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.

SDR 99ZZZX787Line · chafedNR 2 AIR DATA P2 LINE HAS BEEN SLIGHTLY CHAFED BY THE ELEVATOR CONTROL CABLE. IT APPEARS THE ELEVATOR CONTROL CABLE TURNBUCKLE SLAPS PITOT LINE FROM TIME TO TIME. LINE IS NOT DAMAGED TO WARRANT REPLACEMENT. LINE NEEDS TO BE MOVED TO INCREASE CLEARANCE. THIJan 13, 1999 · N800VC · Braero BAE125800ASDR 99ZZZX994Line · misinstalledACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTUE REVEALED WITH FULL AFT ELEVATOR, THE YOKE HIT THE ALTERNATE STATIC SOURCE VALVE T-FITTING RESTRICTING ELEVATOR TRAVEL. RE-ROUTED ALTERNATE STATIC SOURCE LINES AND T-FITTING.Jan 8, 1999 · N494SP · Cessna 172SSDR ARWA981203Pitot Syst · contaminatedDURING CLIMB-OUT, CAPT'S AIRSPEED INDICATOR READS 200 KTS AND F/O'S AIRSPEED INDICATOR READ 33O KTS. ACCOMPLISHED PITOT/STATIC LEAR TEST IAW MM 34-12-00. ALL PARAMETERS WITHIN LIMITS. PURGED SYSTEM PRECAUTIONARY MEASURE IAW 34-12-00 NR 1,2, ADC PITOT STACTIDec 8, 1998 · N8968U · Doug DC862SDR 99ZZZX788Line · chafedDURING 24-MONTH PITOT/STATIC CERTIFICATION INSPECTION, FOUND NR 2 ADC P2 PITOT LINE CHAFED THROUGH BY AUTOPILOT SERVO CABLE. THIS AREA IS DIFFICULT TO SEE WITH INSTALLED COMPONENTS IN PLACE. NOTE: THIS IS SECOND AIRCRAFT AT THIS FACILITY FOUND WITH THIS PRODec 7, 1998 · N805X · Braero BAE125800ASDR 99ZZZX234Line · blockedFAILURE OF PITOT STATIC SYSTEM. BLOCKAGE OF RESTRICTOR FITTING. COMPLETE FAILURE OF STATIC SYSTEM AND LOSS OF MODE C ALT REPORTING.Nov 24, 1998 · N862M · Bell 206BSDR CA981125071Cap · missing(CAN) AIRCRAFT RETURNED TO BASE AFTER LOW AIR SPEED INDICATION. THE CAP ON PITOT STATIC DRAIN WAS FOUND MISSING. NEW CAP INSTALLED AND PITOT STATIC TESTS CARRIED OUT, SERVICEABLE.Nov 10, 1998 · Beech 99SDR SWAA982775O-Ring · failedAIR TURNBACK DUE TO ALTIM AND AIRSPEED CAPTAIN SIDE ERRONEOUS AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED O-RING ON NR 1 AIR DATA PITOT LINE. OPS AND LEAK CK GOOD AS PER BOEING SRM.Nov 8, 1998 · N602SW · Boeing 7373H4SDR AU981436Line · leaking(AUS) PITOT SYSTEM LEAKING FROM SPEED COMM AND AIR SPEED TRANSDUCER.Oct 20, 1998 · Fokker F28MK4000SDR 99ZZZX422Line · cloggedABNORMAL READING ON COPILOT'S ALTIMETER (DIFFERENCE = 1 THOUSAND FEET). AFTER LANDING, STALL SYSTEM WAS CHECKED AND FOUND ALL 20 STATIC LINES IN AIRCRAFT EITHER PARTIALLY PLUGGED OR, IN THIS CASE, ONE LINE ALMOST COMPLETELY PLUGGED. FOUND APPROXIMATELY 50 BOOct 15, 1998 · N125BH · Hwksly DH1251ASDR K3HA980121Static Line · inoperativeCAPTAINS ALTIMETER AND AIRSPEED INDICATION IS IN ERROR. BOTH READ LOW AND ERROR DIFFERENTIAL INCREASES WITH AIRCRAFT ALTITUDE. PERFORMED STATIC CHECK. LEAK INTERMITTANT ON CAPTAINS SIDE. CHECKED ALL LINES, CARGO AND LOWER-43. REMOVED AND REPLACED STATIC LOct 11, 1998 · N8883Z · Boeing 727225SDR CZMA061349Fitting · defectiveDURING ANNUAL INSPECTION, NUT SECURING COVER TO THE THIRD STATIC PORT ON COPILOT'S SIDE WAS REMOVED TAKING THE THREADS OF THE STATIC PORT WITH IT. THE NUT IS A STAINLESS STEEL ELASTIC STOP NUT INSTALLED ON A SOFT ALUMINUM STATIC PORT. THIS MATERIAL COMBINATIOOct 8, 1998 · N911BE · Bell 412SDR 99ZZZX124Drain · corrodedNR 1 PITOT SYSTEM DRAIN VALVE RESERVOIR P/N 25-7SF235 HAS HOLE CORRODED THROUGH THE SIDE OF THE RESERVOIR BODY ASSEMBLY. RESERVOIR BODY HAS PLIER MARKS FROM PREVIOUS REMOVAL/INSTALLATIONS.Oct 2, 1998 · N621MT · Braero BAE125800ASDR 98UAL900472Pitot Probe · malfunctionedALTIMETER IS READING INCORRECTLY. *S/D* MAINTENANCE REPLACED PITOT/STATIC PROBE AND NR 1 AIR DATA COMPUTER. THE REMOVED AIR DATA COMPUTER TESTED NORMAL IN THE SHOP.Sep 26, 1998 · N982UA · Boeing 737291SDR VNAA9809013Pitot Head · bird strikeJUST AFTER TAKEOFF DURING THE CLIMB, A BIRD STRUCK THE NUMBER TWO PITOT HEAD. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO PITOT HEAD, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL Sep 16, 1998 · N426JS · Dorner DO328100SDR AU981307Hose · separated(AUS) ALTIMETER STATIC HOSE DISLODGED AND CRACKED. STATIC HOSE BETWEEN THE ALTIMETER AND AIRSPEED INDICATOR SEPARATED AT A UNION LOCATED BEHIND THE DIRECTIONAL GYRO CASE.Sep 10, 1998 · Cessna 340ASDR JBXA980048Pitot · contaminatedNO AIRSPEED ON TAKEOFF, TAKEOFF ABORTED AT 80 KNOTS. FOUND BUG STUCK ON PITOT HEAT NR 1 SYSTEM. CLEANED PITOT HEAD CAPTAIN'S SIDE. OPERATION CHECK AIRSPEED INDICATION CAPTAIN'S SIDE GOOD IAW 24-11-00. (X)Aug 30, 1998 · N573ML · Cndair CL6002B19SDR COMA9810188Pitot Tube · looseA 40 KT DIFFERENCE BETWEEN PILOT AND CO-PILOT AIRSPEED INDICATION. TIGHTENED LOOSE CONNECTION AT FRAME 8 IN PILOTS PITOT SYSTEM. LEAK CHECK SATISFACTORY.Aug 30, 1998 · N259CA · Emb EMB120RTSDR 98ZZZX3330Pitot Drain · chafedA FLIGHT CONTROL CABLE RUBBED A HOLE IN A PITOT DRAIN LINE (P/N 257SF20735A) THAT CONNECTS TO A PITOT DRAIN VALVE. THIS LINE IS LOCATED UNDER THE COPILOT SEAT AREA. ATTENTION SHOULD BE GIVEN TO THIS AREA DURING INSPECTION TO ENSURE CABLE CLEARANCES.Aug 18, 1998 · N330X · Braero BAE125800ASDR CA980908026Static Valve · leaking(CAN) ON 24 MONTH INSPECTION, FOUND CAPTAIN'S ALT STATIC SOURCE VALVE LEAKING, REPLACED.Aug 12, 1998 · Boeing 727260SDR CA980814008Line · leaking(CAN) AFTER FUSELAGE STRINGER REPAIR, A LEAK CHECK OF THE PITOT STATIC SYSTEM WAS CARRIED OUT AND WAS FOUND TO HAVE AN EXCESSIVE LEAK RATE. A FURTHER CHECK REVEALED THAT THE CAUSE WAS DUE TO PIN HOLES IN EACH AFT STATIC LINE. THE PIN HOLES WERE ATTRIBUTED TOAug 6, 1998 · Beech A100SDR CA980916039Tube · melted(CAN) AIRSPEED INDICATOR READING 30-40 KNOTS LOW IN CRUISE. TUBING FROM PITOT HEAD TO 'T' FITTING HAD A HOLE MELTED THROUGH FROM PROXIMITY TO LANDING LIGHT.Jul 30, 1998 · Bell 206BSDR AU980943Manifold · corroded(AUS) GYRO PRESSURE MANIFOLD CORRODED. MANIFOLD IS CONSTRUCTED FROM CADMIUM PLATED STEEL. STEEL ELBOW ALSO CORRODED.Jul 26, 1998 · Reims F406SDR ARWA9807126B-Nut · loose30 KNOT SPLIT ON AIRSPEED AND 1000 SPLIT ON ALTIMETERS CLIMBING THROUGH FL 310, SPLITS ON BOTH WERE INCREASING, BOTH HIGH ON F/O SIDE. SECURED LOOSE B NUT IN CEILING OF AIRCRAFT BELLY. ACCOMPLISHED PITOT-STATIC CHECK. OPS AND LEAK CHECK ED NORMAL IAW MM 34-Jul 17, 1998 · N802BN · Doug DC862SDR USAASB98178Static Line · leakingCLT - FLT 549 - ON CLIMB-OUT FROM CLT, THE CAPTAINS ALTIMETER AND AIRSPEED INDICATOR BECAME INOP. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESEATED/RERACKED THE NR 1 AIR DATA COMPUTER (P/N 4061100-9Jul 11, 1998 · N436US · Boeing 7374B7SDR 98ZZZX3232Pressure Switch · leakingDURING UNSCHEDULED TEST OF PILOT'S PITOT/STATIC SYSTEM, DETERMINED A SUBSTANTIAL LEAK EXISTED. THE LEAK WAS TRACED TO THE HORIZONTAL STABILIZER DE-ICE SYSTEM DIFFERENTIAL PRESSURE SWITCH (REF: DESIGNATION S39B). THE UNIT IS LEAKING FROM PITOT TO STATIC SIDEJul 9, 1998 · N85CR · Beech 400ASDR CA980521008Tubing · melted(CAN) AIR SPEED INDICATOR SHOWING ONLY 20 KNOTS AT CRUISE. PITOT HEAD TUBING HAD BEEN INSTALLED TOO CLOSE TO LANDING LIGHT AND MELTED CAUSING LEAK.May 12, 1998 · Bell 206BSDR COMA9860098Pitot · contaminatedTAKEOFF ABORTED, DUE TO AIRSPEED COMPARATOR WARNING MESSAGE. DRAINED WATER FROM PITOT STATIC SYSTEM.May 10, 1998 · N940CA · Cndair CL6002B19SDR VTZA98187Pitot Line · contaminatedFLT 6281 - IAD-HPN - DURING CRUISE, AIRCRAFT DIVERTED TO EWR DUE TO NR 1 ALTIMETER FAILURE. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEARED PITOT STATIC LINES OF MOISTURE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNMay 9, 1998 · N477UE · Bag JETSTM3201SDR 98ZZZX2246Drain · deterioratedFOUND PITOT LEAK ON COPILOT SIDE AND STATIC SYSTEM OPEN. TROUBLESHOOTING FOUND PITOT AND STATIC DRAINS WERE SOURCE OF LEAKS DUE TO DETERIORATION OF DRAIN CORES.Apr 29, 1998 · N700BW · Braero HS125700ASDR 98FDEA00301Pitot Tube · malfunction98-0108 - WRI 34-14-02232: CAPTAINS PFD AIRSPEED INDICATOR DOES NOT OPERATE. NO INDICATION ON T/O ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED CAPTAINS PITOT TUBE, PITOT LEAK CHECK OK. NR 3 EFIS CONTROL SYS OK. CLEARED MEL 34-7.Apr 28, 1998 · N667FE · Airbus A300F4605RSDR 98FDEA00296Static Line · dirtyABORTED TAKEOFF FOR LOSS OF AIRSPEED INDICATION ON THE CAPTAINS SIDE. ABORTED AT 120 KNOTS. CHECKED NUMBER 1 ADC, BLEW OUT STATIC LINE WITH NITROGEN, PITOT/STATIC CK OK.Apr 25, 1998 · N667FE · Airbus A300F4605RSDR UPS98226495Pitot · contaminatedLOST CAPTAINS AIRSPEED INDICATOR ON TAKEOFF ROLL CONTINUED TAKEOFF NOTICED STBY AIRSPEED INDICATOR INOP AT 10,000 FT, WINDSHEAR/GRD PRX CAME ON THROUGH 500 FT. AFTER TAKEOFF LOST EPR 3, 2, 1 ABOUT 10 SECONDS APART THROUGH 12,000. FOUND NUMEROUS WORMS AND WATApr 24, 1998 · N909UP · Boeing 72727CSDR RRXA98079Static Hose · collapsedCAPT'S ALTIMETER IS STUCK AT 500 FEET. FOUND STATIC HOSE ASSY FROM CAPTS STATIC SOURCE SELECTOR TO MANIFOLD MOUNTED ON BACK OF INSTRUMENT PANEL TO BE PARTIALLY COLLAPSED. REMOVED AND REPLACED LINE SYSTEM CK NORMAL. PITOT STATIC LEAK CHECK PERFORMED.Apr 21, 1998 · N991CF · Doug DC8F54SDR P2EA98078Pitot Tube · failedFLT 264 - MCI - ON TAKEOFF POWER APPLICATION, CAPTAINS ALTIMETER DROPPED 20 FT TO 980. AN OFF FLAG CME ON. A CROSS CHECK OF THE F/O'S ALTIMETER SHOWED THE SAME. REPLACED UPPER RT PITOT PROBE PER MM 34-11-11, LEAK CHECKS OF CAPTAINS AND F/O'S SYSTEMS NORMAL Apr 17, 1998 · N208AU · Boeing 737222SDR ORJA9873Pitot Tube · malfunctionedRETURN TO GATE DUE TO PITOT/STALL HEAT OFF. NO POWER TO RUDDER LIMIT IN FLT OR GROUND POSITION THROUGH GROUND CONTROL RELY C/B'S. REMOVED AND REPLACED PITOT STATIC TUBE PER MM 34-11-02. LEAK AND HEAT CHECK GOOD. (M)Apr 14, 1998 · N871RA · Doug DC983SDR 98ZZZX1930Pitot Mast · obstructedAT EIGHTY KNOTS, THE NR 1 ADC (AIR DATA COMPUTER) FAILED AND THE FLIGHT CREW ABORTED TAKEOFF. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE CONFIRMED THE NR 1 PITOT TUBE WAS OBSTRUCTED. REPLACED THE PITOT TUBE MAST.Apr 1, 1998 · N5112 · Cessna 750SDR AU980317Hose · deteriorated(AUS) PITOT/STATIC SYSTEM HOSE DETERIORATED. SILICON HOSE APPEARS TO BE BREAKING DOWN AND EXUDING AN OILY FILM WHICH IS PARTIALLY BLOCKING THE STATIC AIR DISTRIBUTOR MANIFOLD.Mar 27, 1998 · Parten P68BSDR CA980325013Pitot Head · failed(CAN) AIRCRAFT RETURNED TO BLOCKS DUE LT ELEVATOR PITOT PROBE HEAT INOP, REPLACED.Mar 24, 1998 · Boeing 737275SDR COMA9860065Pitot · contaminatedAIRSPEED COMPARATOR WARNING DURING TAKEOFF. PURGED WATER FROM THE PITOT SYSTEM.Mar 21, 1998 · N984CA · Cndair CL6002B19SDR REXA98077Pitot · water contamAIRSPEED INDICATORS ARE OFF BY 60 KNOTS. DRAINED PITOT WATER TRAPS. (M)Mar 19, 1998 · N317PX · Bag JETSTM3101SDR Y2PA98014Static Line · damagedCAPTAINS ALTIMETER SEVERALLY LAGS BEHIND CO-PILOTS. AFTER TOUCH DOWN ALTIMETER READ 1400 FEET THEN SLOWLY RETURNED TO 780 FEET. NO EMERGENCY PROCEDURES WERE NECESSARY AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AT YIP. MAINTENANCE DISCOVERED THAT THE CAMar 18, 1998 · N817AA · Amd FALCONDSDR CA980318052Line · chafed(CAN) LINE, PNEUMATIC RELAY TO TEE TO PILOTS DG AND ATTITUDE GYRO CHAFED BY LOCKWIRING ON HOUSING CONTROL SHAFT BEARING. EACH TIME THE CONTROL YOKE IS PULLED BACK THE HOSE CHAFES ON THE LOCKWIRE. REROUTED AND REPLACED.Mar 10, 1998 · Piper PA31SDR SWIA971110Pitot Syst · noiseIMMEDIATELY AFTER TAKEOFF FROM SLC, LEFT AND RIGHT IAS MESSAGES APPEARED FOLLOWED BY STALL FAIL, MACH TRIM ALSO HIGH PITCH NOISE FOLLOWED BY VERY UNRELIABLE AIRSPEED INDICATION FROM CO-PILOTS AIRSPEED INDICATOR. AS AIRCRAFT SLOWED DOWN, LOUD NOISE WENT AWAY. Mar 9, 1998 · N405SW · Cndair CL6002B19SDR 98ZZZX1289Static Drain · corrodedSTATIC DRAIN LEAK AT 24 MONTH CERTIFICATION. COULD NOT REMOVE DRAIN RESERVOIR BODY TO CHANGE O-RING P/N 100-011-8810. REMOVED STATIC DRAIN PLATE AND FOUND CORROSION ON PLATE BETWEEN PLATE AND AIRCRAFT SKIN.Mar 9, 1998 · N84FA · Braero BAE125800ASDR TWAA9803204Pitot Line · brokenSTL - FLT 141 - ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON STEADY. RETURNED TO STL. REPLACED BROKEN PITOT LINE GOING TO ELEVATOR FEEL LOCATED IN BAY FIVE OF VERTICAL STABILIZER. (M)Mar 5, 1998 · N54333 · Boeing 727231SDR AU980237Probe · fod(AUS) PITOT PROBE BLOCKED BY WASP NEST.Mar 2, 1998 · Bac 146300ASDR 99ZZZX800Heat · inoperativePILOT'S LEFT HAND STATIC HEATER FAILED, NO ANNUNCIATION WAS OBSERVED. REPLACED DEFECTIVE STATIC PART. AFTER SEVERAL HOURS OF TROUBLESHOOTING AND SEVERAL PHONE CALLS TO CESSNA TO FIND OUT WHY THERE WAS NO FAIL ANNUNCIATION, IT WAS DETERMINED THE SYSTEM WAS OPFeb 23, 1998 · N591M · Cessna 560CESSNASDR COMA9860047Line · looseTHE CAPTINS AIRSPEED INDICATOR DID NOT RESPOND DURING TAKEOFF, INDICATION STUCK AT 40 KNOTS. INSPECTED AND FOUND NR 1 PITOT LINE LOOSE AT NR 1 ADC. RECONNECTED NR 1 PITOT LINE AND PERFORMED PITOT/STATIC CHECK.Feb 21, 1998 · N915CA · Cndair CL6002B19SDR REXA98050Pitot Tube · dirtyCAPTAINS AIRSPEED INDICATOR READ 40 KNOTS ON TAKEOFF. CAPTAIN CLEARED LEFT PITOT TUBE AND STATIC PORT. (M)Feb 11, 1998 · N326PX · Saab SF340ASDR 98ZZZX789Vent Drain · blockedNR 2 PITOT STATIC VENT DRAINS PLUGGED WITH SILICONE. CLEANED DRAINS, INSTALLED NEW SEALS, AND CERTIFIED NR 2 PITOT-STATIC SYSTEM. AIRCRAFT TSN: 6,492.4 HOURS. AIRCRAFT LANDINGS: 5,782.Feb 10, 1998 · N32HM · Lear 35A
Back to JASC 3411