JASC 3620
Service difficulty reports · 1,276
Reports filed under 3620 · Pneumatic Indicating 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 = '3620' 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 = '3620' 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 REXA201100974Loop · defectiveANTI ICE DUCT WARN MESSAGE ON TAKEOFF. REMOVED AND REPLACED SHORTED LOOP A18WK & OP CHECK GOOD IAW AMM 36-21-04. OK FOR SERVICE.SDR WRNA201100013Sense Line · damagedSOON AFTER T/O, BLEED AIR 2 & PAC 2 OFF LEVEL 1 ALERTS WERE DISPLAYED. PROCEEDED WITH FLT, NO FURTHER ISSUES. TEN MINUTES AFTER TOP OF CLIMB, BLEED AIR 3 TEMP WENT TO APPROX 260C & SHUT THE ASSOCIATED BLEED AIR 3 VALVE OFF. LEVEL 1 BLEED AIR 3 OFF ALERT WAS SDR REXA201100885Sensing Element · defectiveANTI-ICE DUCT CAUTION MSG FOLLOWED BY ANTI-ICE DUCT WARNING ON APPROACH. WINGS AND COWLS ON. T/S DISCREPANCY, FOUND L WING LOOP A & LOOP B (OPEN). REMOVED AND REPLACED INSERT SHELL ASSY AT MT-171 P1 & MT 171 P2. OPS CHECK GOOD AT THIS TIME. OK FOR SVC. PSDR WRNA201100014Sense Line · looseIN CRUISE BLEED AIR 3 OFF LEVEL 1 MESSAGE CAME IN VIEW (NR 2 BLEED ALREADY DEFERRED). DECISION WAS MADE TO DIVERT TO SKBO FOR MX ASSISTANCE. FUEL DUMPED APPROX 27K TO ACHIEVE ACCEPTABLE LANDING WEIGHT. LANDING ACCOMPLISHED NORMAL. MX T/S FOUND SENSE LINE LSDR REXA201100877Switch · defectiveON DEP WITH WING ANTI ICE OFF, GOT ANTI ICE DUCT WARNING, MSG THEN WENT AWAY. LATER WITH IT ON NORM IT CAME BACK, ALSO IN STBY MODE, ALL LEFT LEADING EDGE. FOUND LT O/B SECTION LEAK DET CIRCUIT SHORTING WHEN HOT. REMOVED AND REPLACED ALL O/B SWITCHES & OP CSDR CHQA201100460Sensor · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 2 LOW TEMP MESSAGE ON THE EICAS. THE CREW DIVERTED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED 2 OUTLET TEMPERATURE SENSOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NSDR ASAA11510721Unknown · malfunctionedLG SPLIT ON DUCT PRESSURE. 370 R25 L45. CLIMB TO 380 R25 L40. AT 380 R26 L40. AT 380 OAT 54 N1 91.8 91.7 M.80. ACCOMPLISHED RT ENGINE BLEED AIR SYSTEM HEALTH CHECK. NO DEFECTS FOUND. REF AMM 36 11 00 701 801.SDR FDEA201111235006Element · failedAFTER TAKEOFF, WITH NR 2 PACK OFF, CLIMBING PASSED 14000' MSL. RECEIVED NR 2 MANIFOLD FAILURE LEVEL ALERT, RTB LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE MANIFOLD SENSING ELEMENT IAW MM 36-23-02-4. RAN NR 2 ENGINE REF JRH AND PERFORMED PNESDR UALA2011112106408Warning System · false activationSTATUS MESSAGE BLEED FAMV R. AHM SHOWS IN ADDITION TO MSG 36-10340, MSG 36-10532 FOR RVDT CIRCUIT OPEN OR SHORTED. REPLACED VALVE PER MM. NO HELP, REACTIVATED FAMV, AIR SUPPLY CONTROL SYS TEST PASSED ON MAT & ENG AIR SUPPLY TEST FOR FAMV NORMAL & MSG CLEAREDSDR UALA2011111106173Sensor · out of adjustMAN PRESS LEFT MSG SHOW ON EICAS. DF PER MEL 3621A. -INF- :MSG SHOULD READS MAN PRESS SENSOR LEFT. -ADJ- :MSG 36-10480 LATCHED. PERFORMED FIM 36-21 TASK 805 AND GRD TEST PASSED. MSG ERASED AND NO FAULT NOTED.SDR FDEA201111114874Sensor · failedAIR MANIFOLD 2 FAIL ENROUTE. REPLACED SENSING ELEMENT D1-49C.SDR MYWA110106Sensor · defectiveETOPS SIGNIFICANT SYSTEM: ENG NR 2 NO BLEED WHEN SW SELECTED WITH ENGINE RUNNING. PER HEALTH CHECK REMOVED AND REPLACED 450 SENSOR IAW AMM 36-11-05. REMOVED AND REPLACED HIGH STAGE REG IAW AMM 36-11-07. C/W ENG POWER RUN IAW AMM 71-00-00, ALL PARAMETERS NOSDR CALA2011103100700Warning System · false activationDURING TAKEOFF AT APPROX 75-90 KNTS, REJECTED T/O FOR "LEFT BLEED OFF" LIGHT ILLUM. ON EICAS. PERFORMED FIM TASK 36-10 TASK 816 AND FOUND NO DEFECTS. PERFORMED MM 36 -00-23-705-152-001 (PRSOV TEST) AND FOUND NO DEFECTS. RAN NR 1 ENG AND ALL OPS OK.SDR REXA201100780Warning System · false activationDURING CLIMB - ANTI ICE DUCT WARNING MESSAGE CAME ON JUST AS THE WING ANTI ICE WAS TURNED OFF. STILL HAD COWL ANTI ICE ON. A/ICE SYNOPTIC PAGE SHOWED RED LINE THROUGH LEFT FUSELAGE ONLY. PERFORMED OPC OF BLEED AIR INDICATION SYSTEM IAW AMM 36-20-00. UNABLESDR C2XA11TY162Warning System · false activationTYS - A/C DIVERTED TO TYS FROM GSO TO IAH WITH A NR 1 ENGINE BLEED LEAK INDICATION ON THE EICIAS. MAINTENANCE COMPLIED WITH THE NR 1 BLEED SYSTEM CHECK IAW EMB 145XR AMM 36-00-00-700-803A. OPS CHECK GOOD, COULD NOT DUPLICATE THE PROBLEM AND WAS RELEASED BACKSDR VNAA2011102700023Sensing Element · faultyCREW REPORTED RIGHT 14TH DUCT RED CAS MESSAGE IN FLIGHT EN ROUTE FROM DAY TO DCA. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT PYLON SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUSDR REXA201100764Sensing Element · defectiveANTI-ICE DUCT WARNING IN FLIGHT LEFT SIDE OF FUSELAGE RED ON A/ICE SYNOPTIC PAGE. TROUBLE SHOT AND FOUND LEFT FUSELAGE SENSING ELEMENT A47WK TO BE AT FAULT. REMOVED AND REPLACED A47WK SENSING ELEMENT IAW AMM 36-21-04. OPERATIONAL TEST OF THE BLEED AIR LEAK SDR REXA201100763Sensing Element · defectiveANTI-ICE DUCT MESSAGE (WARNING) CAME ON AT INITIAL APLICATION OF WING A-ICE. CLEARED W/ IN 10 SEC. TWICE. REMOVED AND REPLACED RT FUSELAGE SENSING ELEMENT A38WK IAW AMM 36-21-04. OPC GOOD. VERIFIED PART EFFECTIVITY.SDR REXA201100739Loop · out of positionAPPROX 1 MIN AFTER T/O, "ANTI-ICE DUCT" WARNING MSG ON ED1, FOLLOWED BY "ANTI-ICE DUCT" CAUTION MSG. PERFORMED QRH EP 11-2. BOTH MSGS OUT; DID NOT RE-APPEAR. REPOSITIONED LOOPS AS NEED AT SS184R IAW CRJ900 AMM 36-21-11, PERFORMED HI POWER RUNS & OPS CHECK OFSDR REXA201100738Warning System · false activationANTI ICE DUCT WARNING IN FLT LEFT SIDE FUSELAGE RED ON A/ICE SYNOPTIC PAGE. LT LOOP CIRCUIT INSULATION CHECK GOOD FROM BLCU IAW ESPM 20-12-00 RAN WING ANTI ICE SYS. NO LEAKS NOTED OP CHECK GOOD IAW AMM 36-21-00.SDR REXA201100726Sensing Element · defectiveRT 14TH DUCT MASTER WARNING ON CLIMBOUT - FORWARD SECTION OF ENGINE BLEED SHOWED RED. REMOVED AND REPLACED RT 14TH STAGE PYLON DUCT HEAT SENSE ELEMENT A 58WK IAW AMM 36-21-04 OPC NORMAL. RT COWL ANTI-ICE OPC NORMAL IAW AMM 30-22-00. PART EFFECTIVITY VERIFIESDR UALA2011101205529Detection Sys · failedBLEED LOOP 1 BODY FAILURE OF BODY DUCT LEAK DETECTION LOOP OR LEFT DUCT LEAK OVERHEAT DETECTION SYSTEM (DLODS) CARD. STATUS MSG-2631141 INACTV ER INTER MSG-2631131 INACTV CL INTER. MSG 26-31141 DISPLAYED ON MAT REF FIMMAN 26-18-803 FOR FAULT ISOLATION.SDR C2XA11RI159Warning System · false activationFLT 4400-IAD CREW REPORTED BLEED VALVE FAIL ON EICAS DURING TAKEOFF ROLL UNSURE OF WHICH SIDE FAILED MESSAGE CLEARED OFF EICAS. IAD MX PERFORMED OPERATIONAL CHECK OF AIR BLEED SYSTEM IAW EMB145 AMM 36-00-00 AND EC3610-01075 AND COULD NOT DUPLICATE. OPERATIONSDR ASAA11510407Warning System · false activationAT FL 300 AFTER USING WING ANTI ICE HAD A L BLEED TRIP LIGHT ILLUMINATE. PERFORMED QRH LIGHT EXTINGUISHED. ACCOMP FIM 36 10 00 810 801 STEPS F (1) (2) (B) AND STEPS F (3) (7) NO DEFECTS NOTED. PER TABLE ON PAGE 5 WTAI AT CRUISE CAN CAUSE BLEED TRIP.SDR NOCA09011Element · damagedA/C HAD AN AIR TURNBACK TO KWI DUE TO LEFT BLEED DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. ACCOMPLISHED INSPECTION OF WING/BODY LEAK DECTION LOOPS REPLACED DAMAGED HARDWARE AND DECTOR ELEMENTS AS PER MSDR FDEA201109193954Controller · failedTURNED ON WING ANTI-ICE, LEVEL 3 ALERT MANIFOLD FAILURE. PRV BLEED AUTO CLOSED. OPERATED ENG AT IDLE. EMERGENCY LANDING. REMOVED AND REPLACED NR 1 MANIFOLD FAILURE CONTROLLER IAW AMM 36-23-01-4, OP'S CHECKED GOOD. OK FOR SERVICE.SDR ASAA11510391Switch · faultyRIGHT "BLEED AIR TRIP' LIGHT ILLUMINATED. FL 260, RIGHT DUCT PRESSURE DROPPED TO 5 PSI. RESET TRIP SWITCH PUSHED DUCT PRESSURE RESTORED BRIEFLY LIGHT EXTINGUISHED FOR 1 SECOND THEN REILLUMINATED. IT REMAINED ON FOR THE DURATION OF THE FLIGHT. DIVERSION TIMSDR REXA201100567Sensing Element · groundedL 14TH DUCT FOUND HEAT SENSING ELEMENT AT CONNECTOR A47WK TO BE GROUNDING ON AIRFRAME. REROUTED, RESECURED ELEMENT AND OPS CHECKED IAW AMM 36-21-00. NO DEFECTS NOTED. OK FOR SERVICE. EMERGENCY WAS DECLARED.SDR Q2SA765002Sense Line · looseON 09/16/11, ETH 3718 FROM HAAB TO VHHH - APPROXIMATELY 15 MINUTES AFTER TAKEOFF, CLIMBING THROUGH FL 170, NUMBER FOUR ENGINE FIRE WARNING ANNUNCIATED. THE CREW ACCOMPLISHED ALL MEMORY ITEMS, DECLARED AN EMERGENCY AND COORDINATED WITH ATC TO RETURN TO ADDIS.SDR CHQA201100366Warning System · false activationCREW REPORTED THAT DURING CLIMB RECEIVED A BLEED 1 LEAK MESSAGE. THE CREW RETURNED TO KDCA AND LANDED WITHOUT INCIDENT. MAINTENANCE EXPOSED ALL JOINTS IN THE BLEED 1 SYSTEM WITH NO LEAKS NOTED. HIGH POWER ENGINE RUNS WERE ALSO PERFORMED WITH NO DEFECTS NOTESDR VNAA2011090900006Controller · malfunctionedCREW REPORTED LEFT BLEED DUCT RED WARNING MESSAGE IN FLIGHT EN ROUTE FROM CLT TO ABE. CREW DIVERTED TO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED AILC (ANTI-ICE AND LEAK DETECTION CONTROLLER) AND PERFORMED CHECKS USING AIRSDR YENA20110829328Loop · contaminatedFLT 1126 FLL- RDU HAD AN AIR RETURN TO FLL, DURING CLIMB, BLEED 1 LEAK EICAS COMPLIED WITH QRH. REMOVED AND REPLACED CERAMIC PIN INSERT AT P2145 ENG NR 1 LOOP 3 IAW AMM 36-20-01. REMOVED CONTAMINATION AT P2145. OPS CHECK GOOD. NO DEFECTS NOTED.SDR MASA2011082203524Insulator · defectiveRT BLEED WARNING. R2 INSULATORS AT MT 205 AND 146.SDR SWIA201127132Insulator · defectiveA "R BLEED DUCT" WARNING MESSAGE. (FLT 5474) REPLACED RIGHT BLEED LOOP "A" MT204P1 INSULATOR.SDR CALA2011080500527Sensor · defectiveFIVE MIN AFTER L ENG BLEED MESS R ENG OVERHEAT CAME ON (BOTH ENG OVERHEAT & EICAS MESSAGE) QRH ACCOMPLISH STARTED APU & TURN R BLEED OFF REF L/P 8884944 & L/P 8886900 FOR CORRECTIVE ACTION PERFORMED HIGH POWER ENG RUNS REF AMM 71-00-00. NO DEFECTS NOTED AT THSDR COMA2011080490026Warning System · false activationON CLIMBOUT FROM DFW RECEIVED BLEED AIR DUCT WARNING MSG. A/C DEPRESSURIZED, EMERGENCY DECLARED. A/C RETURNED TO DFW LANDED SAFELY. INTEROGATED MDC FOUND LOOP MT 227 FLAGGED. INSPECTED LOOP MT 227 AND SURROUNDING LOOPS, NO DEFECTS NOTED. PERFORMED ANTI-ICSDR CA110808001Indicator · failedTHE FLIGHT DEPARTED NORMALLY UNDER MEL FOR BLEED 1 INOP. AFTER DEPARTURE THE FLIGHT EXPERIENCED A FAILURE OF THE OTHER BLEED. THE CREW CALLED A PAN PAN AND DID A RAPID DESCENT TO 10,000 FT AND RETURNED WHERE THEY ARE EXPECTED TO LAND OVERWEIGHT . REPLACED LSDR ASAA11510198Sensor · faultyDURING CLIMB HAD A DUCT PRESSURE SPLIT IN EXCESS OF 20 PSI. CLIMB AT FLIGHT LEVEL 350 N1 100.9 PERCENT WING & ENGINE ANTI ICE OFF ISOLATION VALVE AUTO PACK SWITCHES AUTO BLEED AIR SWITCHES ON LEFT BLEED AIR DUCT PRESSURE 42 PSI RIGHT BLEED AIR DUCT PRESSURE 2SDR MYWA110081Sensor · faultyETOPS SIGNIFICANT SYSTEM: NR 1 BLEED LIGHT ILLUMINATES IN FLIGHT. REMOVED AND REPLACED NR 1 450 DEGREE TEMP SENSOR IAW B-737-800 MM REF 36-11-05, CHECKS GOOD.SDR UALA2011080103965Warning System · activatedL ENG HPSOV EICAS & BLEED LT AFTER ENG START.SDR REXA201100475Sensing Element · failedRT 14TH DUCT MASTER WARNING 8,000 FT RED INDICATION BETWEEN 14TH SOV AND WING/COWL VALVES. REMOVED AND REPLACED RT PYLON SENSING ELEMENT (A59WK) IAW AMM 36-21-04. VERIFIED PART EFFECTIVITY. OPS CHECK GOOD. OK FOR SERVICE.SDR USAA2011072500001Sense Line · contaminatedFLIGHT 703, PHL-PIT - BLEED 2 OVERPRESS CAUTION EICAS ON CLIMBOUT. QRH PROCEDURE FOLLOWED. BLEED 2 OVERPRESS REMOVED ANNUNCIATED UNTIL NR 2 THRUST LEVER TO IDLE IAW QRH. NOTE: ON ECS SYNOPTIC PAGE. NR 2 BLEED INDICATED 120 PSI BEFORE BLEED SELECTED OFF. SDR COMA2011072190015Warning System · false activationEN ROUTE FROM MIA TO DCA RECEIVED LEFT BLEED DUCT WARNING MSG. EMERGENCY DECLARED, A/C DIVERTED TO MCO LANDED SAFELY. INSPECTED LEFT BLEED DETECTION LOOPS IN AFT EQUIPMENT BAY. NO DEFECTS NOTED, OPS CHECK GOOD.SDR YENA20110717302Warning System · false activationFLT 975 BOS-FLL DECLARED EMERGENCY, BLEED 1 LEAK EICAS- BLEED 1 FAIL EICAS. INTERROGATED CMC - SHOWS FAULT CODE ABOVE (36113000AM1-2) - BLEED ODS NVM. SHOWING BLEED OVHT AT LOCATIONS 15.10 FOR CH1 AND 16.58 FOR CH 2. INSPECTED AREA FOR LEAKS PER AMM 36-11-0SDR MASA2011071803253Sensor · faultyLEFT ENG BLEED CAUTION IN FLT. REPLACED TEMP SENSOR.SDR C2XA11CL168Sensor · faultyIAH FLT 2167 THE CREW REPORTED A NR 1 BLEED LEAK MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE INSPECTED AND REPLACED THE LEFT PYLON DUCT TEMP SENSOR S0791. OPERATIONAL CHECKS WERE GOOD.SDR MASA2011071803249Sensor · dirtyLT ENG BLEED CAUTION IN FLT. CLEANED TEMP SENSOR AND PRSOV CONNECTOR.SDR ASAA11510063Warning System · intermittentAT TOP OF CLIMB FL350 WITH WING ANTI ICE OFF THE RIGHT BLEED TRIP ILLUMINATED. WENT OUT AFTER RESET. ACCOMPLISHED FIM TASK 36 10 00 810 801 NO FAULTS NOTED. PERFORMED GROUND VERIFICATION TEST PER FIM TASK 36 10 00 810 801 GROUND VERIFICATION SUCCESSFUL. NOSDR FDEA201107102633Sensor · malfunctionedON CLIMBOUT LEVEL ONE "AIR SYS 2 OFF" CAME ON. 30 SECONDS LATER LEVEL 3 "AIR MANF 2 FAIL" CAME ON. STAYED ON FOR 10 SECONDS WENT OUT THEN CAME ON AGAIN FOR 15 SECONDS. COMPLIED WITH QRH RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. R & R NR 2 MANIFOLDSDR MASA2011071103201Loop · faultyLT BLEED DUCT WARNING 4 MIN INTO FLT. R2 LOOPS MT202, 203 AND ALL INSULATORS ON LOOPS.
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