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.

SDR CA000804005Line · leaking(CAN) UPON SELECTION OF THE LANDING GEAR, THE HYDRAULIC QUANTITY DROPPED TO 2 QUARTS. NLG DRAG STRUT ACTUATOR UP HYDRAULIC LINE FOUND LEAKING. LINE REPLACE AND AIRCRAFT RETURNED TO SERVICE.REF P105147Jul 28, 2000 · Dhav DHC8102SDR 0002741160Line · leakingABORTED TAKEOFF AT 80 KNOTS DUE TO COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM. REPAIRED LEAKING NR 1 SYSTEM BRAKE RETURN LINE. REPLACED BOTH NR 1 SYSTEM ENGINE DRIVEN PUMP. OPERATIONAL CHECK OK.Jul 28, 2000 · N160US · Doug DC1040SDR 20010503CW006Hose · rupturedPILOT REPORTED LOW QUANTITY IN NR 1 HYDRAULIC SYSTEM. CAUSE WAS DETERMINED TO BE A RUPTURED HOSE ON THE PRESSURE SIDE OF THE LEFT SPOILER.Jul 27, 2000 · N999BW · Bac 111419EPSDR CA000830036Hydraulic Line · ruptured(CAN) LOSS OF HYDRAULIC FLUID DURING DESCENT AND LANDING. NR2 ENGINE THRUST REVERSER PRESSURE LINE WAS FOUND RUPTURED IN PYLON UNDER A SUPPORT CLAMP.HYDRAULIC PUMP AND FILTER WERE CHECKED FOR CONTAMINATION AND FOUND SERVICEABLE. HYDRAULIC LINE REPLACED AS PERJul 27, 2000 · Boeing 737242CSDR VTZA200001Hose · failedCOMPLETE LOSS OF PRESSURE ON BOTH HYDRAULIC PUMPS DURING FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING CREW FOUND MAJOR FLUID LEAK AT RIGHT ENGINE NACELLE. MAINTENANCE FOUND FAILED HYDRAULIC HOSE (P/N 1379305A77). REJul 27, 2000 · N484UE · Bag JETSTM3201SDR ABXA000359Line · leakingSLOW LOSS OF HYDRAULICS OBSERVED ON HYDRAULIC QUANTITY GAUGE. NEEDLE WENT FROM FULL TO HALFWAY BETWEEN N AND STANDPIPE. EMERGENCY PROCEDURES ACCOMPLISHED. REPLACED NR 3 ENGINE HYDRAULIC PUMP PRESSURE LINE AND RESEALED PUMP FITTING AT PUMP. SERVICED HYDRAULJul 27, 2000 · N804AX · Doug DC862SDR MALA000450Swivel · failedAFTER TAKEOFF, LOST HYDRAULIC FLUID AS PER ORH APPLIED HYD LOSS PROCEDURE, EMERGENCY GEAR EXTENDED WAS SUCESSFUL. AIR TURNBACK, AC LANDED NORMALLY. MAINTENANCE REPLACED LT BRAKE SWIVEL, AND RESET EMERGENCY GEAR SYSTEM. SERVICED HYD SYSTEM, ALL CHECK GOOD.Jul 26, 2000 · N327XJ · Saab SF340ASDR AT0000361Shutoff Valve · crackedRIGHT HYDRAULIC SYSTEM FAILED AND DURING TAXI, HYDRAULIC FUMES ENTERED THE CABIN. ALL PASSENGERS WERE EVACUATED VIA FORWARD STAIRS. FOUND RUDDER HYDRAULIC SHUTOFF VALVE CRACKED.Jul 25, 2000 · N835AT · Doug DC932SDR CA000804006Manifold · failed(CAN) NR 1 PROP STARTED SPINNING WHEN NR 1 HYDRAULIC STANDBY PUMP IN USE. NR 1 PRESSURE MANIFOLD ASSEMBLY REPLACED AND AIRCRAFT RETURNED TO SERVICE.Jul 24, 2000 · Dhav DHC8102SDR CA000905007Line · ruptured(CAN) AIRCRAFT RETURNED TO BLOCKS BECAUSE THE CREW REPORTED THE NR 2 SYSTEM HYDRAULIC PUMP LIGHTS ILLUMINATED AND THEN THE NR 2 SYSTEM QUANTITY AND PRESSURE DROPPED QUICKLY. AIRCRAFT RETURNED TO YVR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED Jul 23, 2000 · Fokker F28MK1000SDR USAASB00195Check Valve · unscrewedPHL-FLT 1451 - EN ROUTE FROM MHT-DCA, AT FL350, A SYS HYD FLUID DROPPED TO 1/4 AND THE LOW PRESS LIGHT FOR THE NR 1 ENG HYD PUMP ILLUMINATED. CREW ACCOMP QUICK REF HANDBOOK PROCEDURES AND SHUT OFF THE PUMP WITHIN 20 SECONDS. FLUID LVL CONTINUED TO DROP TO 1/Jul 21, 2000 · N417US · Boeing 737401SDR DLM88001396Housing · chafedA/C 938 WAS IN THE PROCESS OF HAVING A NR 2 ENGINE CHANGE. AT THAT TIME THE AIRCRAFT CASE DRAIN FILTERS WERE ALSO CHANGED. THE MECHANIC REPLACING THE FILTERS NOTICED A CHAFED AREA AND BURNT SPOT ON THE CASE DRAIN FILTER HOUSING CAUSED BY THE NR 2 ENGINE GENJul 20, 2000 · N938DL · Doug MD88SDR CHQA20000011Swivel · brokenRETURNED TO THE FIELD AFTER LOST HYDRAULIC PRESSURE. CREW PUMPED GEAR DOWN. MAINTENANCE FOUND HYDRAULIC SWIVEL ON RT MAIN GEAR UPPER STRUT BROKEN. THE SWIVEL WAS REPLACED, SYSTEM SERVICED, GEAR SWUNG WITH ALL INDICTIONS NORMAL.Jul 19, 2000 · N108CQ · Saab SF340ASDR CA000731006Line · leaking(CAN) AFTER TAKEOFF, "B" LOW QUANTITY LIGHT ILLUMINATED, FOLLOWED BY A LOW PRESSURE WARNING LIGHT ON "B" PUMPS. RETURNED. FOUND SUPPLY LINE TO RIGHT ELEVATOR ACTUATOR LEAKING. LINE REPLACED, SERVICED HYDRAULIC SYSTEM, LEAK CHECKED OK.Jul 18, 2000 · Boeing 737217SDR AU000548Heat Exchanger · failed(AUS) RT HYDRAULIC SYSTEM HEAT EXCHANGER CORE FAILED ALLOWING THE CONTENTS OF THE RT HYDRAULIC SYSTEM TO DRAIN INTO THE RT FUEL TANK.Jul 17, 2000 · Boeing 767338SDR CA000731005Line · leaking(CAN) ON FINAL INTO YYZ, A COMPLETE LOSS OF A SYSTEM HYDRAULIC PRESSURE OCCURRED. WHEN TRAILING EDGE FLAPS SELECTED, WARNING LIGHTS AND A LEADING EDGE SLAT ASYMMETRIC WARNING INDICATION. AN EMERGENCY WAS DECLARED. FLAPS AND GEAR WERE LOWERED MANUALLY, FLIGHT LJul 16, 2000 · Boeing 737217SDR CA000724002Line · leaking(CAN) LOST OF HYDRAULIC PRESSURE SYSTEM NR 1 AND QUANTITY IN CRUISE AT FLIGHT LEVEL 310. NO QUANTITY OR PRESSURE FOR 36 MINUTES BEFORE ENGINE SHUTDOWN AFTER LANDING. THE EDP AND THE LEAKING HYDRAULIC PRESSURE LINE REPLACED.Jul 16, 2000 · Cndair CL6002B19SDR CA000802009Line · leaking(CAN) HYDRAULIC FLUID QUANTITY ON SYSTEM A DECREASING, CREW SWITCHED THE PUMP OFF AND STOPPED THE LEAK. MAINTENANCE FOUND PRESSURE LINE FITTING LEAKING AT ENGINE DRIVEN PUMP. O-RING REPLACED AND A/C RETURNED TO SERVICE.Jul 14, 2000 · Lkheed 1011385114SDR PCAA0007045Hydraulic Line · crackedFLT 3516, ON CLIMBOUT FROM BWI, NR 2 HYDRAULIC SYSTEM LOST CONTENTS. AIRCRAFT DIVERTED TO MDT. MAINTENANCE INSPECTED, FOUND CRACKED GROUND SPOILER LINE AT SPOILER ACTUATOR. INSTALLED RINGLOCK SPLICE IN ACCORDANCE WITH M/M 20-50-55, REPLENISHED AND BLED SYSTJul 14, 2000 · N824EX · Dhav DHC8102SDR AU000569Pipe · leaking(AUS) HYDRAULIC PIPE CONTAINED A SMALL PIN HOLE LEAK ON THE INSIDE OF THE BEND RADIUS.Jul 13, 2000 · Dhav DHC8102SDR USAASB00188Line · leakingMCO - FLT 2670 - UPON APPROACH INTO MCO, AFTER SETTING FLAPS, FLIGHT ENCOUNTERED SYSTEM A HYDRAULIC FLUID LOSS. BOTH A PUMP LOW PRESSURE LIGHTS ILLUMINATED. CREW ACCOMPLISHED ALTERNATE FLAP EXTENSION AND MANUAL GEAR EXTENSION. FLIGHT LANDED WITHOUT FURTHER Jul 12, 2000 · N260AU · Boeing 737201SDR CA000724004Hydraulic Line · leaking(CAN) ON FLIGHT 5692 FROM CINCINNATI (CVG) TO MYRTLE BEACH SC (MYR), HYDRAULIC NR 2 PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING BACK AT CINCINNATI. MAINTENANCE ACTION: MAINTENANCE FOUND AN HYDRAULIC LEAK IN THEJul 11, 2000 · Cndair CL6002B19SDR COMA0060561Line · leakingHYDRAULIC SYSTEM NR 2 LOW PRESSURE CAUTION MESSAGE. REPLACED EDP PRESSURE LINE.Jul 9, 2000 · N712CA · Cndair CL6002B19SDR DLM88001298Line · looseIN FLIGHT, RT ENG HYDRAULIC QTY WENT TO 1 QT WITH AMBER LIGHT, HAD NORMAL PRESS INDICATION. LATER LOST HYDRAULIC PRESSURE AND QTY. FOUND HYDRAULIC RETURN LINE IN 48 SECTION WITH NUT LOOSE. REMOVED LINE, REPOSITIONED ANTI ROTATION BLOCK AND RE-INSTALLED LINEJul 8, 2000 · N918DL · Doug MD88SDR SWAA001232Fitting · crackedAIR TURNBACK. NR 2 ENGINE HYD PUMP LOW PRESS INDICATION LIGHT ILLUMINATED AND B-HYD SYS FAILED. FOUND MLG B-SYS HYD FLOW LIMITTER UNION FITTING CRACKED. R&R FLOW LIMITTER AND UNION FITTING PER MM.Jul 8, 2000 · N677AA · Boeing 7373A4SDR 20000720SH027Hydraulic Line · leakingTHE LT MLG PRESSURE LINE RUNNING JUST OVER THE FLIGHT CONTROL CABLES IN THE TAIL CONE SECTION OF THE A/C WAS BEAT DOWN INTO THE PATH OF ONE OF THE CABLES. AFTER A LIMITED TIME, THE CABLE WORE THROUGH THE HYDAULIC LINE DUMPED THE RESERVOIR INTO THE TAIL CONE. Jul 7, 2000 · N242WT · Cessna 551SDR CA000718014Drain Line · leaking(CAN) HYDRAULIC FLUID LEAKING FROM LEFT NACELLE. FOUND CASE DRAIN LINE LEAKING. NEW LINE INSTALLED AND AIRCRAFT RETURNED TO SERVICE.Jul 6, 2000 · Dhav DHC8102SDR CA000706017Line · leaking(CAN) DURING MAINTENANCE, HYDRAULIC FLUID WAS FOUND LEAKING FROM UNDER THE LT FLAP AREA. A LEAKING LINE TO THE L/H INBOARD ROLL SPOILER ACTUATOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Jul 6, 2000 · Dhav DHC8102SDR CA000706016Line · leaking(CAN) DURING WALK AROUND INSPECTION, THE FLIGHT CREW OBSERVED A FLUID LEAK IN THE ARMPIT AREA OF THE LT FUSELAGE. MAINTENANCE REPLACED A LEAKING LANDING GEAR DOWN PRESSURE LINE IN THE WING CENTRE SECTION, AND THE AIRCRAFT RETURNED TO SERVICE.Jul 5, 2000 · Dhav DHC8301SDR CA000706019Hydraulic Line · leaking(CAN) DURING WALK AROUND, THE FLIGHT CREW NOTICED FLUID LEAKING FROM THE NOSE LANDING GEAR AREA. MAINTENANCE INVESTIGATION REVEALED THE DOOR CLOSED HYDRAULIC PRESSURE LINE TO THE SEQUENCE VALVE WAS LEAKING. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED Jul 4, 2000 · Dhav DHC8311SDR 20000831SH005B-Nut · looseOWB - GOING INTO OWB, COULD NOT GET LANDING GEAR DOWN. PILOT HAND PUMPED GEAR DOWN, LANDED NO PROBLEMS. SERVICED HYDRAULIC FLUID, TIGHTENED LOOSE B-NUT BACK SIDE OF HYDRAULIC SERV. PORT. (X)Jul 4, 2000 · N525AA · Piper PA31350SDR CA000718015Line · leaking(CAN) HYDRAULIC LINE CHAFED AND LEAKING INTO HYDRAULIC BAY. HYDRAULIC LINE FOUND CHAFED AGAINST PIPE ASSEMBLY WITH BOTH LINES LEAKING.BOTH HYDRAULIC LINES REPLACED AND AIRCRAFT RETURNED TO SERVICE.Jul 2, 2000 · Bag BAE146200ASDR 2000UALA00382Line · leakingLOW HYDRAULIC SYSTEM PRESSURE DISPLAYED ON ENGINE INDICATION AND CREW ALERTING SYSTEM. *S/D* RETURN LINE ON RIGHT MAIN LANDING GEAR DOWNLOCK LEAKING. REPLACED LINE 3.Jul 2, 2000 · N541UA · Boeing 757222SDR ASOA00079Line · failedFLT 4690 - CREW REPORTED THAT HYDRAULIC SYSTEM NR 1 SYNOPTIC PAGE SHOWS ZERO QUANTITY. HYDRAULIC QUANTITY THEN FLUCTUATED BETWEEN 2600-2900 PSI. HYDRAUCLI PUMPS THEN RAN DRY FOR 25 MINUTES WITH NO FLUID. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ATL. FJul 1, 2000 · N830AS · Cndair CL6002B19SDR UPS00433142Line · crackedPILOTS REPORT- NR 3 HYD QTY DROPPED TO APPROX 1.1 GAL 3 HOURS INTO FLIGHT FOUND HYD PRESS LINE IN PYLON CRACKED. REMOVED AND REPLACED NR 3 PYLON HYDRAULIC LINE, LEAK CHECKS OK PLACARD REMOVED.Jun 30, 2000 · N675UP · Boeing 747123FSDR ASOA00078Line · brokenAFTER TAKEOFF, AIRCRAFT LOST GREEN HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MCN. MAINTENANCE REPAIRED BROKEN GE ACTUATOR LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jun 28, 2000 · N244AS · Emb EMB120RTSDR USAASB00180Line · rupturedTPA - FLT 2676 - AFTER TAKEOFF AND GEAR RETRACTION FROM TPA, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW FOLLOWED QUICK REF HANDBOOK PROCEDURES AND SAFE GEAR INDICATIONS WERE RECEIVED. HOWEVER, CREW NOTICED THAT HYDRAULIC PRESSURE HAD DECREASEDJun 27, 2000 · N279AU · Boeing 7372B7SDR C2XA00BT034Hose · leakingEWR - FLT 3616 - CREW REPORTED, LOST THE GREEN HYDRAULICS SYSTEM WITH LANDING GEAR UNLOCK LIGHTS. REMOVED AND REPLACED HYDRAULIC HOSE ON THE RIGHT MLG UNLOCK ACTUATOR. OPS AND LEAKED CHECKED GOOD. REF M602 NR 188540. (M)Jun 25, 2000 · N17831 · Aerosp ATR42320SDR CA000706003O-Ring · leaking(CAN) CREW REPORTED CENTER SYSTEM HYDRAULIC LOW QUANTITY LIGHT ON. TURNED OFF ALL CENTER HYDRAULIC PUMPS. FLIGHT DIVERTED, DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. ON INSPECTION FOUND LEAK AT DELTA P FITTING ON CENTER SYSTEM CASE DRAIN FILTER MODULE. O-Jun 23, 2000 · Boeing 767375SDR SIMA1751Hydraulic Line · crackedPMD - FLT 3056 - HYDRAULIC LEAK DURING FLIGHT AND SUBSEQUENT LOSS OF ALL MAIN HYDRAULIC PRESSURE. MAINTENANCE FOUND THE NOSE GEAR RETRACTION LINE CRACKED. HYDRAULIC LINE WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVIJun 23, 2000 · N312AE · Saab 340BSDR CA000621003Coupling · leaking(CAN) THE FLIGHT CREW REPORTED LOSS OF YELLOW SYSTEM HYDRAULIC FLUID APPROX. 15 MILES BACK ON DESCENT. AN ODOR WAS EXPERIENCED BY PAX IN ROWS 7, 8 & 9 FIRST. A NORMAL LANDING WAS ACCOMPLISHED. MAINTENANCE INVESTIGATION REVEALED A LEAK AT THE B PORT OF THE YELLJun 21, 2000 · Bag BAE146200ASDR AU000804Fuse · cracked(AUS) OUTBOARD HYDRAULIC FUSE ON BRAKE MODULE CRACKED IN VALVE BODY. VALVE IS LOCATED AT THE WING TRAILING EDGE OUTBOARD OF THE LT MAIN LANDING GEAR. LOSS OF RT HYDRAULIC SYSTEM FLUID.Jun 21, 2000 · Boeing 767277SDR PLGA000617Hydraulic Line · rupturedBOS-ATV - FLT 4742 - AFTER DEPARTURE OUT OF BOS, WHEN THE FLIGHT CREW SELECTED GEAR UP THE GEAR CAME UP AND LOCKED BUT HYDRAULIC PRESSURE AND QUANTITY DROPPED TO ZERO. THE CREW WAS ABLE TO SELECT THE GEAR BACK DOWN AND HAD THREE GREEN DOWN AND LOCKED INDICATIJun 17, 2000 · N359BE · Saab 340BSDR CA000706008Line · failed(CAN) HYDRAULIC FLUID LEAK FROM WING ROOT AT OUTER NACELLE. LIFT DUMP PRESSURE TUBE ASSEMBLY REPLACED AND AIRCRAFT RETURNED TO SERVICE.Jun 16, 2000 · Dhav DHC8102SDR SWAA001103Valve · failedAIR TURNBACK. DURING CLIMB, NR 1 ENG HYD PUMP FAILED FOLLOWED BY ELEC A-SYS HYD PUMP FAILURE. REMOVED AND REPLACED A-SYS HYD MANUAL SHUT-OFF VALVE IN TAIL COMPARTMENT.Jun 15, 2000 · N698SW · Boeing 737317SDR CA000621044Check Valve · cracked(CAN) AIRCRAFT LOSS OIL HYDRAULIC PRESSURE AFTER DROPPING A LOAD OF WATER. AIRCRAFT RETURNED TO WABUSH AIRPORT. TANKER DOORS WERE CLOSED USING EMERGENCY SYSTEM, LANDING GEAR LOWERED USING EMERGENCY SYSTEM. MAINTENANCE DISCOVERED A CHECK VALVE IN RIGHT HAND WINJun 12, 2000 · Cndair CL2151A10SDR AALA20000956Fitting · leakingMIA - FLT 918 - EN ROUTE LIM-MIA - GREEN HYDRAULIC RESERVOIR LOW LIGHT ILLUMINATED. GREEN QUANTITY AT RED DOT. AIRCRAFT CREW DECLARED EMERGENCY. LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT KRUEGER FLAP PRESSURE LINE OIL RING FITTING AT WALL. SYSTEM GROUNDJun 12, 2000 · N77080 · Airbus A300B4605RSDR AU000478Pipe · ruptured(AUS) RT HYDRAULIC BRAKE PIPE LOCATED IN THE LANDING GEAR BAY FAILED. LOSS OF HYDRAULIC FLUID.Jun 9, 2000 · Bag JETSTM3201SDR DL76S001124Line · wornDURING CLIMB FROM DFW, HYD QTY EICAS MSG WITH DECREASING QTY LEFT HYD INDICATED. ONCE LEFT ENG PRIMARY PUMP WAS TURNED OFF LEFT HYD QTY STABILIZED AT .40. FOUND HYD LINE OFF OF EDP WORN THROUGH. REPLACED AND REPOSITIONED LINE SVC SYSTEM, OPS CHECK NORMAL. Jun 9, 2000 · N127DL · Boeing 767332SDR SCNA00054Hydraulic Line · leakingAFTER TAKEOFF FROM MSP, THE AIRCRAFT LOST A SYSTEM HYDRAULICS. DECLARED AN EMERGENCY AND RETURNED TO POINT OF ORIGIN. THE HYDRAULIC FLEX LINE ON THE LEFT ELEVATOR POWER CONTROL UNIT WAS FOUND LEAKING. THE FLEX LINE WAS REMOVED AND REPLACED, ALL FLIGHT CONTRJun 7, 2000 · N291SC · Boeing 7272K3
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