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 AU001061Pipe · cracked(AUS) HYDRAULIC PIPE LOCATED IN RT ENGINE BAY LEAKING FROM CRACKED FLARE.SDR CA001108006Line · leaking(CAN) DURING ROUTINE INSPECTION, A HYDRAULIC FLUID LEAK WAS DISCOVERED IN THE RT MLG STABILIZER STRUT DOWN PRESSUE LINE. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2000UALA00641Motor · leakingDIVERTED TO DEN DUE TO THE LOSS OF THE A-SYSTEM HYDRAULIC FLUID. *S/D* FOUND OUTBOARD FLAP DRIVE HYD MOTOR LEAKING. REPLACED OUTBOARD FLAP HYD DRIVE MOTOR. NO ACTIVE LEAKS NOTED ON FLAP CYCLING. SERVICED HYDRAULIC SYSTEM.SDR CA001107003O-Ring · deformed(CAN) DURING FLIGHT ECAM CAUTION OF LOW GREEN HYDRAULIC LEVEL, BOTH ENGINE DRIVEN PUMPS SHUTOFF AND AIRCRAFT PROCEEDED TO DESTINATION AS MOST VIABLE ALTERNATIVE.FOUND THE RT ENGINE HYDRAULIC PUMP PRESSURE DAMPENER, LINE LOSS AND O-RING WAS DEFORMED AND EXTRUDESDR CA001212002O-Ring · deformed(CAN) DURING FLIGHT ECAM CAUTION OF LOW GREEN HYDRAULIC LEVEL, BOTH ENGINE DRIVEN PUMPS SHUT-OFF AND AIRCRAFT PROCEEDED TO DESTINATION AS MOST VIABLE ALTERNATIVE. FOUND THE R/H ENGINE HYDRAULIC PUMP PRESSURE DAMPENER, LINE LOSS AND O-RING WAS DEFORMED AND EXTRSDR CA001212003Hydraulic Line · loose(CAN) AIRCRAFT ON ROUTE, GREEN HYDRAULIC LOW LEVEL WARNING, BOTH ENGINE DRIVEN PUMPS WERE SHUTOFF AND AIRCRAFT RETURNED TO YMX FOR REPAIRS. MAINTENANCE FOUND RT MLG BYPASS VALVE PRESSURE LINE AND UNION LOOSE. LINE AND UNION RE-TIGHTENED, SYSTEM SERVICE, PRESSUSDR SIMA3001Selector Valve · inoperativeMIA - FLT 5305 - AFTER TAKEOFF, GEAR INTRANSIT LIGHT WOULD NOT GO OUT. FOLLOWED AOM PROCEDURES RETURNED LANDING WITH NORMAL GEAR DOWN INDICATIONS. S/D MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW ATR MM. OPS AND LEAK CHECK WAS SATISFACTOSDR USAASB00304Bypass Valve · faultyBTV - FLT 1567 - ON APPROACH INTO BTV, THE FLAPS TO EXTEND AS THEY WOULD NOT MOVE FROM 5 DEGREES. MOVING FLAP LEVER UP OR DOWN WOULD NOT MOVE FLAPS. CREW WAS ABLE TO EXTEND FLAPS TO 15 DEGREES USING ALTERNATE FLAP PROCEDURE. FLIGHT CIRCLED BTV TO ALLOW CREWSDR CA001109004Fitting · broken(CAN) DURING CLIMB NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINTED, SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO. NR 1 HYDRAULIC PUMP THEN FAILED SHORTLY AFTER. MAINTENANCE DISCOVERED AN ALUMINUM HYDRAULIC LINE BROKEN AT THE FLARED FITTING. THIS LINE IS LOCATED SDR CA001214008Fitting · leaking(CAN) INVESTIGATION OF A HYDRAULIC FLUID LEAK IN THE AREA OF THE WING CENTRE SECTION REVEALED THAT A PERMASWAGE FITTING INSTALLED TO JOIN TWO LINES AS PART OF THE RUDDER ISOLATION VALVE MOD WAS WEEPING. A ONE-PIECE STAINLESS STEEL LINE WAS FABRICATED IN ACCORDSDR AALA20001755Hose · leakingFLT 1416 - EN ROUTE SJU-JFK, GREEN HYDRAULIC SYSTEM RESERVOIR QUANITITY SLOWLY DECREASED TO ZERO. AIR INTERRUPTED, RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT MAIN GEAR LOCK ACTUATOR FLEXIBLE HOSE. SERVICED HYDRAULIC SYSTEM. NO LEAKS NOSDR 2000UALA00642Line · leakingA-SYSTEM HYDRAULIC FLUID WENT FROM 3.5 TO 1.0 GAL. THE SYSTEM WAS ISOLATED, A-PUMPS OFF. *S/D* FOUND LINE TO A SYSTEM PRESSURE TRANSMITTER LEAKING. MANUFACTURED AND INSTALLED REPLACEMENT HYDRAULIC LINE. PRESSURE CHECK OK.SDR CA001103005Line · leaking(CAN) INVESTIGATION OF A HYDRAULIC LEAK IN THE NR 1 NACELLE RESULTED IN THE REPLACEMENT OF A PRESSURE LINE WHICH WAS FOUND LEAKING THROUGH A PINHOLE IN A FACTORY BEND.SDR AWXA0000797Switch · failedEMERGENCY LANDING, ECAM MSG, BLUE HYDRAULIC RESERVOIR LOW AIR PRESS. REMOVED AND REPLACED LOW PRESS SWITCH 2387GH.SDR ASOA00120Line · inoperativeFLT 4082 - IN FLIGHT FROM CSG-ATL, CREW REPORTED WHEN THE LANDING GEAR WAS LOWERED A MASTER CAUTION MESSAGE ON THE GREEN HYDRAULIC SYSTEM. THE LANDING GEAR WAS SHOWING DOWN AND LOCKED WITH THE GREEN HYDRAULIC PRESSURE SHOWING ZERO. CREW DECLARED AND EMERGENCSDR QXEA0002887Hydraulic System · lowPDX - EN ROUTE FROM LAX TO EUG, FLIGHT CONTROL HYDRAULIC SYSTEM NOTED DECREASING IN TO YELLOW CAUTION AREA OF INDICATOR DURING FLIGHT. DIVERTED TO PDX. SERVICED AND OPERATIONALLY CHECKED HYDRAULIC SYSTEM. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.SDR CA001103002Power Unit · bypassing(CAN) DURING ROUTINE MAINTENANCE, IT WAS FOUND THAT ACTIVATION OF THE NR 1 STANDBY HYDRAULIC POWER UNIT CAUSED THE NR 1 ENGINE DRIVEN PUMP TO BE DRIVEN, IN TURN CAUSING THE PROP TO WINDMILL..MAINTENANCE REPLACED THE NR 1 HYDRAULIC PRESSURE MANIFOLD WHICH CONTASDR PLGA001019Swivel · shearedBOS-YQB - FLT 4670 - AFTER TAKEOFF, AS THE GEAR WAS SELECTED UP THE INTRANSIT LIGHT REMAINED ON AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE HYDRAULIC PRESSURE LIGHT ILLUMINATED AS THE HYDRAULIC QUANTITY GAUGE DROPPED. FOLLOWED THEIR CHECKLIST THE CREW USED SDR CA001030005Line · failed(CAN) OIL LINE FAILED AT AREA WHERE IT IS CLAMPED TO THE UPPER DECK. (X)SDR RRXA001070Line · brokenUPON GEAR RETRACTION AFTER T/O GEAR RETRACTED NORMALLY WHEN GEAR HANDLE PLACED IN UPLATCH CHECK POSITION NOSE GEAR SOUNDED LIKE IT FELL OUT OF THE WHEEL WELL AND BOTH RED LIGHTS FOR DOORS NOT LATCHED AND GEAR NOT LATCHED ILLUMINATED. CREW THOUGHT THEY HAD MISSDR 20001212SH015Filter · damagedINTERNALS, ITEM (2) WAS FOUND BROKEN IN HALF AT ONE END. POSSIBLE CAUSE: CRACKED FROM CORNER OF NOTCH TO OUTER EDGE. FATIGUE AND/OR WEAK POINT IN DESIGN. (X)SDR DL73K002035Hydraulic Line · rupturedSHIP 363 FLIGHT 2131 ARRIVED EWR AT 2353E. DURING TAXI TO TERMINAL CREW NOTICED A SYSTEM HYDRAULIC QUANTITY DEPLETED. FOUND BRAIDED HYDRAULIC LINE WITH PINHOLE LEAK. LINE IS LOCATED IN AFT SECTION OF NOSE WHEEL WELL. REPLACED HYDRAULIC LINE.SDR 0003803222Hose · rupturedDURING CLIMB AFTER LANDING GEAR AND FLAP RETRACITON, RECEIVED HYD G RSVR LO LVL MESSAGE. PER COM PROCEDURES, SHUT OFF THE GREEN HYDRAULIC SYSTEM PUMPS, GRAVITY EXTENDED LANDING GEAR ON APPROACH TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE RESDR DHL2000366002Line · leakingYELLOW SYSTEM HYDRAULIC FLUID LOSS TO 0 DURING LANDING AT CVG AND PRESSURE WAS 0 ALSO FOUND HYD LINE FROM GROUND SPOILER HYDROMECHANICAL SELECTOR AT FEED THRU JUST ABOVE GEAR LOOSE.RESECURED HYD LINE SERVICED YELLOW SYSTEM A/300 M/M 12-30-00 SYSTEM OPS SERVICASDR 2000UALA00593Line · failedHYDRAULIC SYSTEM A QUANTITY GAUGE INDICATED SLOW PARTIAL LOSS OF FLUID. DECREASED APPROXIMATELY 1 GALLON IN 2 HOURS. DIVERTED TO DEN, LANDED UNDER AMBER ALERT. TOWED TO GATE DUE TO NO NOSE GEAR STEERING. *S/D* FOUND RIGHT HAND GEAR DOOR ACTUATOR LINE LEAKSDR CA001031019O-Ring · cracked(CAN) ON APPROACH TO POS, WITH GEAR UP, GOT HIS NR 2 EDP HYDRAULIC CAUTION LIGHT AND NOTICED HIS NR 2 HYDRAULIC QUANTITY DROPPED TO ZERO. FOLLOWED PROCEDURES PER QRH. AIRCRAFT LANDED IN PORT OF SPAIN & TOWED TO GATE. MAINTENANCE: NR 2 EDP SUPPLY LINE TO THE PSDR DLM88001985Line · rupturedDURING CLIMB RIGHT HYD QTY DECREASED FROM 9 TO 4 QTS. PER POM RTB. GEAR FLAPS EXT NORMALLY W/RT SYS AT 3100 PSI AND 2 QTS. FOUND ENG HYD LINE BAD. REPLACED SAME, SERVICED AND BLEED HYD SYS, ALL CKS GOOD.SDR 0004053107Line · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. DESELECTED THE YELLOW HYDRAULIC PUMPS PER COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING HYDRAULIC SUPPLY LINE TO THE FORWARD CARGO DOOR OPERATING VSDR 0003713260Coupling · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURE AND LANDED AT FINAL DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING PTU QUICK DISCONNECT COUPLING 3718GM. OPERATIONAL CHECK OK.SDR CA001031026Connector · sheared(CAN) THE FOLLOWING WAS REPORTED TO US: INFO GATHERED FROM RETURNING ENGINEER (TODAY 10TH OCT) STATES THAT CAPTAIN REPORTED ON APPROACH HE NOTICED THAT NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED AND WITHIN 3 SECONDS OBSERVED TOTAL LOSS OF NR 2 HYDRASDR RAAA00E8044Control Valve · leakingFLIGHT BETWEEN CDB - ANC, NR 1 HYDRAULIC SYSTEM WENT FROM FULL TO 2.0 GALLONS. REPLACED WINDSHIELD WIPER CONTROL UNIT IAW 30-9-1, LEAK AND OPS CHECKED OK. SERVICED HYDRAULIC RESERVOIR.SDR DL73K001955Line · damagedENGINE HYD PUMP NR 2 PRESSURE LIGHT ON SYSTEM. REPLACED NR 2 ENGINE HYD PUMP AND HYD PRESS LINE. REPLACED FILTERS AND INSP A SYSTEM RETURN MODULE, ALL NORMAL. FLUSHED LINES, NO CONTAMINATION FOUND. RAN ENGINES, CHECKS NORMAL.SDR DL764001933O-Ring · failedCREW OBSERVED THE RT HYD QTY DECREASING EN ROUTE NOTIFIED MCC 1515Z. QTY AT 1.03 DEPARTING ATL DECREASED TO .65 ON ARRIVAL FLL. FOUND RT SYS HYD LINE IN AFT BB RT FWD SIDE PALLET 20. DRIVE BAY-A- UNDER SATCOM E12 RACK AREA PANEL -O-RING FOR CK VLV DAMAGED. SDR CA001026006Line · leaking(CAN) DURING ROUTINE INSPECTION, A HYDRAULIC LEAK WAS DISCOVERED IN THE NR 2 SYSTEM HYDRAULIC LINE FROM THE RESERVOIR TO THE AC PUMP. THE LINE WAS REPLACED AND HE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA2762Control Valve · inoperativeDFW - FLT 3697 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE IAW SAAB MM. OPERATIONAL AND LEAK CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)SDR CA001013033Line · chafed(CAN) NR 1 HYDRAULIC SYSTEM RETURN LINE WAS CHAFED WITH NR 2 PUMP PRESSURE LINE, REPLACED. THIS TUBE ASSEMBLY WAS INSTALLED 293.1 HOURS BEFORE.FOUND PRESSURE LINE WAS ROUTED OTHER SIDE OF NR 2 PUMP.SDR DL72W001904B-Nut · looseA-SYS HYD FAILURE. QTY WENT TO -0-, BOTH LOW PRESS LIGHTS ILLUM ON SHORT FINAL. FOUND B-NUT AT LOWER NR 1 PYLON LOOSE. TIGHTENED SAME. INSPECTED CASE DRAIN FILTERS AND SERVICED.SDR AU001325Fitting · cracked(AUS) HYDRAULIC PIPE FITTING LOCATED IN LH NACELLE AREA CRACKED AND LEAKING. LOSS OF NR 1 SYSTEM HYDRAULIC FLUID.SDR CA001020004Support Bracket · damaged(CAN) FOUND UNSATISFACTORY HYDRAULIC ACTUATOR SUPPORT REMOVED FOR DIMENSIONAL VERIFICATION, RESULTS SATISFACTORY; TRANSMISSION UPPER & LOWER CASE ASSY INSP RESULTS SATISFACTORY; HYDRAULIC ACTUATOR SUPPORT REINST ON A/C WITH NEW HARDWARE.SDR SIMA2723Fitting · leakingMIA - FLT 5284 - ON APPROACH, THE BLUE HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED. THE CREW SHUT DOWN THE BLUE SYSTEM, DECLARED AN EMERGENCY. THE ACFT LANDED SAFELY, NO OTHER INCIDENTS WERE REPORTED. FOUND LOOSE FITTING ON THE BLUE SYSTEM PUMP PRESSURE LISDR RAAAOOE8041Control Valve · stuckAT ANC AIRCRAFT WOULD NOT TAXI WITH NORMAL POWER APPLICATION. BRAKES APPEARED TO BE STUCK ON. REPLACED BRAKE POWER CONTROL VALVE PER L-188 M/M 32-9-3 AND 91-1-1. LEAK AND OPS CHECK GOOD LOCKOUTS BLED, RESERVOIR SERVICED.SDR USAASB00274Swivel · brokenBOS - FLT 1090 - EN ROUTE FROM PHL TO BOS, FLT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. MX CONTROL ADVISED THAT FLIGHT SHOULD PROCEED TO ORIGIN OR DESTINATION, WHICHEVER WAS CLOSER. FLIGHT WAS CLOSER TO BOS, SO IT CONTINUED ONTO BOS. FLIGHT LANDED WITSDR CA001026007Line · leaking(CAN) INVESTIGATION OF A HYDRAULIC LEAK RESULTED IN THE REPLACEMENT OF THE RT OUTBOARD GROUND SPOILER UNLOADING LINE.SDR QXEA0002813Clamp · chafedPDX- RIGHT HAND STUBWING, NR 1 HYDRAULIC SUCTION LINE ATTACHING CLAMP, JUST AFT OF DOOR O2J IS CHAFING AGAINST ENGINE THRUST ROD. REPAIRED IAW FOKKER SRM 29-10-01.SDR HNAA000071Hydraulic Line · crackedAFTER GEAR SELECTED UP, DURING RETRACTION NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED WITH ASSOCIATED LOSS OF QUANTITY. FOUND FLAIR CRACKED ON HYDRAULIC LINE. REPLACED HYDRAULIC LINE. QUANTITY WAS AT ZERO FOR LESS THAN FIVE MIN.SDR USAASA00036Hydraulic System · overservicedMYR-CLT - FLT 134 - RECEIVED LAVATORY SMOKE ALERT AT FL160. NO EVIDENCE OF SMOKE DURING FLIGHT, HOWEVER, ODOR WAS EVIDENT ON THE GROUND IN THE CABIN. ODOR FOUND TO SUBSIDE AFTER APU IS NO LONGER RUNNING. FLIGHT WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE DSDR CA001026005Line · leaking(CAN) INVESTIGATION OF A HYDRAULIC LEAK IN THE NR 2 NACELLE RESULTED IN THE REPLACEMENT OF THE SUCTION LINE FROM THE RESERVOIR TO THE AUX. HYDRAULIC PUMP, WHICH WAS FOUND CHAFED AND LEAKING.SDR TWAA0014602Line · crackedAN ACRID ELECTRICAL TYPE SMELL WAS NOTED IN THE COCKPIT AND CABIN WHEN ENGINE ANTI-ICE WAS TURNED ON. FOUND A PINHOLE CRACK IN A HYDRAULIC LINE, AND THE LEAK WAS GETTING INTO THE AIR CONDITIONING SYSTEM. FABRICATED AND REPLACED THE LINE ON THE RT SIDE OF THSDR C2XA00CL067Line · failedEWR - FLT 4253 - THE CREW REPORTED THAT THEY LOST NR 1 HYDRAULIC SYSTEM PRESSURE. THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HYDRAULIC PUMP PRESSURE LINE IAW EMB145 MM 29-10-00. MAINSDR 20001116SH001Shutoff Valve · leakingBOS/APA - ON LANDING ROLL-OUT, THE COMBINED HYDRAULIC SYSTEM LOW PRESSURE WARNING LIGHT ANNUNCIATED. THE AIRCRAFT WAS STOPPED AND TURNED OFF THE RUNWAY WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE RAMP. AN INVESTIGATION REVEALED THE TWO BOLTS ON THE FLIG
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