JASC 2900
Service difficulty reports · 333
Reports filed under 2900 · Hydraulic Power System, newest first.
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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 = '2900' 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 = '2900' 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 ECW2006F00000Powerpack · defectiveNEW HYD LANDING GEAR POWER PACK WILL NOT EXTEND LANDING GEAR. ANOTHER NEW POWER PACK WAS ORDERED AND INSTALLED. LANDING GEAR WOULD NOT FULLY EXTEND. ONE OF THE NEW POWER PACKS WAS SENT BACK TO MFG AND BENCH CHECKED. THEY FOUND NO DEFECT WITH THE POWER PACKSDR 2006FA0000016Flange · crackedCRACK DETECTED ON LOWER LEE PLUG FLANGE. (K)SDR ENHA2005PA311Hydraulic System · lowPILOT REPORTS AT FIRST DESTINATION, GEAR HANDLE TO LOWER LANDING GEAR, GEAR DID NOT TRANSIT TO DOWN POSITION, PILOT RETURNED AIRCRAFT TO AIRPORT, MANUALLY LOWERED GEAR TO 3 GREEN, DECLARED EMERGENCY, LANDED WITH OUT FURTHER INCIDENT. DETERMINED HYDRAULIC RESERSDR HEEA107316Plate · overtorquedDURING THE GROUND TEST OF THE HYDRAULIC SYSTEM, THE HYD TEST BUTTON ON THE LOWER CONSOLE WAS DEPRESSED AND THE CHECK INITIATED. THE COLLECTIVE LOCKING DEVICE DISENGAGED AND THE AIRCRAFT BECAME AIRBORNE. AIRCRAFT CONTROL WAS REESTABLISHED AND AIRCRAFT WAS LASDR 0500729854Hydraulic System · malfunctionedFLT CREW HAD REPORTED THE FAILURE OF THE RIGHT HYDRAULIC SYSTEM DURING CLIMBOUT FROM CMH. COMPLIED WITH COM PROCEDURES AND THE SYSTEM RETURNED TO NORMAL. FLIGHT CONTINUED TO DESTINATION, REPORTED ALL SYSTEMS NORMAL BUT REQUESTED CFR AS A PRECAUTION, AND DECLSDR 47504123104Servo · failedSCENE FLIGHT FROM BASE 7 LAS VEGAS, NV TO JEAN, NV TO UNIVERSITY MEDICAL CENTER (UMC), LAS VEGAS, NV. APPROXIMATELY 1 MILE SOUTH OF UMC, NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENSDR DLM90040364Circuit Breaker · trippedRIGHT HYD SYSTEM FAILURE. DECLARED EMERGENCY LANDING, NO HYD. FOUND RIGHT INSTR TRANSFER C/B POPPED. RESET L9 C/B, ALL INDICATIONS. OPERATED PUMPS SYSTEM, CHECKS OK. NO LEAKS FOUND.SDR AALA20030846O-Ring · cutAIRCRAFT LOST GREEN SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. FOUND GREEN SYSTEM PRESSURE LINE TO MANIFOLD O-RING CUT AND LEAKING. REPLACED O-RING AND BACK UP RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 2003F00408Cover · brokenDURING TAXIING PROCESS OF FLIGHT, THE 'THS' CONFIGURATION WENT ALL DOWN AND THE AIRCRAFT COULDN'T DEPART FROM LAX STATION. THE AIRCRAFT REMAINED ON GROUND FOR MAINTENANCE. TECHNICIANS CHECKED THE 'THS' MECHANISM PER AMM 27-44-00 AND FOUND ONE OF THE PLASTIC SDR HEEA087187Filter Element · cloggedRETURN BYPASS BUTTON POPS. REPAIRED.SDR C1HA200397012Hydraulic System · leakingAFTER 1 HR IN FLIGHT SYSTEM A-HYDRAULIC QUANTITY STARTED TO DECREASE, QUANTITY FELL TO 2.3 GALLONS.SDR HNAA0300021Hydraulic System · malfunctionedAFTER LANDING WHEN NR 1 PROP WAS FEATHERED, CREW REPORTED LOSING NOSE WHEEL STEERING AND THE NORMAL BEAKES. CREW USED PARK BRAKE TO STOP AIRCRAFT. CREW OBSERVED MAIN AND STANDBY HYDRAULIC PRESSURE AT LESS THAN 1800 PSI FOLLOWED BY NR 1 ENGINE HYDRAULIC PUMP CASDR 2003F00157Switch · intermittentDURING CRUISE FLIGHT THE PILOT FELT THE CONTROLS GET "HARD" LIKE A HYDRAULIC SYSTEM FAILURE, BUT AIRCRAFT STILL FLYABLE. PILOT OPTED TO DO PRECAUTIONARY LANDING IN AN OFF-AIRPORT AREA WITH NO INCIDENT REGARDING PERSONNEL OR AIRCRAFT. AFTER INSPECTING SYSTEM SDR ARWA20030310HoseLOG PAGE 506081 & 506082. DISCREPANCY: ON LANDING AT FJDG, AIRCRAFT SUFFERED LOSS OF HYDRAULICS. EMERGENCY AIR BRAKE PRESSURE BOTTLE USED AFTER LANDING. CORRECTIVE ACTION: FOUND BROKEN HOSE IN RIGHT SIDE BOOGIE TRIM CYLINDER. REMOVED AND REPLACED HOSE IAWSDR FE5F200300002Tube · looseWhen A/C taxied to the gate position, tower informed smoke is observed from R/H ENG site and then cabin crew reported HYD ordor is smelled in the cabin. Captain shutdown the APU and related symptom disappeared and then L/H HYD QTY indicated 7 QT remained. MechSDR DHL2003727001Valve1) DURING PUSH BACK THE HYDRAULIC BRAKE PRESSURE STARTED TO DECREASE TO 2100 PSI.2) FOUND LEAKING SHRAEDER VALVE FOR BRAKE ACCUMULATOR. REPLACED VALVE AND RESERVICED ACCUMULATOR. OPS CHECKED GOOD IAW 29-12-42 AND 12-15-01.SDR 2003UALA00062PipeFLIGHT DIVERTED DUE TO GREEN HYDRAULIC SYSTEM LOW. SUPPLEMENTAL DATA UPDATE FOUND LINE FROM HYD PRESSURE MODULE #1 ENG LEAKING AT FITTING. THE LINE WAS REPLACED. THE ENGINE PUMP CASE DRAIN AND HYDRAULIC CONTROL UNIT FILTERS WERE ALSO REPLACED PRECASDR DHL2002806015Hose1) DURING CRUISE, HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. HYDRAULIC QUANTITY WENT TO THE "AUX" LEVEL. AILERON AND RUDDER CONTROL MANUEL LIGHT ILLUMINATED. (NOTE: DHL EVENT REPORT DATED 12-18-2002 STATES EMERGENCY WAS DECLARED.)2) FOUND LT BOGIE TRIM HYDRAULISDR F3LA200200385Hydraulic Line · damagedDURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DROPPED TO ZERO. STANSDR HNAA0200071Hydraulic Line · leakingON APPROACH TO EWN CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM CONTENTS. RESULTING IN #1 RUDDER ISOLATION. PRESSURE DID NOT GO BELOW 3000 PSI AND QUANTITY DID NOT GO BELOW .6 QUARTS. INSTALLED TEMPORARY FLEX LINE AT LEFT INBOARD ROLL SPLIOLER ACTUATOR UNLOADING SDR 2002FA0000964Fitting · scoredCOMBINED HYDRAULIC SYSTEM INDICATED LOW QUANITY PRESSURE 330PSI TEE FITTING SCORED ON HYD LINE.SDR DL76S020887Line · leakingRT HYD QUANITY SYSTEM TO ZERO RETURN TO LAS VEGAS CA FND LINE TO RT ACMP LEAKING, RPLD SAME.SDR FX72002F00001Hydraulic Line · looseDURING CRUISE SYSTEM (A) HYDRAULICS FAILED, PRESSURE WENT TO (O) A/C DIVERTED TO SAP AND LANDED SAFELY FOUND SYSTEM (A) PRESSURE LINE (B) NUT LOOSE TIGHTENED SAME SERVICED HYDRAULIC AND OPS CHECK GOOD PER MM. AIRCRAFT RETURNED TO SERVICE.SDR AALA20021062Line · brokenENROUTE, CUN-JFK ON DEPARTURE, LEFT HYDRAULIC SYSTEM QUANTITY LOSS. RETURNED AIRCRAFT TO CUN AND LANDED WITHOUT INCIDENT. REPLACED RIGHT GEAR MAIN DOOR SEQUENCE VALVE PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL73K020573Tee Fitting · crackedIRREG/ LOSS OF A SYSTEM HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF PRESSURE AFTER LOWERING THE LANDING GEAR CA/ FOUND TEE FITTING IN THE NOSE WHEEL WELL CRACKED ____REPLACED SAME SERVICED SYSTEM NO LEAKS FOUNDSDR DHL2002806010Hydraulic Line1) PRIOR TO TAKEOFF, LOSS OF HYDRAULIC FLUID LEAD TO DECISION TO RETURN TO THE RAMP. DURING TAXI BACK QUANTITY FELL TO EMERGENCY LEVEL AND HYDAULIC SYSTEM AND BRAKE PRESSURES BEGAN DECREASING. STPPED TAXI AND SET BRAKES FOR TOW IN2) FOUND HOLE IN T/R PUMP SSDR 2002F00356Line · leakingDFW - FLT 1302 - ONE HUNDRED THIRTY MILES FROM ORGINATING STATION, AIRCRAFT LOST HYDRAULIC PRESSURE. CREW RETURNED TO STATION AT MAX GEAR EXTENSION SPEED. GEAR WAS PUMPED DOWN USING EMERGENCY CHECKLIST. HYDRAULIC LEAK CAUSED LOSS OF HYDRAULIC FLUID LEADING SDR HNAA0100077Hydraulic Line · leaking#2 HYDRAILIC SYSTEM FLUID LOSS DOWN TO ISOLATION VALVE ACTUATION. PRESSURE REMAINED NORMAL WITH APPROX. 1/2 QT. INDICATED RESERVOIR QUANTITY. AIRCRAFT DIVERTED TO SAV. FOUND FLEX LINE TO NLG DRAG STRUT ACTUATOR LEAKING. REPLACED FLEX LINE.SDR HNAA0200003Shuttle Valve · inoperative#1 AND #2 HYDRAULIC SYSTEMS FLUID LOSS. #2 RUDDER ISO VALVE CAUTION LIGHT ILLUMINATED. HYD PRESSURES NORMAL. ON LANDING NORMAL BRAKES FAILED. FOUND LEAK AT #3 BRAKE. #3 SHUTTLE VALVE FAILURE ALLOWED FLUID LOSS FROM BOTH HYD SYSTEMS. REPLACED #3 SHUTTLE VALVE.SDR HNAA0100076Brake · leaking#1 AND #2 HYDRAULIC SYSTEMS FLUID LOSS. #2 RUDDER ISO VALVE CAUTION LIGHT ILLUMINATED. HYD PRESSURES NORMAL. ON LANDING NORMAL BRAKES FAILED. REPLACED #3 BRAKE ASSY.SDR IXXA0100073OLine · looseENROUTE FROM AKJ TO AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE AIRCRAFT LOCATING A LOOSE LINE ON THE RIGHT MASDR DL72S011793Actuator · leakingLOST A SYSTEM HYDRAULICS ON CLIMBOUT FROM ABQ. LOST PRESSUREAND QUANTITY BOTH TO ZERO. _REPLD NBR 3 L/E FLAP ACTUATORSDR DL767011418Coupling · brokenLNDG IN JAX "CTR HYD QTY" EICAS MSG ILLUMINATED. TURNING ONTO TAXIWAY, QTY WENT FROM 4.0 TO 0.0 AND LOST NOSEWHEEL STEERING. TOWED INTO GATE. LEFT AND RIGHT HYD SYSTEMS NORMAL. CA FD COUPLING BETWESDR COMA0160653Hose · leakingFLIGHT #5878. HYRAULIC #3 LOW PRESSURE CAUTION MESSAGE RECEIVED DURING DESCENT INTO ORD. HYDRAULIC SYNOPTIC PAGE INDICATED ZERO PERCENT QUANTITY IN #3 SYSTEM, ACCOMPLISHED QRH PROCEDURE; EXTENDING LANDING GEAR MANUALLY. AIRCRAFT LANDED SAFELY AND WAS TOWED SDR COMA0160612PumpFLIGHT #5995. DURING TAXI OUT FROM CVG THE CIRCUIT BREAKER FOR HYDRAULIC PUMP 3A TRIPPED, AIRCRAFT RETURNED TO THE GATE.TRANSFERRED THE ALTERNATING CURRENT MOTOR PUMP 3A TO THE DEFERRED DISCREPANCY LIST PER MEL.SDR SIMA200121401Hose · brokenICT - FLT 3750 - CREW REPORTED THE HYDRAULIC LIGHT CAME ON IN FLIGHT. CREW HAD TO BLOW THE LANDING GEAR DOWN FOR LANDING. MAINTENANCE FOUND A BROKEN LINE AT THE NOSE LANDING GEAR RETRACT ACTUATOR LINE WAS REMOVED AND REPLACED IAW SAAB MM. LEAK CHECK WAS GOOSDR DLM88011281Hose · rupturedLT HYD PRESS LOW LIGHT ILLUMINATED ON OAP HYD PRESS WAS ZERO///FOUND PRESS LINE ON LT ENG LEAKING. REPLD LINESDR DL76G011252Line · crackedRT HYD SYSTEM FLUID LOSS.REPLACED NO.7 SPOILER ACTUATOR LINE WITH TEMP LINE.FWD TO MCO. SDR CA010814003Indicator · leaking(CAN) ENROUTE FROM TEL AVIV TO TORONTO AFTER THE LT SYSTEM WAS TOPPED OFF (IN TLV) LOSS OF HYDRAULIC FLUID OF THE L/H SYSTEM, THE A/C RE-ROUTED AND ASK FOR AN EMERGENCY LANDING. A/C LANDED SAFELY WITHOUT FURTHER INCIDENT. FOUND TO BE A LEAK AT THE DIFFERENTIALSDR AALA20011511Line · leakingDFW - FLT 1744 - EN ROUTE DFW-DTW - AIR INTERRUPTED WITH HYDRAULIC SYSTEM 'A' LOSS OF QUANTITY AND PRESSURE. RETURNED TO DFW LANDED WITHOUT INCIDENT. REPLACED LEFT ELEVATOR PACK HYDRAULIC LINE. SERVICED SYSTEM. LEAK AND OPERATIONAL CHECK OK. SYSTEM GROUNDSDR ZW0A0105401O-RingON FINAL APPROACH, LOST RIGHT HAND HYD SYSTEM DUE TO FLUID LOSS. FOUND RIGHT HAND THRUST REVERSER CONTROL VALVE PRESSURE LINE FITTING HAD A FLAT TORN O-RING. REPLACED O-RING P/N NAS1612-6 DUE TO WEAR. LAST CHECK C 03/12/01 MCI ---CLOSED---SDR AALA20011362Valve · leakingDFW - FLT 1216 - EN ROUTE DFW-PHL, IN FLIGHT B QUANTITY HYDRAULIC SYSTEM AND PRESSURE DECREASED TO ZERO. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE ELEVATOR TRANSFER VALVE AND RIGHT SIDE ELEVATOR POWER CONTROL. (M)SDR BJNA0101603Hydraulic LineTOTAL HYDRAULIC FAILURE, FIRST NR 1 'A' SYSTEM PRESSURE LIGHT CAME ON, 'A' SYSTEM QUANTITY WENT TO ZERO. APPROXIMATELY 2 MINUTES LATER 'B' SYSTEM LOW QUANTITY LIGHT CAME ON. DIVERTED INTO SALT LAKE CITY, UT. INSPECTION FOUND BROKEN 'A' SYSTEM PRESSURE LINE SDR AALA20011246Pump · leakingMIA-DTW - FLT 926 - SHORTLY AFTER TAKEOFF, DETECTED A HYDRAULIC LOW LEVEL LIGHT ILLUMINATE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 HYDRAULIC PUMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR S01629020Hydraulic SystemB-18573 DURING T/O,GEAR RETRACT ECAM WARNING MSG SSDR AALA20011244Fitting · looseDFW - FLT 1594 - EN ROUTE ELP-DFW - NEAR DFW GATE DETECTED SMOKE/HAZE IN CABIN. TURNED OFF PACKS. USED RAM AIR. SMOKE DISSIPATED. ARRIVED AT DFW GATE WITHOUT FURTHER INCIDENT. TIGHTENED T-FITTING AT LEFT SIDE HYDRAULIC PUMP FILTER HOUSING NEAR APU AREA. SDR AALA20011197Hose · rupturedPHL - FLT 1463 - EN ROUTE DFW-PHX - UPON LANDING, LOST LEFT SIDE HYDRAULIC SYSTEM. LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MLG PRESSURE HOSE. SERVICED HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR P2EA01089Hydraulic Line · inoperativeFLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRAULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PARSDR USAAF01029Tube · crackedPIT-CLT - FLT 347 - AFTER TAKEOFF, A VERY STRONG ODOR OF SKYDROL WAS NOTED IN THE CABIN. FLIGHT RETURNED TO THE FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED FLAIR ON THE RIGHT HYDRAULIC LINE TO THE PRESSURE FILTER. REPLACED SDR 01FDEA00342Drain Line · leakingDURING CRUISE GOT HYD SYS 2 FAIL LEVEL 2 ALERT. REPLACED ENGINE HYD CASE DRAIN FILTERS, LT AND RT EDPS AND SERVICED HYDRAULICS. NO LEAKS NOTED.
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