JASC 3610
Service difficulty reports · 7,150
Reports filed under 3610 · Pneumatic Distribution 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 = '3610' 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 = '3610' 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 RAIA00311291Filter · dirty5251 PIT- BLEED 1 OVERTEMP ADVISORY. MAINTENANCE REMOVED AND REPLACED FAN AIR VALVE FILTER.SDR RAIA00311294O-Ring · wornSTL- BLEED 2 LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED O-RINGS LOWER FUSELAGE BLEED LINE.SDR UIEA200300068Duct · leakingON CLIMB-OUT, NR 3 ENGINE NACELLE TEMPERATURE WENT TO 6.0, LOOPS A/B. WITH POWER PULLED BACK TO CRUISE TEMPERATURE DROPPED TO 3.5 - 4.0. REMOVED AND REPLACED FORWARD 8TH STAGE DUCT ASSEMBLY AS PER MM 36, ACCOMPLISHED LEAK CHECK ON ABOVE IDLE RUN UP, ALL NORMSDR CA031119008Pump · inoperative(CAN) AT RT ENGINE RUN UP FOUND LIGHT PNEUMATIC SOURCE MALFUNCTION STAYING ON TILL 2000 RPM. AFTER TROUBLESHOOTING FOUND THE PUMP PN 442CW-6 WOULD NOT DELIVER RATED PNEUMATIC PRESSURE.SDR RAIA00311287Duct · cracked5700-STL- BLEED LEAK INDICATION NR 2. MAINTENANCE REMOVED AND REPLACED PRECOOLER DUCT.SDR IXXA0300071OHeat Exchanger · failedDURING CLIMB FROM KGSO TO KTOL NR 2 ENGINE PNEUMATIC SYSTEM OVERHEATED WITH LOW OR HIGH STAGE BLEED AND PACK FLOW AT MIN. CREW RETURNED TO KGSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER PER ALL APPLICABLE MANUALS. AIRCRAFTSDR DLM88030980Duct · leakingTAIL COMPARTMENT TEMP HI LIGHT CAME ON DURING CLIMB THRU FL250. FOUND HIGH PRESSURE DUCT LEAKING AT CLAMP. SECURED SAME.SDR QXEA200301398Seal · leakingSEA-ON FLIGHT NUMBER 2508, DURING CLIMB A WARNING MESSAGE APPEARED AND DISAPPEARED TO QUICKLY TO READ. THIS WAS FOLLOWED BY A RT BLEED DUCT CAUTION MESSAGE. PACK 2 ON THE SYNOPTIC PAGE CONTINUOUSLY FLICKERED BETWEEN GREEN AND WHITE. THE SHUTOFF VALVE REMAINSDR CA031114006Regulator · failed(CAN) DURING CLIMB, FLOW LIGHT (PRESS) COME ON, UNABLE TO STABILIZE, ACFT LANDED BACK. FOUND AFT GALLEY DOOR SEAL NOT PROPERLY SEATED. DURING SECOND CLIMB, SAME FLOW LIGHT CAME ON WITH BOTH AIRCRAFT PACKS BETWEEN 0-2 PSI ACFT LANDED BACK AND ACFT FERRIED TOSDR C1HA200392005Duct · damagedINFLIGHT NR 2 ENG FIRE LT, BELL ON HIGH EGT AND OIL TEMP CHECKLIST SHUTDOWN NR 2 ENG RETURN. DUMP FUEL, NR 2 ENG THROTTLE FELT STIFF, POSSIBLY BINDING. FUEL CUTOFF LEVER DIFFICULT TO MOVE. PERFORMED VISUAL INOP OF INLET, EXHAUST FOUND 13TH STAGE BLEED SADDLSDR MALA030477Duct · leakingDURING FLIGHT NR 3322, LT BLEED AIR LEAK LIGHT ILLUMINATED,LIGHT EXTINGUISHED AFTER CLOSING BLEED VALVE. AIR RETURN TO MEM. MAINTENANCE FOUND LOOSE CLAMP ON RUBBER DUCT P/N 9303688-100. TIGHTEN CLAMP,RUN ENGINES WITH BLEEDS ON NO FAULT FIND.LEAK CHECK IS GOSDR WRNA200300013Clamp · looseNR 1 ENG NACELLE TEMP READ 300+ ON CLIMB OUT. TEMP. REACTED TO THROTTLE MOVEMENT. DUMPED APPROX. 30K LBS. RETURNED TO FIELD, LANDING NORMAL. MAINTENANCE FOUND IP CHECK VALVE CLAMP OFF DUCT. REINSTALLED CLAMP IAW PROCESS MATERIAL SPEC. MANUAL 01-05-42. ENGINE SDR RAIA00309251Bleed Valve · stuck5316- STL- HIGH STAGE BLEED VALVE FAIL MESSAGE AND REPORTED SMOKE IN CABIN. MAINTENANCE REMOVED AND REPLACED HIGH STAGE VALVE. VALVE STUCK OPEN CAUSED SMOKE IN CABIN.SDR DLM88030860Duct · separatedLOUD NOISE AND VIBRATION IN FLOOR FROM AFT F/A SEAT ON BACK, STARTED WHEN POWER APPLIED DURING T/O RUN. SLIGHTLY MORE NOTICEABLE ON C/P SIDE DURING FLIGHT NOISE AND VIBRATION WOULD INCREASE AS POWER INCREASE AND DECREASE AS THROTTLE RETARDED. FOUND PNEUMATICSDR 03FDEA01595Controller · failedAPPROXIMATELY 2.45 HRS INTO FLIGHT, LEVEL AT 33,000 FT EXPERIENCED NR 3 MANIFOLD FAILURE LIGHT. ACCOMPLISHED RED TABS LIGHT WENT OUT. DIVERTED TO INDY. REMAINDER OF FLIGHT UNEVENTFUL. REMOVED AND REPLACED MANIFOLD FAIL CONTROLLER PER DC-10 M/M 36-23-01-2, SDR 03FDEA01556Precooler · crackedENG NR 1 STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF FROM PHX. ENG ANTI ICE WAS NOT ON. WITH REDUCTION OF POWER TO QUIET EPR LIGHT WENT OUT. LIGHT WAS ON FOR A TOTAL OF 15 SECONDS. SYSTEM TESTED GOOD. CONSULTED QRH. NO FURTHER ACTION TAKEN. FOUND LEAK ATSDR C1HA200395067Duct · leakingON TAKEOFF A RIGHT A/C PACK TRIP, FOLLOWED BY A RIGHT DUCT OVERHEAT, ABOUT A MINUTE LATER WITH AN ENG 3 STRUT OVERHEAT ILLUMINATING ABOUT 30 SEC LATER. COMPLIED COM PROCEDURE 2.36.9 WHICH CAUSED THE STRUT OVERHEAT LIGHT TO GO OUT AND ISOLATED THE LEAK ON REMOSDR COMA0360419Clamp · out of positionFLIGHT 9488 LEFT 14TH STAGE DUCT MESSAGE DURING T/O. REPOSITIONED 14TH STAGE SOV CLAMP.SDR P5CA0300938Duct · looseRT WING L/E OVERHEAT LIGHT CAME ON TAXI OUT. REMAINED ON WHEN ISOLATED. FOUND LOOSE DUCT LEADING TO NR 3 LEADING EDGE FLAP MOTOR. TIGHTENED AS REQUIRED SYS LEAK CK GOOD IAW MM 27-81-00 PG 207.SDR RAIA00309254O-Ring · worn5663-STL=- ENGINE NR 2 BLEED LEAK MESSAGE. MAINTENANCE PLACED ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARING DMI BY REPLACING O-RING AT BLEED COUPLING IN CARGO BAY.SDR SWAA031993Boot · leakingAIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AND REPLACED PNEU BLEED AIR DUCT BOOT AT KEELBEAM AND THREE BODY DRAINS, TIGHTENED CLAMPS AND REMOVED AND REPLACED WATER SEPARATOR SEALS PER MM.SDR 03FDEA01452Clamp · leakingON CLIMBOUT, FROM MEM NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH. LIGHT EXTINGUISHED. FOUND CLAMP BETWEEN SHUTOFF VALVE AND PRECOOLER LEAKING. REMOVED AND REPOSITIONED CLAMP IAW SMP PERFORMED ENGINE IAW JRH. LEAK CK. GOOD. RE-INSTALL LOSDR 03FDEA01437Clamp · looseWHILE DEPARTING LAS, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED FOR (TEMP 37C) APPROX 15 SECONDS DURING INTIAL TAKE-OFF/ CLIMBOUT AT 180 KTS PRIOR TO FLAP RETRACTION, THEN EXTINGUISHED. SYSTEM TESTED OK REFERRED TO QRH AND CONTINUED. FOUND CLAMPS ON ENGINE BSDR ASOA03409Bracket · crackedDURING A HANGAR CHECK IN BTR, THE LT ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 IAW ASA SDR QXEA200301045Valve · failedPDX- ON FLIGHT 2147 AFTER ENGINE START WHEN SELECTING BLEEDS ON, HAD VERY LIGHT SMOKE ON FLIGHT DECK. SMOKE CLEARED OUT IN 2 TO 5 MINUTES. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE P2.5/PD AIR SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVSDR UIEA200300053Relief Valve · failedLIM-MIA - DURING CLIMB AT FL250, NR 4 NACELLE TEMP WENT OT 8.0 WITH A FIRE BELL AND LIGHT IN NR 4 FIRE SWITCH. WHEN NR 4 THRUST LEVER WAS RETARDED TO IDLE, THE FIRE LIGHT WENT OUT AND THE NACELLE TEMP RETURNED TO NORMAL 2.0. CLOSED NR 4 BLEED VALVE AND ADVANSDR DHL2003752005Flex Line · leakingENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF AT MAX THRUST. THRUST REDUCTION TO CLIMB LIGHT EXTINGUISHED. PERFORMED ABNORMAL PROCEDURE OVERHEAT LIGHT REMAIN EXTINGUISHED. REMOVED AND REPLACED 13TH STAGE FLEX LINE P/N: BACH7D0161DL IAW B727 M/MSDR AALA20030907Clamp · looseAFTER TAKEOFF SMOKE OR BURNING SMELL IN CABIN DETECTED. CREW DECLARED AN EMERGENCY AND RETURNED TO BOG WITHOUT FURTHER INCIDENT. TIGHTENED SEVERAL PNEUMATIC DUCT CLAMPS. SWAPPED MINIMUM EQUIPMENT BAY DETECTOR WITH ZONE 125 DETECTOR. HISTORY OF HOT FLOORS ANSDR MWEA030330Clamp · leakingTAIL COMPARTMENT TEMPERATURE LIGHT CAME ON. REMOVED AND REPLACED AUGMENTATION VALVE OUTBOARD DUCT CLAMPS.SDR 03FDEA01384Precooler · failedMOMENTARY INDICATION OF NR 2 BLEED MANF FAILURE. (RED LIGHT ON OVERHEAD AND RED LINE ON NR 2 BLEED MANF SYNOPTIC). ASC DEPRESSURIZED NR 2 MANF. QRH PROCEDURES ACCOMPLISHED. PHONE PATCH W/MEM GOC ADVISED TO CONTINUE TO NANDI. PERFORMED DECAY CHECK AND DECASDR MWEA030329Periseal · leakingTAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AND STAYED ON UNTIL QRH WAS USED. NO LEAKS OBVIOUS. CLEANED TAIL TEMP SENSOR DOORS AND PROBES. FURTHER MAINTENANCE REMOVED AND REPLACED LEAKING PERI SEALS ON LEFT PNEUMATIC DUCT AND PERFORMED ADJUSTMENT TEST OF THE LESDR MEX2003384Clamp · defectiveFLT 266 - MEX-REX - AIRCRAFT ARRIVED WITH CAPTAIN REORTING THAT AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON. THE AUGMENTATION VALVE AND REGULATOR VALVE DUCTS CLAMPS WERE REPLACED IAW MM 36-10-00 AND TEMPERATURE SENSORS WERE CLEANED IAW MM 36-20-02SDR AALA20030891Shutoff Valve · looseRT ENGINE HPSOV EICAS MSG APPEARED IN FLIGHT, COMPLIED WITH QRH PROCEDURE. PLACARDED RT ENGINE HI STAGE HPSOV INOPERATIVE PER MEL. VALVE SECURED CLOSED PER MPM 36-02. ENT IN MIC SHEET AUTH 8 463DC. SECURED LOOSE SENSE LINES AT HP CONTROLLER CLEANED AND LUBSDR UIEA200300045Relief Valve · defectiveMIP/POS-AIR TURNBACK, AFTER T/O AND DURING CLIMB, NR 4 ENGINE FIRE WARNING CAME ON. WHEN NR 4 THROTTLE WAS CLOSED THE TEMP WENT BACK TO NORMAL. THROTTLE WAS ADVANCED AGAIN THE TEMP STARTED TO GO UP. NOTICED HIGH STAGE BLEED VALVE LIGHT, ON AND OFF. CLOSED NR 4SDR P5CA0300907Valve · malfunctionedNR 3 ENG PYLON VLV WOULD NOT OPEN. REMOVED AND REPLACED PYLON VLV IAW 36-11-00, LEAK CHECK OK.SDR 03FDEA01243Bracket · cracked233 ENG HP TURBINE COOLING PNEUMATIC DUCT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW AMM 70-00-00-2.SDR 2003F00517Regulator · stuckSAL - FLT 581 - DURING CRUISE, ENGINE NR 1 BLEED VALVE REMAINS CLOSED AND THE ENGINE NR 2 PRECOOLER REACHED THE LIMITS IN A SINGLE BLEED OPERATION. THE AIRCRAFT WAS DEVIATED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL, TECHS REPLACED THE PRESSURE RESDR 03FDEA01229Manifold · failedABOUT 1 50 2FO FLT AT FL370 LEVEL 3 23 MANIFOLD FAIL OCCURRED. SECURED 232 ENG TO IDLE PER LIST WITH 232 BLEED OFF DIVERTED KDEN. AACN RELEASED FOR SERVICE PER MEL 2 FCDL 36-23-01-02 CATEGORY 3 AC EXPIRATION 3A 18AUG 03 FACT: CHECKED ELEMENTS_D1-50, D1-SDR C8GA20030019Clamp · failedAFTER TAKEOFF, NR 3 BLEED AIR TRIP LIGHT ON, FOLLOWED BY NR 3 ENGINE STRUT OVERHEAT LIGHT ON. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST, AIR TURN BACK AND AC LANDED WITHOUT INCIDENT. A/C WAS INSPECTED AND FOUND CLAMP ON NR 3 BLEED RIGHT SIDE AIR STAIRS AREA SDR DXTA200300080Line · chafedWHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFED THROUGH, AND FLAP RETRACT LINE CHAFED BEYOND LIMITS. - REMOVED AND REPLACED DEFECTIVE HYDRAULIC AND PNEUMATIC LINES IAW CESSDR A6WA200340117Warning Light · illuminatedLEFT 14TH STAGE BLEED AIR DUCT WARNING INFLIGHT COMPLIED WITH QRH MESSAGE WENT OUT AND THEN CAME BACK 10 MINUTES. WITH ENGINE SHUTDOWN MESSAGE PERSISTED ON GROUND. REMOVED AND REPLACED LT PYLON SENSING ELEMENT A59WK IAW AMM 36-21-04. OPS CHECK GOOD. (M)SDR A6WA200340116Warning Light · illuminatedRECEIVED LT 14TH STAGE DUCT MESSAGE, COMPLIED WITH QRH. MESSAGE CLEARED WITH THRUST LEVER RETARDED. INSPECTED LEFT 14TH STAGE DUCT BLEED AIR SYSTEM IAW MM 36-12-04. NO FAULTS FOUND. RAN ENGINES TO POWER, NO FAULTS NOTED. OK FOR SERVICE.SDR UIEA200300042Seal · wornDFW/ANC AIR TURNBACK, AT FL 31 CABIN ALT WENT TO 10 WITH DIFFERENTIAL AT 6.8 AND UNABLE TO PREVENT CABIN FROM CLIMBING 50-100 FPM. AIRCRAFT DESCENDED TO FL 29.0 THEN FL 25.0. MAX DIFFERENTIAL THAT COULD BE HELD WAS 6.5 AND CABIN CONTINUED TO CLIMB 50-100 FPMSDR QXEA200300927Valve · malfunctionedBOI- ON FLIGHT 2196 AFTER ENGINE START AND THE BLEEDS TURNED ON, AIRCRAFT FILLED WITH SMOKE. REMOVED AND REPLACED NR 2 ENGINE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2003F00552Hose · leakingUNIDENTIFIABLE ODOR IN THE CABIN WHEN BLEEDS ARE ON. REMOVED AND REPLACED LEFT ENGINE FUEL PURGE PNEUMATIC HOSE. LEAK CHECK GOOD. (M)SDR 2003FA0000716Pump · wornAVIONICS PERSONNEL FOUND INSTRUMENT AIR PRESSURE LOW ON GROUND RUN UP. ON FURTHER INVESTIGATION FOUND VANES WORN ON PUMP. RECOMMEND PUTTING DIFFERENT TYPE OF VANES IN PUMP TO LAST LONGER.SDR USAASB03120Control Valve · failedON SLOW DESCENT TO PHL, FROM FL370 TO FL350, THE NR 1 ENGINE BLEED TRIPPED FOLLOWED BY A PACK TRIP. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED TO PHL UNPRESSURIZED. BLEED RESET AFTER COOLING PERIOD PER QUICK REF HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUTSDR 2003UALA00585Warning System · activatedRETURNED TO FIELD DUE TO NR 2 BLEED INOPERATIVE ECAM MESSAGE. AIRCRAFT RETURNED DUE TO NON-ICING RESTRICTIONS, NR 2 PRV REPLACED.SDR USAASB03115Clamp · looseON CLIMB-OUT FROM PIT, AT FL170, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE TIGHTENED A LOOSE PNEUMASDR 03FDEA01119Regulator · malfunctionedSMOKE OR FUMES IN COCKPIT CLIMBING THRU FL 180 NO INDICATION ON S/O PANEL EXCEPT VERY HIGH DUCT PRESSURE L AND R ABOVE 65 PSI. BLEED SWAPPED TO 2 AND 3 LOWERED PRESSURE TO NORMAL RANGE (BETWEEN 30 40 PSI). REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE US
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