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 A6WA200340039Line · chafedHYDRAULIC 2 LOW PRESSURE MESSAGE ON EICAS, NO QUANTITY NOTED. REMOVED AND REPLACED NR 2 EDP (HYD) AND CHAFED LINE IN PYLON (HYD). OPS AND LEAK CHECK GOOD. (M)SDR DLM88030326Hose · leakingON CLIMBOUT LT HYD QTY AND PRESS DROPPED TO ZERO QTY BEGAN TO RISE ON ARRIVAL CVG, 4 QTS APPROACH 9 QTS ON SHUTDOWN PUMP OFF. REPLACING LINE P/N 299600044 LT ENG PRESS FLEX LINE.SDR CA030403001Hose · damaged(CAN) AIRCRAFT LOST GREEN HYDRAULIC FLUID DURING FLIGHT . DURING TROUBLE SHOOTING , THE RT MLG TRUCK POSITION ACTUATOR FLEX HOSE WAS FOUND PERFORATED UNDER THE BRADED SURFACE . THE HOSE ASSY WAS REPLACED AND THE SYSTEM WAS TESTED SERVICEABLE.SDR 0300719927Line · rupturedINBOUND TO RIC THE LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND PRESSURE WENT TO ZERO. CREW CONTINUED TO DESTINATION AND PERFORMED MANUAL GEAR EXTENSION ON APPROACH. ALL COM PROCEDURES COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSTALLED GEARSDR 2003F00329Packing · leakingON TAXI OUT, PILOTS AND CO-PILOTS BRAKES FAILED. FOUND HYDRAULIC FLUID LEAK AT THE HYDRAULIC POWER PACK FILTER BOWL. (M)SDR 0300643221O-Ring · leakingRECEIVED YELLOW SYSTEM HYDRAULIC RESERVOIR LOW LEVEL WARNING. ECAM INDICATED ZERO QUANTITY IN YELLOW SYSTEM RESERVOIR. DEACTIVATED YELLOW HYDRAULIC SYSTEM PER COM AND LANDED UNEVENTFULLY. REPLACED O-RING AT THE PTU MANIFOLD AND LEAK CHECKED OK. SERVICED YELLOWSDR C7WA200200042Line · leakingLOST SYSTEM A HYDRAULIC. ENGINE NR 1 PUMP LOW PRESSURE LIGHT FOLLOWED BY FLUID LOSS IN FLIGHT. REMOVED AND REPLACED TWO EACH HYDRAULIC LINES, P/N 65-17844-250 AND 65-17844-17, LEAK CHECK GOOD. (M)SDR FRISBY03003Housing · crackedAFTER TAKEOFF FLIGHT NR IG81 I-SMEV (MSN 49669) HAD FLIGHT INTERRUPTION, DIVERTED AFTER HYD SYST MALFUNCTION. LANDING GEAR WAS RETRACTED, NLG REMAINED EXTENDED WITH (RED) LIGHT (ON), LT AND RT HYD SYST PRESS WAS (0) PSI, AND (L/R HYD PRESS) ADV ON EOAP. ABNOSDR CA030401007Line · chafed(CAN) NR 1 EDP HYDRAULIC CASE DRAIN LINE WAS CHAFING AGAINST NR 1 EDP HYDRAULIC PX LINE, DUE TO INSUFFICIENT CLEARANCE/SYSTEM VIBRATION. CHAFING OCCURRED OVER A LENGTH OF APPROXIMATELY 4 INCHES, AND WAS BEYOND ALLOWABLE LIMITS.SDR AWXA200300319Hose · burstON CLIMB OUT FROM DEN EN ROUTE FOR PHX, THE RT MAIN LANDING GEAR INDICATED BOTH RED AND GREEN, ACCOMPANIED BY HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS. DECLARED EMERGENCY AND TURNED BACK TO DEN, LANDED WITHOUT FURTHER EVENT. CONTRACT MAINTENANCE INSPECTED TSDR 2003F00245O-Ring · wornDURING APPROACH TO AUSTIN AT 29,000 FEET, BOTH B-HYDRAULIC LOW PRESSURE LIGHTS CAME ON. B-SYSTEM PRESSURE INDICATED ZERO AND SYSTEM QUANTITY NORMAL. EMERGENCY PROCEDURES WERE FOLLOWED. AIRCRAFT LANDED AT AUSTIN WITHOUT INCIDENT. REPLACED O-RING AND TIGHTENSDR 2003FA0000423Hose · crackedNOSE LANDING GEAR FAILED TO COMPLETELY EXTEND FOR LANDING. INSPECTION REVEALED HYDRAULIC LEAK NEAR ENGINE COMPARTMENT. FURTHER INVESTIGATION REVEALED THE HOSE WAS CRACKED NEAR THE FITTING WHERE IT ATTACHES TO THE PUMP.SDR SWAA030682Hydraulic Line · leakingAIR TURNBACK, DURING TAKEOFF, A-SYSTEM HYDRAULICS FAILED, LOW QUANTITY AND PRESSURE INDICATED. FOUND HYD LINE ON LT MLG ACTUATOR FAILED. REMOVED AND REPLACED HYD LINE ON LT MLG ACTUATOR PER MM. SERVICED AND BLEED HYD SYSTEM, NO FURTHER LEAKS NOTED PER MM.SDR DL757030277B-Nut · looseRIGHT ENG HYD PUMP EICAS MSG AND RT ENG HYD PRESS LIGHT ILLUM ON TAKEOFF. RIGHT ENG HYD PUMP SWITCH TURNED OFF. FOUND PYLON SUPPLY LINE B-NUT LOOSE, SECURED SAME. MOTORED ENG. GOOD PRESSURE, NO LEAKS.SDR QXEA0300403Line · leakingSEA ON FLIGHT 2293- AT GEAR EXTENSION DOOR WOULD NOT CLOSE. NR 2 HYDRUALIC QUANTITY SHOWED VERY LOW, NEAR ZERO. CREW EXECUTED A MISSED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR RIGHT HANSDR AWXA200300298Selector Valve · leakingEN ROUTE FROM PHX TO PDX APPROXIMATELY 2 HOURS INTO FLIGHT RECEIVED A GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE, FOLLOWED BY A NR 1 ENGINE GREEN SYSTEM HYDRAULIC PUMP LOW PRESSURE. FOLLOWED ECAM PROCEDURES AND SHUTDOWN THE POWER TRANSFER UNIT ANDSDR DLM88030271Line · leakingON DESCENT RT HYD QTY DROPPED TO 2 QTY AND PRESS TO ZERO C/W EMERGENCY PROCEDURES TURNED XFER PUMP OFF. REPLACED RT HYD LINE TO FILTER MODULE.SDR COMA0370009Line · leakingFLIGHT 5741 - NR 2 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPAIRED CHAFED HYDRAULIC TUBING IN AFT EQUIP BAY.SDR CA030321002Tube · damaged(CAN) DURING FLIGHT HYDRAULIC RESERVOIR LOW LEVEL APPEARED ON GREEN SYSTEM. AFTER INVESTIGATION A PIN HOLE WAS FOUND ON THE LT WING SPOILER PRESSURE TUBE. TUBE ASSY WAS REPLACED AS M/M AND SYSTEM SERVICED AIRCRAFT WAS RETURNED TO SERVICE. CAUSE OF FAILURE ISSDR PCAA0303058Hydraulic Line · leakingLGA-ROC FLIGHT#3785. CREW REPORTED LOSS OF #1 HYDRAULIC CONTENTS. RAN LESS THEN ONE MINUTE WITH CONTENTS LOST. CREW DECLARED AN EMERGENCY. FLIGHT LANDED IN BGM WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE FOR FLIGHT SPOILER UNLOADING VALVE FOR SPOILERSDR 03FDEA00341Line · faultyAFTER APPROX 3 HRS OF FLT WHILE CRUISING AT FL 330 NO 1 HYD SYSTEM QTY SLOWLY DECREASED FROM 6.0 GALS TO 2.8 GALS AND STILL SLOWLY DECREASING. TURNED OFF #1 HYD PUMPS C/W RED TABS. TURNED PUMPS ON FOR LANDING, CONFIGURATION TO FLAP 35 EXTENSION NOTED 2.3 SDR ARWA20030311Connector · looseSYSTEM "B" RESERVOIR QUANTITY LOW AND DECREASING. SWITCHING PUMP AND ATM OFF STOPPED FLUID LOSS. TIGHTENED CONNECTOR AT "B" SYSTEM ATM PRESSURE SWITCH IAW M/M 29-11-00. OPERATIONAL CHECK ON GROUND NORMAL.SDR 2004FA0000176Shim · missingHYDRAULIC FILTER BYPASS BUTTON POPPED (NO SHIMS INSTALLED).SDR CA030318017Hose · cut(CAN) DURING A WALK AROUND, THE CREW NOTICED HYDRAULIC FLUID IN THE RT MAIN GEAR AREA.MAINTENANCE FOUND THAT THE RETRACT LINE HAD BEEN CUT CLOSE TO THE IDENTIFICATION CLAMP. THE CUT OCCURED NEAR THE CLAMP WHICH MAY INDICATE A CYCLIC FAILURE WITH THE CLAMP BEINSDR DLM88030243Line · leakingRT HYD PRESSURE AND QTY WENT TO ZERO FOLLOWING LANDING GEAR EXTENSION. REPLACED LEAKING FLEX LINE FWD OUTBOARD ON RT ENGINE HYD FILTER MODULE.SDR MEX2003074Line · leakingDURING OVERNIGHT SERVICE, A BLADE ON T4 (TURBINE STAGE) WAS DETECTED WITH DAMAGE. ENGINE WAS REPLACED IAW MM AND TESTS IAW MM, ALL CORRECT. DURING REVERSE TEST, A HYDRAULIC FLUID LEAK WAS DETECTED AND HYDRAULIC LINES WERE REPLACED.SDR C2XA03CL069Pump · failedCLE FLIGHT#2257 THE CREW REPORTED #2 HYDRAULIC SYSTEM FAILED ON APPROACH INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #2 ENGINE DRIVEN HYDRAULIC PUMP.OPERATIONAL CHECKS WERE GOOD.SDR CA030314003Line · wrong part(CAN) DURING AN UNSCHEDULED INSPECTION IN FORWARD TRANSMISSION DECK AREA, IT WAS DISCOVERED THAT A HYDRAULIC PRESSURE LINE FROM PUMP TO FILTER HOUSING APPEARED TO BE STRESSED AT HYDRAULIC FILTER FITTING. IT WAS REVEALED UPON INVESTIGATION OF HOSE ASSY, P/N WASDR A6WA200330007O-Ring · tornHYDRAULIC MAIN QUANTITY LOW CAS ILLUMINATED AFTER GEAR RETRACTION FOLLOWED BY PRIORITY VALVE CLOSED AND STBY PUMP CONTINUES EXTENDED GEAR WITH AUX. FOUND TORN O-RING INBOARD HYDRAULIC LINE TO PILOT VALVE. REMOVED AND REPLACED O-RING, INSPECTED HYD SYSTEM FILSDR SWAA030550Hydraulic Line · crackedDECLARED EMERGENCY, DURING FLIGHT A-SYSTEM HYDRAULIC QUANTITY IND WENT TO ZERO. FOUND LINE ON HYD MUFFLER CRACKED. REMOVED AND REPLACED HYD LINE, NR 1 ENG HYD PUMP, CASE DRAIN FILTER & A-SYSTEM MAIN FILTER PER MM.SDR AALA20030306O-Ring · damagedDTW - FLT 1461 - EN ROUTE DCA-ORD, EXPERIENCED LOSS OF NR 1 HYDRAULIC SYSTEM FLUID IN FLIGHT. COMPLIED WITH ALL RELEVANT EMERGENCY PROCEDURES. GEAR WAS EXTENDED USING ALTERNATE LANDING GEAR CONTROL. LANDED DTW WITHOUT INCIDENT. REPLACED O-RING ON NR 1 HYDRSDR ARWA20030301Hose · leakingIN FLIGHT LOSS OF HYDRAULIC QUANTITY OF PRESSURE; PERFORMED APPROACH CHECKLIST. FOUND HYDRAULIC PRESSURE HOSE LEAKING AT NR 2 ENGINE. REMOVED AND REPLACED HYDRAULIC HOSE ON HYDRAULIC PUMP IN ACCORDANCE WITH MM 20-12-0. SERVICE HYDRAULIC RESERVOIR IAW MM 12SDR COMA0360137Pump · weakFLIGHT 5546 GEAR DISAGREE WARNING SELECTED DOWN.REPLACED HYDRAULIC PUMP 3A.SDR CA030419001Line · chafed(CAN) AT FLIGHT LEVEL 33000, YELLOW CAS MESSAGE, HYD NR 2 LOW PSI ILLUMINATED.REF /A/ - IPC 29-11-00, ITEM35, P/N 601-75238-43, HYD PUMP PRESS SYS 2 TUBE ASSYREF /B/ - IPC 29-11-00, ITEM 215, P/N 601R75286-51, CASE DRAIN SYS 2 TUBE ASSYIT WAS FOUND BY THE MAINSDR CA030320004Bracket · cracked(CAN) IN COMPLIANCE WITH SB 45 HYDRAULIC SERVO BRACKET D202-2 WAS REPLACED WITH D202-2 REV.F. THE BRACKET WAS FOUND TO BE CRACKED IN THE BEND RADIUS WHICH PROMPTED THE SB.SDR A6WA200340033Line · leakingHYD NR 2 LOW PSI CAS MESSAGE. NR 2 HYD FLUID INDICATES ZERO. REMOVED AND REPLACED NR 2 HYD RETURN LINE. REMOVED AND REPLACED NR 2 HYD PSI LINE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP.SDR CA030307001Line · cracked(CAN) HYDRAULIC LEAK FROM RT ARMPIT AREA. FOUND RT BRAKE PRESSURE HYDRAULIC LINE HAS A 1/4 INCH CRACK AT BEND NEAR FUSELAGE CONNECTION POINT. IPC REF 29-00-00 FIG 60.SDR DL78K030220Fitting · damagedNR 2 ENG HYD QTY DECREASING ON CLIMBOUT. REPLACED NR 2 ENG HYD PUMP PRESSURE HOSE AND QUICK DISCONNECT FITTING AND CASE DRAIN HOSE AT ENG PUMP.SDR COMA0360133Hydraulic Line · leakingFLIGHT 5176 HYDRAULIC SYSTEM #1, LOW WARNING MESSAGE.REPLACED HYDRUALIC LINE TUBE ASSY.SDR 307031Line · chafedDURING A ROUTINE POST FLIGHT INSPECTION, EVIDENCE OF HYD FLUID WAS ON THE AFT EQUIPMENT BAY DRAIN MAST. FURTHER INVESTIGATION REVEALED A HAIRLINE CRACK IN THE NR 2 ENGINE HYD PRESSURE LINE, AS IT EXTENDS INTO THE AFT BAY AREA FROM THE RT PYLON. IT WAS DETERMSDR 00085Line · inoperativePILOT REPORTED AFTER DEPARTURE FROM SHV HYDRULIC PRESSURE DROPPED TO 0 UPON GEAR RETRACTION AND FLAP RETRACTION, AIRCRAFT DIVERTED TO ADS STANDBY PUMP WAS USED TO EXTEND GEAR AND FLAPS FOR NORMAL LANDING. WILL UPDATE THIS REPORT AFTER MAINTENANCE. HYDRULIC (PRSDR HNAA0300011Hydraulic Line · burstLost number 2 hydraulic quantity in flight. Replaced nose gear up line.SDR DLM90030216Line · crackedRT SYS HYD PRESS DROPPED TO 0 PASSING APPROX 18K QTY ON RT SIDE WENT UP TO 27 QTS. RAN CHECKLIST. WHEN RT ENG PUMP WAS OFF WITH AUX PUMPS ON, PRESS ON RT SIDE WENT FROM 0 TO 700 PSI. THE LT PRESS WENT FROM 3000 TO 2800 PSI. AUX PUMPS AND RT ENG PUMPS NOW ISDR VJ32003F00023Line · wornHYDRAULIC LINE WAS FOUND TO HAVE A HOLE WORN IN IT, DURING REGULAR INSPECTION EVENT. THE CAUSE OF THE WEAR AND HOLE WAS FOUND TO BE A BOLT ON THE LANDING GEAR WEARING ON IT DURING EACH EXTENSION/ RETRACTION CYCLE. THIS LINE SUPPLIED HYDRAULIC PRESSURE TO THESDR PCAA0303050Hydraulic Line · leakingSYR-FLIGHT#3963. CREW REPORTED THAT THE #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION. 1.4 QUARTS REMAINING IN #2 SYSTEM. MAINTENANCE REPLACED A HYDRAULIC LINE IN THE LEFT WHEEL WELL IN ACCORDANCE WITH THE DEHAVILLAND DASH 8 MAINTSDR PCAA0303048Warning Light · false indicationPIT-FLIGHT 3890 CREW REPORTED NR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT AND PARTIAL LOSS OF HYDRAULIC FLUID. HYDRAULIC FLUID OBSERVED ON NR 2 ENGINE. MAINTENANCE SERVICED NR 1 AND NR 2 HYDRAULIC RESERVOIRS AND INSPECTED AREA. FLUID SDR JRA2003F00000Line · leakingAFTER MOVING THE LANDING GEAR HANDLE (DOWN) AND SELECTING FLAPS (DOWN); THE HYDRAULIC PRESSURE GAUGE READ ZERO PSI. NO FLUID WAS VISIBLE IN THE HYDRAULIC RESERVOIR SIGHT TUBE. WITH BYPASS VALVE SELECTOR (UP) BRAKES OPERATED. HYDRAULIC LINE WAS REPAIRED.SDR FRISBY03001Housing · crackedAFTER TAKE-OFF OF ALITALIA (ALI) MD-80 AIRCRAFT I-DANV(80C369) ON 26 FEBRUARY 2003, AIRCRAFT EXPERIENCED HYDRAULIC FLUID LEAK DURING FLAP RETRACTION. AFTER THE AIRCRAFT LANDED, PTU, P/N 4100310-6, S/N 730C WAS REPLACED. THE SUBJECT PTU WAS RETURNED TO THE MASDR CH1A200394007Hose · leakingNOTICED HYDRAULIC "A" SYSTEM PRESSURE AND FLUID LOSS SHORTLY AFTER FLAP RETRACTION DURING DEPARTURE FROM MBJSDR COMA0360116Pump · weakFLIGHT 9450 GEAR DISAGREE WARNING.REPLACED HUDRAULIC PUMP 3B.
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