JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, 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 = '2910' 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 = '2910' 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 2003FA0000708Line · chafedLINE CHAFED ON TOP OF SPOILER SHUTOFF VALVE CAUSING HYDRAULIC LEAK. REPLACE LINE AND BLED BRAKE SYSTEM. TIME ON PART: 1194.9 HOURS AND 1099 LANDINGS. INSTALLED CLAMPS WITH SPACING DISTANCE TO PREVENT RECURRANCE. MAY NEED TO INSTALL ADDITIONAL CLAMPS TO ENSSDR CA030708013Line · ruptured(CAN) THE PILOT REPORTED A NOISE (FROM AN UNLOADED HYDRAULIC PUMP) FOLLOWED BY THE ODOR OF HYD FLUID. HYDRAULIC PRESSURE ON SYSTEM NUMBER 2 DROPPED TO ZERO. THE PILOT INITIATED AN UNSCHEDULED LANDINGTO INVESTIGATE THE PROBLEM. AFTER LANDING A CHAFED HYD LINESDR UPS03540933Line · failedON CLIMBOUT FROM CIA LT HYD SYS FAILED. DIVERTED TO CGN. EMERGENCY DECLARED. LANDED W/O INCIDENT. A/C TOWED TO RAMP. REMOVED AND REPLACED TUBE ASSY HYD PRESSURE ON LT ENG STRUT. REMOVED AND REPLACED TUBE ASSY CLAMPS IAW MM 20-10-11-4 & IAW IPC 29-11-61-0SDR XNOA01137B-Nut · looseLOST GREEN HYD FLUID AND PRESSURE. MOTOR DUMPED FUEL TO MAX LANDING AND RETURNED TO SJU. ACTION TAKEN: TIGHTENED LOOSE AND LEAKING B-NUT ON LEFT MLG DRAG BRACE CYLINDER. LEAK CHECK GOOD AND SERVICED GREEN HYD IAW A300 MM 12-12-29.SDR UPS03440923Hydraulic System · failedATB - NR 2 HYD SYSTEM FAILURE. REMOVED & REPLACED NR 2 EDP AS REQUIRED DUE TO OVERHEAT IAW MM 29-11-05. OPS & LEAK CHECK REQUIRED. RAN NR 2 ENG FOR LEAK CHECK OF NR 2 HYD (EDP) PUMP GROUND CK'S NORMAL. OK FOR SERVICE. HYD PRESSURE CHECK NORMAL.SDR AALA20030706Line · leakingAPPROX 5 MINUTES INTO CRUISE ALTITUDE, 37,000 FT, AN EICAS MESSAGE APPEARED INDICATING LOW QUANTITY IN THE CENTER HYDRAULIC SYSTEM. AT THAT TIME THE QUANTITY INDICATED .57 AND CONTINUED TO DECREASE TO .28. THE GEAR AND FLAPS WERE DEPLOYED USING ALTERNATE PROSDR USAABB030106Line · rupturedAFTER TAKEOFF FROM CLT, CREW COULD NOT GET THE LANDING GEAR TO RETRACT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT GEAR TILT ACTUATOR FLEX LINE, WHICH HAD RUPTURED. (M)SDR QXEA200300779Hydraulic Line · crackedEUG- DURING TAXI LOST ALL HYDRAULIC FLUID ON NR 2 SIDE. FOUND HYDRAULIC LINE CRACKED. REPLACED LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2003F00542Hydraulic Line · damagedON TAKEOFF, OUT OF SDF AT GEAR ROTATION LOST SYS 'A' HYD FLUID, SHUT PUMPS OFF ACCOMPLISHED ABNORMAL CHECKLIST. REMOVED AND REPLACED HOSE ASSEMBLY NR 2 ENGINE P/N 10-60563-40, NO METAL FOUND IN CASE DRAIN FILTERS OR SUPPLY FILTERS REPLACED NR 1 AND NR 2 HYDRASDR DL757030593Hydraulic Line · crackedSLOW HYD LEAKING LEFT SYSTEM OVER 3 HRS QTY WENT FROM NORMAL TO 0.24 AT LANDING. FOUND SYS 1 RUDDER RET LINE LEAKING IN VERT FIN 2 BAYS ABOVE STAB COMPARTMENT REPLACED WITH APPROVED FLEX LINE LEAK, OPS CHECK NORMAL.SDR AALA20030690B-Nut · looseIAD - FLT 1088 - EN ROUTE BNA-LGA, LOST RIGHT HYDRAULIC PRESSURE IN FLIGHT, USED ALTERNATE GEAR EXTENSION. LANDED IAD WITHOUT INCIDENT. SECURED RIGHT WHEEL WELL HYDRAULIC B-NUTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AWXA200300733Line · chafedON DECENT, EN ROUTE RECEIVED ECAM MESSAGE GREEN HYDRAULIC SYSTEM LOW QUANTITY; DECLARED EMERGENCY, NO NOSE WHEEL STEERING, AIRCRAFT TOWED OFF RUNWAY. MAINTENANCE FOUND GREEN SYSTEM HYDRAULIC PRESSURE LINE CHAFED AND LEAKING IN LT WHEEL WELL ON AFT SPAR BETWEENSDR CA030620005Valve · failed(CAN) DURING APPROACH INTO YELLOW, HYD SYSTEM FAILURE. MANUAL GEAR EXTENTION CARRIED OUTAND A/C LANDED WITH OUT DIFFICULTY. LT GEAR BLOW BACK VALVE FOUND FAILED (CAP BURST), REPLACED IAW MM AND A/C RETURNED TO SERVICESDR CA030620006Line · misinstalled(CAN) FLT CREW REPORTED THAT NLG UNLOCKED BUT FAILED TO RETRACT. SUBSEQUENT GEAR SELECTS WERE UNSUCCESSFUL UNTIL SPEED REDUCED. GEAR DID RETRACT AT 160 KNOTS IAS, VERY SLOW, RETURN TO YEG. THIS ANOMALY DATES BACK TO 06/4/03, WHEN SKI ACTUATOR ROBBED TO SERVSDR 8564188Fitting · leakingLANDING GEAR WOULD NOT EXTEND ELECTRICALLY. LANDING GEAR WAS EXTENDED USING HAND PUMP. UPON INSPECTION, MAINTENANCE DISCOVERED FLUID LEAKING FROM THE SWAGE FITTING ON THE LT MAIN LANDING GEAR RETRACT ACTUATOR HOSE. SUSPECT CAUSE WAS FLEX FATIGUE. MAINTENANCE PSDR PCAA0306078O-Ring · failedFLIGHT 3867 FROM SYR TO LGA ON APPROACH TO LGA CREW NOTICED NR 2 HYDRAULIC ISOLATION VALVE CONTENTS WERE CLOSE TO ZERO. CREW DECLARED AN EMERGENCY. PUT THE GEAR DOWN MANUALLY AND LANDED WITHOUT FURTHER INCIDENT. LGA MECHANIC INSPECTED AND FOUND O-RING ON ONSDR MEX2003236Packing · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT WITH 1 QUART OF OIL IN ENGINE NR 2. DURING REVISION WAS DETECTED LEAK IN RIGHT HYDRAULIC PUMP. THE RIGHT HYDRAULIC PUMP PACKING WAS REPLACED IAW MM. DURING OVERNIGHT SERVICE RIGHT HYDRAULIC PUMP WAS REPLACED IAW 29-11-40SDR CA030620001Line · cracked(CAN) A HYDRAULIC LINE FROM THE NR 2 HYD SYS THAT FEEDS THE RUDDER PRESSURE REGULATOR DEVELOPED A HAIRLINE CRACK IN THE TAIL SECTION. . THE NR 2 SYSTEM HYDRAULIC QUANTITY DEPLETED TO BELOW MINIMUM. AN EMERGENCY LANDING GEAR EXTENSION WAS CARRIED OUT AND THE ASDR 2003FA0000654Line · crackedAIRCRAFT CAME BACK FROM A TRIP LEAKING HYDRAULIC FLUID FROM THE NOSE GEAR AREA. FOUND LINE PN 6517105-39 CRACKED AND LEAKING HYDRAULIC FLUID.SDR UPS03840852Line · rupturedAFTER LANDING LOST ALL HYDRAULIC PRESSURE AND QUANTITY. AIR BRAKE USED TO STOP AIRCRAFT. FOUND RT MLG BOGIE TRIM CYLINDER PRESSURE LINE RUPTURED, REPLACED SAME. SERVICED RESERVOIR, BLED HYDRAULIC PUMPS, OPERATED ALL HYDRAULIC POWERED SYTEMS TO REMOVE AIR FRSDR HEEA087878Line · corrodedHYDRAULIC LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART.SDR HEEA087877Line · corrodedHYDRAULIC LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART.SDR HEEA087876Line · corrodedHYD LINE HAS DEVELOPMENT OF CORROSION UNDER SLEEVE DUE TO DISSIMILAR METALS USED DURING MANUFACTURE PROCESS. REPLACED WITH SERVICEABLE PART.SDR HEEA087466Hose · corrodedHYD SYSTEM HOSE HAS CORROSION AT SLEEVE NEAR HOSE. REPLACED HOSE.SDR ARWA20030604Line · leakingLOSS OF HYDRAULIC FLUID DOWN TO STAND-PIPE. LOSS OF HYDRAULIC CHECK LIST COMPLETED. INSPECTED NR 3 PYLON FOR EVIDENCE OF HYDRAULIC LEAK, FOUND RIGID LINE DAMAGED INSIDE PYLON AREA; REMOVED AND REPLACED RIGID LINE ASSEMBLY AS REQUIRED IAW MM 20-12-0; OPERATIOSDR UPS03240846Swivel · failedA-SYSTEM HYDRAULIC LOSS AFTER T/O DURING FLAP RETRACTION. AIR TURN BACK TO SDF. ALL CKLISTS ACCOMPLISHED. FOUND NR 4 SLAT ACTUATOR SWIVEL SPRING RETAINER BLOWOUT AND O-RINGS CAUSING MASSIVE LEAKAGE. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM 27-81-01. SDR CA030627012Line · ruptured(CAN) DURING TAXI, CREW APPLIED THE BRAKES AND OBSERVED LOSS OF 'B' SYSTEM HYDRAULIC PRESSURE AND HYD BRAKE PRESSURE. AIRCRAFT STOPPED AND MAINTENANCE TOWED AIRCRAFT BACK TO MAINTENANCE FACILITY. MAINTENANCE OBSERVED LEAKAGE FROM THE RT ELEVATOR PCU. THE SDR HEEA087138Module · cloggedMODULE RETURN FILTER CLOGGING. TO BE SENT TO VENDOR FOR REPAIR.SDR HEEA087137Module · cloggedRETURN FILTER CLOGGING. TO BE SENT TO VENDOR FOR REPAIR.SDR MEX2003220Bypass Valve · leakingFLT 494 - MID-MEX - AIRCRAFT RETURN TO GATE, HYDRAULIC LEAK AT LEFT COMPARTMENT RESERVOIR AND DURING ENGINES STARTING THE 'LIGHT RUDDER PCU' EICAS STATUS MESSAGE TURN ON. THE LEFT SLATS BYPASS VALVE WAS REPLACED IAW MM, TASK CARD 27-81-09-024-001 AND 27-81-09SDR HEEA087183Line · chafedHYD RESERVOIR RETURN LINE CHAFED. SCRAPPED.SDR 2003FA0000718Relay · shortedWHILE PERFORMING GEAR CHECK, THE HYDRAULIC PRESSURE WOULD NOT BUILD UP. FOUND RELAY SHORTED OUT. RECOMMEND INSTALLING AN INLINE FUSE IN THE SYSTEM. WHEN THIS RELAY FAILS, THE RELAY AND DIODES BOARD ALSO FAILS.SDR MALA030297Isolation Valve · failedDURING CRUISE ON FLIGHT 3548 HYDRAULIC GREEN SYSTEM HI TEMP LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED GREEN SYSTEM ISOLATION VALVE P/N OFF HTE9531-101, P/N ON HTE9531-3, S/N FRTR010AW. AMM REF 29-36-00-1 RAN ENGINE NR 3 EDP FOR SDR AUS20030570Line · leaking(AUS) YELLOW HYDRAULIC SYSTEM QUANTITY LOW. INVESTIGATION FOUND PIPELEAKING FROM SWAGE ADJACENT TO T' PIECE CONNECTION FOR THE YELLOW SYSTEM PRESSURE SUPPLY TO THE HP MANIFOLD.SDR QXEA200300679Hydraulic Line · brokenSEA-ON FLIGHT NUMBER 2065, AFTER GEAR EXTENSION, NR 2 HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. NR 2 ENGINE HYDRAULIC PUMP AND NR 2 RUDDER HYDRAULIC CAUTION LIGHTS ILLUMINATED. FOUND BROKEN WIRE FOR NOSE GEAR EXTENSION LINE. INSTALLED NEW NOSE GEAR EXTESDR MALA030293Warning Light · illuminatedDURING CLIMBOUT OF FLIGHT 3478, FROM DTW GREEN HYDRAULIC HI TEMP CAME ON FOLLOWED QRH. AIR RETURN TO DTW. MAINTENANCE GROUND RAN PRESSURIZED HYDRAULIC ON GROUND FOR 1 HOUR AND 20 MINUTES AT NO TIME DID THE GREEN HI TEMP LIGHT ILLUMINATE. INSPECTED GREEN SYSSDR IU62003F00023Housing · brokenVALVE BODY IS BROKEN IN HALF. METAL FATIGUE. MAKE BODY STRONGER. (NR 177979)SDR C2XA03IA059Line · leakingBAN- FLIGHT 2623 (IAH-DAY), THE CREW NOTED THAT HYDRAULIC NR 1 LOW QTY MESSAGE APPEARED ON EICAS WITH HYDRAULIC LEAK. (NOTE: THE FLIGHT WAS DIVERTED TO BNA ). BNA- MAINTENANCE REMOVED AND REPLACED THE SUCTION AND PRESSURE HYDRAULIC LINES AT THE ENGINE DRIVSDR C2XA03IA058Line · leakingTHE CREW NOTED THAT HYDRAULIC NR 1 LOW QTY MESSAGE APPEARED ON EICAS WITH HYDRAULIC LEAK. (NOTE: THE FLIGHT WAS DIVERTED TO BNA. MAINTENANCE REMOVED AND REPLACED THE SUCTION AND PRESSURE HYDRAULIC LINES AT THE ENGINE DRIVEN HYDRAULIC PUMP, NR 1 ENGINE, SERVISDR DL73K030501Tube · crackedSLOW LEAK IN FLT RESULTED IN A-SYSTEM RESERVOIR GOING TO ZERO AND SUBSEQUENT LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 1 ENG TO PYLON PRESSURE LINE CRACKED AT BEND. REPLACED HYD LINE. RAN ENGINES/FLIGHT CONTROLS, NO FURTHER LEAKS NOTED.SDR MEX2003194Valve · failedDURING TRANSIT CHECK, DETECTED HYDRAULIC LEAK AT RIGHT MLG, HYDRAULIC TEST WAS ACCOMPLISHED DETECTING LEAK AT SHUTOFF AND SPOILER DEPRESSURIZATION VALVE. VALVE WAS REPLACED IAW MM 29-10-26, ALL TESTS CORRECT. (M)SDR CA030609004Pressure Switch · failed(CAN) AIRCRAFT FLEW UNEVENTFUL. UPON TAKEOFF, THE CREW SELECTED GEAR UP. THE NOSE AND RT MAIN GEAR BEGAN TO RETRACT. THE LT MAIN GEAR REMAINED DOWN AND LOCKED. CREW SELECTED GEAR DOWN AND RETURNED TO 3 GREEN. ONCE AGAIN, CREW SELECTED GEAR UP. GEAR DID NOT MSDR CA030605009Tube · leaking(CAN) ON FINAL, CREW SELECTED GEAR DOWN, GEAR UNLOCKED AND FAILED TO EXTEND, NO HYDRAULIC PRESSURE, AIRCRAFT DIVERTED TO QUEBEC AIRPORT, GEAR EMERGENCY EXTENDED, AIRCRAFT LANDED WITH NO FURTHER PROBLEM.FOUND LT ENGINE HYDRAULIC PUMP FUSELAGE LINE HAD A CHAFED SDR A6WA200340075Line · leakingWHILE TAXIING AIRCRAFT LOST NR 3 HYDRAULIC. FLUID LEAKING AROUND NOSE LANDING GEAR. REMOVED AND REPLACED RIGHT INBOARD LINE IN NOSE COMPARTMENT. (M)SDR DXTA200300037O-Ring · failedON LANDING ROLL, HAD A COMPLETE LOSS OF SYSTEM HYD FLUID AND EMERGENCY BRAKE WAS USED, AIRCRAFT HYDROPLANED BUT STOPPED SAFELY, NO VISIBLE DAMAGE TO AIRCRAFT. REPLACED ORING PLUG, ON "A" HYDRAULIC MANIFOLD, AND OPERATIONALLY TESTED, BLED SYSTEM AND LEAK CHECKSDR QXEA0300651Hydraulic Line · chafedSEA-SUP-ON FLIGHT NUMBER 2328, AFTER TAKEOFF NR 2 HYDRAULIC SYSTEM FAILED. NOSE WHEEL CAME UP THE REST OF THE GEAR DID NOT. FLIGHT RETURNED TO FIELD, CREW DID ALTERNATE GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED FLEX LINE SDR 03FDEA00813Line · leakingDURING CRUISE, ECAM SIGNALED GREEN HYD RSVR LO LEVEL. GREEN HYD QUANTITY GAUGE AT RED DOT. FOLLOWED ECAM AND QRH PROCEDURES FOR HYD RSVR LO LEVEL, HYD SYS LO PR, AND L/G EXTENDED USING ALTERNATE GEAR EXTENSION. PERFORMED LEAK CHECK FOUND HYD FLUID LEAKINSDR SWIA200312037Line · leakingON A 10 MILE FINAL TO RUNWAY 26 - HYD 2B LOW PRESS MESSAGE APPEARED. HYD 2B RESERVOIR APPEARS TO BE EMPTY. REMOVED AND REPLACED HYDRAULIC LINE ON NR 2 HYDRAULIC SYSTEM SERVICE PORT IAW CL600 20-22-00. OPS CHECK GOOD. RESERVICED HYDRAULIC SYSTEM RESERVOIR ISDR 2003F00387Valve · malfunctionedUNABLE TO GET NORMAL LANDING GEAR EXTENSION. PERFORMED EMERGENCY LANDING GEAR EXTENSION. T/S LANDING GEAR SYSTEM INDICATED A MALFUNCTION OF THE LANDING EAR HYDRAULIC SELECTOR VALVE LOCATED IN THE MAIN WHEEL WELL. REPLACED LANDING GEAR HYDRAULIC SELECTOR/DUSDR 2003F00386Valve · malfunctionedUNABLE TO GET NORMAL LANDING GEAR EXTENSION. PERFORMED EMERGENCY LANDING GEAR EXTENSION. T/S LANDING GEAR SYSTEM INDICATED A MALFUNCTION OF THE LANDING EAR HYDRAULIC SELECTOR VALVE LOCATED IN THE MAIN WHEEL WELL. REPLACED LANDING GEAR HYDRAULIC SELECTOR/DU
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