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 TN8A2015011500001Valve · failedFLIGHT RETURNING TO BASE AFTER FREIGHT CHARTER FLIGHT. UPON APPROACH PILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE A GREEN LIGHT INDICATION FOR THE NOSE GEAR. PILOT RECYCLED GEAR AND REQUESTED TO TERMINATE LANDING. PILOT MANUAL EXTENDED THE LANDING GEAR IAW SDR CA141229006Hose · ruptured(CAN) ARRIVED WITHOUT ISSUE AFTER THE AIRCRAFT EXPERIENCED A LOSS IN HYDRAULIC PRESSURE. RESOLUTION MAINTENANCE CREW FOUND LT HYDRAULIC FLEX LINE BETWEEN RUDDER RATIO CHANGER AND MODULE LEAKING. LINE REPLACED IAW 27-21-15 PB 201 AND AMM 20-10-10.SDR CA150103001Clamp · deteriorated(CAN) THE NR 2 DCMP RIGID HYDRAULIC SUPPLY TUBE LEAKED DUE TO A PIN HOLE CAUSED BY A DETERIORATED CLAMP WHICH CHAFFED THROUGH THE TUBE ASSEMBLY.SDR USAA2014123000007Hydraulic Line · damagedY HYD RESERVOIR EMPTIED IN FLIGHT. Y SYS SHUTDOWN IAW ECAM PROCEDURES. REPLACED BOTH SUCTION & PRESS HYD PIPES IN RT ENG PYLON. LEAK CHECKED GOOD IAW AMM 29-13-49 PB 0401.SDR QXEA2014121401109Pressure Switch · failedNR 2 HYDRAULIC ISOLATION VALVE ILLUMINATED AFTER TAKEOFF. ALL HYD PRESSURES AND QUANTITIES INDICATED NORMAL. NO OTHER LOSS OF SYSTEMS. AFTER GEAR WAS EXTENDED, NR 2 HYD ISOLATION VALVE FLICKERED INTERMITTENTLY DURING LANDING. R & R NR 2 HYD ISOLATION VALVSDR F3LA2014122901095Hydraulic Line · failedGREEN SYS HYD LINE FAILED, FLUID LOSS, RETURNED TO THE FIELD. R & R THE LINE ASSEMBLY IAW AMM 32-31-39-400-001-A. OPERATIONS IAW AMM 32-31-00-710-002-A01 & LEAK CHECKED NORMAL. LOG PAGE 911844 2.SDR 9EKA2014122314Elbow · wornOIL COOLER CAUTION PANEL LIGHT CAME ON DURING FLIGHT. ENGAGED SECONDARY OIL COOLER SYS & RETURNED TO BASE IAW EMER PROCEDURES IN ROTOR FLIGHT CRAFT MANUAL.SDR AALA20141223010Line · leakingEMERGENCY DECLARED, RETURNED TO DEPARTURE, & LANDED UNEVENTFULLY. FOUND HYDRAULIC LINE BROKEN. REPLACED HYDRAULIC LINE ON RIGHT MAIN LANDING GEAR IAW AMM 20-10-10. OPS AND LEAK CHECKED GOOD.SDR CALA2014122692867O-Ring · blownSYSTEM Y HYD QTY LOST IN FLIGHT. RESERVOIR QTY DROPPED WITH NO SYS PRESS. DIVERTED & FOUND PTU O RINGS BLOWN OUT. REPLACED CHECK VLV ASSEMBLY & O RINGS FOR PTU. OPERATIONS CHECKED & LEAK GOOD. SERVICED SYS TO NORMAL.SDR CALA2014122392861Hydraulic Line · leakingHYD Y ENG 2 PUMP LOW PRESS ECAM & YELLOW HYD LOW PRESS ECAM WARNINGS. OBSERVED YELLOW HYD QTY LOW. FOLLOWED QRH, SELECTED NR 2 ENG HYD PUMP OFF, PRESS & QTY STABILIZED. PERFORMED ENG RUNS, NO FAULTS ON ECAM FOUND HYD LINE IN RIGHT WW LEAKING. REPLACED LINESDR YENA20141220277Line · leakingRETURN TO DEPARTURE DUE TO YELLOW HYD SYSTEM QTY DROPPED TO ZERO IN FLIGHT. ACCOMPLISHED TEMP REPAIR OF HYD LINE IN STABILIZER COMPARTMENT IAW AMM 20-23-14-300-004.SDR USAA2014121900007Line · leakingAFTER LANDING ROLLOUT, LOST PARTIAL HYD & NOSE WHEEL STEERING. ACFT TOWED TO THE GATE. FOUND NR 1 ENG RETURN LINE LEAKING IN PYLON AREA. REPLACED HYD LINE IAW AMM 29-00-00-910-004-A.SDR AALA20141220001Switch · malfunctionedEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH TE FLAP DISAGREE MSG RECEIVED. ALTERNATE FLAP EXTENSION USED IAW QRH. CHECKED C SYS ELEC MOTOR PUMP C1 & C2. PERFORMED FSEU BITE TEST IAW FIM 27-51-00 WITH NO FAULTS FOUND. CHECSDR SIMA20141218004O-Ring · missingNUMBER 1 ENG LEAK, DECLARED EMER, LANDED SHOWING 15%. FOUND MISSING O RING ON NR 1 ENG HYD PUMP, SHEAR SHAFT. INSTALLED NR 1 SHEAR SHAFT O RING IAW AMM 29-11-01. OPERATIONS & LEAK CHECKED GOOD.SDR YADA20141218001Hydraulic Line · rupturedON APPROACH FLIGHT CREW SELECTED LANDING GEAR DOWN. THE NOSE GEAR FAILED TO COMPLETELY EXTEND & LOCK, LANDING GEAR PUMP CONTINUED TO RUN. THE PILOT PULLED THE LG CB & THEN THE HYD LOW LEVEL ANNUNCIATOR ILLUMINATED. THE PILOT COMPLETED THE GEAR EXTENSION WITSDR QXEA2014121801101Shuttle Valve · leakingON LANDING, ALMOST NO BRAKING ACTION. ON POST FLIGHT NR 1 BRAKE WARM AND NR 2 SLIGHTLY WARM. NR 3 AND 4 BRAKES ARE COLD. C/W WITH MAIN LAND. GEAR BRAKE FUNCTION, TEST REF 32-42-00-720-801. C/W ANTI-SKID FUNCTION TEST REF AMM TASK 32-46-00-720-802. NO DEFSDR GHEA2014121700001Line · leakingTHE ACFT DEPARTED, THE MASTER CAUTION LIGHT ILLUMINATED. THE HYDRAULIC PRESSURE INDICATED BELOW 2000 PSI. FLIGHT DIVERTED. THE LANDING GEAR WAS EXTENDED BY THE ALTERNATE MEANS AND THE ACFT LANDED. THE ACFT WAS GROUNDED. MAINTENANCE FOUND A SMALL LEAK IN ASDR JIKA2014121701Hydraulic Line · leakingTHE PILOT REPORTED THAT BOTH LT & RT HYD FAILURE LIGHTS ILLUMINATED, WHILE THE HYD PRESS GAUGE WAS FLUCTUATING. UNABLE TO EXTEND THE FLAPS PAST THE ¼ POSITION. WHEN THE PILOT PUT THE GEAR HANDLE TO THE DOWN POSITION THE LG DID NOT EXTEND & THE HYD SYS PRESS GSDR JIKA2014121501Fitting · looseDURING CLIMB OUT, AT 9000’ THE LG IN TRANSIT WARNING LIGHT ILLUMINATED. FOUND THE LG CONTROL RELAY CB POPPED & RESET IT, THE LG WARNING LIGHT REMAINED ILLUMINATED. MADE TWO ATTEMPTS TO RECYCLE THE LG AT THIS POINT THE “HYD FLUID LOW” ANNUNCIATOR LIGHT ILLUMISDR HNAA2014121500363Line · leakingF/A REPORTS STRONG ODOR CAUSING COUGHING, WHILE TAXIING, AFTER LANDING. FOUND HYD LEAK UNDER SEAT 3DF. REPAIRED USING RING-LOCK IAW 20-55-55 AND SEAT WC 25-00-03R. OPS CHECKED GOOD. OK FOR SERVICE.SDR DXTA2014121505945Line · chafedLOW HYD LEVEL LIGHT CAME ON SHORTLY AFTER TAKEOFF. RAISED THE GEAR & THEN THE FLAPS. THE LIGHT CAME ON IMMEDIATELY AFTER THE FLAPS WERE RAISED. THERE WERE NO OTHER INDICATIONS. WENT TO THE ABBREVIATED CHECKLIST WHICH STATED IN PART TO LAND AS SOON AS PRACTSDR CA141212004Module · failed(CAN) CREW REPORTED LOSS OF HYDRAULIC PRESSURE IN THE CENTRE HYDRAULIC SYSTEM. ATC WAS ADVISED. STATION WAS ADVISED. MTC WAS ADVISED. A PAN PAN PAN WAS DECLARED. ATC GAVE AC117 AN EXTENDED DOWNWIND WHILE THE CREW WENT OVER THE HYDRAULICS SYSTEM PROCEDURES. MTCSDR REXA2014121101179Hydraulic System · contaminatedGEAR UP DISAGREE ON CLIMB OUT. MSG WITHIN 6 SEC IN ORDER AS FOLLOWS, HYD 3 CAUTION, GEAR DISAGREE WARNING & NOSE DOOR WARNING. MSGS CLEARED ON THEIR OWN WITHIN 2 MINUTES. R & R NR 3 BRAKE ACCUMULATOR IAW AMM 32-43-16. BLED NR 3 HYD SYS IAW AMM 29-10-00. GSDR CA141211003Union · leaking(CAN) HYDRAULIC FLUID WAS NOTED ON THE AIRCRAFT IN THE VICINITY OF THE NOSE LANDING GEAR. MAINTENANCE INSPECTION CONFIRMED THAT THE LEAK WAS COMING FROM THE NLG LOCK ACTUATOR ASSEMBLY. BOTH UNIONS ON THE ACTUATOR WERE FOUND LOOSE & WERE TIGHTENED. ONE FLEX SDR FDEA201412084078Union · looseLEFT PYLON AFT FAIRING FROM FWD TO AFT NR 4 HYD TUBE CONNECTOR LOOSE. REMOVED THE FITTING OF THE HYD TUBE BETWEEN WING AND PYLON IAW AMM 29-00-00-04 & DWG A29011098. MINOR REPAIR IAW GMM 6-2-100SDR CA141215006Accumulator · leaking(CAN) VERY SLOW LEAK FOUND IN HYDRAULIC LANDING GEAR ACCUMULATOR FOR THE LANDING GEAR. TROUBLESHOOTING DETERMINED THE LEAK TO BE AN INTERNAL LEAK WITHIN HYDRAULIC ACCUMULATOR AND THE UNIT WAS REPLACED WITH OVERHAULED UNIT.SDR UHLA2015010500043Line · looseLEFT WING HYDRAULIC TUBE ADJACENT TO RETRACT ACTUATOR PASSING THRU SPAR 3 SHOWING SIGNS OF LOOSENESS. REPAIRED LT WING SPAR 3 HYD LINE PASS THRU HOLE FCBS57-10-00-001, IAW ETD 2015-170-000300.SDR DALA2014120406421Line · leakingDURING INITIAL CLIMBOUT, CREW REPORTED A HOT HYDRAULIC ODOR BEING EMITTED FROM THE AIR CONDITIONING SYSTEM. BOTH THE FORWARD AND THE REAR LAVATORY SMOKE DETECTORS SOUNDED. ODOR DISSIPATED AND ALARMS SILENCED QUICKLY BUT THEN IT ALL REPEATED DURING APPROACH FSDR SWIA201440293Line · failedLOST ALL GREEN SYSTEM HYDRAULIC FLUID ENROUTE. NO EMERGENCY DECLARED. REPAIRED CHAFED GREEN SYSTEM PRESSURE LINE AT OTBD LOWER NACELLE AREA IAW AMM. R & R LT ENGINE HYDRAULIC DRIVEN PUMP IAW AMM. PRESSURIZATION AND LEAK CHECKED GOOD.SDR SWIA2014120140223Line · failedLOST GREEN HYDRAULIC SYSTEM IN FLIGHT. REPAIRED A HYDRAULIC LINE NEAR BS 3600 IN THE LT NACELLE IAW AMM. LEAK AND OPS CHECKED GOOD.SDR CA150911011Hose · failed(CAN) BOMBARDIER RECEIVED A DISCLOSURE LETTER REGARDING THE CAPABILITY OF HOSE ASSEMBLIES THAT ARE USED ON THE POWERPLANT HYDRAULIC SYSTEM INSTALLATIONS. BOMBARDIER ASSESSED THE POTENTIEL SAFETY CONCERNS THEN. A REVIEW OF THIS FORMER ASSESSMENT WILL BE CONDUCTSDR HALA2014112400196O-Ring · leakingAIR DIVERSION, HYD Y RESVOIR LOW LEVEL. IAW FLT CREW THEY SHUTOFF YELLOW HYD PUMP AND ENGINE PUMP. RESERVOIR NOT EMPTY. PUMPS DID NOT CAVITATE. FOUND ON YELLOW HP MANIFOLD. CAPPED OFF LINE, O-RING BAD, REPLACED O-RING IAW AMM 29-00-00, AND LEAK CHECKED IASDR CALA2014112492744Hydraulic System · lowHYDRAULIC GREEN SYS LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. SERVICED HYDRAULICS IAW AMM 29-31-00-710-001-A. TAXI RUN ACCOMPLISHED, ALL NORMAL.SDR AALA20141123010B-Nut · looseEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT RT HYD SYS QTY INDICATED LOW & DECREASING. PERFORMED QRH & LANDED WITH RT HYD ENG & AUXILIARY PUMPS OFF. FOUND B NUT LEAKING AT LG MANIFOLD. TORQUED NUT IAW SP 20-30-02. PERFORMEDSDR FDEA201411233866Hydraulic System · contaminatedON TAXI OUT DID A FLIGHT CONTROL CHECK & ECAM DISPLAYED BRIEFLY A GREEN HYD PUMP 1 & 2 LOW PRESS. DID A FULL RECHECK OF FLIGHT CONTROLS WITH NO ECAM. ON TAKEOFF ROLL AROUND 60KTS RECEIVED A GREEN HYD PUMP 1 & 2 LOW PRESS WARNING AGAIN ON ECAM. REJECTED TAKSDR YENA20141121256Line · leakingCREW DECLARED AN EMERGENCY DUE TO ECAM HYD GREEN RSVR LOW LEVEL. CREW PERFORMED A MANUAL GEAR EXTENSION. THE TECH SECURED MANUAL EXTENSION HANDLE IAW AMM 32-33-00-860-072A. INSPECTED, FOUND LINE PUNCTURED ABOVE ENGINE NR 1 PYLON REF IPC 29-11-06, FIG 2D ITEM 2SDR IPXA2014112184911Actuator · leakingMAIN CONTROLLER QTY DECREASE .12, SYSTEM DEPRESSURIZED. FLUID LOSS OF CONTROLLER HYDRAULIC SYS, LEAK STOPPED. R & R RT LCCA. OPS CHECK GOOD IAW AMM 22-13-03-004-035 AND 22-13-03-404-046. MCDP GROUND TEST, 07 CHECKS GOOD IAW AMM 22-00-02-201.SDR SWIA201440003Pcu · failedDIVERTED DUE TO HYD 2A LOW PRESSURE CAUTION AT CRUISE. R & R PCU ASSY IAW AMM. OPS CHECK GOOD, NO LEAKING NOTED.SDR REXA2014111801140Packing · damagedTASK CARD 900-53-900-504 2 LT, 4 RT, 6 TOTAL RUBBER DECOMPRESSION PANEL BETWEEN FS 280.00 & FS 477.40 ARE TORN. UPON GEAR RETRACTION RECEIVED NR 3 HYD CAUTION FOLLOWED BY GEAR DISAGREE WARNING HYD NR 3 WAS SHOWING BOTH PUMPS OFF, YELLOW FLOW LINES & 100% CAPASDR VQI2014F00036Hose · leakingDURING APPROACH, REPORTED LOSS OF YELLOW AND GREEN SYSTEM HYDRAULIC PRESSURE AND A LOSS OF GREEN HYDRAULIC FLUID. YELLOW SYS WAS RECOVERED SHORTLY AFTER. CREW REPORTED AN EMERGENCY BUT LANDED SAFELY. MAINTENANCE DISCOVERED A MLG DOOR ACTUATOR HOSE ON THE LTSDR VQI2014F00035Hose · leakingDURING APPROACH, REPORTED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE DISCOVERED A MLG DOOR ACTUATOR HOSE ON THE LT SIDE LEAKING. R & R IAW AMM 32-31-39-401, NO LEAKS NOTED AFTERWARD, ALL OPS CHECKS NORMAL AND THE ACFT WAS PLACED BACK INTO SERVICE AT 1SDR 2015F00003Structure · crackedSTRUCTURE WAS FOUND TO CONTAIN AN INTERNAL CRACK AT THE FILTER BOWL PORT ON THE PACKAGE ASSEMBLY. THIS CRACK APPEARS TO HAVE ORIGINATED AT A HIGH SPOT IN AN INTERNAL PORT, STRESS RISER AND PROPEGATED THROUGH THE HOUSING RESULTING IN EXTERNAL FLUID LEAKAGE.SDR USAA2014111400003Pressure Switch · faultyEMERGENCY VEHICLES CALLED OUT FOR LANDING DUE TO CLASS 1 ECAM HYD GREEN LOW LEVEL DURING CRUISE. TURNED GREEN PUMP ON DURING APPROACH IAW ECAM SYS RECOVERED. REPLACED ENG NR 1 HYD PUMP PRESS SWITCH IAW AMM 29-11-17 PB0401.SDR CA141113001Hose · leaking(CAN) DUE TO A COMPLETE LOSS OF THE GREEN HYDRAULIC SYSTEM OCCURRED IN FLIGHT THE FLIGHT CREW ON AC909 DECLARED A PAN PAN WITH ATC. TOW REQUIRED OFF RUNWAY. SYSTEMS AFFECTED ARE: GREEN HYD, SPLR 1+5, CAT 3 DUAL, N.W.STEER, AUTO BRK, NORM BRK, L/G RETRACT, REVSDR AALA20141110014Hydraulic System · lowDIVERTED, EMER DECLARED. LANDING WAS UNEVENTFUL. ACFT WAS OVERWEIGHT. IN CRUISE RT HYD SYS SHOWED QTY LOSS. EVALUATION IN PROGRESS. FIELD TRIP ENROUTE. PLAN TO TROUBLESHOOT & PERFORM OVERWEIGHT LANDING INSPECTION. SERVICED RT HYD SYS IAW AMM 12-12-01. SDR SWIA201439880Line · failedDURING CRUISE LOST NR 1 HYD FLUID - DROPPED TO 5 PERCENT EDP. RAN WITH 0 PSI FOR APPROX 5 MIN. R & R NR 1 EDP PRESSURE LINE AND NR 1 EDP IAW AMM,SDR CA141110003Hydraulic System · failed(CAN) DURING CRUISE BLUE HYDRAULIC SYSTEM INDICATED FAIL. A LANDING WAS CONDUCTED WITHOUT FURTHER INCIDENT. BLUE HYD FUNCTION CHECKED IAW AMM 29-31-00-710-001-A OPS NORMAL.SDR FDEA201411073567Fuse · crackedHYD 3 FAIL LEVEL 2 AFTER GEAR DOWN ON APPROACH, ALL HYD FLUID EMPTIED & LEAKED FROM HYD SYS 3 AFTER GEAR LOWERED. PUMPS NOT TURNED OFF. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM32-31-06-2.SDR CA141120025Clamp · damaged(CAN) PREMATURE FAILURE OF BLUE CUSHION ON P-CLAMP M85052/2. LACK OF CUSHION CAUSED CLAMP CHAFING INTO THE HYDRAULIC LINE AND DAMAGING THIS LINE, HYDRAULIC LEAK SYS NR 3, LEAKAGE. THE CUSHION USED ON HYDRAULIC LINE SHOULD BE ETHYLENE PROPYLENE RUBBER, COLORSDR CA141107004O-Ring · torn(CAN) ON APPROACH THE HYD 3 LOW PRESS CAUTION LIGHT CAME ON, THE NR 3 HYD SYS QTY WAS OBSERVED AT 5 PERCENT. AN ALTERNATE GEAR EXTENSION WAS CARRIED OUT AND EMERGENCY DECLARED. THE ACFT LANDED UNEVENTFULLY. MAINTENANCE INVESTIGATION FOUND A HYDRAULIC LEAK A
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