JASC 2900
Service difficulty reports · 333
Reports filed under 2900 · Hydraulic Power System, 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 = '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 FDEA202112293158None · nonePDIS 668 29-02 4189 29DEC21 MEM OPEN U ON DECENT IN TO MEM, ECAM ALERTED GREEN SYSTEM QUANTITY LOW, COMPLIED AND TURNED BOTH GREEN PUMPS. FOLLOWED ECAM AND QRH, DECLARED EMERGENCY, CRANKED THE GEAR DOWN AND LANDED UNEVENTFULLY. ENT BY: 228808SDR FDEA202112223118None · nonePDIS 746 29-21 2911 22DEC21 MEM OPEN U DEPARTING KMEM27 AT APPROX 100 KNTS LOST GREEN SYSTEM HYDRAULIC PUMPS. NO APPARENT LOSS OF FLUID, JUST PSI. COMPLETE LOSS OF GREEN SYSTEM PRESSURE. ABLE TO RECOVER GREEN SYSTEM WITH PTU S. INFO 22DEC21 13:SDR FDEA202111232925None · nonePDIS 780 29-02 5877 23NOV21 IND OPEN U L HYD QTY SHGN 23NOV21 08:05 IND U ACFT BLOCKED IN W LEFT HYD SYSTEM QTY READING .55. RAN LEFT SYSTEM ELECTRIC PUMPS AND OPENED MAIN CARGO DOOR AS REQ. W/ NO PUMP CAVITATION. SHGN 23NOV21 08:30 IND SDR ABXA20211118117Anti-Skid Valve · crackedRH HYD SYSTEM DUMPED FLUID AFTER BLOCK OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND RIGHT WING INBOARD ANTISKID VALVE LEAKING. REMOVED AND REPLACED RIGHT WING/GEAR INBOARD ANTISKID VALVE PER B767 AMM 32-42-03 LEAK & OPS CHECK GOODSDR 29GA2021111700001None · noneSUPPLEMENTAL CORRECTED UNIQUE CONTROL NUMBER FLIGHT 122 SJU/STX DURING APPROACH MAIN HYDRAULIC PRESSURE LOSSS IN RIGHT GEAR. (EMERGENCYDECLARED QRH DRIVEN) CORRECTIVE ACTION: PERFORMED HYDRAULIC SYSTEM OPERATIONAL CHECK AND FOUND WORKING PROPERLY.SDR 29GA202111700001None · noneFLIGHT 122 SJU/STX DURING APPROACH MAIN HYDRAULIC PRESSURE LOSSS IN RIGHT GEAR. (EMERGENCY DECLARED QRH DRIVEN) CORRECTIVE ACTION: PERFORMED HYDRAULIC SYSTEM OPERATIONAL CHECK AND FOUND WORKING PROPERLY.SDR AALA202111047010Pump · failedAIRCRAFT WAS GROUNDED: DURING CLIMB YELLOW HYDRAULIC SYSTEM OVERHEAT MESSAGE OCCURRED, CREW SHUT DOWN SYSTEM PER QRH PROCEDURE, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AASDR AALA202111027010None · noneAIRCRAFT WAS GROUNDED: DURING CLIMB YELLOW HYDRAULIC SYSTEM OVERHEAT MESSAGE OCCURRED, CREW SHUT DOWN SYSTEM PER QRH PROCEDURE, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BSDR IPXA2021110175497Pipe · rupturedINSPECTION TYPE:3CAPPX. 250 MILES FROM SDF DURING DECENT AP1 DISCONNECTED AND WE RECEIVED A LEVEL 1 HYD. 2 OFF ALERT, HYD 2 QUANATY WAS 2.6 GALLONS, REDUCED TO 2.1 DURING APPROACH.REMOVED AND REPLACED HYD. PRESSURE LINE IN L/H W/W, LEAK CHECK IS GOOD REF. AMM SDR EBVR20211026001Dump Valve · leakingTROUBLESHOOT LOW HYDRAULIC LEVEL DURING GEAR RETRACTION, UPON INSPECTION IT WAS FOUND THAT THE HYDRAULIC SYSTEM VENTED THE RESERVOIR OUT THE DRAIN MAST NEAR THE NOSE LANDING GEAR. PERFORMED GEAR SWINGS AND FUNCTIONAL CHECKS PER C-550B M.M. 32-01-00 WITH NO DESDR CALA2021102501957None · damagedENG 1 LOW PRESSURE LIGHT LIGHT ON PREVIOUS WRITEUP ENG 1 EVIDENCE FOUND EDP. DAMAGED PLEASE COMPLETE SDR BEFORE UNLOCKING THIS ITEM. TOMC MGR CASEY SETTING SDR FOR IRREGULARITY. FURTHER DETAILS AWAITED. PER LP 7300051 REPLACED EDP AT ENG 1 AS PER AMM 29-11-11/SDR WWQA826102221Hose · leakingIN FLIGHT, RECEIVED A HYD QUANTITY AMBER MESSAGE, NOTICED THE HYDRAULIC QUANTITY COMING UP ON LOW. HYD QUANTITY WENT RED ON THE ON THE COMBINED QUANTITY WHILE THE INFLIGHT QUANTITY REMAINED NORMAL. AIRCRAFT DID NOT HAVE ANY HYDRAULIC FAILURES ON LANDING AND TASDR FDEA202110062474Actuator · nonePDIS 721 29-02 1252 06OCT21 MEM OPEN U GREEN SYSTEM HAD HYD LOW PRESSURE. COMPLIED WITH QRH. INFO 06OCT21 04:43 MC1 R LOST GREEN HYD SYSTEM QUANTITY DOWN TO BOTTOM OF YELLOW BAND. FOLLOWED BY LOSS OF SYSTEM PRESSURE. COMPLIED WITH QRH. MSDR FDEA202110062472None · crackedPDIS 789 29-02 4718 05OCT21 MEM OPEN U DURING CRUISE THE C HYD ELEC 2 EICAS MESSAGE APPEARED FOLLOWED BY A COMPLETE REDUCTION OF C HYDRAULIC QUANTITY. SHORTLY AFTER THE FOLLOWING EICAS MESSAGES APPEARED: C HYD SYS PRESS C HYD RSVR PRES C HYD SDR AALA202110059841Hydraulic Line · leakingAIRCRAFT WAS GROUNDED: YELLOW HYDRAULIC RESERVOIR LOW LEVEL ECAM MESSAGE, FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURE, DECLARED AN EMERGENCY AND RETURNED TO DFW WHERE THE AIRCRAFT LANDED SAFELY AND WAS TOWED OFF THE RUNWAY. **SUPPLEMENTAL REPORT FOR AALA202109SDR AALA202109309841None · noneAIRCRAFT WAS GROUNDED: YELLOW HYDRAULIC RESERVOIR LOW LEVEL ECAM MESSAGE, FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDURE, DECLARED AN EMERGENCY AND RETURNED TO DFW WHERE THE AIRCRAFT LANDED SAFELY AND WAS TOWED OFF THE RUNWAY. **SUPPLEMENTAL REPORT WILL BE SUBMITSDR SWAA2021092722172Valve · looseSUPPLEMENTAL INFORMATION: HYDRAULIC QTY DROPPED 1% EVERY 2 MINUTES. LANDED WITH 50% HYDRAULIC QTY IN SYSTEM A ; / [01] FOUND A SYSTEM HYDRAULIC RETURN LINE FROM #1 ENG TR ISOLATION VALVE LOOSE. RE TORQUED PER AMM 20-50-11; NO LEAKS NOTED. SERVICED A SYSTEM HYDSDR 9WGA2021092341201None · noneLVL 2 HYDRAULIC 2 FAIL.SDR P5CA2021092000350None · noneENG #1 HYDRAULIC PUMP WITH EVIDENCE OF LEAK(<P><SPAN>CLEANED AREA AS REQUIRED, TIGHTENED CASE DRAIN HOSE, SUPPLY HOSE AND PRESSURE HOSE ON ENGINE HYD. DRIVEN PUMP IAW AMM 29-11-05. PENDING LEAK CHECK</SPAN></P> / <P><SPAN>OPS CHECK ASDR FDEA202108232074Ram Air Turb · failedTEST FLIGHT- RAT WOULD NOT DEPLOY WITH BOTH SPEED CAD C/B PULLED. REMOVED AND REPLACED LEFT AND RIGHT ENG SPEED CARDS IAW AMM 77-12-03-4, PERFORMED RAT AUTO DROP TEST IAW AMM 29-21-00-5, TEST PASSED.SDR 2021FA0000241Pump · failedPREMATURE FAILURE OF ENGINE MOUNTED HYDRAULIC PUMP @ 1099.6 HOURS SINCE OVERHAUL.SDR P5CA2021062100247Warning Message · false activationDURING THE LEFT ENGINE START, THE " L HYD SYS PRESS" EICAS MESSAGE APPEARED. AS WELL AS THE MASTER CAUTION LIGHT AND BEEPER. DURING ENGINE START, WE NOTICED THAT THE LEFT " VALVE" LIGHT DID NOT CYCLE WHEN THE ENGINE START SELECTOR WAS SELECTED TO "GDN". THE LISDR OZIA2021082300369Hose · damaged***EMERGENCY DECLARED*** L HYD SYS PRESS CAUTION ILLUMINATED ON FINAL APP. EMERG DECLARE D. FOUND HOLE ON HYDRAULIC HOSE TO DOWN LOCK ACTUATOR. REMOVED AND REPLACED HYDRAULIC HOSE TO DOWN LOCK ACTUATOR IN REF WITH AMM 32-32-02. SERVICED LEFT HYDRAULIC SYSTEMSDR IPXA2018020726294Lcca · malfunctionedA HYD A QTY ANNUNCIATION IN FLIGHT, FOLLOWED BY A HYD C PRESSURE INDICATIONS. RAN CHECKLISTS. EMERGENCY DECLARED, AND LANDED. R & R THE RT LCCA IAW AMM 27-11-14-401, DUE TO A LEAK. OPS CHECKED SATISFACTORY. TEST PERFORMED IAW AMM 22-00-02/201 1. TESTED SATISDR UIEA2017011700059None · noneAUTO PILOT SERVO ASSYS SHOWS SIGNS OF LEAKING ON ASSYS AND LINES/ STRUCTURE IS WET. PERFORMED LEAK CHECK ON AUTO PILOT SERO ASSYS IAW AMM 29-11-00. NO LEAKS AT THIS TIME. NOT AN SDR.SDR DALA2016061604675Warning Light · false activationRIGHT HYDRAULIC "HOT" OAP LIGHT ON, THEN ZERO HYDRAULIC PRESSURE BOTH SYS. ACCOMPLISHED QRH PROCEDURES FOR TOTAL HYDRAULIC FAILURE. ON BASE LEG AT 3000' AGL BOTH HYDRAULIC SYSTEMS CAME BACK TO NORMAL. ACCOMPLISHED NORMAL LANDING. FOUND RT HYD SYSTEM WITH EXSDR QXEA2015091200478Unknown · unknownTAKEOFF ABORT AT 10 KTS. ROLL SPOILER EXTENDED NORMALLY PRIOR TAKEOFF. UPON ADANCING THROTTLES, COINCIDENT WITH SPOILER RETRACTION, THE NR 1 HYD ISO VALVE" AND " ROLL SPOILER INBD HYD" CAUTION LIGHTS MOMENTARLY ILLUMINATED AND THEN WENT OUT WHEN THROTTLES BRSDR CALA2014012790246Unknown · malfunctionedFLIGHT DIVERTING TO SFO DUE TO A CTR HYD SYS QTY AT ZERO.SDR FDEA201307141559Union · leakingDURING CLIMB TO FL 330, RECEIVED LEVEL 1 HYD 3 ELEV OFF. HYD QTY INDICATED 4.7 GAL. QTY DECREASED TO 2.7 AND RECEIVED HYD 3 OFF. USED ALTERNATE GEAR EXTENSION. NR 3 ENGINE RAN FOR APPROX 25 MINUTES WITH HYD 3 OFF. R & R HYDRAULIC LINE UNION AND CHECK VSDR QXEA2013070201151Warning Light · false activationPTU WHEN SELECTED ON INDICATED FAIL WITH NO GREEN LIGHT ON. NO RELATED FAULTS IN CDS. COMPLIED WITH FIM TASK 29-30-00-810-819. PTU SYS OPERATED NORMALLY. FAIL LIGHT ON HYD CONTROL PANEL DID NOT ILLUMINATE. COMPLIED WITH FUNCTIONAL TEST OF THE POWER TRANSFSDR KNNA20130606773Hydraulic System · malfunctionedAPPROX 1200 FT, ACFT ROLLED RT AND PITCHED DOWN. AUTOPILOT WAS ENGAGED AT THE TIME AND FO WAS PF. ACFT WAS FULLY CONFIGURED FOR LANDING, PF DISCONNECTED A/P. PM (CAPT) COMPLETED CHECKLIST. "A" SYSTEM ENGINE HYD LOW PRESSURE LIGHT ILLUMINATED ON OVERHEAD HYSDR 2013FA0000208Cover · crackedCRACK IN COVER IN CENTER.SDR CA110923001Line · leaking(CAN) HYDRAULIC FAILURE ON FINAL TO AIRPORT BASE. FOUND HYDRAULIC PRESSURE LINE WORN THROUGH WHERE CLAMPED TO DECK. CLAMP WAS IN GOOD CONDITION, BUT THE RUBBER CUSHION HAD TURNED VERY SLIGHTLY LEAVING VERY SMALL GAP THAT HOSE RUBBED THROUGH ON. HOSE REPLACESDR QXEA2010051100299Unknown · unknownPTU CONTROL "ON" GREEN LIGHT WILL NOT GO OUT WITH SWITCH PUSHED OUT. MECHANIC THAT TAXIED ACFT FROM GATE SAID AFTER SHUTTING DOWN NR 2 ENGINE, PTU "ON" LIGHT STAYED ON AND NR 2 HYD SYS REMAINED PRESSURIZED, LIGHT EXTINGUISHED AND ALL HYD WENT TO "0" PSI. PTUSDR 2009F00141Warning Light · illuminated" LOW HYD FLOW R (RT) MASTER CAUTION LIGHT ILLUMINATED IN FLIGHT.SDR HEEA123898Pressure Switch · warning lightNR1 HYDRAULIC SERVO LIGHT ILLUMINATED AND FLICKERED INTERMITTENTLY. FOUND WATER IN THE NR 1 HYDR PRESSURE SWITCH CONNECTOR PLUG. REMOVED WATER AND SWAPPED NR 1 AND NR 2 HYD PRESSURE SWITCHES.SDR 2008UALA02460Module · failedTEST FLIGHT, PULLING CBZ25 AND Z26 DEPLOYED RAT BUT DID NOT SHOW HYD PRESSURE TO BLUE SYSTEM. EMERGENCY GEN DID NOT WORK SINCE NO HYD PRESSURE. PUSH MAN RAT BUTTONS BUT NO CHANGE. FOUND THE GROUND CHECK MODULE FAILED. REPLACED GROUND CHECK MODULE. OPS TESTEDSDR SIMA200804301Unknown · unknownON FLIGHT 3686 - CREW REPORTED AUTOPILOT DISENGAGED WITH RUDDER 1-2 INOP EICAS MESSAGE.AFTER A FEW SECONDS, THE MESSAGE DISAPPEARED. THE CREW RE-ENGAGED THE AUTOPILOT AND THE MESSAGE RETURNED. THE CREW FOLLOWED THE PROCEDURE IN THE AOM AND THE RUDDER SYSTEM SDR 2007UALA03490Unknown · unknownCREW COMMENTS: RIGHT HYDRAULIC QTY DROPPED TO .40 IN FLT.SDR QXEA200701094Unknown · unknownSEA FLIGHT NR 2459: NR 2 RUD HYD CAUTION AND NR 2 HYD PRESS BLANK. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND NR 2 HYD CIRCUIT BREAKER POPPED. RESET BREAKER AND GROUND RAN NR 2 ENGINE. NR 2 HYD CAUTION LIGHT EXTINGUISHED. OPS CHECK OF NR SDR QXEA200701379Circuit Breaker · trippedSEA - WHEN SELECTING NR 1 STANDBY HYDRAULIC PRESSURE ON DURING APPROACH CHECKLIST NR 1 STANDBY HYDRAULIC PRESSURE INDICATED ZERO. AFTER FLAP SELECTION INDICATOR STILL READ ZERO. MAIN PRESSURE INDICATED NORMALLY AND NO LIGHTS ILLUMINATED. ALL COCKPIT BREAKERSDR CA070608007Bypass Valve · failed(CAN) ON ARRIVAL, THE IB FLAPS FAILED TO EXTEND WHEN LANDING, CONFIGURATION SELECTED. THE CREW ELECTED TO DIVERT. THE AIRCRAFT COMPLETED A NORMAL LANDING. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND INSPECTED THE SYSTEM FOR LEAKS AND ANOMALIES. THE FLASDR QXEA200700388Unknown · unknownSEA FLIGHT NR 2077 INFLIGHT, NR 2 SPU AUX POWER CAUTION LIGHT ILLUMINATED RAN APPROPRIATE CHECKLIST NO OTHER CAUTION LIGHTS AT THE TIME. MAINTENANCE GROUND RAN ENGINES FOR AC POWER 2 SPU AUX POWER CAUTION LIGHT REMAINS EXTINGUISHED WITH AC GEN POWER APPLIED. SDR QXEA200700111Unknown · unknownBIL FLIGHT NR 2411: NR 3 HYD PUMP CAUTION LIGHT ILLUMINATED. MAINTENANCE RESEATED RELAY RL4. NR 3 HYD PUMP CAUTION CLEARED. NR 3 HYD PUMP OPERATES NORMALLY PER AMM TASK 29-00-00-863-803. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR DJFA2007005Unknown · unknownTRIP NR 1127054, CREW REPORTED (HYDRAULIC VOLUME LOW-B) EICAS MESSAGE 5 MINUTES AFTER TAKEOFF. CREW VERIFIED (0) QTY ON HYDRAULICS PAGE IN EICAS FOR B SYSTEM. CREW PERFORMED CHECKLIST FOR FAILED B HYD SYS AND DIVERTED. NO UNUSUAL FLIGHT CONTROL PROBLEMS WERSDR 2006UALA02324Hydraulic System · unknownLOST RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY. DAMAGED RT SYSTEM HYD RETURN LINE WAS REPLACED.SDR MALA060286Bolt · failedEN ROUTE TO CID, THE AIRCRAFT WAS 30 MILES SOUTH OF RST THE MAIN AND EMERGENCY ACCUMULATOR PRESSURE DROPPED BELOW THE YELLOW. HYDRAULIC QTY NORMAL. HYD PUMP TURNED OFF PER THE QRC. CREW FOLLOWED PROCEDURES. BOLTS WERE BLOWN. MADE AN UNSCHEDULED LANDING IN SDR XN0A1316Priority Valve · leakingRAMP OUT AND RETURN DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. PRESS=0 AND QTY=0. TIGHTENED LOOSE LINE AT PRIORITY VALVE, OPS CK NORMAL IAW A300 AMM CHAPTER 29-16-00 AND SERVICED HYDRAULIC SYSTEM IAW A300 AMM CHAPTER 12-12-29.SDR KBM2006F00088Switch · inoperativeNO HORN LIGHT, REMOVED AND REPLACED. (K)SDR 2006FA0000271Housing · cracked(203230/FXS) HOUSING CRACK AT THE PRESSURE (INLET) PORT FOR THE CHECK VALVE BORE. PROBABLE CAUSE: FATIGUE. REDESIGN HOUSING. (K)
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