JASC 2820
Service difficulty reports · 3,631
Reports filed under 2820 · Aircraft Fuel Distribution 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 = '2820' 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 = '2820' 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 USAA2013052400008Fcu · faultyAFTER DEPARTURE, CLIMB OUT AND CRUISE, CREW REPORTED AN AUTO FUEL FEED FAULT. IT WAS DETERMINED THROUGH MX THAT FLIGHT COULD CONTINUE AND EXPECT MEL ADDITION BY CREW UPON LANDING. HOWEVER, SHORTLY THEREAFTER, CREW REPORTED A FCU 1 FAULT AND MX HAD NO RESET ASDR MASA2013052154244Fuel Line · damaged3 FERRY TANK SYS, 1" RIGID FUEL LINES DENTED/DAMAGED. C/W FABRICATION AND INSTALLED 3 EA. RIGID FUEL LINE SEGMENTS IN THE FERRY TANK SYS IAW AC 43, PARA 8-31 AND 9-29.SDR CA130528004Computer · failed(CAN) CREW REPORTED THE FUELER OBSERVED SMOKE COMING FROM REFUEL PANEL. MAINTENANCE REMOVED AND REPLACED REFUEL/DEFUEL CONTROL PANEL PER AMM 28-25-18. DURING OPS CHECK MAINTENANCE OBSERVED SMOKE VISUALLY ALONG WITH STRONG BURNING ODOR. OPS CHECK FAILED. MAISDR UALA2013052103507Scavenge Pump · inoperative2.5K FUEL STUCK IN CENTER TANK DEF IAW MEL. MEL MAINT PROC ACPD. STRAINER CLEANED AND STOWED IN PARTS BIN AT DOOR 2L. PARTS: 750-3766, M25988-1-126 (PACKING) - CENTER HYD-MECHANICAL SCAVENGE PUMP INOPERATIVE.SDR SWAA2013052016235Pressure Switch · faultyWITH RT CENTER PUMP DEFERRED, A FUEL IMBALANCE WAS CREATED BY NO FUEL BURNING OUT OF THE NR 1 TANK. FUEL BURNING OUT OF NR 2. LESS FUEL BURN OUT OF CENTER. R & R RT CONTROL LOW PRESSURE SWITCH IAW MM.SDR UALA2013052103494Actuator · failedLT MAIN TANK TRANSFERRED INTO "C" TANK. CREW COMMENTS: FROM TAKEOFF TO LEVEL OFF, APPROX 30 MINS, 800 LBS TRANSFERD TO CENTER TANK. REPLACED FAILED LT MAIN TANK FILL VALVE BODY ACCT FAILED AND FILL VALVE ACTUATOR IAW MM.SDR 9JLA2013052206457Valve · leakingPRESSURE FUEL SERVICING VALVE WAS LEAKING. VALVE REPLACED WITH AN INSPECTED UNIT. FUNCTIONAL AND LEAK CHECKED SATISFACTORY.SDR DXTA2013050605378Unknown · unknownAFTER TAKEOFF, AMBER FUEL BOOST ON LIGHT ILLUMINATED. SELECTED LT FUEL BOOST SWITCH TO ON, CAS MESSAGE TURNED WHITE. PLACED SWITCH BACK TO NORM, AMBER CAS STAYED OUT REMAINDER OF FLIGHT. RAN AIRCRAFT AT IDLE & MANIPULATED WIRES AND CONNECTOR PLUGS, NO DEFECSDR CA130507003Line · collapsed(CAN) UPON INSTALLATION OF NEW LINE INTERFACING THE AIRFRAME FUEL FILTER WITH THE HMU TECH NOTED THE LINE COLLAPSED INTERNALLY WHEN APPLYING THE NECESSARY TORSION.SDR HALA2013042900048Override Switch · malfunctionedIAW FUELER ACFT WOULD NOT ACCEPT FUEL. RESET MANUAL OVER RIDE BUTTON ON FUELING MANIFOLD. ACFT WILL ACCEPT FUEL, OK FOR SERVICE. PERFORMED HIGH LEVEL TEST IAW MCC CHECKS GOOD.SDR CA130429015Line · wrong part(CAN) DURING VISUAL INSPECTION DISCOVERED AILERON CABLE RUBBING INTO RIGID FUEL LINE TO WHERE ONLY .0312 OF THE TUBE WALL WAS REMAINING. FURTHER INSPECTION INDICATES FUEL LINE INCORRECTLY INSTALLED. NEW FUEL LINE INSTALLED, AILERON CABLE CLEAR OF FUEL LINE. SDR CA130430022Bypass Valve · failed(CAN) WOULDN`T PRODUCE BYPASS INDICATION AT FUNCTION CHECK DURING A/C INSPECTION. LESS THAN 200 HRS. IN SERVICE FROM NEW. NOT AN AS355 BUT HAD NO CHOICE IN THE DROP BOX.SDR UALA2013042302813Valve · leakingFUEL DRIPPING FROM LEFT WING OUTBOARD DRAIN. REPLACED OUTER VALVE, NO LEAKS NOTED.SDR UALA2013042202766Control Unit · faultyRIGHT TRANSFER VALVE OPEN DISPLAYED ON UPPER ECAM SCREEN. LEFT AND RIGHT TRANSFER VALVES OPENED AS EXPECTED BUT WERE ACCOMPANIED BY ECAM MESSAGES. LEFT TRANSFER VALVE OPEN DISPLAYED ON UPPER ECAM SCREEN. REFUELING PANEL BATTERY POWER SWITCH MUST NOT BE SDR 2013FA0000250Flapper Valve · failedOVER A 4 YEAR PERIOD, THIS ACFT HAS EXPERIENCED 2 INSTANCES OF IN-FLIGHT ROLL BACK AND SHUTDOWN OF THE RT ENGINE. IN BOTH CASES ENGINE COULD BE RESTARTED AND SUBSEQUENT EXTENSIVE EVALUATION AND INSPECTION REVEALED NO DEFECTS. ACFT OPERATED WITHOUT INCIDENT SDR VNAA2013041800011Fitting · looseCREW REPORTED FUEL SMELL IN FLIGHT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, TIGHTENED ONE FITTING ON MOTIVE FLOW LINE IN WHEEL WELL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.SDR UALA2013041802689Packing · leakingFUEL LEAKING IN NR 1 PYLON AT FUEL SUPPLY LINE LOWER COUPLING. REPLACED PACKINGS ON ENGINE FUEL LINE INSIDE NR 1 PYLON. DRY MOTOR LEAK CHECK GOOD. ACCOMPLISHED IDT OF FUEL LINE LEAK CHECK. NO LEAK FOUND.SDR HALA2013041100037Actuator · inoperativeLT FUEL SPAR VALVE LIGHT REMAINED ILLUMINATED AFTER ENG SHUTDOWN. R & R LT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.SDR CA130411001Shroud · corroded(CAN) AFTER FINDING CORROSION ON 2 OTHER AIRCRAFT. THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE FIRST ACFT. THE INSIDES OF THESE COMPONENTS WERE COVERED WITH A BLACK SUBSTANCE, ONCE CLEANED OFF THE CSDR CA130410018Shroud · corroded(CAN) THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE OTHER. ALTHOUGH IT WAS NOT AS SEVERE AS THE INITIAL ACFT, MODERATE CORROSION WAS FOUND IN THE SAME AREAS THOUGH OUT THESE COMPONENTS. AS WITH THE FIRSDR ASAA2013040994433Circuit Breaker · trippedNR 2 ENG SPAR VALVE CIRCUIT BREAKER IS OUT. ACCOMPLISHED CIRCUIT BREAKER RESET PROCEDURE REF MM 20-60-01, NO DEFECTS NOTED. ACCOMPLISHED NR 2 ENGINE FUEL SPAR VALVE ELECTRICAL CONTROL AND INDICATION TEST REF MM 28-22-00-710-801 PARA 4.C.1-2 (N). ALL VOLTAGESDR CA130410014Shroud · corroded(CAN) DURING COMPLETION OF ROUTINE MAINTENANCE, TASK 060-28-900-753, 28-10-00-03, FUEL TANK VENT AND LINE SHROUDS PRESSURE LEAK TEST. WE WERE UNABLE TO PRESSURIZE SYS AND NO AIR, NOT PART OF THE TEST WAS COMING OUT OF THE VENT HOLES AT FS 572.35. FURTHER INVSDR UALA2013040902362O-Ring · damagedFOUND FUEL LEAKING AT LOW PRESSURE FUEL SWITCH ON APU. REPLACED O-RING SEALS AT APU LOW PRESSURE SWITCH. ACCOMPLISHED APU RUN, NO LEAKS NOTED.SDR UALA2013041002440Control Unit · malfunctionedLEFT OUTBOARD REFUELING VALVE OPEN LIGHT REMAINS ON WITH VALVE SWITCH IN THE CLOSED POSITION. REPLACED THE LEFT OUTBOARD REFUEL VALVE CONTROL UNIT IAW AMM.SDR UALA2013032601922Actuator · inoperativeRT WING FUEL ENG SPAR VALVE INOPERATIVE DURING TEST. SPAR VALVE ACTUATOR REPLACED AND OPS CHECKED NORMAL IAW AMM.SDR AALA20130325024Guard · missingELP - INFLIGHT DFW-PHX. CREW REPORTED FUEL IMBALANCE DURING CLIMBOUT. FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FUEL PANEL REFUELING POWER SWITCH GUARD DOWN AND CENTER AND RIGHT TANK SWITCHES IN THE OPEN POSITION. SDR ASAA2013032494257Relay · failedDURING CRUISE, FL350, WITH 10,000 LBS FUEL REMAINING IN CENTER TANK, LT CENTER TANK LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED FUEL PUMP LOW PRESSURE QRH PROCEDURE, TURNED OFF PUMP AND OPENED CROSSFEED. REMAINDER OF CENTER TANK FUEL BURNED NORMALLY VIA RT SDR DXTA2013032205330Pressure Switch · failedJUST PRIOR TO LEVELING OFF AT FL 270, RT FUEL TRANSFER PRESSURE LOW ANNUNCIATOR BEGAN CYCLING ON AND OFF ERRATICALLY. FUSELAGE TANK ALMOST EMPTY, AND TRANSFER PUMP SWITCHES WERE IN AUTO. WITHIN ONE MINUTE, THE LT SIDE DID, AS WELL. ACCOMPLISHED ABNORMAL CHESDR 2013FA0000220Line · leakingPILOT REPORTED FUEL ODOR IN CABIN. AFTER INSPECTION, IT WAS DETERMINED THAT THE RIGID FUEL CROSSFEED LINES THAT RUN THROUGH THE FUSELAGE, INSIDE THE MAIN SPAR BOX, HAD CORRODED INTERNALLY RESULTING IN FUEL POOLING IN THE LOWER SPAR BOX. THIS OCCURRED IN OCT SDR QXEA2013032000641Line · chafedRT WING INTERNAL FUEL FEED LINE IS CHAFING ON WING RIB YW157.825 PASS THROUGH CUT OUT FLAGGED. REPLACED FUEL FEED LINES AND MOUNTING BRACKETS AS PART OF SB84-28-09 IAW TASK CARD SB84-28-09. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1 REVSDR A6WA201303154015Ejector · blockedAFTER TAKEOFF AT 1500 FEET RECEIVED L LOW FUEL PRESS, L EJECTOR CAUTION, ENGINE VIBRATIONS, ENGINE SURGE, NORMAL LANDING. ENGINE OPERATED NORMALLY AFTER LEVELING OFF. INSPECTED FUEL TANKS AND FOUND BLOCKAGE IN SCAVENGE EJECTOR. REMOVED BLOCKAGE. C/W OPS CHSDR REXA2013031300561Drain · unsecureON FLIGHT 4381 (LGA TO MSP) AIRCRAFT DIVERTED INTO JFK WITH A SUSPECTED FUEL LEAK. FUEL INDICATION WAS DECREASING RAPIDLY IN CRUISE FLIGHT. FUEL ON ARRIVAL INDICATION WAS DECREASING FASTER THAN NORMAL AS WELL. FUEL FLOW TO ENGINES LOOKED NORMAL. TOTAL FUELSDR 39LA2013031300004Hose · collapsedAFTER DEPARTURE, FUEL LOAD WAS 2800 LBS, T/O GW 17,594, TEMP 12 DEG MAGW 20,000, CG 265.2. WHEN A POWER CHANGE WAS MADE THE NR 1 ENGINE TORQUE OSCILLATED 30 TO 40 PERCENT, FUEL PRESSURE OSCILLATING 10 TO 15 PSI, AND T5 TEMPS OSCILLATING 30 TO 40 DEGREES. NF ASDR ASOA20130311024Flapper Valve · leakingCREW REPORTED AFTER DEPARTURE AT 10,000, ADVISED OF FLUID LEAKING FROM LT WING. SECONDARY INDICATION WAS OBSERVED ON FUEL PAGE LOSS WAS APPROXIMATELY 10LBS EVERY 2-3 SECS. MX R & R THE LEFT WING FLAPPER VALVE AT RIB 19 WITH LEAK CHECKED GOOD. ACFT WAS APPROSDR GTIA20130308519Warning Light · false activationFUEL SPILLAGE FROM RT WING NACA VENT DURING RE-FUELING RELATED TO INCOMING FUEL PRESSURE GREATER THAN 55 PSI CAUSING REFUELING VALVE TO REMAIN PARTIALLY OPEN. PERFORMED TROUBLESHOOTING AND BITE TEST OF THE FLSS IAW TROUBLESHOOTING MANUAL AND MM AND NO FAULTS WSDR CA130304013Line · gouged(CAN) LT MAIN FUEL LINE ON TOP OF NR 1 ENGINE WAS REMOVED FOR ACCESS. UPON REMOVAL OF THE LINE THE FLANGE ATTACHING THE LINE TO THE FRONT SPAR WAS FOUND TO BE GOUGED. WHILE REMOVING THE FITTING FRON THE FRONT SPAR IT WAS FOUND THAT THE MAIN FUEL LINE IN THE WSDR HAEA2013030100226Switch · out of positionENROUTE, MEM LOW FUEL PRESSURE LIGHT ILLUMINATED FOLLOWED BY NR 2 ENGINE ROLL BACK. DECLARED AN EMERGENCY. ON COMPLETING THE PROPER CHECKLIST AND "O" PROCEDURE, DISCOVERED CROSSFEED VALVE INADVERTENTLY MOVED TO THE CLOSED POSITION. OPENED CROSSFEED VALVE ANDSDR ASAA2013022794016Circuit Breaker · trippedAT FL 350, ATTEMPTED OPENING OF FUEL CROSSFEED VALVE FOR FUEL BALANCING, BLUE LIGHT DID NOT ILLUMINATE EITHER BRIGHT OR DIM. PERFORMED QRH PROCEDURE, NOTICED FUEL CROSSFEED CIRCUIT BREAKER OUT P6-3, B-7 LOCATION. SUSPECT CROSSFEED VALVE REMAINED CLOSED. RESESDR AALA20130225012Unknown · leakingMAO - CREW REPORTED FUEL LEAKING FROM RIGHT WING VENT ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED MAO LANDED WITHOUT INCIDENT. PERFORMED INSPECTION AND TESTS PER 28-21-00-810-801. SURGE TANK AND FUELING SHUTOFF VALVES AT RIGHT WING ARE WORKING PROPERLY. SDR ASAA2013022593991Fuel Cell · contaminatedDURING CRUISE, WHILE STILL BURNING FROM CENTER TANK, RT WING TANK WAS NOTICED TO BE APPROX 400 LBS HIGHER THAN PREVIOUS READING PRIOR TO DEPARTING & AT CRUISE, I.E; 8.5 INCREASED TO 8.9. A SHORT TIME LATER, SIMILARLY, THE LT WING TANK WENT FROM APPROX 8.5 TO 8SDR UALA2013022501113Proximity Switch · brokenNO POWER TO FUEL BAY. FOUND DOOR PROX SWITCH BROKEN. REPLACED AS PER SWP 20 10 13 REF WDG 28 21 11, SYSTEM CHECKS GOOD.SDR UALA2013022501116Fitting · not seatedFUEL LEAK LEFT WING NEAR WING ROOT. RESEATED LEFT WING INBOARD SUMP FITTING. NO FURTHER LEAK.SDR UALA2013022101047Pressure Switch · faultyRIGHT AFT FUEL PUMP LOW PRESS LIGHT NOT ON W PUMP OFF, TESTS OKAY. REPLACED RIGHT AFT BOOST PUMP LOW PRESSURE SWITCH PER AMM, OPS GOOD.SDR UALA2013021800951Drain · leakingOUTER CELL TANK SUMP DRAIN LEAKING. REPLACED SUMP DRAIN REF AMM 28-11-41, NO LEAKS NOTED.SDR CA130128023Line · leaking(CAN) DURING AN L-CHECK, MAINTENANCE DISCOVERED A FUEL LEAK FROM A RT WING REFUEL/TRANSFER LINE, IPC REF 28-23-00, FIG 15, ITEM 140. INSPECTION OF THE LINE REVEALED A PINHOLE IN AN AREA WITH PITTING DUE TO CORROSION. THE LINE WAS REPLACED AND LEAK CHECK PERSDR ASAA2013012493747Actuator · inoperativeFUEL CROSSFEED VALVE TRIPPED IN FLIGHT. CROSSFEED VALVE HAD BEEN CLOSED AND HAD NOT BEEN OPENED BY PILOTS. WHEN CENTER TANK EMPTIED OF FUEL, IMBALANCE BEGAN TO BE EVIDENT. SURMISED THAT VALVE HAD OPENED AND WAS NOW STUCK OPEN. BALANCE MAINTAINED BY SELECTIVSDR VNAA2013012000008Control Panel · failedCREW REPORTED REFUEL /DEFUEL PANEL WILL NOT POWER ON. FUELER OBSERVED SMOKE COMING OUT OF THE PANEL. MAINTENANCE INSPECTED, REMOVED AND REPLACED REFUEL / DEFUEL PANEL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.SDR 39LA2013011600004Filter · cloggedWHILE ENROUTE, AFTER DEPARTING, AFT FUEL FILTER BYPASS LIGHT ILLUMINATED. TURNED TOWARD DESTINATION AND VERIFIED EMERGENCY ACTIONS WITH CHECKLIST. FUEL PRESSURES REMAINED NORMAL FOR DURATION OF FLIGHT. FUEL LOW PRESSURE LIGHT DID NOT ILLUMINATE. LANDED FORSDR ASAA2013011393670Relay · inoperativeLOW PRESSURE LIGHT FOR THE CENTER TANK LT FUEL PUMP FAILS TO COME ON. REF T/C 78128006, PARA. D. (9)-(11). FOUND R936 RELAY BAD. REPLACED R936 REF WDM 28-23-11. NOW T/CS 78128006 AND 78128007, OPS NML.SDR UALA2013011100192Relay · faultedRIGHT FUEL CUTOFF SWITCH DOES NOT TRANSMITT 'OFF' TO LT AIMS. REPLACED RELAY K26206 IN P210 PANEL REF WDM 76-21-12 AND IPC 24-09-01. RIGHT ENGINE FUEL SPAR VALVE OPERATES NORMALLY.
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