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 SIMA2018060420005Gasket · failedDURING CLIMB OUT, THROUGH 13,000 FT, HAD A NR 2 BLEED LEAK ILLUMINATE ON THE EICAS, QRH PROCEDURE COMPLIED WITH & THE MESSAGE EXTINGUISHED. FOUND PRE COOLER OUTLET INTERFACE GASKET BLOWN. REMOVED AND REPLACED PRE COOLER OUTLET DUCT INTERFACE GASKET REF E-1SDR QXEA2018052900198Warning System · false activationNR 2 BLEED HOT CAUTION ILLUMINATED IN FLIGHT ON DECENT. BLEED SELECTION WAS IN MIN AND DE-ICE WAS ALL OFF. REMOVED FROM SERVICE. INTERROGATED CDS AND FOUND ECS FAULT CODES 1302 AND 7006. PERFORMED FIM TASKS 36-10-00-810-866 AND 36-20-00-810-802. PERFORMED AMM SDR ASAA2018053174836Controller · failedAIR BLEED CLASS 2 MESSAGE, ACFT GROUNDED. IAW TSM 36-22-00-810-807-A, R & R BMC NR 1, BITE TESTED OK, NO FAULTS.SDR J7SA20180522001Shutoff Valve · activatedDIVERTED DUE TO SMOKE COMING FROM OVERHEAD VENTS IN THE CABIN. A BRIEF LEFT BLEED OVERHEAT CAS. AIRCRAFT LANDED WITHOUT INCIDENT. R & R LEFT HIGH PRESSURE BLEED SHUTOFF VALVE. MVF SUCCESSFUL.SDR HNAA2018052100097Warning System · false activationBLEED 2 VALVE FAIL MSG IN FLIGHT WITH ICING CONDITIONS. CREW RAN QRH. GROUND RAN AC AND PERFORMED OPS CHECK OF BLEED VALVES IAW AMM 36-11-05. OPERATIONAL CHECK GOOD. OK FOR SERVICE.SDR DALA2018051753363Shutoff Valve · faultedABORTED TAKEOFF BELOW 80 KNOTS DUE TO THE CREW REPORTING THAT THEY LOST THE RT BLEED SYS. ALSO REPORTED THAT DURING ENGINE START ON BOTH ENGINES, THE BLEED LIGHTS FLICKERED. DURING ADVANCING THE THROTTLES, BOTH BLEED LIGHTS REMAINED OUT AND THE BLEEDS STABILISDR SIMA2018051501001Pneumatic System · leakingBLEED 1 LEAK DURING DEPARTURE, RAN QRH, MESSAGE DID NOT EXTINGUISH AND RETURNED TO DEPARTURE. EMERGENCY DECLARED. PERFORMED OPC OF E1 BLEED AIR SYSTEM AS PER EMB145 AMM 36-00-00. OPS CHECKED GOOD. PERFORMED LEAKAGE TEST OF LT AIR BLEED SYSTEM DUCTS IAW AMM 3SDR HNAA2018043000091Warning Message · false activationEICAS MESSAGE FOR THE NR 2 BLEED FAIL DURING TAKEOFF, ABORTED TAKEOFF. MESSGAE CLEARED PRIOR TO CREW ENGINE SHUT DOWN. GROUND RAN CND AND NO EICAS OR CMC MESSAGE. OK FOR SERVICE.SDR UIEA2018042000750Light · inoperativeDUCT PRESSURE GAUGE BACKGROUND LIGHT INOPERATIVE. REPLACED THE PRESSURE GAUGE IAW AMM 36-21-00.SDR HNAA2018032600072Warning Message · illuminatedNR 1 BLEED LEAK EICAS MESSAGE DURING CLIMBOUT, FOLLOWED QRH AND MESSAGE WENT OUT AFTER 3 MINUTES 20 SECONDS. OPEN.SDR UIEA2018031700422Sensor · faultyON CLIMB OUT L ENG BLEED OVHT EICAS. ENG BLEED TRIPPED OFF. RESET AT CRUISE PER CHECKLIST. REMOVED AND REPLACED LEFT ENGINE FAN AIR TEMPERATURE SENSOR IAW AMM 36-11-17 OPS CHECK GOOD.SDR UIEA2018031300383Module · erraticAIR SUPPLY BITE BOX GIVING ERRATIC INDICATIONS. REMOVED AND REPLACED THE AIR SUPPLY BITE MODULE, OPS CHECKED NORMAL IAW 36-23-04.SDR UIEA2018022800302Sensor · faultyLEFT ENGINE FATS FAILED ASM CHECK. REMOVED AND REPLACED FAN AIR TEMP SENSOR. OPS CHECK AND LEAK CHECK NORMAL IAW 36-23-00, 36-11-17.SDR SWIA201844332Detector Loop · failedANTI- ICE DUCT (RT SIDE) WARNING MSG IN FLIGHT WITH WINGS AND COWLS ANTI-ICE SELECTED. COMPLIED WITH QRH. RT FUSE DUCT SHOWED RED. EMERGENCY DECLARED. (FLT 5738) CLOSED REMOVED AND REPLACED THE RT WHEEL WELL LEAK DETECTOR LOOP. OPS CHECK GOOD AT THIS TIME.SDR HNAA2018022600039Warning System · false activationBLEED 1 VLV CLOSED EICAS ADVISORY DISPLAYED ON CLIMB OUT. WOULD NOT EXTINGUISH. CND. FOUND TO BE TRANSITORY CONDITION OF ENGINE BLEED VALVE TROUBBLESHOT IAW FIM 36-11-00-816-001-A. OK FOR SERVICE.SDR YADA2018022218001Gasket · failedRIGHT BLEED AIR ANNUNCIATOR ILLUMINATED INFLIGHT. RIGHT OVERTEMP SENSOR GASKET FAILED MELTING THE EVA TUBING.SDR SIMA20180220002O-Ring · failedNR 2 BLEED LEAK WARNING DURING CLIMBOUT. CLIMB THRUST, O' SAT, 5' TAT, ANTI-ICE SYSTEM ON FL 200. REMOVED AND REPLACED THE O-RINGS AT JOINT 18 IAW AMM 36-11-10. OPS OK.SDR A6WA2018032245634Warning System · false activationCLIMBING THROUGH FL210 RECEIVED ANTI ICE WARNING WITH OVERHEAT INDICATION, C/W QRH MESSAGE PERSISTED. AIR RETURNED TO ROC PER QRH, FLAPS 20 REF 45+30 KNOTS (SPEED WAS 169) NO THRUST REVERSERS AVAILABLE/FULL BRAKING. TEMPS AT GATE 8-10-5-5 LANDING WEIGHT 46,000SDR HNAA2018021900033Clamp · looseDURING TAKEOFF, A BLEED 1 LEAK MESSAGE DISPLAYED ON EICAS FOR 10 SECONDS AND SELF EXTINGUISHED. TIGHTENED THE NR 1 ENGINE BLEED VALVE V-BAND CLAMP IAW AMM 36-00-00-700-804. OPS CHECKED GOOD. OKAY FOR SERVICE.SDR RAIA201801300003Warning Light · false activationNR 1 AND 2 BLEED OVERTEMP ILLUMINATED IN FLT. PERFORMED A BLEED TEST WITH CREW. NO DEFECTS NOTED.SDR REXA2018012900068Connector · defectiveL BLEED DUCT WARNING CAME ON IN CRUISE FLIGHT, FOLLOWED BY RAPID DECENT TO 10000' FOLLOWED QRH CHECKLIST SUCCESSFULLY. AIRCRAFT LANDED UNEVENTFULLY. REPLACED ELBOW CONNECTIONS LT BLEED LOOP A, MT137P2, MT202P2, AND LOOP B MT203P1 IAW AMM 36-21-01 OPS TEST GOODSDR HALA2017123100279Sensor · failedAIRCRAFT 388 DIV TO LAX DUE TO ECAM MESSAGE: AIR BLEED LOW TEMP ON BLEED 1. CORRECTIVE ACTION: REPLACED LEFT EXCHANGE OUTLET TEMP SENSOR 10HA1.SDR UIEA2017112702309Warning System · false activationLEFT BLD VALVE EICAS PRIOR TO ENGINE START. PERFORMED BITE PER FIM 36-10-827 NO FAULTS FOUND, EICAS MESSAGE CLEAR.SDR FDEA201711203281Controller · malfunctionedLEVEL 3 AIR MANIFOLD NR 2 FAILED. DIVERTED. INTERROGATED THE MFC AND FOUND TAIL PYLON Z15 OVERHEAT FAIL CODE 017 , UPPER TAIL POD A SHORT FAIL CODE 094, TAIL PYLON Z14 OVERHEAT FAIL CODE 016, TAIL PYLON A SHORT FAIL CODE 096, AND UPPER TAIL POD B SHORT FSDR UIEA2017103002139Status Message · false indicationSTATUS MESSAGE R ENG PRV. STATUS MESSAGE CLEARED IAW AMM REF 36-00-00.SDR UIEA2017102502025Sense Line · damagedNR 2 PYLON FAN AIR VALE SENSE LINES DAMAGED. NR 2 PYLON FAN AIR VALVE SENSE LINES REPLACED.SDR REXA2017101501099Element · malfunctionedRT 14TH STAGE DUCT WARNING MESSAGE WITH AURAL AND CHIME WARNINGS. COMPLIED WITH QRH BY CLOSING THE 14TH STAGE SOV AND SELECTING 14TH STAGE ISOLATION VALVE TO OPEN. WARNING CLEARED PRIOR TO 40 SECONDS. WARNING REAPPERED WITHIN 2 MINUTES LATER, WITH THE RT 1SDR UIEA2017100401926Warning System · activatedLT ENGINE BLEED OFF LIGHT ILLUMINATED. REF MDDR 89004 DUPLICATE WRITE UP. CLEARS MDDR 83993. PLACARDS REMOVED. MCC NOTIFIED.SDR DXTAT2PL6D005EAU5Sensor · defectiveAT 36000FT. DUCT 2 OVERHEAT. FOLLOWED CHECKLIST. DUCT ONE OVERHEAT SHORTLY AFTER. INSTALLED A NEW NR 1 DUCT TEMPERATURE SENSOR AND NEW ECS TEMPERATURE CONTROLLER IAW MM 21-61-03 AND MM 21-61-01. OPS CHECKS PERFORMED MM 21-61-00-710-801A/500. OPS CHECKESDR MASA2017092512662Warning System · activatedDIVERTED DECLARED EMERGENCY RT BLEED DUCT WARNING. PLACED RIGHT PACK ON MEL.SDR MASA2017092312655Warning System · activatedDECLARED AN EMERG AND RTF DUE TO LT BLEED DUCT WARN.SDR AALA20170902007Thermocouple · unsecureEMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A RIGHT ENGINE BLEED DUCT LEAK WARNING INDICATION. OVERWEIGHT LANDING UNEVENTFUL. ACCOMPLISHED LEAK CHECK PER MCM 36-96-02. RESECURED FIRE LOOP THERMOCOUPLES PER SRM 51-30-01. LEAK AND OPERATIONAL CSDR VNAA2017090111101Clamp · out of positionFLIGHT CREW HAD A LT BLEED MESSAGE DISPLAY. LT PACK AUTOSHUTDOWN. ACFT LOST PRESSURIZATION. EMERGENCY DECLARED AND DIVERTED. MX FOUND A LEAK NEAR THE ACM . THE CLAMP ON THE VALVE POSITION WAS CHANGED TO PREVENT DIRECT FLOW ONTO THE BLEED LOOP. PERFORMED LEASDR HALA2017082800240Sense Line · looseON DESCENT FROM FL250 TO FL230 BLEED DUCT PRESS FLUCTUATED BTN 25 TO 35 PSI. FOUND RT ENG PRSOV PRESSURE SENSE LINE LOOSE AND PACKING DAMAGED. REPLACED PACKING AND TIGHTENED SENSE LINE.SDR HALA2017082810237Sense Line · damagedETOPS / ON DESCENT FROM FL250 TO FL230 BLEED DUCT PRESS FLUCTUATED BTN 25 TO 35 PSI. FOUND RT ENG PRSOV PRESSURE SENSE LINE LOOSE AND PACKING DAMAGED. REPLACED PACKING AND TIGHTENED SENSE LINE.SDR FDEA201708232299Clamp · leakingAIR MANIFOLD NR 2 FAILED. AFTER TAKEOFF. AIR TURN BACK. REMOVED & REPLACED CLAMP ON DUCT ASSY IN LEFT WHEEL WELL IAW MM 36-14-02-4. NO LEAKS NOTED. PERFORMED DECAY CHECK WITH APU IAW 36-00-01-5 AND GAINED 4 SECONDS. TIME IS NOW WELL WITHIN LIMITS AT 22 SECSDR RAIA201708220001Valve · inoperativeBLEED 1 AND 2 OVERTEMP DURING CRUISE. R & R FAN AIR VALVE, OPS CHECKED GOOD.SDR N6WA2017071101Warning Message · illuminatedBLEED DUCT WARNING MESSAGE IN FLGHT. ENSURED BLEED IS SELECTED OFF AND NO OTHER FAULTS ARE ON EICAS, AIRCRAFT IS SAFE FOR ONE TIME FERRY FLIGHT.SDR DXTA2017071206427Valve · failedDURING DESCENT THRU 18000 FEET WITH WING AND ANTI-ICE ON, AN AMBER LEFT BLEED AIR HOT CAS MESSAGE ILLUMINATED. THE HIGHEST TEMPERATURE SEEN AS LIGHT EXTINGUISHED WAS 522F. THE LIGHT WENT OUT AND THEN CAN BACK ON. THE LIGHT EXTINGUISHED AGAIN AND NEVER CAME SDR SIMA20170623002Gasket · failedDURING CLIMB OUT AT APPROXIMATELY 5000 FT, NR 1 BLEED LEAK ON EICAS. QRH PROCEDURES ISOLATED THE SYSTEM. SEVERAL MINUTES LATER BECAME EXTREAMLY HOT AIR IN CABIN COMBINED WITH ODD ODOR. FOUND THE NR 1 ENGINE PRECOOLER DUCT INTERFACE GASKET BLOWN. REMOVED AND SDR DALA2017052504286Sensor · malfunctionedAFTER SELECTING ENGINE ANTI-ICE, LEFT ENGINE BLEED OFF EICAS MESSAGE. WITH OFF LIGHT, FOLLOWED QRH AND IT REOCCURRED WITH FUMES THROUGHOUT CABIN. TURNED ENGINE ANTI-ICE OFF AND RESET WORKED. R & R 450 DEG TEMP SENSOR, AND THE FAN AIR TEMP SENSOR, ALSO THE FASDR SIMA20170519004Gasket · failedBLEED NR 1 LEAK ILLUMINATED ON EICAS, PASSING 3000 FT AFTER TAKE OFF. REMOVED AND REPLACED THE PRECOOLER OUTLET DUCT GASKET ON THE NR 1 ENGINE IAW AMM 36-11-08, SUBTASK 020-013-A, & 420-011-A. OPS & LEAK CHECKED GOOD.SDR HNAA2017051900175O-Ring · failedAFTER PUSHBACK, STARTED NR 1 ENGINE, BLEED 1 LEAK MASTER WARNING AND EICAS MESSAGE ILLUMINATED AND LEAK INSCRIPTION BAR ILLUMINATED. INSPECTED THE NR 1 BLEED SYSTEM, FOUND A BROKEN O-RING ON THE BLEED SYSTEM JOINT UNDER PANEL 271DLW. REMOVED AND REPLACED TSDR HALA2017051400171Regulator Valve · failedRETURNED TO DEPARTURE DUE TO A NR 2 ENGINE BLEED FAULT. REPLACED THE NR 2 ENGINE PRESSURE REGULATOR VALVE.SDR SIMA20170428001Clamp · damagedPASSING 11,000 BLEED 1 MASTER CAUTION. RAN EPC & AOM1 CHECKLIST AND AFTER A PERIOD OF TIME, LESS THAN 3 MINUTES IT WENT AWAY. WAS IN ICING CONDITIONS WHEN HAPPENED. REMOVED AND REPLACED AFT V- CLAMP ON NR 1 ENGINE PRECOOLER IAW AMM 36-11-04. LEAK CHECKED GOSDR FDEA201704201245Warning Message · false indicationAT FL 350, HAD A LEVEL 3 AIR MANIFOLD 3 FAILURE. RAN QRH, ALERT WENT AWAY. DECLARED AN EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT. CHECKED MANIFOLD FAILURE INDICATORS IN CAC AND FOUND RT MANIFOLD PRESSURE SWITCH FAULTING IAW AMM 36-23-03-4-0, 36-0SDR ASAA2017032120263Sense Line · unsecureFOLLOW-UP TO REPORT OF HIGH DUCT PRESSURE RIGHT SIDE GROUNDED - YES. FOUND SENSE LINES AT BLEED AIR REG AND PRSOV NOT SECURE. RESECURED SENSE LINES REF AMM 36-11-03 FOR BLEED AIR REG AND 36-11-04 FOR PRSOV. REF MAINT TASK CARD NG 36WC-0001 NO DEFECTS NOTED.SDR ASMF201703006Sensor · damagedAIRCRAFT PERFORMED AN EMERGENCY DESCENT AT GDL DUE TO DURING CLIMB, THE LEFT BLEED TRIP OFF LIGHT TURNED ON AND CONTROL PRESS AUTO, SEMI AUTO AND MANUAL WITH NO CONTROL, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. MAINTENANCESDR SIMA20170305002O-Ring · failedNR 1 BLEED LEAK WARNING DURING FLIGHT. RAN PROCEDURE, MESSAGE EXTINGUISHED. REMOVED AND REPLACED BLEED O-RINGS IN THE AFT ELECTRONIC COMPARTMENT IAW AMM 36-11-10. OPS CHECKED GOOD IAW AMM 36-00-00.SDR HALA2017030500085Warning Message · illuminatedRETURNED TO DEPARTURE DUE TO AIR BLEED LOW TEMP ON BLEED 2 ECAM MESSAGE DURING CLIMB OUT. REPLACED NR 2 ENGINE FAN CONTROL THERMOSTAT, AND EXCHANGER OUTLET TEMP SENSOR, AND FAN AIR VALVE.
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