JASC 2910
Service difficulty reports · 11,291
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 SWAA2018092525530B-Nut · looseAIR TURNBACK/DECLARED EMERGENCY, LOSS HYDRAULIC SYSTEM A-DURING CLIMB OUT THROUGH 3000' MSL. BOTH ENGINE 1 AND ELEC 2 LOW PRESSURE LIGHTS ILLUMINATED. SECURED B NUT PER AMM.SDR SIMA20180923001Hydraulic Line · leakingAFTER LANDING ON TAXI LOSS OF NOSE WHEEL STEERING CONTROL FOLLOWED BY HYD 3 LO PRESS, STEERING INOP AND SYSTEM 3 QUANTITY AT 0% FLUID REPORTED PUDDLED AROUND NOSE GEAR AND BEHIND AIRCRAFT ON TAXIWAY TOWED TO GATE. REF NRWC 542-ORD-02159 FOR THE R&R OF HYD LINESDR DALA2018092505759Service Panel · missingAPPROXIMATED 3 MINUTES AFTER TAKE OFF CURING CLIMB OUT HEARD 3 BOOMS FROM RIGHT SIDE OF THE AIRCRAFT, NOTICED RIGHT SIDE ENGINE VIB N2 RISE FROM 0.4 TO 2.1 DURING CRUISE ALL INDICATION NORMAL. DURING CRUISE ALL INDICATIONS ARE NORMAL. UPON INITIAL INSPECTION FSDR ASAA2018092516237Hose · damaged#2 ENG HYD LOW PRESS LIGHT AFTER PUSHBACK AND FLAPS SET TO 5 DEGREES. HYD B QTY DROPPED TO 78%. GROUNDED - YES. FOUND PRESSURE LINE FROM ENGINE-DRIVEN PUMP DAMAGED AT PYLON, REMOVED AND REPLACED PRESSURE LINE. PERFORMED GROUND VERIFICATION AND LEAK CHECK, GOODSDR 2018FA0000393Hydraulic Line · leakingDURING CLIMB IN VVI-SRE LEG, THE AIRCRAFT SUFFERED TOTAL LOOS OF SYSTEM NR.2 HYDRAULIC FLUID, QRF TO DEPARTURE STATION. CORRECTIVE ACTION: HYDRAULIC FLUID LOOS WAS CAUSED BY A DEFECTIVE FLEXIBLE LINE LOCATED IN NLG BAY. THE DEFECTIVE HYDRAULIC FLEXIBLE LINE WASDR FDEA2018092502653Tube · severedHYD PRESS SYS, R HYD QUANITY 0. FOUND #12 SPOILER ACTUATOR TUBE SEVERED. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY. ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING. REMOVED AND REPLACED #12 SPOILER PCU REF MM 27-61-SDR FDEA2018092502652Tube · severedHYD PRESS SYS, R HYD QUANITY 0. FOUND #12 SPOILER ACTUATOR TUBE SEVERED. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY. ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING. REMOVED AND REPLACED #12 SPOILER PCU REF MM 27-61-SDR FDEA201809202634Hydraulic Line · severedHYD PRESS SYS, R HYD QUANTITY 0. FOUND NR 12 SPOILER ACTUATOR TUBE SEVERED. REF IPC 27-11-05-66 ITEM 455. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING REF IPC 57-52-51-38 FIG 38 SSDR DALA2018100305854Hydraulic Line · leakingSHIP 997 ON FLIGHT 296 FROM ATL TO RDU DECLARED AN EMERGENCY DUE TO AN EOAP LOW RIGHT HYDRAULIC SYSTEM QUANTITY MESSAGE. CORRECTIVE ACTION: RDU MAINTENANCE FOUND THE RUDDER SHUTOFF VALVE SUPPLY LINE LEAKING. A TEMPORARY LINE WAS INSTALLED AND DEFERRED PER LOG SDR KC8A2018092091818Hydraulic Line · corrodedCREW NOTICED LOSS OF HYDRAULIC PRESSURE, PRESSURE GAUGE FLUCTUATING LOW. PERFORMED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT TROUBLE. REPLACED HYDRAULIC LINE ASSEMBLY WITH NEW ASSEMBLY. PERFORMED SATISFACTORY HYDRAULIC PRESSURE CHECKS AND GEAR RETRACTION CHESDR AALA2018092089014Line · leakingDURING FLIGHT, LOSS OF HYDRAULIC SYSTEM A. WORKED THRU QRH. SYSTEM FAILURE BUT HAD NO LOW PRESSURE INDICATIONS. DIVERTED. AN EMERGENCY WAS DECLARED, AND LANDED WITHOUT INCIDENT. REMOVED FROM SERVICE. REPLACED TWO AFT BRAKE PRESSURE LINES ABOVE THESDR AALA20180918003Hydraulic Line · rupturedAIRCRAFT WAS GROUNDED. PHL-TPA DIVERTED CLT ACCOUNT HYDRAULIC SYSTEM-A LOSS ENROUTE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. HYDRAULIC SYSTEM A FAILED IN FLIGHT, ALTERNATE LANDING GEAR EXTENSION USED. FOUND LEFT ELEVATOR PCA OUTBOASDR W6JA20180919026Control Valve · crackedCOMBINED HYDRAULIC SYSTEM FAILURE ON SHORT FINAL TO BIKF. UPON LANDING NOTED HYDRAULIC LEAK COMING FROM RT LANDING GEAR WHEEL WELL AREA. FOUND "FLIGHT POWER SHUTOFF VALVE" LEAKING IN RT MAIN GEAR WELL. INSTALLED NEW VALVE P/N 1159SCH246-5 S/N 888. INSTALLATIONSDR FDEA2018091432521Hydraulic Line · leakingON SHORT FINAL, L HYD QTY WENT TO ZERO. AS WE WERE FULLY CONFIGURED, WE OPTED TO LAND AND STOP ON THE RUNWAY. PTU KICKED IN ABOUT 150 AGL. WE CAME TO A STOP RAN THE QRH AND SHUT OFF BOTH LT ENG AND LT ELEC HYD PUMPS, PER QRH PROC. TOTAL RUN TIME OF LT HYD PUMSDR SWIA2018091245048Control Panel · deployedON DESCENT THROUGH 9000 FEET LARGE VIBRATIONS BEGAN. NO CAS MESSAGES AND NO MAJOR HYDRAULIC OR MECHANICAL IRREGULARITIES NOTED. (FLT 4970) CLOSED UPON ARRIVAL, FOUND ADG DEPLOYED. PERFORMED ADG DEPLOYMENT CHECK IAW AMM. NO DEFECTS NOTED. RE-STOWED ADG IAW AMMSDR RAIA2018091380001Hose · crackedE1 HYD PUMP FAIL. WHILE R&R E1 HYDRAULIC PUMP, DISCOVERED CRACKED HYD HOSE. R&R HOSE, LK CHK GOOD.SDR FDEA201808292241Packing · damagedDESCENDING IN IDLE POWER, 14000 FT GREEN HYD SYSTEM PUMP ONE AND TWO LO PR ON ECAM. GREEN NEEDLE DROPPED INTO YELLOW ARC. FOLLOWED ECAM AND QRH. REPOWERED SYSTEM WITH ELECTRIC PUMPS. FIRE RESCUE DISPATCHED. FOUND PACKING LEAKING AT TEE FITTING AT RIGHT HASDR ASMF20180918015Fuse · brokenDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING THAT THE HYDRAULIC LEAK WAS OUT OF LIMIT AND HYDRAULIC PRESSURE FUSE WITH THEIR LEVER BROKEN. THE HYDSDR AALA20180829001Hydraulic Line · leakingAIRCRAFT WAS GROUNDED. AIR CONDITIONING AIR FIRST SMELLED LIKE DIRTY SOCKS, BUT THEN SEEMED MORE SMOKY AND TOXIC. FOUND HYDRAULIC LINE LEAKING. PERFORMED APU WASH ON MCM CARD 49-97-11, PACK BURN OUT ON MCM CARD 21-92-12 AND ODOR TROUBLE SHOOTING CARD 05-96-70.SDR AALA2018083089022Fuse · rupturedAFTER TAKE OFF, THE CENTER HYDRAULIC QUANTITY LOW ICAS MESSAGE APPEARED. EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE. AIRCRAFT LANDED. THE AIRCRAFT WAS GROUNDED. FOUND HYDRAULIC FUSE RUPTURED AT THE LEFT MAIN LANDING GEAR, TILT LINE. REPLACSDR UIEA2018082601802Fuse · leakingEICAS 'HYD QTY LOW 1' IN CRUISE, 7:30 INTO FLIGHT. UPON LANDING INTO ANC AIRCRAFT HAD TO BE TOWED OFF OF RUNWAY DUE TO NO NR 1 HYDRAULIC SYSTEM AVAILABLE. INSPECTED AND FOUND LEFT HAND BODY GEAR TRUCK POSITIONING HYDRAULIC FUSE ASSEMBLY LEAKING. SERVICED NR 1 SDR HALA2018082300400Hydraulic Line · leakingDECLARED EMERGENCY FOR IN-FLIGHT HYDRAULIC FLUID LOSS. REMOVED AND REPLACED AUX PUMP HOSE.SDR YGJR2018090500001Hydraulic Line · crackedUPON APPROACH INTO AIRPORT THE NR 1 HYDRAULIC FLUID QUANTITY WENT TO ZERO. AFTER LANDING AND SHUTDOWN MAINTENANCE DISCOVERED THE NR 1 HYDRAULIC CASE DRAIN RETURN LINE HAD BROKEN AT THE SWAGE JUST BEFORE THE FILTER INSIDE THE AFT EQUIPMENT BAY. ALL THE HYDRAUSDR F3LA2018083000418Hydraulic Line · crimpedHYDRAULIC LINE IN THE RT AFT UPPER MLG WW WAS DAMAGED. REMOVED AND REPLACED THE HYD LINE IAW AMM 32-43-00-710-001-A, 32-43-00-870-002-A, 12-12-29-611-002-A, AND 20-23-11-300-001.SDR F3LA2018083000417Hydraulic Line · rupturedHYDRAULIC LINE AT THE LT AFT UPPER MLG WW WAS RUPTURED. REMOVED RUPTURED ALTERNATE BRAKING HYDRAULIC LINE & REPLACED WITH NEW IAW AMM 20-23-11-911-001-A. PERFORMED BLEEDING OF ALTERNATE BRAKING SYSTEM IAW AMM 32-43-00-870-002-A, SUCCESSFUL OPS CHECK OF THESDR QXEA2018082200299Line · leakingDURING CRUISE, RECEIVED A NR 1 HYD ISOLATION VALVE CAUTION, ALONG WITH AN INBD ROLL SPOILER CAUTION. THE NR 1 HYD QTY WAS AT ABOUT 20%. RAN THE CHECKLIST. AT THIS TIME THE NR 1 HYD PRESSURE STARTED TO DROP. THE QTY AND PRESSURE WENT TO 0 % FOR THE NR 1 SYSDR AALA201808229003Hydraulic Line · defectiveAIRCRAFT WAS GROUNDED. MIA-KIN RETURNED TO MIA ACCOUNT SYSTEM A HYDRAULIC QUANTITY INDICATION. EMERGENCY WAS DECLARED. FLIGHT WAS NOT OVER WEIGHT AND LANDED WITHOUT FURTHER INCIDENT. LOSS OF SYSTEM "A" INFLIGHT. SYSTEM A EDP ILLUMINATED FOR DURATION OF FLIGHT SDR AALA201808229002Module · defectiveSYSTEM A HYDRAULIC QUANTITY INDICATION. AN EMERGENCY WAS DECLARED, AND LANDED WITHOUT FURTHER INCIDENT. SYSTEM A EDP ILLUMINATED FOR DURATION OF FLIGHT, GREATER THAN 5 MINUTES. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT ENGINE HYDRAULIC PUMP IAW AMM 29-11-11. SDR SWAA2018082024293Hydraulic Line · brokenDIVERSION, NR 1 ENGINE "LOW PRESSURE" A HYDRAULIC PUMP ILLUMINATED. R&R NR 1 ENGINE HYDRAULIC PRESSURE LINE PER AMM.SDR AALA2018082015006Drain Valve · leakingDURING CRUISE- YELLOW HYDRAULIC QUANTITY LOW ECAM WARNING REPORTED LOW. LATER CAPTAIN REPORTED THAT THE SYSTEM HAD EMPTIED. AN EMERGENCY WAS DECLARED, FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. INSPECTION FOUND LEAK FROM YELLOW RESERVOIR DRASDR CA180822003Line · leaking(CAN) THE PILOT REPORTED WHILE RETRACTING THE LANDING GEAR AFTER TAKEOFF, THE LANDING GEAR CIRCUIT BREAKER TRIPPED WITH THE LANDING GEAR AT MID RETRACTION. THE LANDING GEAR WAS PUMPED DOWN MANUALLY, AND A PRECAUTIONARY LANDING WAS MADE TO A REMOTE MAINTENANCESDR HALA2018081400373Warning Message · false activationRIGHT HYD SYS LOW, RF INDICATION .73 3 HRS INTO FLT. .70 AT TOD .66 AT SHUTDOWN, CENTER SYS AT 1.20 IN FLT, 1.05 AT ENG START. TRANSFERRED CENTER HYD TO RIGHT IAW AMM 29-11-00-862-230. CYCLED LEFT AND RIGHT ANTI-SKID SHUTTLE VALVES. MONITORED CENTER AND RIGHSDR DALA2018081005008Line · leakingAIR TURN BACK DUE TO A COMPLETE LOSS OF THE BLUE HYDRAULIC SYSTEM, AFTER TAKEOFF. REMOVED AND REPLACED THE BLUE HYDRAULIC PUMP FLEX LINE IAW AMM. RETURNED TO SERVICE.SDR DXTA2018090901408Pump · failedHYDRAULIC FLUID LEAK - HYDRAULIC B FAIL. HYDRAULIC OIL ALL OVER RIGHT REAR OF AIRCRAFT. 0 QUANTITY AND 0 PSI. STRONG BURNING ODORS IN CABIN.//SIGNOFF// REMOVED AND REPLACED THE FOLLOWING PARTS REMOVED AND REPLACED RH B SIDE HYRQ ENG. DRIVEN PUMP REF CE-750 AMSDR AALA2018081309002Hydraulic System · malfunctionedAFTER TAKE OFF THE HYDRAULIC GREEN SYSTEM QUANTITY DECREASING AFTER 1.5 HR OF FLIGHT, TO HALF FULL WITH HISTORY OF HYDRAULIC LEAK. DECLARED AN EMERGENY AND DIVERTED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. PERFORMED INSPECTION OF GREEN SYS, FOUNDSDR CVGA20180813001Warning Message · illuminatedDURING CLIMB OUT THRU FL 200, CREW RECEIVED A HYD PWR ON ANNUNCIATOR. CREW LEVELED AT FL 290 AND RAN QRH. CREW WAS UNABLE TO REMEDY THE MALFUNCTION. DECLARED AN EMERGENCY.SDR KW3R2018081033592Hydraulic Line · crackedNR 3 HYDRAULIC SYSTEM FAILURE. FOUND HYDRAULIC TUBE ASSEMBLY CRACKED AD SWAGED FITTING AT NR 3 SYSTEM HYDRAULIC MANIFOLD.SDR IPXA2018081092614Hydraulic System · fluid lossAIR TURNBACK DUE TO A GREEN SYSTEM HYDRAULIC SYSTEM COMPLETE LOSS OF FLUID. PUMPS & FILTERS INSPECTED IAW MM 29-00-00-301. R & R THE FILTERS 291048. 291049, AND 291002. NO DISCREPANCIES FOUND. REMOVED & REPLACED THE HYD CASE DRAIN FILTERS ON LEFT AND RIGSDR DATA20180809701Hydraulic System · leakingCREW OBSERVED A LT HYD LIGHT ILLUMINATED AND QUANTITY FLUCTUATED. AIRCRAFT SLOWED AND GEAR SUCCESSFULLY EXTENDED AS A PRECAUTION. HYD LT AND HYD RT INDICATORS ILLUMINATED AND HYDRAULIC QUANTITY WENT TO LOW RANGE, RED. QRH PERFORMED AND APPROACH INFORMED OF HYSDR ASAA2018080865696Hydraulic System · fluctuatesTHE GREEN HYDRAULIC SYS HAD LOW PRESSURE. ACFT GROUNDED. R & R PTU FIN 1088GM IAW AMM 29-23-41 PB 401 AND TSM 29-23-00-810-812A. FUNCTIONAL CHECK FOUND NORMAL. NO LEAKS NOTED. FOUND THE YELLOW SYSTEM PRESSURE FLUCTUATING WITH THE ELEC PUMP ALONG WITH GSDR CALA2018080601764Line · leakingTHE CREW REPORTED A CENTER HYDRAULIC QUANTITY LOSS THROUGH DURATION OF FLIGHT. ON GATE ARRIVAL, HYDRAULIC FLUID WAS FOUND COMING FROM LEFT INBOARD TE FLAP TRACK FAIRING NEAR THE LEFT GEAR. MX FOUND A FLEX LINE LEAKING ON LEFT MLG EXTENSION AND RETRACTION SYSSDR F3LA2018080700380Hydraulic System · overservicedDURING CRUISE FLIGHT, THE FLIGHT ATTENDANTS IN BACK OF ACFT NOTICED AN ODOR OF DIRTY SOCKS, BURNING FUMES. AFTER TURNING OFF THE NR 2 PACK, THE ODOR DISSIPATED. PERFORMED IDENTIFICATION OF CAUSE OF CABIN ODOR IAW TSM 05-50-00-810-831-A. FOUND GREEN HYDRAULISDR SWAA2018080724092Fuse · faultyAIR TURNBACK, LEADING EDGE FLAPS TRANSIT LIGHT ON - LANDING FLAPS 15 PER QRH. R&R HYDRAULIC FUSE PER MM.SDR ASAA2018080635677Circuit Breaker · trippedON DEPARTURE, ELEC 2 LOW PRESSURE LIGHT ILLUMINATED. ACFT GROUNDED. FOUND THE NR 2 ELEC HYD PUMP CIRCUIT BREAKER WS OPEN INSIDE P92 PANEL, GVI NR 2 PUMP AND ASSOCIATED ACCESSIBLE WIRING WAS OK, REPLACED CASE DRAIN FILTER, NO CONTAMINATION FOUND, RESETSDR CALA2018080601752Hose · leakingLEFT HYDRAULIC SYSTEM FAILED ON SHORT FINAL. HYDRAULIC PUMPS WERE ON FOR ABOUT 20 MINUTES. REMOVED AND REPLACED A HOSE. OPS AND LEAK CHECKED GOOD. NO TOTAL LOSS OF LT SYS HYD, QUANTITY AT .2 0. IAW AMM 29-11-00-201, CONDITION 1, NO DPIS POPPED.SDR C77A2018080600001Line · leakingDECLARED EMERGENCY ON DESCENT FOR HYDRAULIC QUANTITY EMPTY MESSAGE. THE AIRCRAFT LANDED SAFELY AND HAD TO BE TOWED OFF THE RUNWAY. NO INJURIES REPORTED. LOSS OF HYD 2 QTY AFTER GEAR EXTENSION, FLUID FOUND IN LT MLG WHEEL WELL. R & R THE HYD LINE TO THE NR 1SDR AALA201808029005Pressure Switch · leakingDURING FLIGHT CREW REPORTED THAT THE CENTER HYDRAULIC SYSTEM WAS LOOSING QUANTITY AND WOULD LIKELY BE EMPTY UPON ARRIVAL INTO ORD. CAPTAIN DELCARED EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLE SHOOTING FAULTY/LEAKING DELTA-P AT PRESSURE AND CASE DRAIN FILTESDR AALA2018080201003Filter · leakingDURING FLIGHT CREW REPORTED THAT THE CENTER HYDRAULIC SYSTEM WAS LOOSING QUANTITY AND WOULD LIKELY BE EMPTY UPON ARRIVAL INTO ORD. DELCARED EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLESHOT THE FAULTY/LEAKING DELTA-P AT PRESSURE AND CASE DRAIN FILTER AC MOTOSDR DALA2018080204821Hydraulic Line · unsecureFLIGHT ATTENDANT REPORTED SMOKE/FUMES IN THE AFT CABIN. MAINTENANCE FOUND AND REPAIRED A HYDRAULIC LEAK AT THE LEFT THRUST REVERSER ISOLATION VALVE BY SECURING THE RETURN LINE. NO-GO ODI PREVENTION PROCEDURES WERE COMPLIED WITH.SDR CA190220031Line · leaking(CAN) HYDRAULIC LINE FOUND LEAKING THROUGH THE BRAID (TC# 20190220031)
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