JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, newest first.
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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 2009FA0000005Hose · burstRT NLG DOOR ACTUATOR HOSE FAILED CAUSING COMPLETE HYD FLUID LOSS . RESULTING IN LT MAIN GEAR NOT ABLE TO BE FULLY EXTENDED TO DOWN AND LOCKED POSITION. ACFT MADE EMERGENCY LANDING WITH LT MAIN GEAR PARTIALLY EXTENDED. MINOR DAMAGE. FAILED HOSE APPEARS TO BESDR ANCF200800031Ring · cutPILOT REPORT: HYD SYS LEAK DURING CRUISE AT FL 390 AFTER 1 HR AND 30 MIN FLIGHT TIME. IN RT ENGINE: ON DUMPER HYD PULSATION (GREEN SYSTEM) THE SEAL WAS FOUND BROKEN PROCEDURES IAW TSM 29-11-00-810-820 WERE PERFORMED WITH ELEC PUMPS. IAW AMM 29-11-54-400-802 SDR ASMF 20081204Line · leakingDURING TRANSIT CHECK, A HYD LEAK ON THE LT WHEEL WELL LANDING GEAR WAS DETECTED. MX REPLACED AND TESTED THE HYDRAULIC LINE IAW AMM 20-50-00, ALL CORRECT.SDR DXTA2008122303416Hydraulic System · lowAT FL350 WE GOT THE RT HYD LEVEL LOW CAS MESSAGE. DID THE EMERGENCY GEAR EXTENSION PER CHECK LIST.SDR CA081222003Hose · failed(CAN) ON DEPARTURE FROM YVR, WHEN GEAR SELECTED UP, HYDRAULIC `A` SYSTEM FAILED. HYDRAULIC QUANTITY INDICATION 0, HYDRAULIC PRESSURE INDICATION 0. CREW EXTENDED GEAR IN ACCORDANCE WITH FLIGHT MANUAL PROCEDURES. THE AIRCRAFT RETURNED TO YVR, STOPPED ON THE RSDR CA081222001Circuit Breaker · unserviceable(CAN) THE FLIGHT CREW REPORTED THE 35 AMP HYDRAULIC PUMP CIRCUIT BREAKER POPPED. THEY ELECTED TO RETURN TO BASE AND USED HYDRAULIC HAND PUMP FOR BRAKE OPS. MX TROUBLESHOT THE SYSTEM, REPLACED 35 AMP CIRCUIT BREAKER, GROUND TESTED THE SYSTEM, AND RETURNED THESDR YENA200812180128Drain Line · leakingFLT NR 300, LGB-IAD, GREEN HYD SYS FAIL IN FLIGHT. FOUND CASE DRAIN LINE NR 1 ENG PYLON LEAKING. REPLACED CASE DRAIN LINE, OPS AND LEAK CHECK GOOD. REPLACED NR 1 ENG DRIVEN PUMP AS PER AMM 29-11-40 PRECAUTIONARY, OPS CHECK OK.SDR MALA080223Pdu · malfunctioned"AFTER T/O SELECTED GEAR UP AND HYDRAULIC CAUTION LIGHT ILLUMINATED. COMPLETED MEMORY ITEMS THEN COMPLETED AFTER T/O CHECK. COMPLETED EMERGENCY/NON-NORMAL CHECKLIST HYDRAULIC PROC 2. RETURNED TO TRI. DECLARED EMERGENCY AND RETURNED TO GATE. FLAPS REMAINEDSDR IXXA080037OElbow · brokenDURING CLIMB FROM KMCC, THE CREW NOTICED A LOSS OF HYDRAULIC QUANTITY TO THE FIVE GALLON LEVEL. THE CREW RETURNED TO KMCC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATING CYLINDER, UPPER SDR DLM88081718Control Panel · arcedBATTERY CIRCUIT BREAKER POPPED INFLIGHT ELECTRICAL ARCING AND FLASH FROM HYDRAULIC PANEL F/O RECEIVED SHOCK FROM YOKE ELECTRICAL BURNING SMELL BUT NO SMOKE. FOUND BATTERY CHARGER C/B POPPED, REPLACED C/B, BATTERY CHARGER & BATTERIES, REPLACED HYD AUX PUMP & TSDR AALA200803069Filter · failedDFW INFLIGHT - CREW REPORTED NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT CAME ON AT FL410 FOLLOWED BY NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE INDICATION. CREW TURNED OFF BOTH RIGHT AND LEFT ENGINE DRIVEN HYDRAULIC PUMPS. LANDED DFW WITHOUT INCIDENT. REPLACED NSDR HNAA2008120800341Hydraulic System · contaminatedJUST AFTER TAKEOFF, THE 'RUDDER PRESSURE' AND 'RUDDER FULL PRESSURE' CAUTION LIGHTS ILLUMINATED. THE CREW ELECTED TO RETURN TO THE ORIGINATING AIRFIELD. AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED, THE CAUTION LIGHTS EXTINGUISHED. BOTH HYDRAULIC SYSTEMS SDR AALA200803061Module · faultedLAX INFLIGHT - NUMBER ONE AND TWO ENGINE HYDRAULIC PUMP LOW PRESSURE INDICATIONS CAME ON IN FLIGHT. LANDED LAX WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO ENGINE DRIVEN PUMPS AND HOSES AND HYDRAULIC RESERVOIR PRESSURE MODULE. SYSTEM GROUND CHECKED NORMAL SDR SWIA200820619O-Ring · leakingFLT 6562 - GEAR DISAGREE WARNING ON GEAR EXTENSION WITH HYDRAULIC SYSTEM 3 SHOWING ZERO. REPLACED DAMAGED O-RING AND SWUNG GEAR.SDR AALA200802625AHose · leakingFLL INFLIGHT - CREW REPORTED RIGHT HYDRAULIC QUANTITY AND PRESSURE LOSS. EXTENDED LANDING GEAR MANUALLY. LANDED FLL WITHOUT INCIDENT AND AIRCRAFT WAS TOWED OFF RUNWAY. REPLACED RIGHT HYDRAULIC SYSTEM HOSE AND SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKESDR DL76L081667Line · leakingINFLIGHT L HYD QUANTITY BLED TO ZERO WITH ASSOCIATED L HYD QTY EICAS MESSAGE. FOUND RIDGED PIPE FROM LT HYD SYS RESERVOIR SUPPLY, HOLEDSIGN(?) OF CHAFING ON HOLD OPEN STAY. REPAIRED PIPE IAW AMM 20-10-09-358-151. RAN LT HYD PUMP. NO LEAKS. LT SYSTEM FILLSDR DL76P081666Valve · leakingINFLIGHT LEVEL 340, R HYD QTY EICAS MSG WARNING WITH ASSOCIATED LOSS TO 0.45 ON ARRIVAL AT GATE. RIGHT HYD QTY WENT TO 0.01.\D MODULE SHOWS NO FAULTS. REPLACED SELF RESETTING FUSE VALVE AT LEFT ANTI-SKID VALVE MODULE NR 5 LK CHECK OPS CK OK.SDR AALA200802596AB-Nut · looseINFLIGHT LEFT HAND HYDRAULIC SYSTEM QUANTITY DROPPED TO .18. LANDED MCO WITHOUT INCIDENT. TIGHTENED LOOSE B-NUT ON LEFT HAND PRESSURE LINE TO ALT SHUTTLE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA081125002Flex Line · broken(CAN) AFTER LANDING AND PARKING, VISIBLE SMOKE FROM RT LDG. SMOKE DUE TO AN HYD LEAK FROM BRAKE NR 3 BOKEN FLEXIBLE HOSE. HOSE REPLACED IAW AMM 32-42-52.SDR Y9PA663P112508Hydraulic System · low pressureENROUTE, THE CREW DECLARED AN EMERGENCY AND LANDED. THE REPORT IS BOTH HYDR SYS QUANTITY WAS INDICATING LOW, LOCATED A LOCAL TECH IAW AIR CARRIER MM SECTION 3.02. CHECKED THE QUANTITY IN THE HYDR RESERVOIRS AND VERIFIED THAT THEY WHERE LOW, SERVICED IAW COMPUSDR DXTA200811193363Relief Valve · inoperativeAT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND THE HYD PRESS LIGHT REMAINED ILLUMINATED. REPEAT WRITE UP. FOUND HYD SYS RELIEF VALVE OPENING AND REGULATING AT 1100 PSI. SHOULD BE 1500 PSI. REMOVED AND RESDR C2XA08CL121Hydraulic System · contaminatedMKE - FLIGHT 2948 - THE CREW REPORTED THE NR 1 HYDRAULIC SYSTEM FLUID SHOWED 1/4 LEVEL AFTER 43 MINUTES IN FLIGHT. THE SYSTEM WAS SERVICED PRIOR TO DEPARTURE FROM IAH. RECEIVED A HYD SYS 1 LOW QUANTITY ON FINAL APPROACH. EMERGENCY WAS DECLARED AND THE AIRCRSDR GUUA11170801Hydraulic System · contaminatedFLIGHT 9193 FLL/TLH - DURING APPROACH TRIED TO EXTEND THE LANDING GEAR AND THE LANDING GEAR CIRCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND THE GEAR EXTENDED. CONTINUED TO TLH LANDED WITHOUT INCIDENT. INSPECTED THE LANDING GEAR SYSTEM BLED AIR FROM THSDR CA081118004Line · cracked(CAN) ON DESCENT AT NIGHT IN HEAVY RAIN, FLIGHT CREW GOT NR 2 HYD PUMP CAUTION FOLLOWED BY TOTAL LOSS OF QUANTITY IN NR 2 HYD SYS. LEVELED AT F110 FOLLOWED QRH, DECLARED PAN, BRIEFED F/A AND PASSENGERS ON RETURN TO BASE FOR NORMAL LANDING WITH PRECAUTIONARY SSDR DL76L081529Actuator · leakingCENTER HYDRAULIC SYSTEM WAS LOSING FLUID, ATB TO SVO. FOUND LCCA LEAKING.SDR YENA200811100106Switch · leakingFLT 705, JFK-SJU, HYD BLUE LOW DURING CLIMBOUT, AIR RETURN TO JFK. FOUND BLUE PUMP PRESS SWITCH LEAKING. REMOVED AND REPLACED BLUE ELECTRICAL PUMP PRESSURE SWITCH AS PER MM 29-12-17, OPS CHECK AND LEAK CHECK OK, SERVICE BLUE HYD SYSTEM TO LIMITS.SDR AALA200802474AHose · leakingDFW INFLIGHT - RIGHT MAIN LANDING GEAR RED LIGHT ON WITH GEAR UP. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC FLEX LINE FOR RIGHT MAIN LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA081121007Line · chafed(CAN) ACFT LOST ALL HYD FLUID IN THE RT SYS DURING FLIGHT. NO INFO ON FLIGHT PROFILE, CAS MESSAGES OR QTY`S NOTED. CREW UNAVAILABLE FOR DEBRIEF AT THIS TIME. REPLACED AFFECTED LINE, CLAMP AND HARDWARE.SDR UALA2008111306414Hydraulic Line · leakingRIGHT MLG WHEEL WELL HYD LEAK. FOUND TUBING THAT IS LEAKING. REMOVED LEAKING HYDRAULIC LINE FROM AIRCRAFT AND ROUTED TO TUBE SHOP FOR MANUFACTURING OF NEW LINE. NEW LINE WILL BE READY AROUND 2100. INSTALLED NEW DOOR LOCK LOWER HYD LINE FROM ACTUATOR TO TEESDR 2008UALA06414Hydraulic Line · leakingRT MLG WHEEL WELL HYD LEAK. FOUND TUBING THAT IS LEAKING. REMOVED LEAKING HYDRAULIC LINE FROM AIRCRAFT AND ROUTED TO TUBE SHOP FOR MANUFACTURING OF NEW LINE. NEW LINE WILL BE READY AROUND 2100. INSTALLED NEW DOOR LOCK LOWER HYD LINE FROM ACTUATOR TO TEE FISDR 2008UALA06360Hydraulic System · unknownLOSS OF HYDRAULICS. FLIGHT DIVERTED.
SDR AALA200802460AB-Nut · leakingJFK INFLIGHT MIA TO CDG - LEFT HYDRAULIC QUANTITY LOW INDICATION. LANDED JFK WITHOUT INCIDENT. FOUND RUDDER AREA WET AND LEAKING B NUT FITTING AT HYDRAULIC BLOCK IN VERTICAL FIN. REPLACED SEAL AND SECURED B NUT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA081105005Line · leaking(CAN) DURING FLIGHT, CREW NOTICED NR 2 HYD ISO VALVE CAUTION LIGHT CAME ON, NR 2 HYDRAULIC PRESSURE REMAINED NORMAL, AND THERE WAS A "SMALL QUANTITY" OF FLUID REMAINING IN NR 2 SYSTEM. CREW DECLARED EMERGENCY LANDING. CREW PERFORMED AN ALTERNATE GEAR EXTENSIOSDR CA081105004Line · ruptured(CAN) CREW NOTICED HYD QTY LOSS ON NR 2 SYS. REPORTEDLY, NR 2 HYD ISOLATON VALVE CAUTION LIGHT CAME ON, BUT HYD PRESSURE REMAINED NORMAL. THE CREW DECIDED TO PERFORM ALTERNATE GEAR EXTENSION FOR LANDING. ACFT TOWED TO HANGAR, WHERE TECHNICIANS DISCOVERED RUPTSDR ASOA200801443Hydraulic System · malfunctionedLOST BLUE HYDRAULIC PRESSURE AND LOW LEVEL ILLUMINATED. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED & REQUESTED EMERGENCY VEHICLES. FLT 5200 DEL 181 MINS.SDR CA081103003Line · chafed(CAN) DURING CRUISE FLIGHT, THE ACFT REPORTED LOSING NR1 HYD SYS FLUID AND ACTIVATION OF NR1 ISO VALVE. COMMERCIAL DECISION MADE FOR ACFT TO RETURN TO ORIGINATING AIRPORT. FLAP (0) DEGREES AND LANDING CARRIED OUT THAT WAS DUE TO ACTIVATION OF NR1 HYD SYS ISO VSDR A6WA200840603Hydraulic Line · leakingRECEIVED HYDRAULIC 2 LOW PRESSURE WARNING MSG ON GROUND. COMPLIED WITH QRH. ENGINE DRIVEN PUMP 2A RAN 2 MINUTES WITH QUANTITY ZERO. NOTED TEMPERATURE OF 46C. R&R LT OTBD SPOILER HOSE ASSEMBLY AND LT INBD SPOILER RETRACT HOSE ASSEMBLY IAW 51-10. R&R HYD NRSDR YYE2009F00000Powerpack · failedHYDR PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILURE PROBABLY CAUSED BY DEBRIS FROM PRIMARY PUMP - YET TO BE DETERMINED. WILL SEND FOLLOW UP REPORT. LATE REPORT IS BEING DELT WITH BY FSDO. (K)SDR QXEA2008110401158Hydraulic Line · failedPDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3/4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN. REPLACED CRACKED NOSE GEAR DOWN LINE, CHECK GOOD. PERFORMED EDP HYD FLUID LOSS INSP IAW MM 05-SDR HALA2008102900830Fitting · looseETOPS SIGNIFICANT SYSTEMS - ON ETOPS1 CK FOUND ADP MODULE IN LT WHEEL WELL LEAKING AT UNION. RE-TORQUED UNION AND B-NUT, LEAK CHECK GOOD. SERVICED HYD, OK FOR SERVICE.SDR DXTA2008102903326Relief Valve · faultedGEAR "UNLOCK" LIGHT, "HYD PRES" LIGHT, AND "STAB MISCOMPARE" LIGHT ALL ILLUMINATED AFTER TAKEOFF. THEY REMAINED ILLUMINATED WHILE RUNNING THE CHECKLIST AND DID NOT EXTINGUISH UNTIL THE GEAR WAS EXTENDED. REPEAT WRITEUP. REMOVED FAULTY HYD RELIEF VALVE. INSTALSDR DL76G081436O-Ring · leakingON FLIGHT 30 ATB TO JFK DUE TO CTR SYS HYD QTY LOSING FLUID. FOUND NR 10 SPOILER PCA PLUS LEADING REF IPC FOR SPOILER P ITEM 425. REMOVED AND REPLACED DAMAGED O-RING PER AMM. OPS 2 LEAK CHK OK. ACFT RETURNED TO NML CONFIG ACFT OK FOR SERVICE. CTR HYDS SVCSDR FDEA200810244538Bypass Valve · leakingDURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS VALVESDR ASOA200801390Hydraulic System · failedHYDRAULIC SYSTEM 3 FAILURE. EMERGENCY DECLARED.SDR 08FDEA04538Valve · leakingDURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A. ALT FLAPS AND MANUAL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPLACED RT FLAP BYPASS SDR CA081024002Heat Exchanger · cracked(CAN) ENROUTE AT 7000 FT, ACFT STARTED TO NOD UNCHARACTERISTICALLY. IT WAS NOTED THAT THE NR 1 HYD SYS PRESSURE WAS HIGH (IN THE RED). DECISION TO RETURN MADE AND NR 1 HYD SYS DE-SELECTED BUT PRESSURE REMAINED HIGH. NO OTHER ADVISORY/CAUTION LIGHTS WERE ON AT SDR RU3A004Hydraulic Line · chafedNUMBER 2 HYDRAULIC SYSTEM LOST PRESSURE ON APPROACH. FOUND PRESSURE HOSE ASSY IN PYLON CHAFED BY HOSE CLAMP WHERE RUBBER LINER WAS ERODED AND THE CLAMP AND HOSE WERE METAL TO METAL. REPLACED HOSE, CLAMP, AND ENGINE DRIVEN HYDRAULIC PUMP. INSPECTED FILTERS, SDR CA081017005Line · burst(CAN) AFTER TAKEOFF IN CRUISE AND ON THE WAY NR 2 HYD PRESS LOST MASTER CAUTION ON REPORT BY THE CAPTAIN, HE STILL HAD HIS NR 1 AND NR 3 HYD SYSTEM. ACFT LANDED SAFELY WITHOUT ANY EMERGENCY REQUEST. NR 2 ENGINE HYD PUMP OUTLET LINE FOUND BUSTED, LINE REPLACED.SDR SWIA200820204Quick Disconnect · disconnectedFLT 3981 - AFTER TAKEOFF "HYDRAULIC 1 LO PRESS" AND "HYD 1 EDP" CAUTION MESSAGES DISPLAYED. RECONNECTED NR 1 EDP QUICK CONNECT FITTING 'P' SAFETY FITTING.SDR 2008UALA06130Hydraulic Line · crackedHYDRAULIC PROBLEM. RTFL. FOUND HYDRAULIC LANDING GEAR UP TUBE ASSY CRACKED. ALSO 2 OTHER TUBES INTERFERING AND DAMAGING. REPLACED TUBES OKAY. LEAK CHECK CARRIED OUT NO FAULTS FOUND. SURROUNDING AREA CLEANED OKAY.
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