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 MASA200602367Spu · failedASH 2858 FLG. RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT. MX IS IN THE PROCESS OF TROUBLESHOOTING MX. REMOVED AND REPLACED SPU AND EDP.SDR 06FDEA03457Module · crackedSHORTLY AFTER LEVELOFF AT FL310, SYS A HYDRAULIC PUMP LIGHTS FLICKERED AND QUANTITY RAPIDLY DROPPED TO (ZERO). COMPLIED W/QRH AND LANDED IN MEM. FOUND HYD PRESS. LINE FROM NR 1 ENG TO "A" SYS MODULE CRACKED. INSTALLED NEW HYDRAULIC LINE AT "A" SYSTEM MODSDR HNAA0600117Hydraulic System · contaminatedAFTER CLIMBOUT RUDDER PRESSURE RUDDER FULL PRESSURE AND NR 2 RUDDER HYDRAULIC CAUTION LIGHTS ILLUMINATED AND EXTINGUISHED AFTER 30 SECONDS. BLED NR 1 AND NR 2 HYDRAULIC SYSTEMS AS REQUIRED.SDR SIMA200626803Line · looseAFTER TAKEOFF FROM LGA HYDRAULIC SYSTEM 2 FLUID DROPPED TO `0` QUANTITY FOLLOWED BY ENGINE 2 HYDRAULIC PUMP FAILURE AND HYDRAULIC 2 LOW QUANTITY MESSAGE. FOUND LOOSE ENGINE 2 HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE. TIGHTEN NUT AND PERFORMED ENGINE DRIVEN PSDR XN0A1353Hydraulic System · leakingON ENGINE START, BLUE HYDRAULIC SYSTEM LEVEL LOW LIGHT CAME ON. INSPECTED SYSTEM FOR LEAK, SERVICED BLUE SYSTEM WITH 2 GALLONS IAW A300 AMM CHAPTER 12-12-29.SDR MASA200602308Spu · malfunctionedASH 2843 PHX. PILOT DECLARED AN EMERGENCY FOR THE NR 2 HYD QTY AT ZERO IN FLIGHT. MX REPLACED THE NR 2 SPU AND BRAKE LINE AT WING ROOT. OP'S CHECK GOOD.SDR QXEA200603359Line · leakingSEA FLIGHT NR 2399: ON APPROACH, WITH GEAR DOWN, CREW HEARD LOUD NOISE WHEN THEN NR 2 ENGINE HYD PUMP CAUTION LIGHT AND NOTICED NR 2 HYD QUANTITY DECREASING ON TAXI. HYD QUANTITY IN NR 2 WENT TO ZERO AND GOT MULTIPLE CAUTION LIGHTS. SHUT DOWN ENGINE 5-7 TIMESDR HEEA111184Guide · unknownWHILE ENROUTE, HYD BLOCK AND HYD ONE LIGHTS ILLUMINATED. REPLACED GUIDE ASSY.SDR HALA0600716Control Unit · failedLT ELECT DRIVEN HYD PUMP INOP WHEN SELECTED ON. REPLACE ELECT LOAD CONTROL UNIT OPS CHECKS OK.SDR UPS06847986Line · leakingLOST HYD FLUID - DROPPED TO AUX - FOLLOWED BY MAIN SYSTEM PRESS FLUCTU ATIONS + - 1500 - 2000 PSI. DIVERT TO RICKENBACKER AFB (THIS INFO DIRE CTLY OFF LOGPAGE AS NOTED BY FLIGHT CREW). FOUND INBOARD HYD FLEX HOSE FROM NOSE GEAR RETRACT CYLINDER LEAKING. R/R HSDR KCSA06082Line · leakingNR 1 HYD LOW LIGHT FOR SYS NR 1 ILLUMINATED. NR 1 HYD SYS QTY WAS 2 GALS WHEN ADP TURNED OFF AND ADP DEPRESSURIZED. ON POST FLT, FOUND NR 1 ADP BLOWOUT DOOR OPEN AND SKYDROL LEAK FROM ACCESSORY PANEL. REPLACED NR 1 HYD SYSTEM RETURN LINE IAW AMM 29-11-00.SDR MASA200602242Line · unknownASH 7281 IAD. HYDRAULIC SYSTEM NR 2 LOW PRESSURE CAUTION WITH ASSOCIATED INBOARD SPOILERS, INBOARD FLIGHT SPOILERS AND INBOARD BRAKES CAUTION MESSAGES. THE CREW REPORTED THAT ATC DECLARED AN EMERGENCY DUE TO THE REPORTED BRAKES CAUTION MESSAGE. MX R/R PRESSSDR F3LA200600107Line · leakingDURING CRUISE, FLIGHT CREW REPORTED ECAM READING: HYD GREEN RSVR LO LVL G ENG 1 NR 1 PUMP LO PRESS. FOUND NR 1 ENG HYD LOW PRESSURE SWITCH LINE LEAKING. REPLACED LINE AND LEAK CHECKED NORMAL IAW AMM 29-11-49-000-009 AND 29-11-49-400-005.SDR DJFA2006316Line · chafedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A (D) LEVEL INSPECTION A BRAKE RETURN LINE WAS FOUND TO BE CHAFING FROM A SCREW THAT SECURES THE CENTER COCKPIT TO CABIN FLOORBOARD. INSPECTION AND REPAIR OF THIS AREA IS OUTLINED IN MFG SB 53-3511. THE CSDR 2006UALA01744Valve · failedBRAKE & ANTI-SKID MESSAGES ON TAXI. THE DISCREPANCY WAS DIAGNOSED AS A FAILED TWO PORT MOTOR OPERATED HYDRAULIC VALVE ASSY. REPLACED PARK VALVE, AND THE MESSAGE CLEARED.SDR DJFA2006315Line · brokenDURING CLIMBOUT AFTER GEAR RETRACTION RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WERE CYCLED BACK DOWN AND THREE GREEN LIGHTS WERE RECEIVED INDICATING THE GEAR WERE DOWN AND LOCKED. SHORTLY AFTER EXTENDING THE GEAR AN AMBER -HYDRAULIC VOLUMSDR HALA0600680Pressure Switch · unknownETOPS SIGNIFICANT SYSTEM, LOW PRESS LIGHT ILLUM EICAS MSG DISPLAYED C HYD PRIM1. EICAS MSG C HYD SYS MAINT WAS NOT DISPLAYED. OPS CK CENTER HYD SYS COULD NOT DUPLICATE PROBLEM. REPLACED C1 ELECTRIC HYD PUMP PRESSURE SWITCH IAW MM 29-11-18. OPS AND LEAK CK OK SDR UPS06647931Line · leakingAIR TURNBACK, LEFT HYDRAULIC QUANTITY LOSS. T/S & FOUND HYD LEAKING AT THE L/H ENG STRUT HYD. BAY. OPENED & IN- SPECTED, FOUND DIFF PRESS IND. ON PRESS & DRAIN CASE FILTER MODULE LEAKING. R/R D.P.I. AS PER AMM 29-11-17-4; LEAK CK'D SATIS.SDR RYNA200600007Pcu · failedLOST LT SYSTEM HYDRAULIC FLUID DURING FLIGHT. REMOVED AND REPLACED RT ELEVATOR, CENTER POWER CONTROL UNIT (PCU) IAW MM 27-31-05. OPERATIONAL/FUNCTIONAL AND LEAK CHECKED GOOD.SDR 06FDEA03191Hydraulic System · unknownAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT INDICATION WAS THREE REDS DOOR LIGHTS THREE GREEN DOWN AND LOCKED LIGHTS ON. HANDLE WOULD NOT GO ABOVE NEUTRAL POSITION . TRIED BOTH SYST NR 1 AND SYST NR 2 AS PER QRH AND C/BS. PERFORMED VISUAL INSPECTION TO PISDR HALA0600670Hydraulic System · unknownETOPS SIGNIFICANT SYSTEM - DURING CLIMBOUT DURING THE LAST 10,000FT OF CLIMB L ENG PRIMARY HYD PRESS LIGHT CAME ON FOLLOWED BY THE L ELECT DEMAND PRESS LT. CREW NOTED PRESS WOULD DROP TO APPX 1700 PSI, RTN TO NORMAL & PRESS LIGHT WENT OUT. HYD QUANTITY 1.4 ISDR 06FDEA03178Hydraulic System · unknownAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. INDICATION WAS THREE RED DOOR LIGHTS THREE GREEN DOWN AND LOCKED LIGHTS ON. HANDLE WOULD NOT GO ABOVE NEUTRAL POSITION. TRIED BOTH SYST NR 1 AND SYST NR 2 AS PER QRH AND C/BS. PERFORMED VISUAL INSPECTION TO PISDR COMA0660527Hydraulic Line · looseFLIGHT 5080 - HYD SYSTEM NR 3 LOW PRESSURE CAUTION MESSAGE. INSPECTED NR 3 HYD SYSTEM, FOUND LOOSE LINE AT NR 3 ACCUMULATOR, TIGHTENED LINE, SERVICED SYSTEM LEAK AND OPS CHECK GOOD.SDR AT0600031Line · chafedON APPROACH HYD RT QTY LO RT RESERVOIR SHOWED 0. FOUND HYDRAULIC LINE PN NR 7972148-520 CHAFED. PREFORMED PERMA SWAGE TYPE 2 REPAIR REF MM 20-10-01 LEAK CHECK GOOD. SERVICED RT HYDRAULICS REF MM 12-13.SDR QXEA200602371Valve · malfunctionedSEA FLIGHT 2002 DURING PUSHBACK, WHEN BRAKES APPLIED THE NR 1 HYDRAULIC PRESSURE DROPPED TO 1000 PSI. ROLL SPOILER CAUTION. MAINTENANCE REPLACED THE NR 1 SYSTEM UNLOADING VALVE AND ADJUSTED SPOILER DISCONNECT SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNSDR GNL2006F00000Hydraulic Line · crackedIN FLIGHT, AC EXPERIENCED A HYD PRESSURE WARNING LIGHT ON THE RT ENGINE HYD PUMP, THEN THE LT ENGINE DRIVEN HYD PUMP. THE LANDING GEAR WAS EXTENDED WITH THE EMERGENCY BLOW DOWN SYSTEM. THE AC LANDED WITH NO OTHER ISSUES. THE AC WAS TOWED FROM THE RUNWAY TO SDR CA060907007Line · leaking(CAN) PILOT REPORTED THAT LANDING GEAR DID NOT RETRACT. 2.5 QUARTS OF HYDRAULIC FLUID WERE LOST AND HYDRAULIC PUMP CIRCUIT BREAKER POPPED AND LOW FLUID LEVEL CAUTION LIGHT ILLUMINATED. MANUAL EXTENSION WAS CARRIED OUT AND AIRCRAFT LANDED SAFELY. INVESTIGATION SDR CA060829001Fitting · corroded(CAN) DURING INSPECTION, A LEAK WAS DISCOVERED IN THE HYDRAULIC SYSTEM PRESSURE SIDE CROSS FITTING (AN 937-D6). DISASSEMBLY REVEALED CORROSION AT MATING SURFACE OF O-RING AND CROSS. PART REPLACED WITH NEW. O-RINGS AND RETAINING RING REPLACED. SYSTEM SERVICED SDR MASA200602191Hydraulic System · contaminatedASH 7069 DEN - THE NLG WOULD NOT EXTEND NORMALLY ON FINAL IN EGE BUT IT DID EXTEND ALTERNATELY. AC FERRIED TO GJT FOR REPAIRS. MX BLED AIR FROM THE NR 2 HYDRAULIC SYSTEM. OP'S CHECK GOOD.SDR HNAA0600090Line · leakingNR 2 ISO HYDRAULIC CAUTION LIGHT CAME ON AFTER TAKEOFF AND NR 2 HYDRAULIC QUANTITY SHOWS ZERO. FOUND LANDING GEAR ACTUATOR LINES LEAKING. REMOVED AND REPLACED LINES.SDR HALA0600629Tee Fitting · leakingETOPS SIGNIFICANT SYSTEM - RUDDER RETURN CENTER SYSTEM HYDRAULIC LINE LEAKING AT TEE FITTING LT SIDE CROWN AREA SECT 48. FOUND CRACKED TEE FITTING AT P/N TUBE 272T4800-338 END. REMOVED AND REPLACED MS21905D10 TEE PER AMM 20-10-09-404-007, LEAK CHECKED AND SESDR 06FDEA03089Hydraulic Line · brokenEN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN. REMOVED AND REPLACED BOTH NR 1 AND NR 2 HYDRAULIC SDR 06FDEA3089Hydraulic Line · brokenEN ROUTE TO KFNT SYS A HYDRAULIC FLUID WENT TO ZERO QUANTITY. ALONG W/ 2 SYS A LOW PRESSURE LIGHTS. HYDRAULIC SYSTEM LEAK OR LOSS PROCEDURES ACCOMPLISHED IAW QRH. FOUND NR 2 SPOILER HYD RETURN LINE BROKEN.SDR CA060921002Union · sheared(CAN) CREW REPORTED NR 2 ENG HYD PUMP CAUTION ILLUMINATED, PRESS AND QTY DEPLETED. FOLLOWING GEAR EXTENSION ON APPROACH. NO EMERGENCY DECLARED. MAINTENANCE FOUND THE HYD FITTING FROM THE EDP TO THE PRESS MANIFOLD SHEARED. SYD 8-29-002, REPLACEMENT OF ALUMINIUSDR 2006UALA01651Hydraulic System · malfunctionedRETURN TO FIELD DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. YELLOW SYSTEM PRESS AND QUANTITY ARE NORMAL FROM BOTH THE EDP AND THE PTU. REPLACED YELLOW SYSTEM TRANSDUCER AND SWITCH-TEMPERATURE [P/N TM113-1]. REPLACED THE YELLOW SYSTEM ELECTRIC HP CHECK VALVE [P/SDR CA060824004Line · leaking(CAN) AIRCRAFT WAS IN CRUISE, CREW NOTED HYDRAULIC LEAKAGE ON THE COCKPIT FLOOR. CONDUCTED A NORMAL LANDING, NOSE GEAR UP LINE IN COKPIT WAS LEAKING. REPLACED LINE, ON NEXT LEG, A LINE FAILED IN THE LH GEAR WELL, CREW ACTIVATED EMERGENCY EXTENSION AND NORMAL SDR 2006UALA01637Hydraulic System · malfunctionedRETURNED TO FIELD DUE TO LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE. INDICATION WENT TO ZERO FOR CENTER HYD TANK WHICH VISUALLY VERIFIED FULL. REPLACED CTR HYD PRESSURE QTY TRANSMITTER. NO RECURRENCE PROBLEM REPORTED.SDR CA060822003Line · chafed(CAN) DURING ROUTINE MAINTENANCE INSPECTION, FOUND NR 1 ENGINE DRIVEN PUMP OUTLET PRESSURE TUBE OF GREEN HYDRAULIC SYSTEM CHAFED BY THE AILERON TRIM INPUT CABLE AT REAR SPAR OB OF RIB 5A. HYDRAULIC TUBE REPLACED. CAMPAIGN INITIALIZED TO VERIFY THE REST OF THE SDR ASMF200608012Control Valve · leakingCAPTAIN REPORTED THAT AFTER LANDING, THE LT HYDRAULIC SYSTEM WAS LOST AND LT REVERSE REMAINED EXTENDED. AIRCRAFT WAS TOWED TO PLATFORM AND RECHARGED OF HYDRAULIC LIQUID, DETECTING A LEAK IN THE LT HYDRAULIC REVERSE VALVE CAP. THE LT HYDRAULIC REVERSE VALVE WASSDR UPS06847707Manifold · leakingATB - HYDRAULIC SYSTEM QUANTITY LOSS. NO HYD BRAKE PRESSURE. AIR BRAKES STOPPED A/C. NR 1 & 2 T/R STOWED NR 3 & 4 WOULD NOT STOW. CHECKED ENGINE 2 & 3 EDP'S CASE DRAIN FILTER CHIP DETECTORS-NO DEBRIS FOUND. R&R RT HYD POWER MANIFOLD PER MM 29-10-20-02. OPS/LSDR MASA200602099Hydraulic System · lack of lubeASH 2730 PHX - NR 2 HYDRAULIC SYSTEM AT 20 PERCENT. MX SERVICED THE SYSTEM.SDR WRLA2006039Seal · blownRCH764/14 KGTB/KGTB DURING CLIMB (HYD 3 ELEV OFF) LEVEL 1 ILLUMINATED. HYD 3 WENT TO 3.8GAL. CONFERED WITH MX AND ACCOMPLISHED AIR RETURN TO KGTB. AFTER GEAR DOWN HYD 3 QUANTITY WENT TO 2.1 AND THE (HYD 3 QTY LOW) LEVEL 1 ALERT ILLUMINATED. FOUND HYD SYSTEM SSDR CA060809001Line · leaking(CAN) FOUND HYD LEAK IN LT WHEEL WELL. GEAR UP LINE FOUND CRACKED. LINE REPLACED, GEAR SWINGS CARRIED OUT. AIRCRAFT RETURNED TO SERVICE (TC NR 20060809001)SDR 06FDEA2914Control Unit · jammedGREEN SYSTEM SERVO CONTROL JAMMED. T/S AND REMOVED AND REPLACED JAMMING DECTECTION CONTROL UNIT (4CB) PERFORMED OP`S TEST AND NO HELP REINSTALLED OLD UNIT BACK ON A/C. ALL WORK DONE IAW AMM 27-14-17-4. STILL TROUBLESHOOTING AT THIS TIME. REMOVED AND REPLACESDR 06FDEA2919Reducer · brokenHYD 3 FAIL LEVEL 2 ALERT AT ALTITUDE. QUANTITY .2, PUMPS OFF WHEN SD CHECKED. DIVERTED TO KIX. FOUND NR 3 HYD RESERVOIR DRAIN VALVE REDUCER IS BROKEN. REMOVED REMAINING PART OF REDUCER THREAD & CAPPED TO RELEASE A/C WITH EA REMOVED AND INSPECTED. SYS ANDSDR CA060815001Line · cracked(CAN) HYDRAULIC FLUID NOTICED BY MAINTENANCE ON BELLY AREA OF AIRCRAFT. GEAR UP LINE FOUND CRACKED. LINE REPLACED AND GEAR SWINGS CHECKED SERVICIBLE. (TC NR 20060815001)SDR DXTA200601542Line · leakingON TAXI OUT OF RAMP. CO-PILOT SIDE BRAKES FAILED. REPEAT WRITE UP. BOTH PEDALS WERE FULLY DEPRESSED TO THE FLOOR WITH NO BRAKING ACTION. INSPECTED ALL MASTER CYLINDERS. NO LEAKS. C/W BRAKE FUNCTIONAL CHECK WITH POWER ON. PILOT AND CO-PILOT BRAKES HAVE SDR C2XA06IA125O-Ring · failedIAH - FLIGHT 2278, THE CREW REPORTED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE O-RINGS ON THE RIGHT HAND SPOILER HYDRAULIC CONNECTIONS, SERVICED THE AIRSDR 2006UALA01520Hydraulic System · leakingLOST GREEN HYDRAULIC SYSTEM ON GEAR EXTENSION. REQUIRED A TOW TO THE GATE.SDR CA060818001Line · cracked(CAN) HYD LINE IN UPPER FORWARD AREA OF NR 1 NACELLE CHAFED THROUGH AT ADJACENT ADELE CLAMP, LEAKAGE LOCATED AND LINE ASSY P/N 82970410-115 REPLACED, SYSTEM BLED AND REPRESSURIZED WITH NO FURTHER FAULTS. GOING THROUGH THE LAST 1 MONTH PERIOD THERE HAVE BEEN N
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