JASC 2913
Service difficulty reports · 4,062
Reports filed under 2913 · Hydraulic Pump (Electric/Engine), 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 = '2913' 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 = '2913' 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 7GMB201611040001Pump · leakingDURING POST FLIGHT, THE CREW NOTICED FLUID LEAKING FROM LEFT ENGINE COWL. MAINTENANCE WAS CALLED UPON AND IT WAS FOUND THAT LEFT ENGINE DRIVEN HYDRAULIC PUMP WAS LEAKING FROM PUMP END FITTING TO THE BODY. REPLACED THE PUMP WITH REPAIRED UNIT. OPS CHECKED GOSDR ASOA201610277003Pump · failedNR 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED INFLIGHT, FOLLOWED BY LOW FLUID QUANTITY. REMOVED AND REPLACED THE NR 1 PUMP AND PRESSURE LINE. LEAK AND OPS CHECKED SATISFACTORY. RELEASED AND RETURNED TO SERVICE.SDR DALA2016102507590Sleeve · tornTORN SLEEVE ON CONDUIT AT AUXILIARY HYDRAULIC PUMP. SLEEVE IN CONDUIT AUX HYDRAULIC PUMP WAS INSTALLED IAW ER/A 467688-14MAAD REV. D.SDR U9FR20161025002Pump · failedLANDING GEAR FAILED TO EXTEND IN FLIGHT. PILOT PERFORMED SUCCESSFUL EMERGENCY EXTENSION OF LANDING GEAR WITH UNEVENTFUL LANDING. TROUBLESHOT LANDING GEAR SYSTEM AND FOUND HYDRAULIC PUMP NOT PRODUCING SUFFICIENT PRESSURE TO EXTEND LANDING GEAR.SDR 2016F00219Pump · failedACFT EXPERIENCED A LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILURE. THIS FAILURE RESULTED IN LOSS OF SEVERAL HYDRAULIC SYSTEMS INCLUDING THE LANDING GEAR. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT.SDR HALA20161020372Pump · inoperativeLOG PAGE 665330 DEFECT: LT HYDRAULIC PRIMARY PUMP EICAS MSG WITH ASSOCIATED PRESSURE SWITCH LIGHT ILLUMINATED. REMOVED & REPLACED THE NR 1 ENG HYD ADP IAW AMM 29-11-05-401. RAN THE NR 1 ENGINE IAW AMM 71-00-00-712-021-N00, NR 1 ENGINE ADP. NO LEAKS NOTEDSDR SIMA20161018005Pump · failedHYD SYS NR 2 FAIL IN FLIGHT. REMOVED AND REPLACED THE NR 2 ELECTRIC HYD PUMP IAW AMM 29-10-04, OPS AND LEAK CHECKED GOOD.SDR QXEA2016101800652Pump · failedUPON GEAR RETRACTION ON TAKEOFF NR 2 HYD PUMP CAUTION, NR 2 RUD CTRL, NR 2 HYD ISO VALVE CAME ON. THE RT MLG DID NOT RETRACT. THE NR 2 HYD QTY , AND NR 2 HYD PRESS WERE AT ZERO. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDING. INSPECTED NR 2 HYD EDP REF AMM TSDR SWAA2016101308757Pump · faultyLOSS OF B SYSTEM HYDRAULIC PRESSURE AND QUANTITY. R & R NR 2 ENGINE DRIVEN PUMP IAW AMM.SDR M7KA201610111134Pump · leakingDURING ROUTINE INSPECTION, A HYDRAULIC FLUID LEAK WAS NOTED ON THE BELT DRIVEN HYDRAULIC PUMP DRIVE AND A PREVIOUSLY REPAIRED YELLOW TAGGED PUMP ASSEMBLY INSTALLED. THE REPLACEMENT PUMP DRIVE SHAFT LIP SEAL HAD BEEN REPLACED AS PART OF THE REPAIR. A NORMAL GROSDR HALA2016092700361Pump · leakingDURING WALK AROUND FOUND FLUID DRIPPING FROM NR 1 ENGINE DRAIN. TROUBLESHOT & FOUND NR 1 ENGINE HYD PUMP LEAKING FROM DRAIN PAD. SIX DROPS EVERY TEN SECONDS. REMOVED AND REPLACED THE NR 1 HYD PUMP IAW AMM 29-11-05. OPS AND LEAK CHECKED GOOD.SDR IPXA2016091408255Pump · low pressureAFTER TAKE OFF, RECEIVED INDICATIONS OF BOTH GREEN SYSTEM HYDRAULIC PUMPS WERE PRODUCING LOW PRESSURE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. ACCOMPLISHED GEAR RETRACTION AND EXTENSION TEST IAW MM 32-31-00-501 AND MLG AND NLG INDICATING AND WARNING TESDR SWAA2016092007999Pump · failedELECTRICAL B SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. DIVERTED. R & R ELECTRIC B PUMP IAW AMM.SDR HEER20160912219Pump · failedHYDRAULIC NR 3 PUMP FAIL CAUTION AND RESERVOIR LOW DUE TO HYDRAULIC FLUID DUMPING OVERBOARD FROM APU DRAIN THROUGH FAILED APU STARTER SEAL. REPLACED APU HYDRAULIC STARTER FOR FAILED SEAL AND NR 3 HYDRAULIC PUMP DUE TO CAVITATING. ACFT RAN AND ALL SYSTEMS CHESDR CALA2016090600626Shaft · shearedNR 2 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP TURNED OFF IAW CKLST. SYS B QTY WENT TO ZERO. HYD PUMP SHAFT FOUND SHEARED, REPLACED THE HYD PUMP SHAFT, ASSOCIATED FILTERS, SYSTEM FLUSHED, RUNS AND LEAK CHECKED GOODSDR FDEA201609053118Pump · shearedHYDRAULIC QUANTITY LOW RT, EICAS ALERT MESSAGE FOLLOWED BY HYDRAULIC QUANTITY LOW CHECKLIST. R & R RT ENGINE EDP IAW MM 29-11-05-4-2 AND CHECK VALVE IAW MM 29-11-06-4-0. FLUSHED RT HYDRAULIC IAW MM 29-11-00-2. REPLACED CASE DRAIN FILTER, PRESS FILTER AND RESDR QMLA2016090316101Bearing · seizedENROUTE, THE NR 2 HYDRAULIC LIGHT ILLUMINATED AND SHORTLY AFTER THE CABIN FILLED WITH SMOKE. THE AIR CONDITIONER WAS TURNED OFF. THE LANDING WAS MADE IN A PASTURE. AFTER SHUTDOWN THE HYDRAULIC BELT WAS DISCOVERED IN THE TRANSMISSION AREA. IT WAS TWISTED AND CHSDR UIEA2016082600709Pump · leakingSTATUS HYDRAULIC PRESSURE ENGINE 2 AND EICAS HYDRAULIC QTY LOW 2. REMOVED ENGINE 1 EDP AND INSTALLED ON 2 ENGINE IAW AMM 29-11-05. OPS CHECK
AND LEAK CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.SDR SIMA20160821002Pump · failedHYD 1 LOW QTY, ENG 1 HYD PUMP FAIL, THEN RECOVERED, ALSO LEAKING HYD FLUID, ENGINE 1. R & R ENGINE 1 HYD ENGINE DRIVEN PUMP IAW AMM 29-10-03.
ITEM NR 2 ON THIS LOG PG FOR LEAK TEST. PERFORMED EDPM NR 1 ENGINE LEAK TEST IAW AMM 29-10-03 SECTION J, ITEM 7. SDR RAIA201608150001Pump · leakingNR 2 HYDRAULIC SYS FLUID LOW. SERVICED THE NR 2 HYDRAULIC SYS AND R & R THE NR 2 ENGINE HYD PUMP. OPS LEAK CHECKED GOOD.SDR CALA2016081595649Pump · failedAIR RETURN FOR ECAM CAUTION MESSAGE B HYD RESERVOIR OVEHEAT. R & R BLUE SYSTEM ELECTIC HYD PUMP, CASE DRAIN FILTER, LP FILTER. SERVICED. OPS NORMALSDR AALA201608159014Pump · failedFLIGHT CREW REPORTED RECIEVING A BLUE SYSTEM LOW PRESSURE FAULT WARNING AND A FLIGHT CONTROL ELAC 1 PITCH FAULT AT CRUISE. THE FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED, AND LANDED SAFELY. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE BLUE SYSTEM ELECTRIC PSDR UIEA2016080500669Pump · inoperativeDUE TO ADP INOPERATIVE. HMG WILL BE DEEMED INOPERATIVE, TRANSFERRED TO MEL 24-25-01-01C CAT-C. RE-ACTIVATED AND PERFORMED OPERATIONAL CHECK OF HMG IAW AMM 24-25-00. CHECK NORMAL.SDR FDEA201608042798Warning Light · false activationREJECTED T/O AT 60 KTS FOR AN EICAS R HYD ENG PUMP AND PRESSURE LIGHT ILLUMINATED FOR RT ENG HYD PUMP AND ON THE OVERHEAD PANEL. QRH RTO AND HYDRAULIC ENGINE PUMP PROCEDURES ACCOMPLISHED. RAN RT ENGINE, EDP WAS READING 3020 PSI WITH RT ACMP SELECTED OFF ASDR SIMA20160803001Pump · failedDURING FLIGHT, RECIVED A HYD 1 LOW QTY ADVISORY ON THE EICAS. THE LOW QTY WAS CONFIRMED ON THE HYD PAGE OF THE MFD LATER RECEIVED AN E1 HYD PUMP FAIL ADVISORY ON EICAS AFTER PARKING. FOUND HYDRAULIC FLUID DRIPPING OUT OF NR 1 ENGINE COWLING. REMOVED AND RESDR CALA2016080300494Indicator · leakingHYDRAULIC LEAK. LEFT QUANTITY WAS .46. OCCURRED AT FL 330. RETURNED TO DEPARTURE. FOUND DIFFERENTIAL PRESSURE INDICATOR TO BE LEAKING ON NR 1 ENGINE DRIVEN PUMP PRESSURE CASE DRAIN FILTER MODULE, REMOVED AND REPLACED THE DIFFERENTIAL PRESSURE INDICATOR. OPSDR CALA2016080495606Pump · failedGREEN HYDRAULIC RESERVOIR OVERHEAT ILLUMINATED FOLLOWED BY LOSS OF HYDRAULIC FLUID PRESSURE. REMOVED AND REPLACED THE NR 1 ENGINE HYD PUMP, GROUND TESTED, & LEAK CHECKED SATISFACTORYSDR CALA2016080295603Pump · failedDURING CRUISE, LOSS OF GREEN HYDRAULIC SYSTEM. LOW PRESSURE PUMP OVERHEAT. R & R THE NR 1 ENGINE HYD PUMP, GROUND RUN, NO LEAKS NOTED. SERVICED TO FULL. NOT OVERHEAT INDICATIONSSDR GLBA2016080200601Motor · failedPILOT REPORTED THAT THEY HAD A GEAR ISSUE, LOW HYD LIGHT ILLUMINATED, MANUALLY EXTENDED THE GEAR, DECLARED AN EMERGENCY, HAD 3 GREENS ILLUMINATED, LANDED SAFELY. CIRCUIT BREAKER POPPED, RESET, POPPED WITHIN 4 SEC. HYD FLOW LOW ANNUNCIATOR ILLUM IN FLT. HYD SDR CALA2016080100478Switch · crackedLOW RIGHT HYD QTY, FOLLOWED QRH AND RETURNED TO DEPARTURE. FOUND DIFFENTIAL INDICATOR ON RT EDP PRESSURE MODULE BROKEN AND LEAKING. REPLACED IAW AMM 29-11-17 AND SERVICED RT HYDRAULIC SYS AS REQUIRED. NO FURTHER LEAKS NOTED. ACFT OK FOR CONTINUED SERVICESDR AALA20160801011Pump · leakingDURING CRUISE, RIGHT HYDRAULIC QUANTITIY STATUS MESSAGE DISPLAYED. QUANTITY DROPPED TO ZERO, RIGHT PRIMARY HYDRAULIC PUMP WARNING ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND LEAK AT RIGHT PUMP FILTER MODULE. REMSDR FDEA201607282648Pump · leakingRECEIVED GREEN HYD RESERVOIR OVERHEAT DURING CRUISE. TURNED GREEN PUMPS OFF. IAW QRH, TURNED ONE PUMP ON TO DETERMINE AFFECTED PUMP. FOLLOWED BY GREEN HYD RESERVOIR LOW LEVEL WITH ASSOCIATED ECAM WARNING. GRAVITY EXTENDED GEAR, TOWED TO GATE. ALSO NR 1 ENSDR RAIA201607270001Pump · failedHYD 2 FAIL EICAS MESSAGE. R & R NR 2 ENGINE HYD PUMP IAW AMM 29-10-03. OPS CHECK AND LEAK CHECK GOOD IAW AMM 29-10-03.SDR IPXA2016072706390Warning Message · false activationCENTER HYDRAULIC PRIMARY 1 EICAS MESSAGE DISPLAYED. DIVERTED FLT. OPS CHECKED C HYD PRIMARY PUMP IAW MM 29-11-00-715-896, NO DEFECTS NOTED.SDR AALA201607229002Pump · failedTHE FLIGHT CREW REPORTED A STRONG HYD FLUID ODOR COMING FROM THE NR 2 PACK. AFTER ARRIVING AT THE GATE AND SHUTTING DOWN THE ENGINES. AIRCRAFT GROUNDED. MAINTENANCE DETERMINED THE SOURCE OF THE ODOR TO BE THE YELLOW ELECTRIC HYDRAULIC PUMP. REPLACED YELLOW SDR 6EER20160722001Seal · leakingHYDRAULIC PUMP WITH INTEGRATED RESERVOIR DEVELOPED LEAK AT HYDRAULIC PUMP SHAFT SEAL WHILE AIRCRAFT WAS STATIC WITH ONLY 6.6 AIRCRAFT HOURS. HYDRAULIC OIL WAS OBSERVED LEAKING FROM CASE DRAIN ONTO HANGAR FLOOR. LEAKING ASSEMBLY REPLACED WITH NEW ASSEMBLY.SDR COZA20160718081Pump · leakingRIGHT ENGINE HYDRAULIC PUMP FOUND LEAKING HYDRAULIC FLUID FROM SHAFT SEAL DRAIN. REPLACED PUMP AND OPERATIONAL CHECKED NORMAL.SDR QXEA2016071200450Pump · failedDURING APPROACH, NR 2 HYD ISOLATION VALVE CAUTION ILLUMINATED. FOLLOWED BY A LOSS OF NR 2 HYD SYSTEM PRESSURE. THEN ALL ASSOCIATED CAUTION LIGHTS WITH THAT MALFUNCTION. ACCOMPLISHED EAC CHECKLIST TO COMPLIETION AND THEN LANDED IAW PROCUDURE. NR 2 HYD EDP RSDR AALA20160709005Pump · faultyDURING CLIMB CREW REPORTED HYDRAULIC SYSTEM B LOW PRESSURE LIGHT ILLUMINATED WITH FLUID QUANTITY NORMAL. EMERGENCY DECLARED, LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-11.SDR FDEA201607092334O-Ring · damagedNOTICED A SLOW LEAK IN HYD QTY NR 3 RESERVOIR ,WITH A LEVEL 1 "HYD 3 ELEV OFF" ALERT. CONFIGERED AND GEAR DOWN EARLY THE GTY CONTINUED TO DECREASE WITH EVENTUALLY GOING TO 0GALLIONS QTY AND LEVEL 2 "HYD 3 FAIL" ALERT. ALSO NR 1 HYD SYSTEM LEFT EDP APPEARSSDR UHLA201607080357Pump · failedTOTAL LOSS OF HYDRAULIC SYSTEM 2 IN FLIGHT (TOTAL LOSS). RAN QRH. FREE FALLED THE GEAR. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. R & R NR 2 HYDRAULIC PUMP PRESSURE UNION AND REPAIRED LINE AT RT WING AFT SPAR AFT OF PYLON AREA IAW AMM 20-10-03. LSDR SWAA2016071253705Pump · failedDURING CLIMB, RECEIVED A NR 1 ENGINE HYDRAULIC `A` LOW PRESSURE LIGHT. PERFORMED THE HYDRAULIC PUMP LOW PRESSURE CHECK LIST. SAW HYDRAULIC A QUANTITY DOWN TO 19% WITHIN 10 MINUTES, DOWN TO 15% ON APPROACH. R & R THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMSDR SIMA20160708006Pump · failedHYD2 LO QTY FOLLOWED BY HYD SYS 2 FAILED. REMOVED AND REPLACED ENGINE NR 2 HYDRAULIC EDP IAW EMB 145 AMM 29-10-03 PERFORMED LEAK AND OPS CHECK IAW AMM 72-00-00 NO LEAKS DETECTEDSDR QXEA2016070600445Pump · malfunctionedNR 1 ENGINE HYD PUMP WARNING LIGHT ILLUMINATED DURING CLIMB. IAW EA CHECKLIST USED STBY HYD SYSTEM FOR RETURN TO FIELD. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF THE FIREWALL SHUT OFF HYD VALVE IAW AMM TASK 29-11-06-710-801. SYSTEM OPERATES NORMALLSDR AALA20160707001Drain Valve · failedRT ENG LOW PRESSURE HYD PUMP LIGHT ON DURING CLIMB. RT ELECTRIC PUMP LOW PRESSURE LIGHT WITH COMPLETE LOSS OF SYSTEM B HYD PRESSURED FLUID. EMERGENCY DECLARED, RETURNED TO DEPARTURE, AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED SDR HALA2016070300267Pump · faultyHYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AT 19000 FT AFTER LEVEL OFF. RE-PRESSURE DID NOT WORK. R & R NR 1 EDP IAW AMM TASK 29-11-01-000-801. OPS AND LEAK CHECK GOOD.SDR CALA2016070195502Pump · leakingGREEN RESERVOIR LOW LEVEL TO NEAR ZERO DISPLAYED ON ECAM. FOUND NR 1 HYDRAULIC PUMP LEAKING, REPLACED PUMP, OPS GOODSDR EVCA201606291Pump · leakingDURING FLIGHT, PILOT REPORTED HEARING A GRINDING NOISE AT VARIOUS PITCHES COMING FROM THE TRANSMISSION AREA. WHEN MAINTENANCE ARRIVED TO INSPECT ACFT THEY FOUND HYDRAULIC FLUID COVERING THE DECK FROM THE HYDRAULIC PUMP AFT AND THE HYDRAULIC FLUID RESERVOIR WASDR UIEA2016062000433Pump · leakingAFTER TAKEOFF HYDRAULIC QTY LOW 4 EICAS MESSAGE. RAN ECL NR 4, SYSTEM OFF. REF LP 812459, ITEM 11. FOUND NR 4 ADP HYDRAULIC PUMP LEAKING. R & R NR 4 ADP AND OPS AND LEAK CHECKS OK IAW MM 29-11-17.SDR UIEA2016061800431Pump · leakingLEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED PUMP OPS LEAK CK OK IAW AMM 29-11-05.
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