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 CA050830006Line · cracked(CAN) FLIGHT CREW NOTICED HYD FLUID LEAKING FORM THE LEFT SIDE OF THE NACELLE. MAINTENNACE INSPECTED LEAK AND FOUND UP GEAR HYD LINE FROM POWER PACK TO GEAR ACTUATORS LEAKING. CRACKED IN 90 DEGREE BEND RADIUS. LINE REPLACED,GEAR SWINGS CARRIED OUT AND AIRCRAug 29, 2005 · Swrngn SA227*SDR HEEA107325Heat Exchanger · rupturedDURING CRUISE FLIGHT, THE NR 1 HYDRAULIC RESERVOIR LOW LIGHT ILLUMINATED, FOLLOWED BY OTHER ASSOCIATED LIGHTS CONFIRMING THE NR 1 HYDRAULIC SYSTEM FAILURE. MAINTENANCE FOUND THE HYDRAULIC SYSTEM HEAT EXCHANGER RUPTURED.Aug 27, 2005 · N292PH · Skrsky S92ASDR 2005UALA00906Hydraulic System · malfunctionedRETURNED TO ANC UNDER AN AMBER ALERT DUE TO A HYDRAULIC PROBLEM. LEFT HAND ENGINE HYDRAULIC PUMP FAILED. REPLACED LEFT HAND PUMP PER MM29-11-05. ALSO REPLACED PRESSURE FILTER AND CASE DRAIN FILTERS. CHECKED AND REPLACED ELECTRIC HYDRAULIC PUMP CASE DRAIN FAug 27, 2005 · N568UA · Boeing 757222SDR HNAA0500079Check Valve · crackedAT GEAR RETRACTION NR 2 ISOV CAUTION LIGHT ILLUMINATED FOLLOWED BY ROLL SPOILER HYD. CAUTION LIGHT NR 2 QUANTITY DROPPED TO 1/2 QT. SYSTEM PRESSURE REMAINED NORMAL. REPLACED CHECK VALVE.Aug 26, 2005 · N912HA · Dhav DHC8102SDR XN0A1261Hydraulic System · failedON TAXI, YELLOW HYD AIR PRESS LOW INDICATION AND QTY DECREASE TO YELLOW BAND. VERIFIED YELLOW SYS, FALL AT RESERVOIR. SERVICED HEAD PRESSURE, SYS NORMAL PER A300 MM 29-00-00.Aug 25, 2005 · N371PC · Airbus A300B4203SDR DXTA200500926Line · leakingEXCESSIVE BRAKE PEDAL PRESSURE NEEDED ON LANDING ROLL OUT. REQUIRED LARGER THAN NORMAL INPUT TO STOP AIRCRAFT. THIS WAS A DRY RUNWAY NOT CONTAMINATED. PERFORMED VISUAL INSPECTION OF BRAKES AND PLUMBING. PERFORMED POWER BRAKE BLEEDING IAW CITATION 750 MM CHAug 25, 2005 · N947QS · Cessna 750SDR DXTA200500925Hydraulic System · leakingCOMPLETE LOSS OF THE NR 1 HYDRAULIC SYSTEM IN FLIGHT AT FL410. HYD QTY DROPPED TO 15 PERCENT, PRESSURE FELL TO 100PSI. UPON LANDING HYDRAULIC FLUID NOTED ALL OVER BELLY OF ACFT AND COVERING INSIDE OF "HELLHOLE" COMPLIED WITH NORMAL AND ABNORMAL CHECKLIST PERAug 25, 2005 · N277QS · Amd FALCON2000SDR MALA050673Ptu · malfunctionedGREEN HIGH TEMP HIGH. REMOVED AND REPLACED PTU PN 4204002, SN OFF LM54 ON BX63. REMOVED AND REPLACED NR 3 EDP PN 521499 SN ON 60010412 OFF F991164 AND GREEN ISO VALVE PN HTE9531-3 SN ON 290VB151, OFF FR020BA IAW AMM 29-10-17-201, 29-10-14. RAN FOR 45 MINUTEAug 25, 2005 · N532XJ · Bac AVRO146RJ85ASDR WRNA200500020Solenoid Valve · leakingWHILE IN FLT, CLIMB, LOSS OF GREEN HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. FOUND GREEN SYSTEM EDP SOLENOID VALVE LEAKING. REMOVED AND REPLACED EDP SOLENOID, OP'S CHECK SATISFACTORY IAW 29-11-32. AIRCRAFT LANDED OVERWEIGHT. IAug 24, 2005 · N821SC · Airbus A300B4203SDR CA050824018Line · chafed(CAN) DURING PHASE 5 INSP, 2 HYDRAULIC LINES FOUND CHAFING ON STRUCTURE. P/N 6617077-19 AND 20. REF. AC MFG PROVIDED ENG MFG WITH DRAWING TO INSTALL MISSING LINE SUPPORT HARDWARE TO PREVENT CHAFING.Aug 23, 2005 · Cessna 560XLSDR C2XA05CL069Pressure Switch · crackedROC - FLIGHT NR 2040, THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY IN FLIGHT. REPORTED LOSS OF ALL NR 1 HYDRAULIC FLUID IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE PRESSURE SUPPLY PRESSURE SWITCH. ALSO, REPLACED THE NR 1 HYDRAULIC PUMP AND FILTER.Aug 22, 2005 · N12934 · Emb EMB145EPSDR HEEA107335Line · rupturedNR 2 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE FOUND NR 2 HYDRAULIC PUMP DISCHARGE HOSE HAD RUPTURED. REPLACED HOSE.Aug 21, 2005 · N192PH · Skrsky S92ASDR AALA20050547Line · rupturedBOS INFLIGHT T1752/21AUG - ON FINAL APPROACH, AIRCRAFT UNABLE TO EXTEND RIGHT MAIN GEAR. EXENDED GEAR THROUGH EMERGENCY PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND FLEX LINE AT RIGHT GEAR DOWNLOCK ACTUATOR RUPTURED. REPLACED BOTH FLEX LINES. AIRCRAFT MAINAug 21, 2005 · N652AA · Boeing 757223SDR C2XA05CL067B-Nut · looseCLE - FLIGHT NR 2275, THE CREW REPORTED A HYDRAULIC SYSTEM NR 2 FAIL IN FLIGHT. THE AIRCRAFT DIVERTED INTO BUF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED LOOSE "B" NUT ON THE NR 2 ENGINE HYDRAULIC PUMP. SERVICED THE NR 2 HYDRAUAug 20, 2005 · N13989 · Emb EMB145LRSDR ASMF200508011O-Ring · leakingDURING TRANSIT CHECK, DETECTED HYDRAULIC LEAK IN NOSE LANDING GEAR. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE LANDING GEAR STRUT O-RING SEALS WERE REPLACED IAW MM 32-21-02, TESTED CORRECT.Aug 20, 2005 · N158PL · Doug MD88SDR CA050819001Check Valve · leaking(CAN) AN OPERATOR EXPERIENCED A LOSS OF HYDRAULIC SYSTEM NR 2, IN FLIGHT, DUE TO A FRACTURED CHECK VALVE. A VISUAL INSPECTION OF THE CHECK VALVE REVEALED A CRACK AROUND THE CIRCUMFERENCE OF THE VALVE BODY. THE CHECK VALVE IS BEING RETURNED TO MFG FOR INVESTIAug 19, 2005 · Dhav DHC8301SDR YTRR105444Servo · leakingON ROUTINE INSPECTION FOUND HYDRAULIC SERVO LEAKING BEYOND ACCEPTABLE LIMITS.Aug 19, 2005 · N4125C · Bell 412SDR AALA20050535Line · rupturedBOS - AT PUSHBACK WHEN BRAKES WERE RELEASED HYDRAULIC FLEX LINE IN LEFT WHEEL WELL RUPTURED. REPLACED LEFT HAND GEAR WHEEL WELL HYDRAULIC LINE IN UPPER SECTION OF LEFT HAND GEAR AFT OF REAR SPAR. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 18, 2005 · N603AA · Boeing 757223SDR WRNA200500019Line · leakingLOST GREEN HYD FLUID DURING GEAR RETRACTION. FOUND LT MAIN GEAR DOOR ACTUATOR LINE FAILED. REPLACED WITH TEMPORARY LINE IAW MM 20-23-11. SERVICED HYD'S IAW 12-12-29 OPS CK AND LEAK CK SATISFACTORY. ITEM PLACED ON CI, DMI NR 1927, TO BE REPLACED BY 9-17-05 Aug 18, 2005 · N505TA · Airbus A300B4203SDR 2005UALA00835Hydraulic System · malfunctionedRETURNED TO SFO UNDER AMBER ALERT DUE TO NR 4 HYDRAULIC SYSTEM PROBLEM .Aug 15, 2005 · N196UA · Boeing 747422SDR 2005UALA00833Hydraulic System · failedGREEN HYDRAULIC SYSTEM FAILURE AND YELLOW SYSTEM OVERHEAT.Aug 15, 2005 · N435UA · Airbus A320232SDR MALA050654Valve · failedLOSS OF GREEN HYD SYSTEM. RAN CHECK LIST AND PERFORMED EMERGENCY GEAR EXTENSION. REPLACED GREEN SYSTEM HYD SELECTOR VALVE NR 3 ENGINE HYD PUMP AND FLUSHED GREEN SYSTEM HYD SYSTEM AND REPLACED FILTERS. REMOVED AND REPLACED SELECTOR 71149-3 SN ON/OFF F9748464Aug 15, 2005 · N526XJ · Bac AVRO146RJ85ASDR RAIA00508019Line · brokenFLT 3537-PIT-NR 4 BRAKE INBOARD HYDRAULIC QUICK DISCONNECT LINE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRAKE HOSE ASSEMBLY.Aug 13, 2005 · N811HK · Emb EMB145LRSDR 2005UALA00794Hydraulic System · leakingFLIGHT EXPERIENCED GREEN HYD QTY LOSS AND ECAM INDICATION.Aug 9, 2005 · N484UA · Airbus A320232SDR MALA050637Hydraulic System · failedCREW RETURNED TO MSP AFTER DEPARTURE, DUE TO HYDRAULIC SYSTEM FAILURE. GEAR WAS SUCCESSFULLY EXTENDED AND CFR CALLED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME.Aug 8, 2005 · N361PX · Saab 340BSDR 2005FA0001095Line · leakingDURING FLIGHT, THE LT AND RT HYDRAULIC LOW LEVEL LIGHTS ILLUMINATED ALONG WITH A MASTER CAUTION LIGHT. AFTER A SAFE LANDING, THE ENTIRE TAIL OF THE AIRCRAFT WAS FOUND TO BE SOAKED WITH HYDRAULIC FLUID. FURTHER INVESTIGATION FOUND THAT HYDRAULIC LINE HAD RUPTUAug 8, 2005 · N247CW · Cessna 525SDR 2005FA0001094Line · scoredDURING FLIGHT, THE LT AND RT HYDRAULIC LOW LEVEL LIGHTS ILLUMINATED ALONG WITH A MASTER CAUTION LIGHT. AFTER A SAFE LANDING, THE ENTIRE TAIL OF THE AIRCRAFT WAS FOUND TO BE SOAKED WITH HYDRAULIC FLUID. FURTHER INVESTIGATION FOUND THAT HYDRAULIC LINE HAD RUPTAug 8, 2005 · N247CW · Cessna 525SDR DJFA2005127Line · rupturedON LANDING ROLL AS THE A/C SLOWED THROUGH 55 KTS BRAKE PRESSURE WAS LOST AND THE THRUST REVERSERS WOULD NOT DEPLOY. THE EMERGENCY BRAKES WERE APPLIED TO STOP THE A/C. AT THAT POINT, THE HYD PRESSURE WAS INDICATING ZERO. WHILE AWAITING PARKING INSTRUCTIONS, Aug 7, 2005 · N708TA · Beech 400ASDR DL75K050427Line · leakingCOMPLETE LOSS OF LEFT HYD SYSTEM AFTER CONFIGURING FOR LANDING IN BDL. DECLARED EMERGENCY. LANDED UNEVENTFULLY. WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. FOUND HYD LINE TO NOSE WHEEL STEERING LEAKING AT COUPLING. INSTALLED APPROVED HYD LINE, LAug 4, 2005 · N650DL · Boeing 757232SDR 0501196744Hose · failedAFTER TAKEOFF, HAD A TOTAL LOSS OF NR 4 HYDRAULIC SYSTEM. COM WAS FOLLOWED, AN EMERGENCY WAS DECLARED WITH ATC AND RETURNED TO SIN, LANDING WAS UNEVENTFUL. FOUND LEFT HAND WING GEAR ACTUATOR UP FLEX LINE BROKEN AND REPLACED. REPLACED (EDP) ENGINE DRIVEN HYDAug 3, 2005 · N644NW · Boeing 747212FSDR AT0500025Line · crackedLOSS OF HYD PRESSURE AND QUANTITY AFTER TAKE OFF. FOUND CRACKED END ON GROUND SRV RETURN/PRESS LINE. REPAIRED END OF TUBING WITH PERM-A-SWAGE FITTING REF M/M 20-10 SERVICED HYD LEAK AND OPS CK GOOD. RAN NR 2 ENG, OPS CK EDP, OPS CK GOOD.Aug 3, 2005 · N977AT · Boeing 717200SDR DJFA2005124Hydraulic System · leakingAFTER TAKEOFF CREW REPORTED HEARING A CAVITATION SOUND FROM THE REAR OF THE AIRCRAFT. AROUND 10,000 FT HYDRAULIC FLOW LOW LEFT AND RIGHT ANNUNCIATORS AND MASTER CAUTION LIGHTS WERE FLICKERING ON AND OFF. AFTER APPROXIMATELY 30 SECONDS, THE HYDRAULIC FLOW ANDAug 2, 2005 · N247CW · Cessna 525SDR MALA050623Hydraulic System · failedCREW RETURNED TO MEM FOLLOWING FAILURE OF THE GREEN HYDRAULIC SYSTEM. EMERGENCY NOT DECLARED BUT ARFF ON STANDBY. FLIGHT LANDED WITHOUT FURTHER INCIDENT.Aug 2, 2005 · N504XJ · Bac AVRO146RJ85ASDR ASMF200507025Valve · failedACFT RETURNED OF FLT AS A CONSEQUENCE OF RT VELOCIMETER OSCILLATED FROM 0-400 KTS & ALARM ACTIVATED. DIRECTOR BUSS DISAPPEARED IN BOTH PFD AND FMA W/O IND, AUTOMATIC ACCELERATORS DISCONNECTED, MACH TRIM LIGHT TURNED ON INFLT, AUTOPILOT DISENGAGED FREQUENTLY & Jul 31, 2005 · N751RA · Doug DC987SDR ALG2005F00056Line · leakingENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE Jul 30, 2005 · N390AL · Bell 214STSDR PNSA050703Line · failedDURING CRUISE ENROUTE, 100 MILES WEST, LT HYDRAULIC LIGHT CAME ON FOLLOWED WITH RT WARNING LIGHT. CREW CONFIRMED ON HYD PRESSURE GAUGE LOSS OF PRESSURE. CREW DECLARED AN EMERGENCY WITH CENTER AND DIVERTED WHERE MAINT WAS AVAILABLE. MAINT FOUND HARD HYDRAULIC PJul 29, 2005 · N2719H · Swrngn SA227ACSDR DLM88050412Tube · leakingLEFT AFT LAV SMOKE DETECTOR ACTIVATED WITH SLIGHT ODOR PRESENT. REPAIRED HYDRAULIC LINE AT LEFT THRUST REVERSER CONTROL VALVE. PERFORMED DUCT BURNOUT PROCEDURE. CHECKS GOOD.Jul 28, 2005 · N965DL · Doug MD88SDR DHL2005806001O-Ring · leakingDURING CLIMB OUT,HYD PRESS DROPPED TO ZERO AND HYD QTY DROPPED TO AUX LEVEL. DURING ABN PROC SYSTEM LEVEL DROPPED WELL BELLOW AUX LEVEL WHEN CONFIGURING TO LAND. FOUND WING SLOT CNTL VALVE IN R. W/W LEAKING AT RETAINING PLUG/STUD. R & R UPPER AND LOWER O-RINGJul 27, 2005 · N806DH · Doug DC873FSDR 2005F00091Hose · failedHYDRAULIC HOSE TO NOSE LANDING GEAR CYLINDER FAILED IN FLIGHT. THIS CAUSED TOTAL DEPLETION OF HYDRAULIC FLUID AND SUBSEQUENT HYDRAULIC PUMP FAILURE. PILOT WAS UNABLE TO EXTEND LANDING GEAR MANUALLY BECAUSE OF NOT ENOUGH FLUID. A GEAR UP LANDING WAS MADE WITH Jul 26, 2005 · N545PZ · Cessna 177RGSDR XN0A1249Hydraulic System · lowGREEN & YELLOW HYDRAULIC SYSTEM AIR PRESSURE LOW LIGHT REMAINS ON AFTER BOTH ENGINES STARTED. SERVICED GREEN SYSTEM RESEVOIR HEAD PRESSURE CKS NORMAL PER MM 29-14-00. YELLOW SYSTEM - X-FERRED TO DMI LIST IAW A300 MEL 29-32-03 ASSIGNED 5587 S.P. 29-32-03. C/WJul 26, 2005 · N372PC · Airbus A300B4203SDR DXTA200500865Hydraulic System · leakingWHILE WAITING FOR CLEARANCE FOR T/O, SMELLED A VERY BAD ODOR FOLLOWED BY THE HYD PRESS B LOW AND THE HYD PUMP B-SYSTEM FAIL, THEN THE RUDDER STANBY SYSTEM FAIL LIGHT. LEAKING APPEARED TO COMING FROM THE PYLON AREA. ITEM IS UNDER INVESTIGATION.Jul 25, 2005 · N987QS · Cessna 750SDR ARWA20050703Line · leakingFOUND HYDRAULIC LINE LEAKING; LOCATED ON TOP OF RIGHT LANDING GEAR WHEEL WELL. REPAIRED HYDRAULIC LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. NO LEAKS FOUND IN ACCORDANCE WITH DC-10 M/M 29-00-00Jul 24, 2005 · N526MD · Doug DC1030SDR AWXA200500843Manifold · leakingDURING CLIMB HAD GREEN HYDRAULIC FAILURE. AIRCRAFT RETURNED TO PHX, CREW DECLARED AND PREPARED CABIN FOR EMERGENCY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GROUND LEAKAGE MEASUREMENT MODULE LEAKING. REMOVE AND REPLACED THE GROUND LEJul 24, 2005 · N634AW · Airbus A320231SDR QXEA200501134Hydraulic System · malfunctionedSEA FLIGHT NR 2203 - RIGHT OUTBOARD SPOILER DOES NOT INDICATE DEFLECTION ON PFCS, APPEARS TO DEFLECT NORMALLY FROM COCKPIT. MAINTENANCE BLED NR 2 HYDRAULIC SYSTEM IAW 29-00-00-870-805. PERFORMED OPERATIONAL TEST OF ROLL SPOILER CONTROL SYSTEM IAW -8(200) AMJul 24, 2005 · N347PH · Dhav DHC8202SDR KMB2005F00000Accumulator · leakingACCUMULATOR, DURING HYDRAULIC TEST, ACCUMULATOR LEAKED. REMOVED AND REPLACED. (K)Jul 23, 2005 · N1188P · Snias AS350BASDR QXEA200501133Relay · failedNR 1 STANDBY HYDRAULIC PRESSURE READS ZERO AFTER SWITCH SELECTED TO NR 1. MAINTENANCE REPLACED RELAY 292-K5, NR 1 STANDBY HYDRAULIC PUMP OPERATES NORMALLY AS PER AMM 29-11-17-710-801. CIRCUIT BREAKER REMAINED SET. AIRCRAFT RETURNED TO SERVICE.Jul 23, 2005 · N354PH · Dhav DHC8202SDR 2005FA0001097Union · looseHYD UNION WAS FOUND TO BE LOOSE ALLOWING O-RING TO FAIL OVER TIME. O-RING WAS REPLACED AND FITTING TORQUED. (K)Jul 21, 2005 · N970SK · Cessna 750SDR CA050803005Line · leaking(CAN) CAPTAIN REPORTED A LOSS OF FLUID FROM NR 1 HYDRAULICS. EVERYTHING SEEMED TO OPERATE NORMALLY, BUT CREW ELECTED TO DO THE FLAPLESS LANDING IN CASE OF A GO AROUND. NR 1 HYDRAULIC SYSTEM DRAINED DOWN TO 1 QUART INFLIGHT. FOUND IB ROLL SPOILER PRESSURE CJul 20, 2005 · Dhav DHC8311SDR UPS05844933Hydraulic System · leakingATB - HYDRAULIC FLUID LOSS, EMERGENCY DECLARED. FOUND LEFT MAIN GEAR DOWNLOCK BUNGEE CYLINDER PRESSURE LINE LEAKING/ DAMAGED. R/R LINE PER MM 30-12-2. SVCD HYD SYSTEM PER MM 12-30-01-3 LEAK CK O.K.Jul 20, 2005 · N702UP · Doug DC871FSDR 2005FA0001257O-Ring · failedNAS1612-6, O-RING LOCATED ON AN814-6K, PLUG INSTALLED IN (A) HYDRAULIC SYSTEM MANIFOLD, PN 6717277-3 FAILED, CAUSING LOSS OF SYSTEM (A) HYDRAULIC FLUID AND SUBSEQUENT PILOT SHUTDOWN OF (A) HYDRAULIC SYSTEM. FOUND TORQUE ON PLUG TO BE LESS THAN 30 INCH POUNDS Jul 18, 2005 · N15RL · Cessna 750
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