JASC 3411
Service difficulty reports · 1,587
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 CA130422003Pitot Tube · failed(CAN) REJECTED TAKE OFF AT APPROXIMATELY 100 KTS DUE TO AUTO THROTTLE ANNUNCIATION (RED), FUEL INDICATION NOT NORMAL AND SPEED DIFFERENCE. DUTY PILOT/FLIGHT SAFETY ADVISED. INTEGRATED PITOT/STATIC/AOA SENSOR NR 3 REPLACED IAW AMM 34-13-01, PB 401. CRITICAL SSDR UALA2013042202752Pitot Tube · failedIN FLIGHT, EICAS MESSAGE DISPLAYED FOR PITOT. PITOT PROBE HEAT LIGHT ILLUMINATED. PERFORMED FIM TASK AS 30-31-00, FOUND F/O PITOT AT FAULT. REMOVED AND REPLACED PITOT PROBE AS PER MM. OPS CHECKED GOOD, ALL INDICATIONS GOOD.SDR HALA2013041700043Pitot System · malfunctionedSECOND ATO & BTB RTO AT 60 KTS IAS. R & R ADM1 MM 34-11 SYS TEST OK IAW MM 34-13 MCO/PLAC/LIDS REMOVED. PERFORMED A FLUSH OF THE PRESSURE LINES IAW MM 34-11. PERFORMED A LOW RANGE LEAK CHECK OF THE TOTAL PRESSURE LINES CAPT AND F/O IAW AMM 34-11. NO LEAKSDR HALA2013041700042Pitot System · malfunctionedSECOND ATO & BTB RTO AT 60 KTS IAS. R & R ADM1 IAW MM 34-11 SYS TEST OK IAW MM 34-13. PERFORMED A FLUSH OF THE PRESSURE LINES IAW MM 34-11. PERFORMED A LOW RANGE LEAK CHECK OF THE TOTAL PRESSURE LINES CAPT AND F/O IAW AMM 34-11. NO LEAKS FOUND.SDR SIMA20130410003Pitot System · contaminatedON FLIGHT 2907 THE CREW REPORTED THAT IN CRUISE FLIGHT IMC AIRSPEED INDICATOR A PERT CAME ON AND CA AIRSPEED INDICATOR SHOWED A SLOW DECREASE IN AIRSPEED. F/O AND STANDBY AIRSPEED SHOWED SAME INDICATION STARTED A DESCENT AND F/O AIRSPEED STARTED TO SHOW A DECSDR UALA2013040802307Probe · faultyF/O ALTIMETER 120 FT LOWER THAN CAPT ALTIMETER AT FL300. PRESSURIZED PITOT STATIC SYSTEM IAW AMM. FOUND CAPT PITOT UPPER PROBE AT FAULT. REMOVED AND REPLACED IAW AMM, ALL OPS GOOD. NO LEAKS OR FAULTS NOTED.SDR UALA2013032601905Pitot Tube · failedCREW REPORTS R AUX PIPOT EICAS ON TAXI OUT AFTER ENG START. REPLACED R AUX PITOT TUBE L. LEAKED AND OP CHECKED REF AMM. CHECKED OKAY.SDR SIMA20130322009Pitot Tube · inoperativeON FLIGHT 3639 THE CREW REPORTED THEY RECEIVED A R PITOT CAUTION MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCEDURES AND DESCENDED OUT OF RSVM AIRSPACE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROSDR FDEA201303200618Pitot Line · blockedRTO DUE TO IAS ALERT AT 90 KTS ON CAPTAIN`S SIDE. REPLACED CAPTAINS PITOT TUBE, FOUND BLOCKAGE.SDR CA130320007Pitot Head · frozen(CAN) DURING DESCENT, THE CREW INDICATED THEY SLOWLY BEGAN LOOSING ACCURACY OF THE PRIMARY AIR DATA INDICATION STARTING WITH AIRSPEED. THE CAPTAIN`S PFD WAS REPORTED TO BE, ALL RED WITH NO INFORMATION SHOWN. THE F/O SIDE ALSO EXPERIENCED A SIMILAR PROBLEM. SDR A6WA201302114012Pitot Line · contaminatedRECEIVED EFIS COMP FOR IAS (INTERMITANTLY) AT FL330, C/W QRH CORRECT AIR SPEED INDICATION WAS HARD TO DETERMINE, BOTH SIDES READ CORRECT AT DIFFERENT TIMES. CHOSE ADC 2 AND AP DIDN'T MAINTAIN ALTITUDE, CHOSE ADFC 1 AP WORKED BUT AIRSPEED (SLOWLY). PURGED (BOSDR CA130129007Pitot Line · melted(CAN) CREW REPORTED TO MAINTENANCE THAT THE CAPTAINS AIRSPEED INDICATOR WAS READING UP TO 40 KNOTS LOWER THAN CO-PILOTS AIRSPEED IN FLIGHT. PITOT STATIC LEAK CHECK AND VISUAL INSPECTION OF AIRCRAFT REVEALED BOTH CAPTS PITOT AND STATIC PLASTIC LINES MELTED FROSDR 2013FA0000152Drain · leakingWHILE PERFORMING DOCUMENT 45, TASK 34-90-10-210, FOUND STANDBY STATIC SYS LEAKING AT A RATE OF 211 FT/MIN. INSPECTED SURROUNDING CONNECTIONS WITH NO NOTICEABLE DEFECTS NOTED. CONNECTED ADC TESTER AND CONFIRMED LEAK RATE OF 200-250 FT/MIN. FOUND ELBOW FITTSDR J7SA201301001Pitot Head · failedERRATIC AIR DATA INFORMATION ON BOTH SIDES AFTER ENTERING ICING CONDITIONS. AN IFE WAS DECLARED. AIRSPEED, VERICAL SPEED AND ALTITUDE DATA READOUTS ON BOTH LT AND RT SIDES STARTED TO FLUCUATE ERRATICALLY IN FLIGHT. AIRCRAFT DIVERTED. LANDING AND TAXI UNEVENTSDR QXEA2013011200032Pitot Head · obstructedDURING TAKEOFF WARNING HORN ACTIVATED. AIRSPEED WAS APPROX 30K, AND HORN ACTIVATED WHEN POWER LEVERS HIT THE 60 PERCENT SWITCH. WARNING TEST WAS OK DURING TAXI- CHECKED THREE TIMES, TAKE OFF ABORTED. RETURNED TO GATE. COMPLIED WITH FUNCTION TEST OF TAKEOFF WSDR CA121213005Pitot Head · leaking(CAN) RECERTIFICATION OF PITOT AND STATIC SYS, AN ABNORMAL LEAK WAS FOUND, ON CLOSE INSPECTION THE ALUMINUM LINE BETWEEN PITOT TUBE AND DRAIN COCK FOR THE PITOT SYSTEM WAS FOUND TO HAVE A PIN HOLE DUE TO BUILD UP OF FIRE RETARDANT THAT CAUSED CORROSION TO SETSDR CA121213010Valve · misinstalled(CAN) THERE IS A POSSIBILITY THAT THE STATIC SWITCH VALVE AND STATIC VALVE HANDLE HAVE BEEN INSTALLED INCORRECTLY ON SOME ACFT. IF INSTALLED INCORRECTLY, THE VALVE WOULD OPERATE AS FOLLOWS: THE VALVE HANDLE WOULD INDICATE NORMAL SOURCE WHEN THE VALVE IS IN THESDR CA121126011Pitot System · malfunctioned(CAN) ON TAKEOFF AT 70 KNOTS, CREW OBSERVED AN IAS INDICATED AIRSPEED DISAGREE MESSAGE ON BOTH PRIMARY FLIGHT DISPLAYS. TAKEOFF WAS ABANDONED. MAINTENANCE PERFORMED FIM 31-62, TASK 876. FOUND RT, F/O PITOT SYS SLOW TO RESPOND AND LAGGING BY 4-6 KNOTS AT ALLSDR HALA2012112100228Pitot Head · failedAFTER ENGINE START CAPTAIN`S PITOT HEAT EICAS MESSAGE. FOUND CAPTAIN'S PITOT TUBE OPEN, REPLACED PITOT STATIC PROBE IAW 34-11-01 NOW TESTS NORMAL ALL TAPE AND TEST EQUIPMENT VERIFIED REMOVED.SDR CA121123001Drain · cracked(CAN) ACFT HAD A ROUTINE FLIGHT THE MORNING BUT RETURNED AFTER TAKEOFF SINCE THEY HAD FALSE INDICATIONS AND SEVERAL MESSAGES POSTED ON EICAS. ONCE THEY LANDED, THE MESSAGES CLEARED. THE TECH INVESTIGATING FOUND A COUPLE OF PITOT VISUAL DRAINS FULL OF WATER ASDR SWIA201232060Probe · failedEFIS ALTITUDE DISCREPANCY OF 200-250 FEET. (FLT 5887) REPLACED RIGHT PITOT/STATIC PROBE. P/N: 0856KV10 S/N OFF: 243159SDR SIMA20121015003Pitot Line · crackedON FLIGHT 3261 THE CREW REPORTED THAT DURING CRUISE AT FLIGHT LEVEL 370 IN VISABLE MOISTURE AT 200 KNOTS AND ENTERING A HOLD, THE FIRST OFFICER’S INDICATOR BECAME UNRELIABLE AND THEN DECREASED TO ZERO SHORTLY AFTER THE F/O'S ALTIMETER BECAME UNRELIABLE AND DIFSDR UALA2012101105790Probe · faultyA-C RETURNED TO BLOCKS FOR :L AUX PITOT EICAS MSG AND ANNUNCIATOR LT FOR SAME. VERIFIED CB NOT POPPED AND L AUX PITOT DOES NOT OPERATE WHEN TEST SW ACTUATED. REPLACED LEFT AUX PITOT PROBE, OP CHECKS NORMAL, LEAK CHECKS WITHIN LIMITS PER MM.SDR FDEA201210023530Pitot Tube · obstructedON TAKEOFF AT 80KTS - F/O'S PFD SHOWED "0" AIRSPEED, CAPTAIN'S PFD AND BOTH STBY AIRSPEED INDICATORS SHOWED 80KTS. FOUND F/O'S PITOT TUBE PARTIALLY BLOCKED. CLEANED BLOCKAGE, REF MM 34-11-15-04 , PERFORMED PRESSURE TEST ON PITOT SYS. OPS CHECK NORMAL. ACFT SDR FDEA201209273478Static Wick · missingDURING CLIMBOUT, WE WERE INSTRUCTED TO RETURN TO DEPARTURE DUE TO POSSIBLE DAMAGE DURING PUSHBACK. LEFT UPPER WINGLET MISSING STATIC WICKS. REPAIRED L/H UPPER WINGLET CAP PER PART 2 OF EA 1-5720-162680. INSTALLED UPPER WINGLET CAP IAW MM 57-31-01-4 A/C OSDR YENA20120924610Probe · failedFLT 765 MCO-BQN, AIR RETURN TO MCO DUE TO NAV TCAS DISCREPANCY NR 1 CAPT PFD AIRSPEED NOT DISPLAYING LOST DURING TAKEOFF ROLL WOULD NOT RETURN TO NORMAL IN FLIGHT. REMOVED AND REPLACED CAPT'S PITOT PROBE (9DA1) PER AMM 34-11-15. PERFORMED OPS CHECK, OK FOR SSDR A6WA20120925503Pitot System · obstructedON TAKEOFF CAPT AIRSPEED IND 80 KNOTS, F/O IND 60 KNOTS ABORTED TAKEOFF. PURGED MAIN PITOT STATIC SYSTEM, RAN PITOT STATIC LEAK CHECK. OPS CHECK GOOD IAW 34-11-00.SDR KKYA20120924001Pitot System · obstructedCOMPUTER MONITOR NR 1 AND NR 2 AIRSPEEDS PLUS ALTITUDE DISCREPANCIES. FOUND DEBRIS IN BOTH PITOT SYSTEMS AND ADC NR 1 SYSTEM WAS PLUGGED.SDR A6WA20124J502Line · contaminatedABORTED TAKEOFF ROLL AT 70 KNOTS FOR ZERO A/S ON STANDBY ASI. FLAPS AT 20, AIRSPEED 70 KNOTS ON CAPT'S AND F/O'S AIRSPEED TAPES. PURGED P1, P2, AND P3 PITOT/STATIC SYSTEMS AND PERFORMED FUNCTION CHECK OF MAIN AND STANDBY PITOT/STATIC SYSTEMS IAW AMM 34-11-00SDR CA120831001Fitting · corroded(CAN) THE RT, CO-PILOTS, AIRSPEED INDICATOR WAS BEING REPLACED DUE TO A LIGHTING ISSUE. A NEW INDICATOR WAS INSTALLED AND PITOT/STATIC TEST PERFORMED. A MASSIVE LEAK WAS DETECTED AND AN INVESTIGATION WAS INITIATED. AN INSPECTION OF THE NR 2 PITOT/STATIC SYS SDR UALA2012082804830Transformer · failedSTATIC INVERTER IS FAILED TEST. REPLACED NR 2 TRANSFORMER RECTIFIER PER AMM, OPS CHECK GOOD.SDR AALA20120827014Pitot Tube · damagedDFW - CREW REPORTED BIRD STRIKE WITH PITOT TUBE INGESTION AND FLAP CONTACT. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICERS PITOT TUBE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR SIMA20120818005Pitot System · contaminatedFLIGHT 2726, CREW REPORTED DURING DESCENT OUT OF FL370, RECEIVED "IAS" COMPARE FLAGS ON BOTH FIRST OFFICERS AND CAPTAINS PFD. CAPTAIN`S IAS WAS UNRELIABLE, SHORTLY AFTER RECEIVED AN AMBER "ALT" COMPARE FLAGS AS WELL. SELECTED NR 2 ADC ON CAPTAIN`S REVERSIONSDR CA120817003Hose · chafed(CAN) DURING SCHEDULED MAINTENANCE, THE PITOT HOSE TO THE INTEGRATED STANDBY INSTRUMENT WAS FOUND CHAFING ON THE FWD OUTFLOW VALVE. THE PITOT HOSE WAS REPLACED. THE INSPECTION BEING CARRIED OUT IS AN IN-HOUSE TASK CARD TO SPECIFICALLY CHECK FOR THIS ISSUE ASSDR SIMA20120803001Pitot Line · contaminatedFLIGHT 3584, CREW REPORTED IN CRUISE AT FLIGHT LEVEL 370 HAD WING ICE FAIL. TROUBLESHOT PAIR AND PERFORMED AOM VOL 1. NOTHING DETECTED TO FL 210 AND EXITED IN AFTER ABOUT 5 MINUTES ICE DISAPPEARED AND AIRFRAME WAS CLEAR. IAS FLAGGED ASSOCIATED TO PROBE HEATSDR UALA2012072303966Hose · leakingLEAK TEST FAILED. PER MM TOLERANCE IS 300 KTS (+-5 KTS), ACTUAL WAS 293.5 KTS, EXCEEDS LIMITS. FIRST OFFICERS PITOT LEAK WAS IN ELBOW AT ADC HOSE TO 'T'. REPLACED ELBOW, LEAK CHECKED SYSTEM. ACCOMPLISHED PER MM.SDR USAA2012072300012Pitot Tube · cloggedON TAKEOFF ROLL CAPTAIN LOST AIRSPEED INDICATION AROUND 100 KNOTS. CONTINUED TAKEOFF WITH REFERENCE TO FIRST OFFICERS AIRSPEED. AT 200 FEET LOST AUTO THRUST, AUTO FLIGHT, F/CTL ELAC 1 PITCH FAULT, NAV IAS DISCREPANCY, ELAC1. FOUND CAPTAIN'S PITOT TUBE CLOGGSDR V2JA201207110001Pitot Line · obstructedADC NR 1 AND 2 SLOWLY WENT TO ZERO, CREW DIVERTED, AND AFTER A FEW MINUTES THE BOTH ADC’S CAME BACK UP. ACFT LANDED WITHOUT INCIDENT. CLEANED PITOT LINES FOR PILOT & COPILOT ADC`S BY PURGING MOISTURE FROM LINES. LEAK CHECKED GOOD. OPS CHECKED GOOD. WORK PESDR ASAA2012071892558Pitot Tube · failedCAPT PITOT LIGHT ILLUMINATED ON OVERHEAD WITH SWITCH ON - CB DID POP BUT DELAYED. ACFT GROUNDED. R & R CAPT PITOT PROBE IAW AMM 34-11-01-000-801 & 34-11-01-400-801. PERFORMED LT PITOT PROBE SYS LEAK CHECK, CHECK GOOD IAW MM34-11-00-790-810. CONFIRMED C/B POPSDR AALA20120629004Probe · malfunctionedLHR - INFLIGHT FRA-LHR CREW REPORTED CAPTAINS PITOT SYSTEM FAILED AND CIRCUIT BREAKERS POPPED. EICAS MESSAGES FOR BOTH ELECTRONIC ENGINE CONTROLS, AILERON LOCKOUT AND RUDDER RATIO. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT RESDR USAA2012062900018Pitot Tube · faultyCAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED CAPTAIN'S PITOT PROBE IAW AIRBUS MAINTENANCE MANUAL 34-11-15. ALSO REFERENCE SDR'S USAA2012091800002 & USAA2012091800003.SDR FDEA201206152248Elbow · leakingON TAKEOFF DISCREPANCY BETWEEN CAPTAIN`S AIRSPEED AN F/O AIRSPEED OF 40KIAS. REJECTED T/O AT 100KIAS BASED ON F/O AIRSPEED INDICATOR. CLEARED RWY & PERFORMED RTO CHECKLIST. BRAKE COOLING TIME OF 51 MIN. FOUND CAPT'S PITOT TUBE CLOGGED WITH ORGANIC MATTER. RSDR UALA2012061103194Pitot Line · chafedMAIN CABIN, STA 760 RT SIDE ABOVE THE G2A GALLEY, THE NR 1 PITOT PRESSURE LINE IS CHAFED THROUGH. REMOVED PITOT LINE ABOVE G2A GALLEY RT SIDE PER MM 20-10-09. REPAIRED PITOT LINE USING 2 SLEEVES P/N BACS13AP6, 1 P/N MS21921-6, AND 1 IAW MM 20-10-09. REPAIRESDR UALA2012052903011Pitot Line · obstructedTAKEOFF ABORTED ABOUT 90 KTS DUE TO FIRST OFFICERS AIRSPEED INOPERATIVE. AUTOBRAKES ACTIVATED. REPLACED ADM 19FP2 PER MM. SYSTEM RETURNED TO NORMAL. REPLACED FIRST OFFICERS PITOT TUBE DUE TO OBSTRUCTION. LEAK CHECK AND HEAT CHECKS GOOD.SDR CA120530005Pitot Tube · contaminated(CAN) PITOT HEAT CAUTION LIGHT AFTER 20 MINS OF USE. DUE TO HEAVY RAINS, THE PITOT STATIC TUBE ASSY, SUPPORT ASSY, FILLED UP WITH WATER. THE WATER CAUSED A SHORT AT THE CONNECTOR INSIDE THE TUBE. WIRES REPAIRED AND PITOT STATIC TUBE REPLACED. SUGGEST A DRAISDR 9JLA201207172237Pitot Head · obstructedTHE CREW REPORTED THAT ON TAKEOFF ROLL, THE COPILOTS AIRSPEED NEVER CAME ALIVE (INDICATED). GAINED ACCESS TO THE NR 2 PITOT AND FOUND DIRT AND DEBRIS CONSISTANT WITH THE MUD DOBBER WASP NEST. TUBE WAS CLEANED AND SYS CHECKS WERE SATISFACTORY. THE CREW WAS ADSDR SWIA201230634Probe · failedCAPTAIN ALTIMETER READS 250 FEET LOWER THAN FIRST OFFICER'S ALTIMETER AT ALL CRUISE ALTITUDES ABOVE FL 250. (FLT 5415) REPLACED THE NR 1 PITOT STATIC PROBE. P/N: 0856KV9 S/N OFF: 242809SDR UIEA2012042600167Pitot Head · failedAFTER ENGINE START, RT AUX PITOT EICAS MESSAGE DISPLAYED, RETURN TO BLOCKS. R & R RT LOWER PITOT PROBE, OPS AND LEAK CHECKED OK. OK FOR SERVICE IAW MM 34-11-01.SDR HNAA2012042600753Pitot Head · failedCAPTAIN LOST AIRSPEED, HEADING DATA AND YAW DAMPER FAILED. REPLACED RUBBER PITOT HOSE BETWEEN CAPTS PITOT TUBE AND FLOOR V THROUGH. R & R CAPT'S PITOT TUBE. OPS CHECKED GOOD IAW MM 34-11-00.SDR UIEA2012042100160Circuit Breaker · trippedON LANDING, RT AUX PITOT EICAS MESSAGE APPEARED. FOUND CIRCUIT BREAKER TRIPPED, RESET IAW SWPM 20-60-05. PERFORMED SYS TEST IAW AMM 30-31-00. OPS CHECKED GOOD.
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