETER INDICATES 400 FOOT HIGHER THAN LT ALTIMETER AT 41,000 FT MSL) VERIFIED SPLITS IN ALTIMETERS AND PILOTS PITOT/STATIC SYS. INSTALLED NEW CO-PILOTS STATIC PORT FITTING P/N CM2933-7. LEAK CHECK, SAND, FILLED, PRIMED, PAINTED AND SDR 07FDEA02876Pitot Head · obstructedREJECTED TAKEOFF AT APPROX 90 KNOTS DUE TO NO F/O A/S. FOUND BUG DEBRIS IN F/O PITOT PROBE CLEANED. INSPECTED PROBE PER AMM 34-11-15-6, NO DEFECTS NOTED. F/O'S AIRSPEED CHECKED GOOD WITH PITOT TESTER. INSPECTED A/C BRAKES PER AMM 05-51-16-0. NO DEFECTS NOSDR FJ7A116867Pitot Head · unknownINDICATION OF NO PITOT HEAT ON ANNUNCIATOR PANEL.SDR DHLA200700040Pitot Tube · malfunctionedNO AIRSPEED INDICATION ON STANDBY AIRSPEED INDICATION AT 80 KTS ON CAPT AND FO'S INDICATORS. REJECTED T/O TO WEIGHT 231.2 OAT 26 DEGS C PA 103FT BRAKE TEMP 200 DEGS C 1. REMOVED AND REPLACED STANDBY AIRSPEED PITOT PROBE AS PER A300 MM 34-11-15. PERFORMED LESDR DHLA200700039Pitot Line · obstructedNO AIRSPEED INDICATION ON STANDBY A/S IND AT 80KTS ONCA AND FO IND REJECTED T/O WEIGHT 273.6 26C OAT P.A 73FT BRAKE TEMP230 1. FLUSHED PITOT STATIC SYSTEM AS PER 34-11-10. OPS NORM AS PER MM 34-11-22 A/C RVSM COMPLIANT.SDR DHLA200700042Indicator · inoperativeREJECTED T/O NO CAPT A/S EITHER DIGITAL OR ANALOG. REJECTED AT 80 KTS, 273000 GTOW TEMP 25 DEGS C, NORMAL BREAK ENERGY. FLUSHED NR 1 PITOT SYSTEM AS PER MM 34-11-10. DEBRIS CLEARED FROM LINES. PERFORMED PITOT/STATIC LEAK TEST NO LEAKS NOTED SYSTEM CHECKS NSDR MASA20700487Pitot System · contaminatedASH 2920 FAT-PHX - REJECTED TAKE OFF DUE TO STALL FAIL CAUTION MESSAGE. MX FOUND WATER IN THE STAND BY PITOT SYSTEM AND DRAINED. NO FURTHER FAULTS NOTED.SDR 2007FA0000836Static System · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS SYSTEM WAS NOT CROSS COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TO MEET STC NR ST SDR 2007FA0000703Static Line · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS STATIC SYSTEM INSTALLATION WAS NOT CROSS-COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TSDR CA070813002Pitot Tube · blocked(CAN) THE AIRCRAFT BEGAN TO DEPART ON THE TAKE-OFF ROLL WHEN THE FLIGHT CREW OBSERVED THAT THE CAPTAINS AIRSPEED INDICATION HAD FAILED. THE TAKE-OFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE CAPTAINS SDR RAIA00707022Sensor · malfunctionedFLT NR 5529 - STL - PITOT 2 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED PITOT NR 2 SENSOR. OPS AND LEAK CHECK GOOD.SDR HALA0700262Pitot System · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB: FO'S PITOT HEAT EICAS MESSAGE AFTER ENGINE START. T/S PER FIM 30-31-01-05 IDENTIFIED F/OS PITOT STATIC PROB B28 INOP. REMOVED AND REPLACED PER AMM 34-11-01. PERFORMED PITOT STATIC PROBE TEST PER AMM TASK 34-11-01-725-001. LKSDR DXTA200702235Pitot Tube · contaminatedON TAKEOFF AT 40-50 KNOTS FG B FAIL CAME ON WITH AMBER (YAW DAMP FAIL) AND MACH TRIM OFF). FOUND EXCESSIVE WATER IN THE COPILOTS PITOT TUBE. PURGED SYSTEM AND PERFORMED OPERATIONAL CHECK AND LEAK CHECK IAW CHP 34-11-08 OF MM. SYSTEM OPERATIONAL CHECK AND LESDR CA070531003Pitot System · obstructed(CAN) THE AIRCRAFT BEGAN THE TAKEOFF ROLL WHEN THE FLIGHT CREW NOTICED A LAG IN THE FIRST OFFICERS AIR SPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE FIRST OFFICERS PITOT INSTSDR VQMA051807001Static Port · leakingDURING AVIONICS MAINTENANCE FOUND PILOT'S STATIC PORT LEAKING.SDR 2007FA0000465Pitot Line · looseWHILE TROUBLESHOOTING A LEAK IN NR 2 STATIC SYSTEM, THE RT SIDE STATIC PLATE HAD TO BE TAKEN LOOSE. UPON REMOVAL OF THE PLATE, SILICONE RTV WAS FOUND ON THE FITTING FOR THE NR 1 STATIC SYSTE. WHEN THE FITTING WAS LOOSENED, FOUND A LAGRE AOUNT OF TEFLON PIPE SDR RAIA00705010Drain · contaminatedFLT NR 7902 - IAD - F/O'S ALTITUDE INFORMATION (ALTIMETER & ALT SELECT) WENT MISSING ON T/O ROLL. MAINTENANCE DRAIN WATER OUT OF F/O PITOT DRAIN. RESET BOTH ADCS. OPS CHECK NORMAL
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