JASC 3697
Service difficulty reports · 222
Reports filed under 3697 · Pneumatic System Wiring, 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 = '3697' 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 = '3697' 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 HALA2018122400672Connector · brokenETOPS SIGNIFICANT SYSTEM - AFTER APU BLEED & PACKS COMMANDED ON. ENG 2 BLEED VALVE NOT CLOSED FAULT DISPLAYED ON ECAM.// INSPECTED ENG 2 BLEED VALVE & FOUND CONNECTOR BROKEN. REPLACED CONNECTOR(FIN 4001HA)PER AMM 71-71-20. RAN #2 ENG. ECAM WARNING "ENG 2 BLEEDSDR SIMA2018121009001Connector · looseBLD 1 LEAK IN FLIGHT QRH PROCEDURES COMPLIED WITH MESSAGE EXTINGUISHED.-C/A-INSPECTED PACK 1 FOR LOOSE DUCTING/CLAMPS. NO DEFECTS NOTED IAW EMB 145 AMM 21-20-04. FOUND #1 ENG BLEED VALVE CONNECTOR LOOSE. RESECURED CONNECTOR IAW EMB 145 AMM 36-11-05. NO DEFETCSSDR UIEA2018120402779Connector · dirtyLT ENG PRV EICAS MESSAGE ON DEPARTURE QRH COMPLETE. TROUBLE SHOOTING AND CLEAND CONNECTOR TO PRV ON LEFT ENGINE. PERFORMED BITE TEST AND PERFORMED OPS CHECK NORMAL IAW AMM 36-11-18 AND OPS CHECK GOOD AT THIS TIME.SDR HNAA2018112600289Connector · disconnectedPDIS 628 36-12 2006092 23NOV18 PHL CLOSE
ON INITAL TAKE OFF ROLL HSV 2 FAIL EICAS MESSAGE DIS
PLAYED. BROUGHT POWER BACK MESSAGE EXTINGUISHED BUT
CAME BACK ON AT TAXI POWER.
FACT 23NOV18 20:24 PHL
UPON FOUND CANONSDR UIEA201811092530Terminal · damagedFOUND THE LT ENGINE PRV TERMINAL LUGS DAMAGED AND CHAFED TO GROUND. REMOVED AND REPLACED THE TERMINAL LUGS IAW SWPM 20-30-11.SDR P5CA2018102900331Connector · looseRIGHT ENGINE STATUS MESSAGE (<P>PER FIM PROCEDURES 36-10-00 BITE TEST C/O WITH NIL FAULTS INDICATED, MESSAGE ERASED, PRV AND PRVC OPERATION CHECKED SATISFACTORY. PNEUMATIC CONNECTION AT PRVC FOUND BELOW TORQUE AND TIGHTENED IAW AMM 36-11-19. </P>)SDR UIEA2018101802281Connector · dirtyDURING CLIMB OUT EICAS MSG RT ENG HPSOV ILLUMINATED FOR 30 SECONDS THEN STATUS MSG. RT ENG HPSOV ILLUMINATED REST OF FLIGHT. VERIFIED ELECTRICAL CONTINUITY OF RT HPSOV SYSTEM IAW WDM 36-11-62. NO FAULTS FOUND, CLEANED LIGHT DIRT FROM CONECTOR D17066P. AS PRECASDR UIEA2018101502264Wire · missingDURING ENG RUN NR 2 BLEED LIGHT ILLUMINATED. TROUBLESHOOT ENG NR 2 BLEED IAW FIM 36-10-00 TREE 847 FOUND WIRE MISSING, SAME INSTALLED IAW WDM 36-11-62 OF THE P37. OPS CHECK CARRIED OUT IAW AMM 71-00-00, OPS CHECK SATISFACTORY.SDR UIEA2018081301677Connector · defectiveDURING CRUISE LEFT DUCT PRESSURE 10 PSI. THE BLEED DISCRETE LIGHT ON OVERHEAD PANEL CAME ON FOR SEVERAL SECONDS. REPLACED ELECTRICAL CONNECTOR D4156P, WHICH IS DAMAGED IAW SWPM 20-35-11. SECURED CONNECTOR ON STRUT DISCONNECT PANEL. OPS CK REQUIRED.SDR UIEA2018070301324Connector · dirtyLT ENG BLEED OFF. REMOVED PANEL 431AL, INSPECTED, CLEANED CONNECTOR. MANUALLY OPENED/CLOSED PRSOV IAW AMM 36-11-00-501. ENGINE RUN PERFORMED BY AIR CREW. INSTALLED PNL 434AL, OPS NORMAL.SDR UIEA2018061101121Wire · broken'L ENG HPSOV" IN CRUISE AT FL280. FOUND WIRE BROKEN AWAY FROM TERMINAL RESECURED WIRE TO TERMINAL IAW SWPRM 20-20-00 PERFORMED FIM36-20 FT 804 NO FAULTS NOTED AT THIS TIME OPS CHECK GOOD.SDR UIEA2018060601047Wire · brokenL ENG HPSOV IN CRUISE AT FL280. LT ENG HPSOV DEFERRED. PROCEDURES C/W, FOUND WIRE BROKEN AWAY FROM TERMINAL. RESECURED WIRE TO TERMINAL IAW SWPM 20-20-00. PERFORMED FIM 36-20 FT 804 NO FAULTS NOTED AT THIS TIME. OPS CHECK GOOD.SDR UIEA201805250948Circuit Card · malfunctionedMOMENTARY RT ENGINE PRV ADVISORY MESSAGE DISPLAYED AFTER TAKEOFF. REPLACED THE BLEED AIR CONTROL CARD IAW AMM 36-11-16.SDR UIEA2018040400557Jumper · deterioratedDETERIORATED NR 2 PYLON PRSOV JUMPER WIRE. REPLACED THE JUMPER WIRE IAW AMM 20-10-21-964-001, REV 122, AND SWPM 20-20-00 AND 20-20-10, REV 66, CHECKED NORMAL.SDR UIEA2018011600078Terminal · dirtyPRV INDICATION VALVE POSITION FAULTY DURING OPS CHECK. CLEANED THE TERMINAL AT THE PRV D4156P CONNECTOR IAW AMM 36-00-30, INDICATIONS NORMAL.SDR UIEA2017121302401Wire · damagedL ENG BLEED LIGHT ON.(<DIV>REMOVED AND REPLACED WIRE W5310-20-18 IAW WDM 36-11-61 AND SWPM 20-10-11, 20-30-11 AND 20-61-11. OPS CHECK GOOD IAW AMM 36-11-07.</DIV>)SDR HALA2017112100282Wire · damagedLEFT ENGINE BLEED VALVE EICAS MESSAGE. RETURNED TO DEPARTURE. FOUND HPSOV TERM 1 CONNECTOR D4210P PIN 10 OPEN AND HPSOV TERM 2 TO D4210P OPEN. REPLACED THE TERMINAL 1 ON WIRE.SDR UIEA2017103102146Terminal · brokenDURING A TEST, THE LT PRV FAILED, TROUBLESHOT IAW WDM 36-11-61. FOUND WIRE W3312-007-18 BROKEN OFF AT TERMINAL. REPLACED THE TERMINAL TO WIRE STUD.SDR AALA20171024004Connector · looseAIRCRAFT EXPERIENCED CABIN PRESSURE FAULTS AFTER TAKE OFF, DIVERTED. NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TSM 36-11-00-810-810-A, BMC 2 FAULT MESSAGE RECEIVED. FOUND A LOOSE CONNECTOR ON THE NR 2 ENGINE. SECURED THE CONNSDR UIEA2017100201914Valve · inoperativeLEFT ENGINE DUCT PRESSURE FLUCTUATED DURING CLIMB. REMOVED AND REPLACED FAMV, VALVE HANGS UP. LT FAMV HAS OPEN CIRCUIT BETWEEN CONNECTORS D2378A PIN 8A AND V343 PIN 1 IAW AMM 36-11-16. FAMV REACTIVATED, CLEANED ELECTRICAL TERMINAL STRIPS. FAMV CHANGED. OSDR UIEA2017091801690Terminal · brokenLEFT ENGINE PRV, FOUND A BROKEN GROUND TERMINAL. REPAIRED THE WIRE AND REPLACED TERMINAL LUG AT PRV LT IAW SWPM 20-30-00. OPS CHECKED GOOD IAW 36-11-18-501.SDR P5CA2017091000320Washer · missingRIGHT ENGINE HPSOV EICAS MESSAGE. THE HPSOV WAS LOCKED CLOSED ON THE RIGHT ENGINE. PERFORMED AN HPSOV AND HPC TUBE LEAK TEST. NO AIR LEAK FOUND. CRANK HPSOV FUNCTION NORMAL, BUT FOUND HPSOV NR 2 TERMINAL LACK OF ONE WASHER, INSTALLED ONE WASHER COMPLETEDSDR JJBA20170824023Ground Wire · brokenAPU BLEED LEAK MESSAGE. APU WAS SHUTDOWN AT GATE. RAN QRH AND MESSAGE PERSISTED. FOUND BROKEN GROUND WIRE ON THERMAL SWITCH 34. R & R THE THERMAL SWITCH.SDR P5CA2017072400225Jumper · brokenFOUND GROUND JUMPER AND RETAINING CABLE BROKEN ON NR 1 ENGINE HPSOV IAW AMM TASK 70-50-00-912-001-H00, REV 12. REPLACED THE GROUND JUMPER AND RETAINING CABLE AND CONDITION CHECKED NORMAL.SDR UIEA2017071701235Connector · looseLEFT ENGINE OFF, BLEED OFF EICAS MESSAGES DISPLAYED NUMEROUS TIMES DURING DECENT, AT HIGH ALTITUDE AND DURING APPROACH BELOW 3000 FT. FOUND THE PRSOV CONNECTOR M22 LOOSE. TIGHTENED THE CONNECTOR AND CHECKED GOOD IAW AMM 36-11-04.SDR P5CA2017062500210Circuit Card · malfunctionedRIGHT ENGINE HPSOV, REPLACED AIR SUPPLY CARD IAW AMM 36-11-12-004-001/404-026. REPLACED HIGH PRESSURE CONTROLLER IAW AMM TASK 36-11-08-004-006-007/404-014-007. LEAK CHECK OK. ASBM BITE TEST OK. NO FAULT. PERFORMED OPS CHECKS FOR ENG RUN IAW AMM 71-00-00/50SDR REXA2017061800716Connector · defectiveTHRU 17,000 FT ON CLIMB OUT BOTH PACKS FAILED, AIRCRAFT DEPRESSURIZED. WE LEVELED THEN DESCENDED TO 10,000. WE COMPLETED THE QRH AND RETURNED TO CVG. DUE TO ANTI-ICE LEAK DETECTION CONTROLLER (AILC) DETECTING A BLEED LEAK IN BOTH A AND B SYSTEMS. THE BLEED AISDR FDEA201706071590Loop · wornLEVEL 3 AIR MANIFOLD NR 2 FAILED DURING CLIMBOUT. TROUBLESHOT THE NR 2 LOOP MANIFOLD IAW FIM 36-23-00-2, AND SSM 36-23-00. CHECKED RESISTANCE ON D1-17 AND FOUND GOOD. LOOP IS DISCONNECTED BETWEEN LOOP D1-17 AND LOOP D1-13 FOR TROUBLESHOOTING. FOUND D1-38 SDR UIEA2017012200099Connector · not seatedEICAS MESSAGE RT ENGINE HPSOV , QRH PERFORMED. FOUND THECONNECTOR D10984 NOT SEATED , INSPECTED THE CONNECTOR, RESEATED AND TIGHTENED OPS CHECKED IAW AMM 36-23-00.SDR HNAA2016120500375Connector · looseAT 60 KNOTS, HS VALVE 2 FAIL MESSAGE ILLUMINATED. ABORTED TAKEOFF, FOUND HS VALVE PRESSURE SWITCH CONNECTOR LOOSE. TIGHTENED THE CONNECTOR. PERFORMED HS VALVE FUNCTIONAL TEST. OPS CHECKED GOOD IAW MM 36-11-02-700-801 A/500. OK FOR SERVICE.SDR HALA2016110200401Connector · damagedNR 1 ENGINE BLEED PRESSURE REGULATOR VALVE CONNECTOR HAS LOOSE BACKSHELL. CONNECTOR REPLACED IAW ESPM 20-33-45 REV 32.00, AMM 36-11-52 REV 55.00, AMM 70-50-02 REV 55.00 AND 73-21-00 REV 55.00.SDR P5CA2016082500239Connector · dirtyRIGHT ENGINE HPSOV EICAS PERFORMED FIM 36-10, FT 833, WDM 36-11-62. CHECK RT ENGINE HPSOV POSITION SWITCH FUNCTION NORMAL, CLEAN HPC CONNECTOR; PERFORMED ENGINE RUN UP CHECK NORMAL. NO MSG IAW AMM 36-11-08, BITE AIR SUPPLY MODULE NO FAULT IAW AMM 36-23-00.SDR ASAA2016061817063Connector · looseNR 2 BLEED AIR VALVE INOPERATIVE. ACFT GROUNDED. PERFORMED FIM 36-10, TASK 805. FOUND CONNECTOR ON BLEED AIR REGULATOR LOOSE, NOT FULLY SECURED. RESECURED, REF AMM 36-11-03. ON ENGINE RUN NR 2 ENGINE BLEED, OPS NORMAL.SDR UIEA2016052100342Connector · dirtyRIGHT ENG BLEED OFF & RT PACK OFF, EICAS MSG INTERMITTENT DURING CLIMB. RAN BITE ON PNEUMATIC CONTROLLER FAULTED FAN AIR MOD VLV. INSPECTED VLV, CLEANED CONNECTOR & CYCLED VLV IAW AMM 36-11-16. PERFORMED BITE AGAIN, ALL CHECKED NORMAL.SDR REXA2016013000124Connector · dirtyEMERGENCY WAS DECLARED & FLIGHT DIVERTED. DURING CLIMB OUT, A RT 14TH DUCT WARNING MSG WAS OBTAINED. IAW QRH, RT 14TH DUCT WAS CLOSED, BUT MSG STAYED ON. ENG BROUGHT TO IDLE, MSG STAYED ON. DURING MEL PROCESS, FOUND RT 14TH DUCT WARNING WOULD NOT EXTINGUISSDR OZCA20160128020Connector · looseRIGHT BLEED LEAK LIGHT ILLUMINATED, JUST PRIOR TO SELECTING, TAKE OFF INHIBIT, ON TAKEOFF. INSPECTED BLEED DUCTS & LOOP IN RT FLAP COVE. NO LEAKS NOTED ON DUCTS & NO DAMAGE NOTED TO LOOP. FOUND LOOSE CONNECTION IN FLAP COVE LOOP. SECURED IAW MM. OPERATIONSDR UIEA2015121800774Connector · dirtyRIGHT PNEUMATIC ISOLATION VLV INOPERATIVE. TROUBLE SHOT RT PNEUMATIC ISOLATION VLV IAW WDM 36-11-21. CLEANED CONNECTOR IAW SWPM 20-60-01. OPERATIONS CHECKED GOOD IAW AMM 36-11-04.SDR P5CA2015111800175Connector · looseSTATUS MESSAGE FOR LT ENGINE, AIR SUPPLY BITE MODULE CHECKED IAW MM 36-23-00 WITH NO FAULTS, FOUND PRV PLUG LOOSE, RETIGHTENED IAW AMM 36-11-19, PRV OPS CHECKED IAW MM 36-11-18, PRV ACTUATOR LEAK TEST IAW MM 36-11-18, ALL OPS OK.SDR REXA2015083000843Connector · defectiveWHILE CLIMBING THROUGH 28000, RECEIVED A LT BLEED DUCT WARNING. IT PERSISTED FOR MORE THAN 30 SEC, WHICH LED TO AN UNPRESSURIZED LANDING. FOLLOWED NON-NORMAL CHECKLIST FOR LT BLEED DUCT 8-252 & UNPRESSURIZED LANDING 8-256. DEFERRED LT AIR LEAK DETECTION SYSSDR IPXA2015083092872Wire · brokenLT ENGINE HPSOV EICAS MESSAGE ILLUMINATED DURING CLIMB. LEFT BLEED LIGHT REMAINED ILLUMINATED AFTER QRH PROCEDURES COMPLIED WITH . FOUND WIRE BROKEN OFF TERMINAL L2 OF HPSOV V347. INSTALLED NEW TERMINAL IAW WIRING DIAGRAM 36-11-61 AND SWPM 36-11-61. DMP RESDR WX0A2015062272681Connector · dirtyAFTER TAKEOFF WITH APU RUNNING, TAIL COMPARTMENT TEMP HIGH MASTER CAUTION ILLUMINATED. COMPLIED WITH THE QRH PROCEDURE 21.4 & THE WARNING EXTINGUISHED AFTER TURNING BOTH AC SUPPLY SWITCHES TO HP BLEED, AT 10,000 FT APU WAS SHUT DOWN. FLIGHT CONTINUED AS DIRESDR ASMF201507009Wire Harness · damagedAIRCRAFT RETURNED TO PLATFORM, AFTER LT ENG START, THE BLEED DUCT PRESS INDICATOR SHOWED 5 PSI & IT WAS STABILIZED AT 10 PSI. PERFORMED REVISION, DETECTING THE ELEC HARNESS NR MW0311 DAMAGED. THE LT ELEC HARNESS NR MW0311, BLEED AIR REGULATOR & TUBE WERE REPSDR HALA2015040400056Wire · brokenAIR TURNBACK, EICAS MESSAGE, LT ENGINE BLEED VALVE AND OVERHEAD PANEL LT ENGINE BLEED LIGHT ILLUMINATTED DURING CRUISE AT FLT 340. FOUND AND REPAIRED BROKEN WIRE AT PRSOV VALVE TERMINAL 1, IAW STANDARD PRACTICE 12-00 RAN ENGINE AND OPS CHECKED IAW AMM 36-11-0SDR HALA2015040400051Wire · brokenEICAS MESSAGE, BLEED VALVE AND OVERHEAD PANEL LT ENGINE. BLEED LIGHT ILLUMINATED DURING CRUISE AT FLT 340, PRIOR TO ETOPS AIRSPACE ATB. REPAIRED BROKEN WIRE AT PRSOV VALVE TERMINAL 1, IAW STANDARD PRACTICE 12-00. RAN ENGINE AND OPS CHECKED IAW AMM 36-11-09.SDR N6WA2015040201Connector · looseRIGHT BLEED DUCT WARNING. FOUND LOOSE CONNECTOR, RETORQUED & SAFTIED CONNECTOR MT145 IAW AMM 20-51-00. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR RAIA201502140001Wire · brokenBLEED 1 LEAK MESSAGE, RAN CHECK LIST AND MESSAGES WENT AWAY, LOUD POP AT 8-9000 FT, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND BLEED 1 LEAK WAS POSTING WITH NO AIR, FOUND WIRES BROKEN IN AFT EQUIPMENT BAY, REPAIRED WIRES, OPS CHECK GOOD.SDR SIMA20150124006Wire · brokenCLIMBING THROUGH ICING CONDITION INDICATION OF BLEED 2 LEAK. ACFT BACK TO NORMAL AFTER RUNNING PROCEDURE IN AOM 1. PERFORMED PHYSICAL INSPECTION OF ALL NR 2 BLEED SYS JOINTS, NO LEAKS NOTED. AT GND ENG START CONNECTOR FOUND TEMP SENSOR WIRE W772-0004 BROKENSDR FDEA201501220261Connector · damaged25 MINUTES INTO FLIGHT, FL 280 ENGINE ANTI-ICE ON, WING TAIL OFF, LEVEL 3 AIR MANIFOLD 2 FAIL. QRH PROCEDURE FOLLOWED. REMOVED AND REPLACED C5-87 CONNECTOR IAW EA1-3622-T0314946 REV PS P2. PERFORMED TEST OF THE MANIFOLD FAILURE CONTROLLER AND PASSED IAW AMSDR HALA2014122400218Wire · damagedDURING TAKE OFF ROLL, BELOW 80 KTS RT ENGINE HPSOV EICAS CAME ON ENGINE HIGH STAGE BLEED VALVES. REPAIRED BROKEN TERMINAL LUG NR 3 ON ENGINE 2 AND UN-LOCKED VALVE & STOWED PIN, ACCOMPLISHED. OPS CHECK IAW AMM 36-11-07, OPS CHECK GOOD, OK FOR SERVICE, MIC SHESDR SWIA201439972Connector · dirtyDURING CRUISE, RECEIVED A LEFT ANTI-ICE DUCT WARNING MESSAGE. INTERROGATED MDC AND FOUND LT WING LOOP B FLAGGED. PERFORMED CHECK WITH BREAKOUT BOX, LOOP B TO BE 400 OHMS & FOUND CONNECTOR JB11 TO BE LOOSE. CLEANED CONNECTOR & PERFORMED OHM CHECK OF LOOP B T
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