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 CA050718001Line · brokenOPERATOR EXPERIENCED A LOSS OF HYD SYSTEM NR 1 AFTER TAKEOFF. FLIGHT CREW MADE AN UNSCHEDULED LANDING. EDP NR 1 PRESS LINE FOUND BROKEN IN LT NACELLE. HYD LINE AND EDP NR 1 REPLACED. PURGED SYSTEM. AIRCRAFT RTS.Jul 18, 2005 · Dhav DHC8301SDR COMA0560395Line · leakingFLIGHT 5667- NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HYDRAULIC LINE.Jul 16, 2005 · N937CA · Cndair CL6002B19SDR P9RA20050094Pressure Switch · intermittentAT BEGINNING OF TAKE OFF ROLL, CENTER HYDRAULIC SYSTEM PRESSURE LOW MESSAGE APPEARED ON EICAS. RETURNED TO GATE. ASSIGNED MEL 29-31-2-01. REMOVED AND REPLACED CENTER HYDRAULIC SYSTEM PRESSURE SWITCH IAW THE M/M. GROUND CHECKED GOOD AND CLEARED MEL.Jul 16, 2005 · N708TW · Boeing 757231SDR SIMA200520301Line · rupturedDISC, UPON GEAR SELECTION UP THE HYDRAULIC QUANTITY STARTED DROPPING TO -0-, MANUAL PUMP OVERRIDE FAILURE. REPLACED RUPTURED NOSE LANDING GEAR RETRACT/EXTENSION ACTUATOR HYDRAULIC LINE. LEAK AND OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)Jul 15, 2005 · N301AE · Saab 340BSDR 05FDEA01962Hose · leakingAT APPROXIMATELY 1000 FT ON CLIMB-OUT RECEIVED ECAM WARNING FOR GREEN HYD SYSTEM RESERVOIR LOW. THIS CONFIRMED ON OVERHEAD PANEL ACCOMPLISHED ECAM ITEMS AND RED TABS. GEAR EXTENDED BY GRAVITY EXTENSION METHOD SYSTEM QTY DID NOT GO TO ZERO. FOUND RUPTURED LIJul 15, 2005 · N425FE · Airbus A310SDR RAIA00507008Warning Light · illuminatedFLT 3545 - PIT - HYD 1 LOW FLUID WARNING INDICATION. MAINTENANCE BLEED AND SERVICED NR 1 HYDRAULIC SYSTEM.Jul 14, 2005 · N811HK · Emb EMB145LRSDR DLM88050369Line · leakingAFTER T/O AND T/O CHECKLIST STEP WHERE HYD AUX AND TRANS PUMPS OFF. ACFT LOST RT HYD SYSTEM PSI AND QTY, DID CHECKLISTS INCLUDING ALTERNATE GEAR EXT CONFIGURED AND LANDED NORMALLY. GEAR DOOR OPEN, LAND WEIGHT 134,000 SINK RATE AT LANDING APPROX 50 FT PER MINJul 14, 2005 · N948DL · Doug MD88SDR 2005UALA00663Packing · leakingRETURNED TO FIELD DUE TO INDICATION OF LOSS OF HYDRAULIC FLUID. HYDRAULIC FLOW LIMITER PACKINGS WERE LEAKING AT THE UNIONS, THE PACKINGS WERE REPLACED. THE LEFT HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE.Jul 14, 2005 · N509UA · Boeing 757222SDR XN0A1248O-Ring · failedYELLOW HYDRAULIC SYSTEM LOST FLUID. FOUND O-RING BROWN ON YELLOW SYSTEM FILTER HOUSING MANIFOLD. REMOVED AND REPLACED O-RING OPP & LEAK CHECK GOOD.Jul 14, 2005 · N370PC · Airbus A300B4203SDR ASOA05600Seal · wornFLT 4508 - DURING CLIMB-OUT FROM TUP-ATL, AT APPROX 18,000-19,000 FT, THE CREW RECEIVED AN INTERMITTENT ENG OIL PRESSURE AURAL AND A R ENG OIL PRESSURE WARNING FOR APPROXIMATELY TEN SECONDS. IT THEN WENT OUT AND REOCCURRED THREE TIMES WITH THE OIL PRESSURE FLJul 13, 2005 · N875AS · Cndair CL6002B19SDR DLM88050367Line · leakingDURING DESCENT, LEFT HYDRAULIC QTY DECREASED TO 4 QTS. RECEIVED AN AMBER WARNING LIGHT BUT NO OAP MESSAGE. RAN HYD QTY LOW OR DECREASING CHECKLIST AND DECLARED AN EMERGENCY WITH CVG APPROACH CONTROL. RECEIVED GOOD GEAR INDICATION DOORS UP, ND AFTER LANDING Jul 13, 2005 · N939DL · Doug MD88SDR COMA0560386Hose · leakingFLIGHT 5234 - NR 1 HYDRAULIC SYSTEM CAUTION. REPLACED LEAKING HYDRAULIC LINE.Jul 9, 2005 · N988CA · Cndair CL6002B19SDR 2005UALA00729Warning Light · illuminatedLOST GREEN SYSTEM HYDRAULIC QTY INDICATION. CREW HAS SHUTDOWN EDP AND PTU. WILL REQUIRE TOW OFF RUNWAY. GREEN HYD QTY LOSS, CREW HAS SHUTDOWN EDP AND PTU. NO SIGNS TH AT PUMP WAS RUN DRY. WILL REQUIRE TOW OFF RUNWAY. INDLM/AFTER MEETING ACFT ON RUNW AY FOJul 8, 2005 · Airbus A319131SDR CA050706008Line · leakingLOSS OF A SYSTEM HYDRAULICS. RECTIFICATION INVESTIGATION FOUND THE NUMBER 2 ENGINE THRUST REVERSER HYDRAULIC RETURN LINE HAD FAILED CAUSING THE LOSS OF A SYSTEM FLUID, PART NUMBER B432E0562C. UPON DELIBERATION WITH FLIGHT OPERATIONS, IT WAS DECIDED TO DISPATJul 5, 2005 · Boeing 737275CSDR 0500989881Packing · leakingWHILE INBOUND FOR LANDING AT MYR, THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO AND THE PRESSURE DROPPED. COM PROCEDURES WERE COMPLIED WITH AND THE RIGHT HYDRAULIC SYSTEM FUNCTIONED NORMALLY. NO EMERGENCY DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIJul 5, 2005 · N676MC · Doug DC951SDR LR7A05096Packing · splitVISIBLE FLUID LEAK NR 2 ENGINE. SHUTDOWN IAW AFM. RESEALED NR 2 ENGINE HYD PUMP PRESSURE LINE FITTING. OPS CHECK GOOD SMP581 CHAP 29-11 PG 201, NO LEAK.Jul 5, 2005 · N405LC · Lkheed 382GSDR HNAA0500062Line · leakingWHEN GEAR SELECTED UP, NR 2 HYD ISO C.L. ILLUMINATED AND QUANTITY DROPPED TO 0.5 QTS. REMOVED AND REPLACED NOSE GEAR DRAG STRUT UP LINE. INSPECTED CASE DRAIN FILTER. NO CONTAMINATION FOUND. REPLACED NOSE LANDING GEAR DRAG STRUT "UP" LINE.Jul 3, 2005 · N328HA · Dhav DHC8102SDR AALA20050423Line · leakingYELLOW SYSTEM HYDRAULIC QUANTITY LOST ON CLIMB-OUT. FOUND HYDRAULIC LINE IN LT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE IN LT WHEEL WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 3, 2005 · N11060 · Airbus A300B4605RSDR WRNA200500018Line · unserviceableT/O FROM TPE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. AIRCRAFT RETURNED TO BASE, LANDING NORMAL. FOUND HYDRAULIC LINE TO TRUCK POSITION ACTUATOR LEAKING (BLOWN). REMOVED AND REPLACED LINE IAW 32-13-05, OP'S CHECK SATISFACTORY, NO LEAKS NOTED. A/Jul 3, 2005 · N922FT · Boeing 7472U3BSDR CA050712003Line · leakingTHE GEAR WOULD NOT COME UP ON DEPARTURE. THERE WERE PROBLEMS WITH THE NR 2 HYDRAULIC SYSTEM. THE FLIGHT RETURNED FOR MAINTENANCE TO INVESTIGATE. AN EMERGENCY WAS DECLARED. DEFECT 437568 NR 2 HYD ISO VALVE LIGHT ILLUMINATED, LOSS OF SYSTEM 2 FLUID NLG RETRAJul 1, 2005 · Dhav DHC8102SDR 05FDEA01745Hydraulic System · leakingAT ROTATION A-SYS HYD FLUID WENT TO ZERO, RAN QRH, KEPT GEAR DOWN AND FLAPS 15, HAD A-SYS FLUID SHUT OFF SWITCHED OFF 23 MIN. DECLARED EMERGENCY. R & R INBOARD FLAP FLOW LIMITING VALVE PER MM. R & R NR 1 & 2 ENGINE PUMP CASE DRAIN FILTERS PER MM. R & R BOTHJun 29, 2005 · N180FE · Boeing 727100SDR MASA200500500Line · leakingASH 6932 OKC - ACFT WAS REPOSITIONING TO PHX WHEN PILOT OBSERVED HYD SYS 3B WAS SHOWING DASHES ON THE QUANTITY READING. PILOT FOLLOWED THE CFM, MANUALLY DEPLOYED LANDING GEAR AND DECLARED EMERGENCY. ACFT LANDED WITH NO FURTHER INCIDENT. PRELIMINARY INVESTIGJun 28, 2005 · N17337 · Cndair CL6002B19SDR SB05075Shutoff Valve · leakingPHL FLT 1085 AFTER TAKEOFF AND GEAR RETRACTION, CREW REPORTED A SUBSTANTIAL DROP IN THE A-HYDRAULIC SYSTEM QUANTITY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLIGHT CONTROL SHUTOJun 28, 2005 · N393US · Boeing 7373B7SDR CA050630010Line · leakingAFTER TAKEOFF AND GEAR RETRACTION, CREW NOTICED LOSS OF HYDRAULIC FLUID IN THE NR 2 SYSTEM. AIRCRAFT RETURNED FOR NORMAL LANDING. MAINTENANCE INSPECTION FOUND THE HYDRAULIC FLEX LINE TO THE NOSE GEAR DRAG STRUT ACTUATOR LEAKING. LINES REPLACED. FLUID TOPPEJun 26, 2005 · Dhav DHC8301SDR DHL2005741003Feel Unit · malfunctionedON TEST FLIGHT LOST A-SYSTEM HYDRAULICS ON APPROACH BACK INTO JAX, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. LOST A-SYSTEM HYDRAULICS, ALL QUANTITY LOST ABNORMAL PROCEDURE COMPLETED HYD FLUID SHUT OFF VALVES CLOSE FOR ONLY 1.5 MINUTES (APPROXJun 26, 2005 · N741DH · Boeing 7272Q9SDR CA050715001Hose · leakingNR 2 HYD SYS FLUID LOSS DURING APPROACH. GO-AROUND CARRIED OUT L/G WAS LEFT IN DOWN POSITION. DIVERTED A/C TO EXT. INSPECTION CARRIED OUT AND FLUID LOSS FOUND DUE TO A LEAK FROM LEFT MLG STABILIZER STRUT DOWN LOCK JACK, LOWER FLEXIBLE HOSE P/N 115503-008. Jun 25, 2005 · Bombdr DHC8400SDR AWXA200500749Line · crackedDURING FLIGHT, LT HYDRAULIC QUANTITY SHOWED ZERO. RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE TO PTU PRESSURE SWITCH CRACKED. REMOVED AND REPLACED LINE IAW BOEING 757 MM 29-31-00 AND BOEING 757 MM 20-11-00. NO LEAKS WERE NOTED.Jun 24, 2005 · N902AW · Boeing 7572S7SDR 20058Line · leakingNR 2 HYD SYSTEM LEAK. NR 2 HYD AND NR 2 ENG HYD PUMP LIGHTS ILLUMINATED. FOUND A LEAK IN NLG WHEEL WELL BEHIND THE DEBRIS GUARD ON LINE (P/N 82910010-207) WHICH EMPTIED NR 2 HYD RES. INSTALLED A TEMP LINE IAW DHC -8 MM CH 20-06-03 PG 6 & SERVICED NR 2 HYD RJun 24, 2005 · N805WP · Dhav DHC8103SDR DXTA200500802Hydraulic System · malfunctionedAUX HYD PRESS, SPOILER HOLDDOWN, HYD PRESS LOW LT AND RT. AILERON BOOST OFF. ANNUNCIATORS ALL ILLUMINATED. UPON GEAR RETRACTION GREEN LIGHTS WENT OUT BUT RED UNLOCKED LIGHT STAYED ON. AUDIBLE DRAG NOISE AND CLUNK NOISE HEARD. DRAG NOISE DISSIPATED AND RED UNJun 23, 2005 · N797QS · Cessna 650SDR DJFA2005113O-Ring · leakingAT FL290 THE NR 2 HYDRAULIC LOW PRESSURE ANNUNCIATOR ILLUMINATED AND THEN EXTINGUISHED. A FEW SECONDS LATER THE ANNUNCIATOR ILLUMINATED AGAIN AND THE HYDRAULIC PRESSURE GAUGE WAS FLUCTUATING BETWEEN 2,000 TO 3,000 PSI FOR THE REMAINDER OF THE FLIGHT. SHORTLYJun 22, 2005 · N840LX · Raythn HAWKER800XPSDR IXXA0500079OConnector · looseDURING CRUISE, ACFT STARTING LOSING HYDRAULIC FLUID. CREW ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED ACFT. LANDED WITHOUT INCIDENT. MX FOUND LOOSE HYDRAULIC CONNECTOR RT SIDE OF NR 2 ENGINE. SECURED LINE. OPS CHECK GOOD PER ALL APPLICABLE MANUALS. ACFJun 21, 2005 · N71CX · Doug DC862FSDR CA050629001O-Ring · deformedTHREE HOURS INTO FLIGHT, AIRCRAFT EXPERIENCED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. GREEN SYSTEM ENGINE DRIVEN PUMPS SELECTED OFF FOR THE REMAINDER OF FLIGHT. LANDING GEAR GRAVITY EXTENSION CARRIED OUT AND AIRCRAFT LANDED WITHOUT INCIDENT. LEAK IDENTIFIED AJun 20, 2005 · Airbus A330243SDR HK200522ALine · rupturedACFT SUFFERED AN EMERGENCY APPROACH & LANDING DUE TO COMPLETE HYD FLUID LOSS. LINE NEAR GROUND TEST PRESSURE COUPLING IN LT OF ACFT BETWEEN LOWER FUSELAGE & CARGO PACK RUPTURED. ALL HYD FLUID LOST, ENTERED COCKPIT THROUGH THE LT AIR CON DUCT, SOAKING CREW & Jun 17, 2005 · N4381 · Bag JETSTM3201SDR COMA0560355Line · leakingRECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING NR 2 EDP PRESSURE LINE.Jun 16, 2005 · N797CA · Cndair CL6002B19SDR 06152005BLine · leakingUPON LANDING, NO HYDRAULIC PRESSURE OR FLUID. REMOVED AND REPLACED RT MLG DOWN HYDRAULIC LINE.Jun 15, 2005 · N252CJ · Saab 340BSDR DL75K050324Line · leakingLT HYD SYS FAILURE. QUANITY DROPPED TO 1.6. GEAR AND FLAPS EXTENDED NORMALY. REPAIRED LEAK.Jun 15, 2005 · N649DL · Boeing 757232SDR TRB2005F00004O-Ring · damagedON FINAL APPROACH, HYDRAULIC BLUE SYSTEM LOW PRESSURE INDICATION CAME ON. AIRCRAFT LANDED WITHOUT PROBLEM. REPLACED HYDRAULIC MODULE PRESSURE SWITCH O-RING THAT WAS FOUND LEAKING. (M)Jun 13, 2005 · N448AM · Aerosp ATR72212SDR AWXA200500684Hydraulic System · overservicedAIR TURNBACK, AFTER TAKEOFF DURING FLAP AND GEAR RETRACTION YAW DAMPER, FEEL DIFFERENTIAL AND FLIGHT CONTROL BELOW PRESSURE LIGHTS ILLUMINATED. WENT TO STANDBY RUDDER -B- AND LIGHTS EXTINGUISHED. AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENJun 12, 2005 · N158AW · Boeing 7373G7SDR MALA050464Line · leakingAFTER LANDING, THERE WAS HYDRAULIC MIST IN CABIN FOLLOWED BY LOUD BANG. PASSENGERS EVACUATED. REPLACED HYD PIPE.Jun 10, 2005 · N530XJ · Bac AVRO146RJ85ASDR DXTA200500763Hose · rupturedLOST A-SYSTEM HYDRAULICS IN FLIGHT. HYD VOL LOW (A), HYD PUMP FAIL (A). BLEW GEAR DOWN AND USED EMERGENCY BRAKE SYSTEM. FOUND NOSE CENTER HYDRAULIC LINE RUPTURED. REMOVED AND REPLACED NOSE CENTER HYDRAULIC LINE AND BLEED MAIN SYSTEM IAW CESSNA 750 M/M 32-3Jun 10, 2005 · N902QS · Cessna 750SDR CA050617003Line · failedDURING TAKEOFF, THE CREW SAW THE HYDRAULIC FLOW WARNING LIGHTS ILLUMINATE. THE FLIGHT WAS TERMINATED AND THE AIRCRAFT RETURNED WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE INVESTIGATION REVEALED THAT THE TOP CONNECTION UNION ON HP HYDRAULIC PIPE WAS LEAKJun 9, 2005 · Braero HS7482ASDR VTZA200500109Tube · leakingNR 3 HYD SYS QTY DROPPED TO 0 DURING DESCENT. REMOVED AND REPLACED NR 3 A PUMP TUBE ASSY.Jun 9, 2005 · N657BR · Cndair CL6002B19SDR CA050606003Fitting · leaking(CAN) ACFT GROUNDED DURING A PRE-FLIGHT CHK WHEN HYD OIL FOUND LEAKING ON RT FWD SERVO TEE-FITTING. LINES CHECKED FOR TIGHTNESS. FITTINGS FOUND LOOSE. FITTINGS TIGHTEN & SYSTEM CHKD WITH HYD POWER PACK. NO LEAKS FOUND.Jun 6, 2005 · Robsin R44RAVENIISDR 06062005Pressure Switch · malfunctionedHYDRAULIC LIGHT ON. BOTH MAIN AND EMERGENCY PRESSURE LOW IN FLIGHT THEN MAIN READ 0 PSI. PERFORMED EMERGENCY GEAR EXTENSION.Jun 6, 2005 · N338CJ · Saab 340BSDR ASMF200506010Line · leakingDURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT WING. DURING REVISION IN RIGHT INBOARD SPOILER ACTUATOR LINE WAS DETECTED LEAKED, HYDRAULIC TUBE WAS REMOVED AND HYDRAULIC HOSE WAS INSTALLED IAW MM 20-12-04, TESTED CORRECT. DURING OVERNIGHT SERVICE,Jun 6, 2005 · N754RA · Doug DC987SDR DXTA200500756Line · leakingLEFT BRAKE PEDAL (PILOTS SIDE) DEPRESSED TO FLOOR WITH NO RESISTANCE AND NO BRAKING UPON LANDING. DURING TAXI, PEDAL WAS DEPRESSED TO FLOOR WITH NO RESISTANCE OR BRAKING. RIGHT SIDE PEDAL OK, RIGHT SEAT L/R PEDAL OK. FOUND COPILOT, LEFT BRAKE PEDAL, UPPER BJun 6, 2005 · N676QS · Cessna 560XLSDR HNAA0500050Line · leakingON APPROACH, CREW NOTICED NR 2 HYDRAULIC QTY AT 0 PSI. AFTER NORMAL SELECTION OF GEAR DOWN NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. ENGINE HYDRAULIC PUMP RAN FOR 10 MINS AT 0 QTY FOUND DOWN LINE FOR NOSE LANDING GEAR DOORS LEAKING. INSTALLED TEMJun 6, 2005 · N940HA · Dhav DHC8102SDR 2005FA0000822Hose · leakingPILOT SELECTED GEAR DOWN ON FINAL APPROACH AND THE GEAR FAILED TO EXTEND. THE INVESTIGATION FOUND THAT THE NOSE GEAR DOWN LINE WAS LEAKING AT THE BULKHEAD END CAUSING TOTAL LOSS OF HYDRAULIC FLUID. THE AIRCRAFT LANDED GEAR UP WITH NO INJURIES AND MINOR DAMAGJun 5, 2005 · N7972V · Cessna 177RGSDR MASA2005434Spu · malfunctionedASH 6288 PHX. NR 2 SPU AUX POWER LIGHT ON TAKEOFF ROLL. MX REPLACED ANOTHER SPU. TEST FLIGHT CHECKED OUT GOOD.Jun 3, 2005 · N989HA · Dhav DHC8202SDR MALA050463Switch · leakingTHE CREW REPORTED THAT THE GREEN HYD FLUID GOING TO EMPTY. LOST GREEN HYDS. CREW FOLLOWED QRH AND LANDED IN DTW. MAINTENANCE FOUND HYD BAY FULL OF FLUID. FOUND GREEN SYSTEM PRESSURE SWITCH LEAKING INTERNALLY. REPLACED PRESSURE SWITCH P/N HE15258-1, S/N ONJun 2, 2005 · N512XJ · Bac AVRO146RJ85A
Back to JASC 2910