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 UALA2010060701984Hydraulic System · leakingGREEN HYD ECAM, FLIGHT DIVERTED. FREEFALL EXTENTION OF GEAR WAS UTILIZED. CREW REPORTED THAT THEY FOLLOWED ECAM PROCEDURE AND SHUTOFF GREEN PUMP AND PTU. FOUND FLUID LOSS TO GREEN SYS. SERVICED GREEN SYS & ACCOMPLISHED MANUAL EXTENSION RESET.SDR XSK2010F00000Line · weakON A FLIGHT, 06/05/2010, WE EXPERIENCED A LT HYD SYS FAILURE AND SOON AFTER, APRATIAL RT HYD SYS FAILURE. WERE IN A CLIMB TO FL260 AND PASSING ABOUT 16,000 FT WHEN THE INITIAL INDICATION OF A LT HYD SYS PRESSURE LOW WAS ANNUCIATED. THE LT HYD PRESSURE GAGE VSDR DALA1012439009B-Nut · leakingDURING PHASE OF FLIGHT F/A'S NOTICED BURNED SMELL BY AFT GALLEY. CREW TURNED PACKS OFF AND ON TO DISSIPATE SMELL. ACTION DIDN'T MAKE DIFFERENCE IN SMELL. ONCE ON GROUND, MX INSPECTED AFT GALLEY AND AFT LAVATORIES NO TROUBLE FOUND. ON CONTROL NR C06050773, OPSDR UALA2010060701961Line · leakingHYD FLUID LEAKING FROM NR 2 PYLON DRAIN. FOUND ENG DRIVEN PUMP CASE DRAIN FILTER RETURN LINE FWD FROM MODULE CHAFING ON A PRESS LINE IN PYLON. REPLACED LINE AND LEAK CK OK.SDR YENA20100603076Line · leakingFLT 46, DECLARED EMERGENCY AND RETURN TO MCO. AFTER TAKEOFF LANDING GEAR DOORS WOULD NOT RETRACT DUE TO LOSS OF GREEN HYD SYS PRESSURE. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. MAINTENANCE FOUND RT LANDING GEAR LOCK STAY ACTUATOR HOSE LEAKING. SDR AALA20100603TUL06Hydraulic Line · leakingHNL - INFLIGHT KOA-LAX. CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. QUANTITY INDICATION WENT TO ZERO. EMERGENCY DECLARED DIVERTED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLEX HOSE ON C2 ELECTRIC PUMP LEAKING. REPLACED PSDR YLXA201072101Hydraulic Line · chafedFOLLOWING DEPARTURE FROM TREASURE CAY BAHAMAS, THE CREW NOTED A HYDRAULIC SYSTEM WARNING LIGHT. THE CREW CONTINUED THE FLIGHT TO ITS DESTINATION, FORT LAUDERDALE, WITHOUT INCIDENT. ATC WAS ADVISED AND AN EMERGENCY DECLARED. AS A PRECAUTION, THE EMERGENCY GESDR 2010FA0000574Tee Fitting · crackedFOUND NR 3 HYD SYS PRESSURE LINE PN 600-75239-788 COMING FROM MANIFOLD LEAKING AT LINE "B" NUT FITTING PN MS21905D6 CRACKED. ALSO NOTED LINE CONNECTION TO TEE FITTING WAS IN A BIND. FAILURE WAS UNDER NORMAL OPERATIONS, SYS PRESSURE AT 3,000 PSI. RECOMMENDATSDR UALA2010060101855Line · leakingLOSS OF THE YELLOW HYD FLUID. FOUND LEAK FROM RT ENG PYLON SIDE FIREWALL DISCONNECT, LINE ON AOG ETA OPEN. INSTALLED RING LOCK REPAIR ON HYD LINE.SDR CA100602001Line · crackedWHILE ON A TRAINING MISSION, THE PILOT EXPERIENCED LOSS OF NR 1 HYD SYS PRESSURE. THE ACFT RETURNED TO BASE AND LANDED WITHOUT INCIDENT. MX DISCOVERED A CRACKED RIGID HYD LINE, BETWEEN THE CUTOFF BLOCK AND THE 3 WAY SHUTOFF VALVE. CRACK DEVELOPED UNDER A SWSDR DJFA2010014Line · rupturedAFTER LANDING, CREW REPORTED A LARGE PUDDLE OF HYD FLUID UNDER THE ACFT. MX FOUND THE NR 3 BRAKE LINE RUPTURED. THE LINE WAS REPLACED.SDR UALA2010060101896Line · leakingFOUND HEAVY HYD LEAK AT RT MLG DURING WALK AROUND. LEAK ISOLATED ON A BROKEN HYD FLEX LINE ON THE TOP RT OF MLG ON A FLEX HYD LINE PN 00624-AC127J-0300SS OR AS4624J-0300SS AT 3000 PSIG 275F AS4623*. FLEX HYD LINE REPLACED IAW AMM. LEAK CHECK PERFORMED, NO LEAKSDR UALA2010060101880Line · brokenGREEN & YELLOW HYD ISSUE, RTFL. CONFERED WITH LM, CREW SHUT SYS PUMPS OFF TO GREEN SYS, HYD QTY DID NOT DEPLETE. FOUND LT GEAR DOOR ACTUATOR HYD LINE BROKEN, RPLED LINE AND RPLED SYS HYD FILTERS PRECAUTIONARY. SVC HYD SYS QTY TO FULL AND PERFORMED OPS CHECK SDR YENA20100529073O-Ring · damagedFLT 16 JFK-BTV A/C DIVERTED TO BOS WHILE AT 21000 GOT GREEN HYD LOW FLUID, PERFORMED ECAM ITEM AND DECLARED EMERGENCY. SHUT OFF ENG DRIVEN PUMP WITHIN 60 SEC, FOUND LEFT ENG HYDRO DISCONNECT CHECK VALVE 1050GM PACKING DAMAGED, REPLACED 1050 GM CHECK VALVE ANDSDR CA100603004Flex Hose · ruptured(CAN) AFTER TAKEOFF, THE CREW OF ANT 207 SELECTED THE LANDING GEAR TO RETRACT. THE LANDING GEAR RETRACTED PART WAY AND THE HYDRAULIC PUMP LOW PRESSURE LIGHTS ILLUMINATED. A CHECK OF THE PRESSURE GAUGE INDICATED ALMOST NO HYDRAULIC PRESSURE. THE CREW DIVERTESDR UALA2010052801840Computer · malfunctionedON FLT CONTROL CHECK L-R AILERON HAVE HYD NOISE-VIBRATION HEARD AND FELT IN COCKPIT. ISOLATED RT AILERON HYD SYSTEMS, RT AILERON FLUTTERS WITH ONLY GREEN HYD SYSTEM ON. ATTEMPTED ELAC 1 AND 2 RESET, NO HELP. SUSPECT RT GREEN AILERON SERVO ISSUE. THERE WERE SDR UALA2010052701832Line · leakingGREEN HYD LOW PRESS: FOUND LT MLG NORMAL BRAKE SUPPLY FLEX LINE LEAKING. FOUND HYD LINE TO BRAKE LEAKING LT GEAR. REPLACED 2 LINES, LEAK CKS OK, BLED BRAKES.SDR CA100526003Hydraulic System · leakingACFT ENCOUNTERED A HYD SYS 1 FAILURE AFTER DEPARTURE. FLIGHT DID AN AIR TURNBACK. ATC HAD CFR ON STANDBY FOR ARRIVAL. FOUND THAT NR1 HYD QTY DROPPED TO ZERO, FOLLOWED BY PRESSURE DROP TO ZERO PSI. L3 MULTIFUNCTION SPOILER WAS LEAKING. REPLACED LT L3 MFS IASDR AALA20100522MIA01Hydraulic Line · leakingMIA - INFLIGHT ORD-MBJ CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY DECREASING SLOWLY IN FLIGHT. FLIGHT DIVERTED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC LINE THAT WAS LEAKING. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA100528014Hydraulic Line · crackedDURING ACFT TAXI, THE NR2 HYD SYS LOST PRESSURE. AFTER SHUTDOWN, A HYD LEAK WAS DISCOVERED IN THE NLG WW. THE NLG DOOR CLOSE PRESSURE LINE WAS FOUND CRACKED. IPC 32-30-00, FIG 5, ITEM 340. THE LINE WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR ANCF2010052000061Hydraulic System · malfunctionedAIR TURN BACK AND EMERGENCY LANDING. LOSS OF GREEN HYDRAULIC SYSTEM (1+2 FAULT) BOTH. IN ACCORDANCE WITH AMM TASK 29-11-34-000 -801 THE HSMU WAS REMOVED AND IN ACCORDANCE WITH AMM TASK 29-11-34-400- 801 THE HSMU WAS REPLACED AND INSTALLED IN ACCORDANCE WITH SDR A6WA201040366Hydraulic System · lowAT CRUISE, HYD NR1 LO PRESS CAUTION, CW QRH PRESSURE WENT TO ZERO, DIVERTED. REPLACED FLEXIBLE PRESSURE LINE IN LT PYLON IAW AMM 29-11-01. LEAK CHECK GOOD AT THIS TIME.SDR PCSA2010051801Check Valve · leakingWHEN THROTTLES RETARDED FOR DESCENT A STRANGE ODOR IS DETECTED FOLLOWED BY A HAZE. THEN A SHORT BURST OF SMOKE. LEFT AND RIGHT PACK TEMPS 40 DEGREES. ADVANCED AND RETARDED 1 AND 3 THROTTLES. MORE SMOKE APPEARED AFTER NR 1 THROTTLE ADVANCED AND RETARDED. MSDR 2010FA0000480Fitting · brokenAT TAKEOFF, HELICOPTER EXPERIENCED A NR 2 HYD SYS CAUTION LIGHT ILLUMINATION AND THE NR 2 HYD PRESSURE GAUGE NEEDLE INDICATED ZERO PRESSURE. THE HELICOPTER LANDED WITHOUT INCIDENT ON THE NR 1 HYD SYS. UPON INSPECTION, THE FWD MAIN ROTOR SERVO HYD PRESSURE PORTSDR CA100512003Hose · leakingAFTER A SHORT (0.3 H) FIRST FLIGHT OF THE DAY, THE PILOT LANDS AND SHUTS DOWN NORMALLY THE ENGINE. AFTER GETTING OUT OF THE ACFT, HE DETECTS PRESENCE OF HYD OIL IN THE MAIN TRANSMISSION DECK AREA. OPENING THE COWLINGS, HE DISCOVERS A LOT OF HYD OIL ON THE EQSDR 2010FA0000457Muffler · crackedDURING A ROUTINE INSPECTION NEAR THE MAIN HYDRAULIC MANIFOLD, A LARGE OF INSULATION MATERIAL WAS NOTED. FURTHER INVESTIGATION REVEALED THE INSULATION WAS FROM THE OUTER COVERING OF THE MUFFLER. CRACK WAS FOUND AT THE TOP OF THE MUFFLER P/N 12945-096-001.SDR AALA20100510ORD02O-Ring · damagedORD - INFLIGHT SFO-JFK. CREW REPORTED CENTER HYDRAULIC FLUID LOSS IN FLIGHT. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND O-RING PROTRUDING FROM FITTING ON HYDRAULIC PRESSURE MODULE. REPLACED O-RING. SYSTEM GROUND CHESDR CALA2010051000194Hydraulic Line · damagedAFTER T/O CTR HYD SYSTEM INDICATIONS WENT TO ZERO, LOST CTR HYDS SYSTEM WENT TO SBJ VOR DUMPED FUEL. ACCOMPLISHED ALL PERTINENT CHECKLISTS, RETURNED TO EWR FOR LANDING, TOWED TO GATE. DAMAGE INCURRED FROM NR 6 MAIN TIRE FAILURE TO LEFT MLG HYD LINE CAUSED CTRSDR DYV2010F00000Powerpack · failedON 5/6/2010, THE LANDING GEAR DOWN CYCLE WAS INTERRUPTED BY A SURGE AND THE PILOT DISCONTINUED THE APPROACH TO LAND AAT THE AIRPORT AND RECYCLED THE LANDING GEAR AND FOUND NORMAL OPERATION AND INDICATION. AS A PRECAUTION, THE FLEW TO THE AIRPORT WHERE MX IS LSDR SWAA102713Valve · faultyDECLARED EMERGENCY - TOTAL LOSS OF "B" SYSTEM HYDRAULICS AT FIRST FLAP POSITIONING. REMOVED AND REPLACED FLOW LIMITING HYDRAULIC VALVE PER MM.SDR MASA2010050900472Hydraulic System · malfunctionedNR 4 BRAKE APPEARS TO LOCK UP. MX RE-SECURED HYD QD & R2 TIRE.SDR FDEA201005051466Hose · leakingCLIMBING THRU 16,000 FT NOTICED SYS A HYD QTY WAS ZERO, SHORTLY AFTER SYS PRESSURE WENT TO ZERO & BOTH LOW PRESSURE LIGHTS CAME ON. PERFORMED STABILIZER & QRH SYS A LEAK OR LOSS CHECKLIST, PERFORMED MANUAL GEAR EXTENTION & ALT MASTER FLAP EXTENTION. LANDED 16SDR FDEA201005041462Pcu · failedTOTAL LOSS OF HYD SYS A QUANTITY AFTER TAKEOFF, HYD SYS A PUMPS WERE SHUTOFF AT 0235Z, HYD SYS A FLUID SHUTOFF SWITCHES WERE CLOSED AT 0240Z AND ENGINES NR 1 AND NR 2 WERE SHUTDOWN AT 0303Z. BROKE SHEAR WIRE ON ALT FLAP AND GPWS FLAP INHIBIT. PREVIOUSLY ENTESDR UALA2010050401506Filter · faultyRT ENG NO START RT HYD WENT TO 0. FOUND HYD LEAK AT FITTING OF EDP. ALSO REPLACED CASE DRAIN FILTER AND PRESSURE FILTER. FOUND STARTER VALVE FULL OF HYD FLUID. RPLC'D STARTER VALVE. LEAK CK AND ENGINE RUN REQUIRED IAW AMM TO CK OPS OF NR 2 ENGINE DRIVEN HYSDR UALA2010050301488Priority Valve · leakingYELLOW SYS LOW IND, FLIGHT DIVERTED. REPLACED LEAKING HYD PRIORITY VALVE 3015GM. OPS ARE GOOD.SDR 2010FA0000460Pressure Switch · bindingLANDING GEAR DID NOT EXTEND AND GEAR-UP LANDING WAS MADE. POST INCIDENT INSPECTION AND OPERATION CHECK DEMONSTRATED REPEATABLE FAILURE CONDITION. HYDRAULIC PRESURE SWITCH WAS SHOWN A SOURCE OF FAILURE.SDR 22AA201000069Flex Line · leakingLT HYD DECREASED TO ZERO. AFTER LANDING AND ENGINE SHUTDOWN UNABLE TO OPEN LT COCKPIT WINDOW. CRANK SKIPPING FRM 56-11-XA-02. R & R DOWNLOCK ACTUATOR FLEXIBLE HOSE IAW AMM 20-10-10/401. SERVICED LT HYD RESERVOIR IAW AMM 12-12-01/301. SYS OPS CHECKED GOOD, NOSDR UALA2010042901447Line · leakingNR 1 ENG LEAKING HYD FLUID. FOUND HYD SUPPLY LINE FOR NR 1 REVERSER, MFG NEW LINE, PRESSURE TESTED LINE. INSTALLED LINE, LEAK CHECKED GOOD.SDR UALA2010042801422Hydraulic Line · leakingDURING EXTERNAL CHECK FOUND HYD LEAK AT THE PRESSURE HYD LINE FROM THE RIGHT BRAKE STABILIZER CONTROL BMS UNIT. REPLACED RIGHT HYD HORIZONTAL STAB TRIM CONTROL LINE P/N 271N6482-1116. OPS CHECK HORIZONTAL STAB. OPS CHECK NORMAL, NO LEAKS NOTED.SDR UALA2010042901434Motor · faultyHYD GEN MOTOR TEST FAILED. SUSPECT HYD MOTOR GCU M10622. REPLACED HYD SHUTOFF VALVE IAW MM, OPS TESTED SYS, VALVE & PUMP OPS GOOD, NO INDICATION ON HYD PAGE LOWER EICAS. STILL FAILED TEST. DURING TROUBLESHOOTING, HYD GEN ON & HYD GEN VALVE NOT SHOWN ON LOWERSDR MASA2010042500404Hydraulic Line · defectiveEMERGENCY DECLARED, HYD 3 QUANTITY AT ZERO. R2 O-RING AT PUMP 3A AND PRESSURE LINE AT PUMP 3B.SDR MASA2010042400397Hydraulic Line · defectiveDECLARED EMERGENCY DUE TO HYD 3 QUANTITY AT ZERO. MX R2 O-RING AT PUMP 3A AND PRESSURE LINE AT PUMP 3B.SDR IPXA10559501O-Ring · leakingLOST HYD QUANTITY IN LT SYS IN FLIGHT, .21 REMAINING. PERFORMED AS AN EMERGENCY. R & R O-RING AT LT SYS PRESS TRANSMITTER, SERVICED RESERVOIR TO FULL, LEAK AND OPS CHECKED GOOD IAW MM 29-31-01-4.SDR UALA2010042601384Modulating Valve · faultyIN CRUISE FL350 AIR SYNOPTIC SHOWS PRESS TO AIR C2 HYD PUMP. DURING TROUBLESHOOTING FOUND DEFECTIVE VALVE. REPLACE MODULATING VALVE, ALL OPS OK.SDR SWAA102228Hydraulic Line · leakingAIR TURNBACK / DECLARED EMERGENCY. HYD A-SYS FLUID LOSS. REMOVED AND REPLACED LEAKY A-SYS SPOILER RETURN LINE PER MM.SDR FDEA201004181243Hose · failedLT MLG TIRES DEFLATED DURING TAXI CHECK. SHOWS EVIDENCE OF FIRE/OVERHEAT AND FIRE SUPPRESSION AGENTS. R & R THE NR 1 FWD BRAKE LINE, THE NR 1 AFT BRAKE LINE AND SWIVEL ASSY AND THE NR 5 BRAKE LINE. R & R LT MLG BRAKE ASSEMBLIES IAW MM 32-45-07-4-0. BLEED SDR UALA2010041901291Line · leakingCTR HYD QTY LIGHT AND EICAS ILLUMINATED. CTR HYD FLUID IS LOW. FLUID LEAKING FROM PINHOLE LEAK ON ONE OF THE SUPPLY LINES ON THE ELEVATOR CONTROL VALVES ON THE ELEVATOR TORQUE BOX. LEAK WILL FUMIGATE TAIL AREA WITH JUST PRESSURE ON CTR HYD SYS. WITH NO MOVSDR COMA2010041950100Hydraulic Line · leakingON APPROACH INTO MCI RECEIVED HYD 2 LOW PRESSURE CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. INSPECTED A/C FOUND NR 2 SYSTEM HYD PRESSURE HOSE IN RIGHT PYLON LEAKING. REMOVED AND REPLACED NR 2 SYSTEM HYD PRESSURE HOSE IN RIGHT PYLON.SDR YENA20100416063Pipe · leakingFLT 1206 RSW-HPN (A/C DIVERTED TO MCO) HYD GLOW LEVEL ECAM AT CRUISE FOLLOWED BY LOW PRESSURE. FOLLOWED ECAM AND QRH PROCEDURES NORMAL DESCENT, MANUAL GEAR EXTENSION, NORMAL LANDING. L/G SYSTEM BACK TO NORM MODE OK REF MM 32-00-00-02 CHECK PERFORMED. REF LOSDR DXTA2010041904072B-Nut · looseLT BRAKE PEDAL ON THE CAPTAIN'S SIDE GOES ALL THE WAY TO THE STOP WITH LITTLE TO NO BRAKING EFFECT. FOUND LOOSE B-NUT ON LOW SIDE OF SYS. TIGHTENED B-NUT; BLED BREAKS. TAXI CK GOOD. WORK DONE IAW MM CHAP 32-42-00.
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