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 DALA13006899263B-Nut · leakingSTRONG EXHAUST TYPE ODOR REPORTED BY F/A. TURNED OFF RT PACK, ODOR DISSIPATED. MX REMOVED AFT STAIRWELL PANELS AND FOUND LOOSE B-NUT AND HYD FLUID LEAKING FROM BLEED VALVE FORWARD OF HYD CONTROL VALVE, LT SIDE OF STAIRWELL. TIGHTENED B-NUT AND LEAK CHECKED.SDR CA130208003Hose · unserviceable(CAN) HYD FLUID LOSS WAS DISCOVERED ON DAILY INSPECTION. HYD FLUID WAS NOTICED COMING FROM THE HYD PRESSURE LINE, LT SERVO TO EPICYCLIC JUNCTION, WHERE THE BRAIDED PORTION OF THE LINE IS CRIMPED TO THE FITTING. FLUID LEAKING OBSERVED AT BOTH ENDS OF THE CRIMSDR UA2R20130207001Fitting · crackedUPON INSPECTION FOUND HYDRAULIC LEAK COMING FROM MANUFACTURED FITTING GOING TO INLET SIDE OF HYDRAULIC PUMP. UPON EXAMINATION WITH AIRCRAFT HYDRAULIC PRESSURE ON PUMP, SAW FLUID COMING FROM SOLDERED JOINT IN FITTING WHERE IT IS BRAZED TOGETHER. ON DISASSEMBSDR SWAA2013020712345Hydraulic Line · rupturedAIR TURNBACK, DECLARED EMERGENCY - HYD B-SYS FAILURE. FOUND B-SYS FLEX LINE ACOUSTIC FILTER & MODULE CHAFED & RUPTURED. REMOVED AND REPLACED LINE PER MM.SDR ULXR201302060001Line · leakingHYDRAULIC LINE LEAKING AT SWAGGED FITTING.SDR L7OA20130204001Hydraulic Line · failedLEFT BRAKE FAILURE, RESULTING IN A DAMAGED PROPELLER. BRAKE WAS FOUND TO HAVE AIR IN THE HYD LINE.SDR JJBA20130202002Hydraulic System · contaminatedDURING CLIMB, CREW REPORTED THE LEFT NOSE DOOR WOULD NOT CLOSE AND THAT THE NR 2 ENGINE HYD PUMP LIGHTS ILLUMINATED, AND THE ROLL SPOILER HYD CAUTION LIGHT ILLUMINATED. GROUND MX CREW BLED AIR FROM THE HYD SYSTEMS. THE GROUND MX CREW PERFORMED A RETRACTION CSDR ASAA2013020293798Hydraulic Line · leakingHYD LEAK NR 1 ENGINE. ACFT GROUNDED. VERIFIED LEAK AT QD FOR HYD AT PYLON. R & R NR 1 ENGINE DRIVEN HYD PUMP PRESSURE LINE. LEAK CHECKED GOOD. REF MM 29-11-11-400-801, 71-00-02-001-801 AND 71-00-02-400-801.SDR UALA2013020400686Fuse · leakingFOUND HYD FUSE ASSY RIGHT MLG WHEEL WELL LEFT SYS LEAKING BEYOND DISPATCH LIMITS. REMOVED AND REPLACED LEAKING FUSE EXTENSION HYDRAULIC FLOW FUSE.SDR SIMA20130204002Hydraulic System · lowON FLIGHT 4512 THE CREW REPORTED THEY RECEIVED A HYD PUMP E1 FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED HYD NR 1 AS PER AMM 12-13-01. CHECK FOR LEAKAGE PER AMM 29-10-00. NO LEASDR CA130201006Line · leaking(CAN) WHILE CARRYING OUT A DAILY INSPECTION OF THE A/C AN AME NOTICED HYDRAULIC FLUID ON THE TRANSMISSION DECK. A GROUND RUN WAS CARRIED OUT TO DETERMINE THE LOCATION OF THE LEAK. THE LEAK WAS FOUND TO BE COMING FROM THE T/R SERVO PRESSURE LINE WHERE THE BRASDR UALA2013013100582Hose · missingHYD Y RSVR LO LVL ECAM SHORTLY AFTER POWER ADVANCED FOR TAKEOFF. TAKEOFF REJECTED. REPLACED MISSING HYD SERVICE HOSE. REPLACED FCDC 1 AND TESTED IAW AMM.SDR FDEA201301310240Check Valve · leakingMAIN CARGO DECK SMOKE DETECTOR ACTIVATED WHEN APU BLEED SELECTED ON. SMOKE FILLED MAIN DECK. CLOSED APU BLEED AND SHUTDOWN APU, BATTERIES. FOUND BOTH RELIEF VALVES STUCK OPEN ON BOTH SIDES. REPLACED APU PRESSURE LINE CHECK VALVE IAW MM 29-14-17-04, REPLACSDR ULXR020120132001Hydraulic Line · leakingHYDRAULIC LINE LEAKING AT SWAGED FITTING.SDR ULXR201202050001Line · leakingLEAKING AT SWAGED FITTING.SDR ULXRTP02012013Line · leakingLINE LEAKING AT SWAGED FITTING.SDR HNAA2013013000028Line · leakingIN FLIGHT, NR 1 SYS LOST HYD PRESSURE. 1/2 QT REMAINED. PRESSURE AT 3000. NR 1 HYD ISOLATION VALVE AND ROLL SPOILER INBD HYD CAUTION LIGHT ILLUMINATED. INSTALLED TEMP FLEX LINE IAW SP 20.2 FROM PRESSURE PORT OF NR 1 ENGINE DRIVEN HYD PUMP TO FIREWALL. SERVICSDR ASMF201303016Packing · damagedDURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED ON HYDRAULIC SYSTEM B. MX PERSONNEL DETECTED A NIPPLE PACKING DAMAGE ON FILTERS MODULE, THE PACKING WAS REPLACED IAW AMM 29-11-00, TESTED CORRECT.SDR DJFA2013F00035Flex Hose · chafedDURING TAKE OFF, LT AND RT HYDRAULIC LEVEL LOW LIGHTS CAME ON CLIMBING THROUGH 5000 FT AND WITHIN TWO MINUTES LT AND RT HYD PRESSURE LOW LIGHTS CAME ON. HYD PRESS WENT TO 0 WITHIN 15 SEC RAN CHECKLISTS DECLARED AN EMERGENCY AND LANDING UNEVENTFULLY. LT ENGINSDR USAA2013012800013Hydraulic Line · chafedCREW RECEIVED A GREEN HYDRAULIC LOW LEVEL ECAM WARNING IN CRUISE. FLIGHT CONTINUED TO CLT, CREW DECLARED AN EMERGENCY FOR LANDING, AND AIRCRAFT WAS TOWED OFF RUNWAY TO GATE. FOUND HYDRAULIC LINE CHAFED ON NR 1 ENGINE COMING FROM ENGINE DRIVEN PUMP PRESSURE SSDR SIMA20130127004Hydraulic System · contaminatedFOR FLIGHT 2759 THE CREW REPORTED THAT DURING THE HYDRAULIC FLIGHT CONTROL CHECK NR 2 HYD RIGHT RUDDER DIFFICULT TO PUSH FORWARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLED RUDDER SYSTEM NR 1 AND SYSTEM NR 2 IAW EMB 145 AMM 27-22-00. THE OPERATIONAL CHECK SDR CA130128017Servo · leaking(CAN) ACFT HAD WARNING LIGHT ON GREEN HYD SYSTEM FLUCTUATING IN AND OUT OF AMBER. EMERGENCY SERVICES WERE ON STAND BY FOR FLIGHT ARRIVAL. ACFT LANDED WITH NO FURTHER ISSUE AND TAXIED ON ITS OWN POWER TO THE GATE. REPLACED G SYS LT YAW DAMPER SERVO IAW AMM 27SDR MU1Z2013022200002Support · brokenDURING MAINTENANCE CHECK, AVA HAS FOUND THE HYDRAULIC SUPPORT P/N D93570603200 COMPLETED BROKEN, AFTER AMAGE IF IT REMAINS UNDETECTED, THE TUBE ASSY P/N D2917002101100 (AIPC 29-13-03-12A ITEM 10A) AND P/N D2917000902000 (AIPC 29-13-03-15C ITEM 70C) MUST BE REPSDR SWAA2013012811997O-Ring · faultyDIVERSION -- A HYDRAULIC SYSTEM LEAK. REPLACE O-RING ON NR 1 ENGINE PRESSURE LINE.SDR DJFA20130125001Hose · meltedCREW REPORTED HYD LEVEL LOW ANNUNCIATOR ILLUMINANTED FOLLOWED BY LT PUMP PRESSURE LOW AND RT PUMP PRESSURE LOW ANNUNCIATOR. MX FOUND THE LT HYD PRESSURE HOSE IN CONTACT WITH THE BLEED AIR LINE, WHICH HAD MELTED THROUGH THE INSULATION OF THE HYD LINE. THE HYD SDR 2013FA0000057Housing · crackedFAILURE OF THE LT HYDRAULIC FILTER HOUSING. HOUSING CRACKED BETWEEN LOWEST AND SECOND LOWEST ATTACHING THREADS. THE HOUSING THEN BENT AWAY FROM UPPER HOUSING CAUSING THE SEALING O-RING TO LEAK SIGNIFICANTLY. ACFT BACK UP SYS WORKED CORRECTLY AND THE LANDING SDR CA130125003Hose · leaking(CAN) AFTER TAKEOFF LOSS ENTIRE NR 2 HYD SYSTEM QTY. RESOLVED ON W/O: 369977, TASKCARD: NR-00001, NLG DRAG STRUT ACTUATOR HYD LINE, PN-AE2463510E0124, LEAKING. REPLACED IAW 32-20-00. INSPECTION OF ENGINE DRIVEN PUMP AFTER FLUID LOSS IAW 05-50-33 AMM, REQUISDR AXSA20130124007Hydraulic System · contaminatedAFTER TAKEOFF FROM MHT PILOT TRIED TO RETRACT LANDING GEAR AND NOSE GEAR WOULD NOT RETRACT. PILOT TRIED TO RETRACT ONE ADDITIONAL TIME AND CB POPPED. CB WAS RESET AND GEAR EXTENDED WITH THREE GREEN INDICATIONS. AIRCRAFT LANDED AT MHT WITHOUT INCIDENT. MAINSDR CA130125006O-Ring · leaking(CAN) DURING FINAL DESCENT, THE LEFT-HAND HYDRAULIC ANNUNCIATOR ILLUMINATED WITH THE HYDRAULIC PRESSURE CONSISTENT AT NORMAL PRESSURE. THE CREW ELECTED TO CONTINUE ON WITH NORMAL OPERATIONS AS LANDING WAS WITHIN 2 - 3 MINUTES. SHORTLY AFTER FLAP EXTENSION THESDR UALA2013012500456Fitting · looseON WALKAROUND, FOUND FLUID ON AIRPLANE AT NOSEGEAR AND DRIPS ON GROUND AROUND NOSEGEAR. CLEANED NOSE WHEEL WELL AREA. WRENCHED CHECKED LINES. PRESSURE LINE FITTING TO NLG ACTUATOR LOOSE. TIGHTENED FITTING.SDR CA130125008Line · leaking(CAN) DURING CRUSE AT 14,000 FT, THE PORT LOW FLOW HYDRAULIC LIGHT ILLUMINATED, FOLLOWED WITHIN 60 SECONDS BY THE STARBOARD LOW FLOW HYDRAULIC LIGHT. APPROXIMATELY FIVE MINUTES LATER THE PORT D.C. GENERATOR FAILED. THE PILOTS TURNED BACK, DECLARED AN EMERGENCYSDR CA130125007Tube · leaking(CAN) UPON LANDING AT AIRPORT HYDRAULIC FLUID WAS OBSERVED LEAKING FROM THE NOSE AREA OF THE ACFT. THE LEAK WAS COMING FROM LT FLAMMABLE FLUID DRAIN DUE TO A CRACKED GEAR UP LINE. LINE WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR COZA20130124022Hydraulic System · lowAIRCRAFT LANDED WITH "A" HYDRUALIC SYSTEM AT 64% AND REFILL ANNUNCIATED. INSPECTION FOUND SIGNS OF FLUID INBOARD OF RIGHT WING AND RIGHT SIDE OF FUSELAGE. RESERVOIR WAS SERVICED. LEAK CHECKS WERE PERFORMED BY ACTUATING LEADING EDGES, FLAPS, SPOILERS AND AILSDR JJBA20130120010Transmitter · fluctuatesDURING CLIMBOUT, CREW REPORTED THAT THE NR 1 HYD PRESSURE WAS FLUCTUATING. THE GROUND MX CREW REPLACED THE PRESSURE TRANSMITTER. ALL OPS CHECKS PRODUCED SATISFACTORY RESULTS AND THE ACFT WAS RETURNED TO SERVICE.SDR ANCF2013012000145Hydraulic Line · brokenPILOT REPORT: DURING CLIMB HYD G SYS LO PR WAS PRESENTED IN THE ECAM. TROUBLESHOT FOUND RIGHT LANDING GEAR DOOR SWIVEL ACTUATOR LINE BROKEN. REPLACED HYD LINE FLEX HOSE ASSY AS PER AMM 32-31-39 PB 401 SERVICED 22 QTS OF HYD FLUID. PERFORMED A TEST OPERATIOSDR USAA2013012200030Hydraulic Line · leakingFLIGHT CREW EXPERIENCED LOSS OF YELLOW HYDRAULIC PRESSURE ENROUTE FROM MBJ TO PHL AND REPORTED 'HYD Y LO LEVEL' FAULT. AN EMERGENCY WAS DECLARED FOR LANDING. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC TUBE LEAKING. REPLACED TUBE.SDR F3LA2013012400824Line · failedDURING CRUISE FLIGHT LOST GREEN SYSTEMS HYD; GREEN SYS HYD INOPERATIVE. FOUND BROKEN HYD LINE AT RT MLG DOOR ACTUATOR. R & R AFT HYD LINE ON RT MLG DOOR ACTUATOR. SERVICED GREEN HYD SYSTEM. LEAK AND OPS CHECKS NORMAL. REF 32-31-35 PB 401.SDR SWIA201332599Hydraulic System · contaminatedHYDRAULIC NR 3 LOW PRESSURE MESSAGE APPEARED ON EDI ALONG WITH GEAR DISAGREE MESSAGE. (FLT 2975) FOUND AIR IN HYDRAULIC SYSTEM NR 3. PURGED SYSTEM. OPS CHECK GOOD.SDR UHLA2013011800012Tube · leakingHYD 2 LOW QTY IN FLIGHT, OBSERVED SYSTEM 2 QUANTITY THEN FALLING FROM APPROX 24% TO 0% WITHIN 90 SECONDS. RAN QRH FOR HYD 2 LOW PRESSURE. DECLARED EMERGENCY, DIVERTED TO IND. LANDED WITHOUT INCIDENT. FOUND PRESSURE TUBE ASSY ON NR 2 ENGINE LEAKING. REMOVESDR CA130121009Line · cracked(CAN) RUDDER DUAL PRESSURE REGULATOR, SYS NR 2, HYDRAULICS, PRESSURE TUBE ASSY RUPTURED PRIOR TO FLIGHT. WHEN PREFORMING RUDDER ACTUATOR TEST, NR 1 RUD SHUTOFF PRESSED, SYSTEM DEACTIVATED, RUD FULL PRESSURE LIGHT DID NOT COME ON. NR 2 RUD SHUT OFF PRESSED, SYSDR CA130117010Line · failed(CAN) APPROXIMATELY 1 HR AFTER TAKEOFF THE CREW REPORTED THEY HAD LOST THEIR BLUE HYDRAULIC SYSTEM. AT THE TIME OF THIS REPORT THERE HAVE BEEN NO FURTHER COMPLICATIONS, ITEM RESOLVE UNDER MDDR: 87626, HYD LINE TO BLUE SYSTEM DAMPENER REPLACED IAW AMM 29-12-00SDR 2013FA0000046Line · leakingDEFECTIVE HYD HOSE - AFTER 5.2 HRS TIME INSERVICE - PILOT LANDED, WHILE LETTING PASSENGERS OFF, NOTICED ALOT OF FLUID - MX WENT TO SITE AND DISCOVERED FLUID COMING OUT OF FITTING OF HOSE.SDR ULXR2012011800001Line · leakingHOSE LEAKING AT SWAGED FITTING.SDR UALA2013011600283Switch · failedCENTER ELEC HYD PUMP DOES NOT PROMPT AN EICAS WHEN TURNED OFF. REPLACED C2 SWITCH BASE ASSY IAW SWPM 20-84-14, WD 29-11-31 AND MM 29-11-00 CENTER HYD SYS TEST. NO FAULTS FOUND EICAS AND PRESSURE LIGHT NORMAL.SDR DXTA2013011705247Hose · leakingUPON GEAR EXTENSION, HYD VOLUME LOW CAS MESSAGE POSTED. CYCLED ON AND OFF UNTIL TOUCHDOW. HYD FLUID IS VISIBLE FROM THE NOSE AND TRAILS THE ENTIRE LENGTH OF THE FUSELAGE. REMOVED AND REPLACED NOSE GEAR ACTUATOR FLEX HYDRAULIC EXTENSION LINE IAW MM 20-10-01. SDR 2013FA0000034Hose · leakingHYDRAULIC HOSE LEAKING AT SWAGED FITTING.SDR CA130116015Line · cracked(CAN) IN CRUISE, CREW NOTICED A HYDRAULIC SYSTEM B LOW PRESSURE LIGHT AND A CORRESPONDING LOSS OF QUANTITY. CREW DIVERTED TO NEAREST AIRPORT WHERE A HYDRAULIC PUMP PRESSURE LINE WAS FOUND TO BE CRACKED. THE LINE WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR 2013F00018Swivel Fitting · blew outAFTER TAKEOFF PILOT REPORTED NO HYD PRESSURE. UPON LANDING SAFELY AND TROUBLESHOOTING THE ISSUE , FOUND THE MLG ACTUATOR RETRACT SWIVEL FITTING HAD FAILED. R & R THE SWIVEL FITTING WITH A NEW PART (PN 142870). PERFORMED ALL GEAR SWINGS AND ASSOCIATED HYDSDR UALA2013011400203O-Ring · leakingHYDRAULIC FLUID LEAKING FROM STAB COMPARTMENT DRAIN ON BELLY. FOUND LEFT STAB TRIM CONTROL MODULE BRAKE PRESSURE SWITCH LEAKING 30 DROPS MIN. REPLACED O-RING SEALS. LEAK CHECKED GOOD. CLEANED AND FLUSHED COMPARTMENT OF RESIDUAL FLUID.SDR HNAA2013011400006Line · rupturedNR 2 HYD QTY AT .5 WITH FLUID LEAKING IN NR 2 NACELLE WITH RUDDER ISOLATION VALVE CAUTION LIGHT ILLUMINATED. INSPECTED NR 2 WHEEL WELL AND FOUND HYD LINE FOR AFT GEAR DOOR FROM ELECTRIC SEQUENCE VALVE ACTUATOR RUPTURED. INSTALLED TEMP FLEX LINE IAW SP20.1 S
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