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 TSAA0829008Hose · failedNON-ETOPS FLIGHT 215 HNL-LIH, DURING CRUISE FLIGHT, THE CREW NOTED THE HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO. CREW COMPLETED THE HYDRAULIC SYSTEM A FAILURE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCSDR B3OR2008046Servo Control · leakingON A ROUTINE PREFLIGHT INSPECTION, THE LT HYDRAULIC ROLL CONTROL SERVO WAS DISCOVERED TO BE LEAKING HYDRAULIC FLUID AT THE PISTON SHAFT SEAL. THE LEAK COULD NOT BE DUPLICATED DURING GROUND TESTING WITH A HYDRAULIC POWER CART IAW THE MM INSTRUCTIONS. SUBSEQUESDR COMA0860131Hydraulic System · malfunctionedFLIGHT 5381- EN ROUTE FROM JFK TO RIC, 31 HYDRAULICS READING 30% DURING HOLDING. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO ORF AND LANDED SAFELY. PERFORMED LEAK CHECK AND DIRECT READING GAUGE CHECK. ALL CHECKS GOOD. DEFERRED PER MEL 29-32-01.SDR 0211Line · chafedFOUND BOTH LT AND RT MLG UPLOCK HYD LINES P/N 5927120-10 AND 5927120-11 WITH TOOLING MARKS. THESE MARKS EXCEEDED THE MIN WALL THICKNESS AND HAD DENTED THE LINE. THE TOOLING MARKS ARE CAUSED BY YEARS OF REMOVING AN INSPECTION PANEL DIRECTLY BEHIND THE LINE. MORSDR 2008UALA00783O-Ring · leakingLANDED UNDER AMBER ALERT DUE TO CENTER HYDRAULIC SYSTEM INDICATION. CONDUCTED TROUBLESHOOTING. FOUND NR 3 SPOILER ACTUATOR PLUG FOR FINGER FILTER O'RING BAD. REPLACE O'RING. OPERATES NORMALLY WITH NO LEAKS NOTED. SERVICED CENTER HYD SYSTEM FLUID TO FULL. SDR 2008FA0000107Powerpack · wornSMOKE IN COCKPIT, GEAR NOT FULLY RETRACTED, EXTENDED OK. FOUND HYDRAULIC POWERPACK MOTOR (ORIGINAL) WORNOUT. REMOVED AND REPLACED WITH O/H UNIT. OPS, OK.SDR HNAA0800061Hydraulic Line · leakingNR 2 HYD QTY DROPPED TO .5 QTS AFTER T/O ASSOCIATED W/ISO LIGHT ILLUMINATED. RETURNED TO FIELD. INSTALLED TFL BEHIND NOSE GEAR GRAVEL GUARD, PLACED ON 70HR DMT, REMOVED FLEX LINE AND INSTALLED RIGID LINE.SDR 2008UALA00658Pressure Switch · faultyRIGHT HYDRAULIC SYSTEM RESERVOIR LIGHT ILLUMINATED. FOUND PRESSURE SWITCH FAULTY. REPLACED PRESSURE SWITCH, NO REPEATS.SDR DXTA200802836Line · wornON FO SIDE, RT BRAKE FEELS SLUGGISH COMPARED TO THE LT BRAKE. REMOVED AND REPLACED CO-PILOTS LT AND RT BRAKE MASTER CYLINDER PRESSURE AND RETURN LINES (4EA) AND BLED HYD SYS ALL WORK PERFORMED IAW MM, CH 32-42-02 AND 32-42-00.SDR NWAA080389758O-Ring · failedIN CRUISE FLT AT FL310, THE RT HYD SYS FAILED. QTY AND PRESSURE WERE BOTH LOST REQUIRING CREW TO SECURE SYSTEM. FLT CONTINUED AS SCHEDULED AND THE EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED ON APPROACH. LANDING AT TPA INVOLVED THE GEAR DOORS MAKING CSDR SWIA200819169Line · leakingFLT 3776 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. REPLACED LEAKING FLEX LINE TO ACTUATOR. NO LEAKS NOTED.SDR USAA920080340Hydraulic System · lowFLT NR 9205 - PIT-PHX - EMERGENCY LANDING, DURING DESCENT RECEIVED HYDRAULIC GREEN RESERVOIR LOW LEVEL ECAM. VERIFIED INDICATION AT TOP OF AMBER BAND. COMPLIED WITH ECAM AND SHUT DOWN GREEN SYSTEM UNTIL GEAR EXTENSION REQUIRED. AFTER GEAR EXTENSION LEVEL INSDR CA080213007Hose · leaking(CAN) DURING INSP OF FLAP SYS FOUND 6 HYD HOSES FOR SPEED-BRAKE/LIFT-DUMP ACTUATORS WITH MINOR HYD FLUID SEEPAGE. THE FOLLOWING PN HOSES WERE REPLACED. AE1011925E0087, AE1011925E0094, AE1011925E0121, AE1011888E0132, AE1011924E0103, AE1011933E0086.SDR F3LA200800041Tube · leakingDURING DESCENT & APPROACH, CREW REPORTED AN ECAM INDICATION OF LOW HYD PRESSURE & LOW HYD FLUID LEVEL FOR GREEN HYDC SYS. AN EMERGENCY DECLARED & CREW MANUALLY EXTENDED MLG. ACFT MADE AN UNEVENTFUL LANDING. MX FOUND A HYD TUBE ASSY LEAKING ON NR 1 ENGINE. SDR NWAA080303240Manifold · leakingYELLOW HYDRAULIC LOW LEVEL AT CRUISE. FOLLOWED ECAM AND COM PROCEDURES. AIRCRAFT LANDED UNEVENTFULLY. REPLACED YELLOW HP MANIFOLD, LEAK CHECKS OK.SDR 08FDEA00325Module · failedAFTER POWER TO FLEX AROUND 40K HAD TO ABORT TAKEOFF DUE TO YELLOW HYD LOW AER ECAM, AFTER ABORT, ALL RESET TRIED AGAIN SAME OUTCOME ABORTED T/O AROUND 52K. REMOVED AND REPLACED YELLOW SYSTEM RESERVOIR CHECK VALVE. REMOVED AND REPLACED DIODE MODULE 35VD. ALLSDR AALA200800196Line · leakingSJU INFLIGHT T1692/29JAN - CREW REPORTED HYDRAULIC ODOR IN CABIN AROUND SEAT ROW 17AB. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LEAK AT SEAT ROW 16AB. REPAIRED HYDRAULIC LINE AT SEAT ROW 16AB AND CLEANED AREA. SYSTEM GROUND CHECKED NORMSDR SIMA200803106Valve · leakingON FLIGHT 4078, CREW REPORTED ON DESCENT WHEN SELECTING GEAR DOWN NR 3 HYD PRESSURE AND QUANTITY WENT TO ZERO, DECIDED TO DO A FLY BY AND DECLARED AN EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOW LIMITER VALVE PER CRJ AMM 29-12-13 AND 8SDR UPS08851569Hose · chafedTHE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN TO AUX AT THE "X" AND AIL CTRL MANUAL AND RUDDER CTRL MANUAL LTS ILLUM. RAN LOSS OF HYD FLUID/PRSDR SIMA200803105Line · crackedON FLIGHT 3626 CREW REPORTED DURING CRUISE THE NUMBER 3 HYDRAULIC SYSTEM DROPPED TO 5 PERCENT QUANTITY AND 0 PSI. CREW DECLARE AN EMERGENCY AND DIVERTING TO OKC DUE TO WEATHER IN DFW. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 3A HYDRAULIC PUMP PRESS LINE SDR AALA200800177Module · inoperativeAUS INFLIGHT T1622/26JAN - LEFT AND RIGHT HYDRAULIC LOW PRESSURE INDICATION DURING DESCENT. LANDED AUS WITHOUT INCIDENT. REPLACED HYDRAULIC PUMP MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR 2008FA0000078Hydraulic System · contaminatedHYD POWER PACK PRE-CLOGGING INDICATOR IS DISPLAYED BEFORE FLIGHT.SDR A6WA200840052Hydraulic System · leakingIB CREW REPORTED HYD NR 2 LEAK ON SHORT FINAL. HYD NR 2 CAUTION MESSAGE RECEIVED. HYD QUANTITY NO READS 25 PERCENT. (K)SDR CA080124002Swivel · leaking(CAN) AC WAS DISPATCHED AND DURING CRUISE FLIGHT, THE FLIGHT ENGINEER NOTICED THAT THE (A) SYS HYDRAULICS INDICATED .1250 OF A TANK REMAINING. THE CREW DECIDED TO DECLARE AN EMERGENCY AND THE LANDING GEAR NEEDED TO BE CRANKED DOWN. THE AC LANDED SAFELY AND WASSDR C2XA08ON074Line · disconnectedFLT 0017 - TUS TO SAT - DURING CRUISE FLIGHT CREW REPORTED HYD SYS 1 INDICATED 0 PRESSURE AND 0 QUANTITY. CONTRACT AND ONT MX PERSONNEL WERE DISPATCHED. AIRCRAFT DIVERTED TO TUS AND DECLARED NO EMERGENCY AND LANDED SAFELY. MX PERSONNEL AFTER VISUAL INSPECTISDR CA080214007Hydraulic Line · cracked(CAN) WHILE ENROUTE THE "IB ROLL SPL HYD" AND NR 1 "HYD ISO VLV" CAUTION LIGHTS ILLUMINATED. CHECKED THE HYD QUANTITY AND NOTICED NR 1 QUANTITY AT 1.0 AND DECREASING. COMPLETED THE QRH CHECKLIST AND THEN BRIEFED THE F/A AND PASSENGERS. MADE A VISUAL APPROACH ASDR AALA200800122Drain · crackedORD INFLIGHT T538/21JAN - RIGHT HYDRAULIC QUANTITY INDICATION ILLUMINATED SHOWING DECREASE IN FLIGHT. LANDED ORD WITHOUT INCIDENT. FOUND HYDRAULIC DRAIN ON NR 2 ENGINE CRACKED. REPLACED HYDRAULIC DRAIN ON NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPESDR NWAA080233224Line · leakingHYDRAULIC "G" LOW QUANTITY, ALSO LOW ON ECAM. FOLLOWED COM, LANDING GEAR GRAVITY EXTENDED AND LANDED UNEVENTFULLY. AIRCRAFT TOWED TO GATE. REPLACED HYDRAULIC LINE ON NR 1 THRUST REVERSER. CHECKS GOOD.SDR 08FDEA00192Hydraulic System · lowREJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE.SDR NWAA080183264Hydraulic System · emptyALL HYDRAULIC FLUID GONE FROM YELLOW HYDRAULIC SYSTEM. PERFORMED HYD RSVR LO LVL PROC AS PER COM. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE.SDR NWAA080163240O-Ring · leakingDURING CRUISE FLIGHT HYD Y RSVR LO LVL, FOLLOWED COM PROCEDURE. AIRCRAFT LANDED UNEVENTFULLY WITH ZERO HYD QUANTITY. REPLACED O-RING ON YELLOW HP MANIFOLD, LEAK CHECKS GOOD.SDR A6WA200840012Cooler · vibrationAIRFRAME VIBRATION FELT AF VIBES FELT FROM T/O, TO DESCENT , WENT AWAY ON FINAL APPROACH. FELT IN REAR ON LT SIDE OF THE AC EVIDENT AT ROW 13 BUT NOT EVIDENT IN LAV. REMOVE AND REPLACED HYDRAULIC COOLER REF AMM 29-11-42, OPS CHECK GOOD. (K)SDR 2008UALA00201Fitting · damagedDIVERTED UNDER AMBER ALERT DUE TO HYDRAULIC PROBLEM. FOUND LOOSE GROUND SPOILER PRESSURE FITTING AT THE NR 5 SPOILER INBOARD ACTUATOR. REPLACED UNION AND PACKING.
SDR AALA200800053Hose · leakingLAX INFLIGHT T2454/12JAN - RECEIVED RIGHT HYDRAULIC LOSS INDICATION. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND RIGHT HYDRAULIC LINE DAMAGED AT RIGHT WHEEL WELL REAR SPAR. REPLACED RIGHT HYDRAULIC LINE AT RIGHT WHEEL WELL REAR SPAR. SYSTEM GROUND SDR SWAA080317O-Ring · leakingDIVERSION - ON CLIMB TO CRUISE "B" HYDRAULIC SYSTEM SLOWLY DECREASED TO "0" QUANTITY. DID NOT LOOSE "B" SYSTEM PRESSURE UNTIL FLAPS LOWERED ON APPROACH. REMOVED AND REPLACED "O" RING LEAKING ON PRESSURE SWITCH AT "B" SYSTEM HYDRAULIC MODULE PER MM.SDR UG8A08P011002Line · bentHYDRAULIC LINE IN TAIL COMPARTMENT JUST AFT OF LT ELT IS BENT/DENTED.SDR DL76G090028Hose · leakingRIGHT HYD QTY EICAS MESSAGE WITH RT HYD QTY LIGHT. RT SYSTEM QTY INDICATING 0.47 WITH RF AND DECREASING SLOWLY 5 HOURS AND 20 MIN INTO FLIGHT. REPLACED LINE WITH BORROW PART FROM AIR FRANCE. FOUND RT ENG EDP HYDRAULIC PRESS HOSE ASSEMBLY LEAKING. REPLACED SDR AALA200800041Module · dirtyDEW IN-FLIGHT T1105/07JAN - LEFT ENGINE HYDRAULIC INDICATION FLICKERING FOLLOWED BY RIGHT ENGINE HYDRAULIC INDICATION FLICKERING. LANDED DEW WITHOUT INCIDENT. FOUND RESERVOIR MODULE AND FILTER DIRTY. REPLACED RIGHT RESERVOIR PRESSURE MODULE AND FILTER. SYSSDR CHQA200800007Line · leakingSTL TO EWR - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE WITH THE SYSTEM 2 HYDRAULIC PRESSURE AT ZERO AND QUANTITY IN THE AMBER RANGE. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOSDR C8GA20080002Line · chafedFLT 246 FROM EWR TO BDA. DURING DESCENT INTO BDA, THE NR 2 HYDRAULIC "B" SYSTEM PUMP LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY A PRESSURE DROP TO ZERO PSIG. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FIGHT INSPECTION REVEALED THAT THE PRESSURE AND RETURN LISDR HNAA0800025Hydraulic Line · failedNR 1 HYDRAULIC ISO CAUTION LIGHT ILLUMINATED, NR 1 HYDRAULIC QUANTITY DROPPED TO 0 AND NR 1 HYDRAULIC PRESSURE DROPPED TO 0 PSI WITH CORRESPONDING CAUTION LIGHTS. NR 1 ENGINE HYDRAULIC PUMP OPERATED APPROXIMATELY 14 MINUTES WITH NO PRESSURE. FOUND FLUID DRIPSDR UIEA200800006O-Ring · leakingAPPROX 1 HOUR 15 MIN AFTER T/O NR 1 ENGINE OIL QTY IND ZERO, TEMP AND PRESS NORMAL ABOUT 2 HOURS 30 MIN AFTER T/O PRESSURE BEGAN VERY SLOW DROP WITH SLOW FLUX 5 PSI DURING DESCENT WITH ENGINE AT IDLE OIL PRESSURE LIGHT ILLUMINATED OCCASIONALLY BUT PRESS NEVER SDR CHQA200800005Line · crackedIAH TO CMH - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE THEN CONFIRMED THAT THE SYSTEM 2 QUANTITY WAS ZERO. THE AIRCRAFT RETURNED TO FIELD AT IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND A HAIRLSDR HNAA0800017Hydraulic Line · leakingA HEAVY CHEMICAL SMELL IN CABIN DURING FINAL PHASE OF FLIGHT WAS NOTICED. REMOVED AND REPLACED THE LEAKING SECTION OF HYDRAULIC LINE FOR LANDING GEAR DOWN SELECT UNDER THE CABIN FLOOR AT FORWARD EMERGENCY EXIT. LEAK CHECK GOOD.SDR 2008UALA0039Hydraulic System · failedLANDED UNDER AMBER ALERT DUE TO A FAILED GREEN HYDRAULIC SYSTEM.SDR CA080105002Switch · broken(CAN) SDR BEING SUBMITTED DUE TO (3) OCCURRENCES OF (RUD PRESS) AND (RUD FULL PRESS) CAUTION MESSAGES OVER A PERIOD OF (4) DAYS. (1ST) EVENT OCCURRED DECEMBER 30, 2007 JUST AFTER TAKEOFF AND CAUSED AN AIR TURN BACK TO THE DEPARTURE AIRPORT. MAINT PERFORMED GROSDR 08FDEA00005Control Valve · failedARM LIGHT AND CARGO DOOR IN TRANSIT LIGHT ILLUMINATED IN FLIGHT. PRESSURIZATION REMAINED NORMAL. REPLACED HYDRAULIC SOLENOID SHUTOFF VALVE PER MM 52-34-129-4. REPLACED HYDRAULIC CONTROL VALVE PER MM 52-34-101-4. OPS OK PER MM 52-34-009-5.SDR HSYA20080101Line · rupturedJUST AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. SHORTLY AFTERWARDS BOTH OF THE HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND PERFORMED THE ABNORMAL PROCEDURES LIST FOR HSDR TRAX200800052Hydraulic Line · chafedLT WING T/E-HYD LINE CHAFING ON WIRE BUNDLE AT WING STA 50 "FLAGGED". E/C PERFORMED IAW NTM CRACK CONFIRMED IN X AXIS, END OF CRACK MARKED. NO CRACK FOUND IN Y AXIS.
SDR ARWA20071206O-Ring · leakingLOST HYDRAULIC QUANTITY BELOW 6 GALLONS SYSTEM 3; HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT "ON". REMOVED AND REPLACED "O" RING AT LOWER FITTING OF REVERSIBLE MOTOR PUMP SHUTOFF VALVE NR 1-3 IN ACCORDANCE WITH M/M 29-22-01; OPERATIONAL CHECK AND LEAK CHECKED IN A
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