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 2003FA0000145Housing · crackedHOUSING CRACKED AROUND THE OUTER DIAMETER OPPOSITE THE SUPPORT MOUNT THROUGH BOLT.SDR DL76L030035Pressure Switch · failedIR - AFTER T/O RT ENGINE PRIMERY HYD PUMP PRESS LIGHT CAME ON OVERHEAD AND EICAS. FLUID QUANTITIES OK. REPLACED S31 PRESSURE SWITCH, OPS CHECK/LEAK CHECK OK.SDR QXEA03000008Hydraulic Line · leakingPDX - FLIGHT 2069 - UPON GEAR SELECTION DOWN, THE NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE NR 2 HYDRAULIC FLUID WENT TO 0. MAINTENANCE INSPECTED THE AIRCRAFT AND THE NUMBER 2 HYDRAULIC SYSTEM AND REPLACED THE NUMBER 2 ENGINE DRIVEN PUMP AND A HYSDR AALA20030008Hydraulic Line · puncturedMIA - FLT 938 - EN ROUTE CCS-MIA, EICAS MESSAGE DISPLAYED LOSS OF HYDRAULIC QUANTITY OF CENTER HYDRAULIC SYSTEM. LEFT AND RIGHT CENTER ELECTRIC HYDRAULIC PUMP SWITCHES TURNED OFF. CAPTAIN DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FSDR PCAA0301004Hydraulic Line · leakingITH-LGA FLIGHT 3672 CREW REPORTED TOTAL LOSS OF THE NR 2 HYDRAULIC SYSTEM. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND A HYDRAULIC LINE LEAKING UNDER RIGHT NACELLE ACCESS PANEL. LINE WAS REPLACED WITSDR 2003UALA00015Actuator · leakingLOSS OF GREEN HYDRAULIC SYSTEM INFLIGHT. GREEN HYD RSVR LOW LEVEL ECAM. REPLACED GREEN SYSTEM RETURN FILTER ELEMENT AND YAW DAMPER SERVO ACTUATOR. RESERVICED HYDRAULIC SYSTEM. THE EVENT REOCCURED ON THE NEXT FLIGHT. AN INTERNAL HYD LEAK CHECK AND A VERSDR AALA20030005Hydraulic Line · rupturedDFW - FLT 1108 - EN ROUTE CUN-DFW, CAPTAIN REPORT LEFT HYDRAULIC QUANTITY LOSS. CAPTAIN DECLARED EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. FOUND RUPTURED LINE IN LEFT WHEEL WELL. REPLACED LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR PCAA0301006Hydraulic Line · crackedPIT- FLIGHT#3847. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED ON GROUND.FLUID LOSS ON #2 SIDE, DOWN TO 3/4 OF A QUART. MAINTENANCE FOUND HYDRAULIC LINE PART NUMBER 82950010-351 CRACKED. INTERIM FLEX LINE INSTALLED AND SECURED. LEAK CHESDR COMA0360001Reservoir · unreliableFLIGHT 6811 GEAR DISAGREE WARNING - L/H MLG INDICATED INTRANSIT.REPLACED THE #3 HYDRAULIC RESERVOIRSDR CA030106009Line · chafed(CAN) AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID AND PRESSURE IN FLIGHT. EMERGENCY EXTENSION CARRIED OUT WITH A SAFE LANDING. CHAFED HYDRAULIC LINES FOUND RUBBED THROUGH BY PLASTIC DRAIN LINE IN LT NACELLE. HYDRAULIC LINES FOUND CHAFED WERE PN 2781006475 SDR USAASB02240Motor · malfunctionedCLT - FLT 948 - ON DESCENT INTO CLT, CREW REPORTED THE FLAPS WOULD NOT COME DOWN WHEN SELECTED. HYDRAULIC PRESSURE WAS AT 3,000 PSI AND HYDRAULIC FLUID QUANTITY WAS ABOVE RE-FILL. CAPTAIN DECLARED AN EMERGENCY AND FOLLOWED PROCEDURES FOR AN ALTERNATE FLAPS 1SDR YENA200235Tube · leakingAPPROX 1 HOUR AFTER DEPARTURE FROM JFK, FLT. 91, CREW REPORTED GREEN HYD SYSTEM QTY LOW. APPROX 1 HOUR LATER CREW REPORTED ECAM GRN RES LOW QTY. CREW C/W ECAM ACTION, DISCUSSED OAK ARRIVAL ACTION. GRAVITY GEAR EXTENSION, ALT BRAKES AVAILABLE AND HAVING A/C SDR AALA20021892Coupling · defectiveDFW - FLT 1024 - EN ROUTE MEM-DFW, LOST SYSTEM 1 HYDRAULIC QUANTITY, SHUT OFF PUMPS. EMERGENCY EXTENDED LANDING GEAR. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED QUICK DISCONNECT COUPLING AND O-RING ON PRESSURE AND SUCTION PORTS ON LEFT ENGINE NR 1 SYSTEMSDR CA030106014Tube · leaking(CAN) DURING MAINTENANCE A HYDRAULIC LEAK WAS NOTICED IN L/H MAIN LANDING GEAR WHEEL WELL. NR 2 SYSTEM DOORS CLOSED TUBE ASSY WAS REPLACED.SDR AUS20021458Line · bird strike(AUS) AIRCRAFT SUFFERED BIRD STRIKE IN AREA OF NOSE LANDING GEAR WHEEL WELL AND NR 2 LEADING EDGE FLAP CAVITY. BIRD DAMAGED RIGID HYDRAULIC PIPE PN 272A415117 LOCATED BETWEEN NLG MANIFOLD AND LOCK ACTUATOR. HYDRAULIC FLUID LEAKING.SDR AALA20021869Hydraulic Line · damagedEN ROUTE PAP-JFK, PILOT RECEIVED ECAM MESSAGE STATING THAT BLUE HYDRAULIC SYSTEM RESERVOIR LOW. LANDED AT MIA WITHOUT INCIDENT. FOUD LEFT ENGINE HYDRAULIC LINE LEAKING. REPLACED LINE AND SERVICE HYDRAULIC SYSTEM. SYSTEM GROUND AND FLIGHT CHECKED NORMAL OPESDR CA021224002Hose · split(CAN) AFTER TAKE-OFF DURING GEAR RETRACTION, GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST . UPON ARRIVAL AT DESTINATION, ALTERNATE GEAR EXTENSION WAS USED , NORMAL LANDING . INSPECTION FOUND LT MLG RETRACTION ACTUATOR HOSE SPLIT (SMALL BURST ). LINE REPLACED, GEASDR UPS05145889Hydraulic Line · brokenINSPECTION TYPE: N/A GREEN SYS RSVR LOW LEVEL WARNING CAME ON IN FLT FOLLOWED ALL ECAM PROCEDURES AND CHECK LIST. **** SUPPLEMENTAL MRR **** REPAIRED HYD LINE NEAR GREEN SYS SERVO CONTROL UNIT IAW M/M 20-23-11-0. LEAK CHECKS OK. SERVICED GREEN SYSTEM RES.SDR CA021227004Line · leaking(CAN) DURING INSPECTION A LARGE AMOUNT OF HYRAULIC FLUID WAS FOUND IN THE LT WHEEL WELL, FURTHER INVESTRICATION REVEALED A SMALL PIN HOLE IN THE LINE. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR DL72S021457Actuator · leakingON APPROACH AFTER FLAPS 15 COMPLETE LOSS OF A SYSTEM QUANTITY AND PRESSURE. EMERGENCY PROCEDURES CHECKLIST FOLLOWED WITH MANUAL LANDING GEAR EXTENSION. A SYSTEM HYDRAULIC PUMPS WERE DEACTIVATED WITHIN 2 MINUTES CA_FOUND NBR 4 KREUGSDR A6WA200260077Fuse · malfunctionedRIGHT MLG FAILED TO RETRACT ON TAKEOFF. RECYCLED 3 TIMES. MAINTENANCE REPLACED RIGHT HYDRAULIC FUSE. (M)SDR AALA20021817Control Valve · leakingORD - FLT 1547 - VERY STRONG FUMES IN COCKPIT AND CABIN JUST AFTER TAKEOFF ORD. AIRCRAFT WAS SMOKEY WITH FUMES. CABIN FIRE/SMOKE CHECKLIST COMPLETED. FUMES PARTICULARLY STRONG IN FIRST CLASS CABIN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPAIRED HYDSDR 2003FA0000013Line · leakingTHE POWERPACK CONTROL LINE WAS LEAKING HYDRAULIC FLUID, CAUSED BY AN IMPROPER SECURITY AND/OR ROUTING OF THE HYDRAULIC POWERPACK CONTROL LINE IN PROXIMITY TO THE MIXTURE CONTROL CABLE. AREA AROUND THE HYDRAULIC POWERPACK CONTROL LINE SHOULD BE INSPECTED UNDERSDR FPI2003F00000Line · chafedLANDING GEAR DOWN LINE CHAFED THRU BY AILERON RUDDER INTERCONNECT CABLE. WHEN SELECTING DOWN, ALL FLUID WAS PUMPED OUT OF SYSTEM. NOSE GEAR CAME DOWN AND LOCKED, MAIN GEAR DID NOT.SDR HEEA082858Hose · leakingHYDRAULIC HOSE LEAKING. SCRAPPED.SDR SWIA200211578Hydraulic Line · brokenON THE TAXI OUT, #1 HYDRAULIC 1B CAUTION ILLUMINATED, FOLLOWED BY #1 HYDRAULIC LOW PRESSURE CAUTION MESSAGE. #1 HYDRAULIC RESERVOIR ON SYNOPTICPAGE SHOWED NO FLUID. REPAIRED BROKEN HYDRAULIC LINE FOR BLUE #1 HYDRAULIC SYSTEM (HYDRAULIC SERVICE LINE/SYSTEM RESDR MEX2002363Check Valve · failedAIRCRAFT RETURN TO PLATFORM DUE TO A LT HYD SYSTEM LEAK. DURING CHECK, DETECTED DAMAGE TO THE CHECK VALVE. A LINE WAS INSTALLED AT THE FLUID QUANTITY LIMITER OF BRAKE NR 1, LEAK CHECKED IAW MM. DURING OVERNIGHT SERVICE, LINE WAS REMOVED AND CHECK VALVE WASSDR ARWA20021205O-Ring · leakingON FINAL APPROACH LOSS OF HYDRAULIC FLUID TO THE STAND PIPE. FOUND EMPENNAGE FILTER BOWL LEAKING AT MAGNETIC PLUG. REMOVED AND REPLACED O-RING LEAK CHECK NORMAL IAW MM.SDR CA021219001Line · leaking(CAN) DURING A LINE CHECK MAINTENANCE FOUND A HYDRAULIC LEAK IN NOSE GEAR WHEEL WELL. TRACED TO NOSE GEAR DOOR RETRACT LINE BEHIND DEBRIS GUARD COVER. TEMPORARY FLEX LINE INSTALLED AND WORK CARD ISSUED TO REPLACE WITH RIGID LINESDR QXEA0202182Hydraulic Line · out of positionPDX - STAINLESS HYDRAULIC LINE FOR RETRACTION ACTUATOR IS CHAFING YOKE. REPAIRED IAW DHC8-400 CMM 32-11-04, PAGE 603, PARAGRAPH 3A, STEP 1.SDR AUS20021422Pressure Switch · failed(AUS) HYDRAULIC POWERPACK LOW PRESSURE SWITCH FAILED.SDR ARWA20021203Hose · damagedLOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULIC HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMOVED AND REPLACED HOSE IAW MM, OPERATIONS CHECK OK IAW MM.SDR CA030107015Line · chafed(CAN) R/H ENGINE FLUCTUATING. OVERSHOOTING & CAUSING THROTTLE SPLIT IN ALTITUDE, LEAK CHECKED THE PRESSURE SENDING LINE FROM THE ENGINE COMPUTER TO THE ENGINE INLET PRESSURE & TEMPERATURE SENSOR (P2T2). FOUND LINE LEAKING IN PYLON. LINE WAS TOUCHING HARD AGAINSDR CA021216002Line · cracked(CAN) NR 2 HYDRAULIC SYSTEM FOUND DEPLETED. RT NACELLE TOTALLY SOAKED WITH FLUID. MAINPRESSURE LINE IN RT NACELLE FROM EDP INTO PRESSURE MANIFOLD FOUND TO HAVE A CRACKED FLARE. LINE REPLACEDSDR SWIA200211568Shutoff Valve · malfunctionedHYDRAULIC SYSTEM NR 1 LOW PRESSURE AMBER MESSAGE AND HYD 1A AMBER MESSAGE ON SYNOPTIC PAGE. RETURNED TO DEN. INSTALLED NR 1 HYDRAULIC SHUT OFF VALVE IAW MM 29-11-36. OPS CHECK GOOD. NO DEFECTS NOTED.SDR 2003FA0000063Relay · shortedDURING PROGRESSIVE INSPECTION AND CYCLE OF THE LANDING GEAR WE HAD A FAILURE OCCURED. FOUND A BAD HYDRAULIC CONTROL RELAY THAT SHORTED. BECAUSE OF THAT SHORT, IT ALLOW TO MUCH CURRENT TO FLOW TO PC BOARD AND SHORT OUT BOARD BETWEEN RELAY K13 PIN 13 AND 16 TOSDR AUS20021404Ptu · faulty(AUS) YELLOW HYDRAULIC SYSTEM POWER TRANSFER UNIT (PTU) FAULTY.SDR VJ32003F00012Relay · shortedDURING PROGRESSIVE INSPECTION FOUND BAD RELAY THAT CAUSED THE LANDING GEAR SYSTEM TO FAIL. BELIEVE THE CAUSE IS BECAUSE THE HYDRAULIC CONTROL RELAY SHORTED INTERNALLY. STILL TROUBLESHOOTING THE SYSTEM TO FIND WHAT CAUSE THE RELAY TO SHORT.SDR VJ32003F00011Relay · shortedDURING PROGRESSIVE INSPECTION FOUND BAD RELAY THAT CAUSED THE LANDING GEAR SYSTEM TO FAIL. BELIEVE THE CAUSE IS BECAUSE THE HYDRAULIC CONTROL RELAY SHORTED INTERNALLY. STILL TROUBLESHOOTING THE SYSTEM TO FIND WHAT CAUSED THE RELAY TO SHORT.SDR VJ32003F00010Relay · shortedDURING PROGRESSIVE INSPECTION AND CYCLE OF THE LANDING GEAR WE HAD A FAILURE OCCUR. FOUND A BAD HYD CONTROL RELAY THAT SHORTED. BECAUSE OF THAT SHORT IT ALLOWED TOO MUCH CURRENT TO FLOW TO PC BOARD AND SHORTED OUT BOARD BETWEEN RELAY K13 PIN 13 AND 16 TO BOASDR VJ32003F00009Relay · shortedDURING PROGRESSIVE INSPECTION AND CYCLE OF THE LANDING GEAR, WE HAD A FAILURE OCCUR. FOUND A BAD HYD. CONTROL RELAY THAT SHORTED. BECAUSE OF THAT SHORT, IT ALLOWED TOO MUCH CURRENT TO FLOW TO PC BOARD AND SHORT OUT BOARD BETWEEN RELAY K-13 PIN 13 AND 16 TO BSDR CNQ2003F00000Hose · rupturedON CLIMB OUT, HYDRAULIC SYSTEM (A) LOST ALL FLUID. UPON INSPECTION THE HOSE THT RUNS FROM SYSTEM (A) PRESSURE FILTER TO POWER TRANSFER UNIT WAS NOTED TO BE REPTURED. THE HOLE WAS SENT TO TEAM (X) AT ICT.SDR RAIA00212345Line · leaking5514 STL HYDRAULIC PRESSURE WENT TO ZERO. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP PRESSURE LINE.SDR ALG2003F00015Hydraulic System · lowIN CRUISE FLIGHT PILOT NOTICED A KICK IN THE FLIGHT CONTROLS AND A SLIGHT FLUCTUATION IN NR 2 HYDRAULIC GAUGE THIS WAS FOLLOWED BY CHATTERING IN THE CYCLIC CONTROL, AIRCRAFT RETURNED TO BASE AND UPON INSPECTION MECHANIC DISCOVERED THE NR 1 HYDRAULIC SYSTEM WASSDR IXXA0200116OO-Ring · leakingEN ROUTE FROM NKW TO BAH. FLIGHT CREW NOTED MAIN HYDRAULIC SYSTEM FLUID QUANITY DECLINING. CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED WITHOUT INCIDENT TO BAH. MAINTENANCE DISCOVERED O-RING LEAKING AT MAIN HYDRAULIC SYSTEM SELECTOR VALVE. REPLACED O-RING ANSDR DLM88021394Line · leakingLT HYD QTY DECREASED FROM 11 T0 5 QTS AT FL 280. FOUND ELEVATOR PRESSURE TUBE WORN THROUGH AT CLAMP. LOCATED IN TAIL COMPARTMENT LT SIDE. REPLACED LINE LEAK CHECKS OKSDR AUS20021366Line · cracked(AUS) HYDRAULIC LINE CRACKED AT FLARE.SDR CA021126002Servo Valve · cracked(CAN) HYDRAULIC UNIT RECEIVED FROM THE USA. UNIT SENT FOR SCHEDULED INSPECTION AND REPAIR OF LEAKAGE. DURING FINAL FUNCTION TEST IT WAS NOTED THAT SYSTEM NR 1 LONGITUDINAL ACTUATOR SERVO VALVE CENTERING PLAY EXCEEDED THE LIMIT. ACTUATOR DISASSEMBLED AND SERVOSDR CA021129006Line · leaking(CAN) DURING OVERNIGHT CHECK HYDRAULIC LEAK NOTICED FROM RT ARMPIT. LOST NR 1 SYSTEM FLUID. MLG DOWN PRESSURE TUBE ASSY IN RT WING REPLACED.SDR SWIA200211511Fitting · leakingWHILE INFLIGHT RECEIVED A LOW RESERVOIR PRESSURE LIGHT. WHEN EXTENDING GEAR THE MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED. TURNED ELECTRIC PUMP TO ON. IMMEDIATELY LOW LEVEL LIGHT ILLUMINATED AND GAUGE WENT TO 0. PRESSURE FLUCTUATED BUT FLAPS CAME DOWN. PRE
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