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.

SDR LS1R076732Vent Line · bentFUEL VENT LINE IS BENT.Oct 22, 2001 · N5027P · Hughes 369DSDR QXEA0202010Switch · failedPDX - CREW RECEIVED A RIGHT FUEL LOW PRESSURE CAUTION MESSAGE ON TAXI-IN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 16, 2001 · N601QX · Cndair CL6002C10SDR HEEA076513Valve · stuckFUEL VALVE STICKING.Oct 5, 2001 · N402PH · Bell 407SDR SABA011050Fuel Line · kinkedFLIGHT 5018 CLT TO OAJ ABORTED TAKEOFF, LEFT FUEL CAPTION LIGHT ILLUMINATING AT 70 KNOTS. AIRCRAFT RETURNED TO GATE WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE MAIN FUEL SUPPLY LINE KINKED. REMOVED AND REPLACED FUEL LINE, RUN, LEAK AND OPS CHECKED GOOD. Oct 2, 2001 · N966AE · Bag JETSTM3201SDR WTXR200100277Line · crackedAFTER LANDING AND TAXING TO RAMP, PILOT NOTICED FLUID RUNNING OUT OF BOTTOM OF ENGINE COWLING. ENGINE WAS SHUT DOWN AND MAINTENANCE WAS CALLED.MAINTENANCE FOUND A CRACK IN THE FUEL MANIFOLD AT THE 6 O'CLOCK POSITION,IN THE "B" NUT FITTING NECK. INSTALLED SERVISep 26, 2001 · N332BA · Swrngn SA226TCSDR HEEA075944Check Valve · intermittentINTERMITTENT LIGHT. SCRAPPED AND REPLACED WITH SERVICEABLE PART.Sep 10, 2001 · N2148K · Bell 412SDR JJB2001F00004Hose · missingDURING SCHEDULED MAINTENANCE, (FUEL TANK INSPECTION) FOUND RIGHT AFT TRANSFER PUMP FUEL STRAINER AND HOSE NOT INSTALLED ON AIRCRAFT. NOTE: NOT INSTALLED BY MFG.Sep 8, 2001 · N852CA · Beech 1900DSDR COMA0160682Check Valve · frozenFUEL TRANSFERRING FROM RT TANK TO LT TANK WITH POWER OFF AND A/C SITTING ON LEVEL GROUND.REMOVED APU XFEED CHECK VALVE WHICH WAS STUCK OPEN BY A PIECE OF FOREIGN MATERIAL. INSTALLED NEW VALVE.Sep 4, 2001 · N767CA · Cndair CL6002B19SDR CA010831008Indicator · failed(CAN) THE AIRCRAFT RETURNED TO THE STATION AFTER 2 HOURS OF FLIGHT DUE TO FLIGHT CREW EXPERIENCED DIFFICULTY TO USE FUEL FROM TANK NR 2 RT. DURING INITIAL INVESTIGATION AN ACTUAL UNBALANCE WAS FOUND BETWEEN TANK NR 2R AND TANK NR 2 LT. ENGINES GROUND RUN CONFIAug 27, 2001 · Lkheed 10113853SDR AUS20010922Tube · chafed(AUS) LT ENGINE FUEL FEED MOTIVE FLOW TUBE CHAFED AND LEAKING IN AREA OF O-RING SEAL CONTACT POINT.Aug 23, 2001 · Dhav DHC8102SDR HEEA075510Valve · leakingLEAKING FROM FUEL COCK. REPLACED WITH SERVICEABLE PART.Aug 21, 2001 · N42EA · Bell 206L3SDR HEEA075509Fitting · corrodedFWD. FUEL SUMP FITTINGS CORRODED. REPLACED WITH SERVICEABLE FITTINGS.Aug 21, 2001 · N3108E · Bell 206L3SDR AWXA0002213Packing · brokenD: Las - L/H plyon /engine fire - Flt 69 - while taxing in to the gate personnel observed smoke and flame at the top of the #1 ENG. and pylon area. Ground crew advised the pilots who followed QRH procedures. Maintenance opened the thrust reversers / core cowlsAug 18, 2001 · N629AW · Airbus A320231SDR CA010831006Tube · leaking(CAN) NR 5 CYLINDER FUEL DISTRIBUTION TUBE RUPTURED DURING CRUISE FLIGHT. TUBE BREAK IS AT THE CONNECTION TO FUEL DISTRIBUTOR VALVE. CONNECTION POINT A CYLINDER REMAINED INTACT. FAILURE OCCURRED AT FLANGE END WHERE TUBE FLARE END IS BRAZED TO TUBE ASSY. NO POSAug 17, 2001 · Cessna U206GSDR MJQ2001F00000Fitting · leakingFITTING DEVELOPED A CUT IN THE RUBBER ALLOWING FUEL TO LEAK INTO SHROUD, DRAINING OVERBOARD, THRU DRAIN.Aug 6, 2001 · N604PM · Cndair CL6002B16SDR 2001FA0000594Gascolator · crackedDURING ENGINE START, AN INDUCTION FIRE STARTED WHEN THE CARBURETOR BACKFIRED. THE FIRE COULD NOT BE EXTINGUISHED AND DESTROYED THE AIRCRAFT. DURING AN INVESTIGATION THE GASCOLATOR COVER WAS FOUND CRACKED. IT APPEARS THE FUEL LEAKING FROM THE COVER APPEARS TJul 24, 2001 · Piper PA28*SDR DL76G011202Manifold · crackedRT ENG FUEL MANIFOLD LEAK.REMOVED AND REPLACED FUEL PIPE. Jul 19, 2001 · N153DL · Boeing 7673P6SDR Z4MR601462AGasket · leakingA RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GASKET. THIS PUMP INCORPORATES THE SAME (OR VERY SIMILAR) RELIEF VALVE AND GASKET ASSEMBLY USED ON ROTARY FUEL PUMP WHICH WAS THE SUBJECT OF Jul 14, 2001 · N325MW · Pilats PC1245SDR 2001FA0000118Check Valve · misinstalledRIGHT FUEL QUANTITY GAUGE FALLS TO ZERO WHEN RIGHT TANK WAS SELECTED. FOUND FUEL QUANTITY TRANSMITTER WAS CORRECT, INBOARD TRANSMITTER MOUNTED IN THE HEADER TANK WAS GOING TO ZERO WHEN FUEL WAS BEING USED FROM THE RIGHT TANK. CAUSE: THE FUEL INLET CHECK VALJul 6, 2001 · N960CM · Cirrus SR20SDR SWIA972665Pressure Switch · failedINFLIGHT LEFT SCAVENGER EJECTOR CAUTION MESSAGE REPEATELLY ILLUMINATES, INCREASES FREQUENCY WITH VERTICAL SPEED GREATER THAN 1,000 FPM. INSTALLED SCAVENGE EJECTOR PRESSURE SWITCH IAW 28-42-07.Jun 28, 2001 · N427SW · Cndair CL6002B19SDR HEEA073540Connector · dirtyWHILE IN CRUISE FLIGHT, THE NR 2 ENGINE FUEL FLOW INDICATOR BEGAN TO FLUCTUATE. CLEANED CANNON PLUG AT TRANSMITTER.Jun 20, 2001 · N1546K · Skrsky S76ASDR 01FDEA00436Actuator · faultyIN CRUISE NR 2 FUEL PUMPS ON, ALL CROSS FEEDS OPEN, TANK NR 1 & 3 FUEL PUMP OFF. FUEL STILL BURN TANK TO ENG. *S/D* REMOVED AND REPLACED ACT ASSY PER MM 28-22-011-4, REMOVED AND REPLACED CANNON PLUG D40 REF 727-200 MM CH 20.Jun 13, 2001 · N276FE · Boeing 727233SDR HEEA073199Fuel Filter · chafedFUEL FILTER CHAFED ON BOWL.Jun 1, 2001 · N493PH · Bell 407SDR AUS20010561Switch · faulty(AUS) FUELLING CONTROL PANEL POWER SWITCH FAULTY. PANEL POWER REMAINEDON WITH THE SWITCH IN THE OFF' POSITION. INVESTIGATION FOUND THE ACCESS PANEL CAM OPERATING THE PANEL POWER SWITCH WHEN THE PANEL IS CLOSED WAS OUT OF ADJUSTMENT AND NOT OPERATING THESWITCHMay 27, 2001 · Fokker F28MK0100SDR 20010529CW003Fuel Tank · brokenFIBERGLASS WINGTIP FUEL TANK STC SA1480WE HAS AN EDGE DISTANCE OF .2500 INCH SCREW HOLES WHICH BROKE FIBERGLASS OUT CAUSING THE WINGTIP TO FALL OFF, WHILE AIRCRAFT WAS ON GROUND. FIBERGLASS TIP DOES NOT HAVE SUFFICIENT STRENGTH DUE TO FIBERGLASS THICKNESS ANMay 8, 2001 · N21551 · Piper PA23250SDR HEEA072581Valve · leakingLEAKING SHAFT SEAL. REPLACED WITH SERVICEABLE PART.Apr 12, 2001 · N7128R · Bell 412SDR HEEA072486Valve · stuckSTICKING OPEN. REPLACED WITH SERVICEABLE PART.Apr 11, 2001 · N45RP · Bell 206L1SDR HEEA072485Check Valve · malfunctionedCHECK VALVES POSSIBLY CAUSING ENGINE FLAME OUT. REPLACED WITH SERVICEABLE PART.Apr 11, 2001 · N3178K · Bell 206L1SDR HEEA072383Valve · leakingLEAKING FUEL VALVE. REPLACED WITH SERVICEABLE PART.Apr 9, 2001 · N5019F · Bell 206L1SDR HEEA071989Valve · leakingFUEL VALVE LEAKING THROUGH WEEP HOLE. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR.Apr 5, 2001 · N2149S · Bell 412SDR 20010423CW016Line · leakingFOUND FUEL RETURN LINE LEAKING THROUGH THE STEEL BRAID. HOSE IS LESS THAN 3 YEARS OLD, WITH NO VISIBLE DAMAGE. EVEN THOUGH THIS TYPE HOSE IS APPROVED FOR FUEL, AVIATION FUEL SEEMS TO DETERIOATE IT. HOSE HAS STEEL BRAID EXTERIOR.Apr 4, 2001 · N5VA · Cessna U206FSDR DL76G010508Flow Valve · failedA/C RESTRICTED FROM ETOPS OPERATIONS DUE TO REPETITIVE FUEL MIGRATION HISTORY. FOUND MOTIVE FLOW VALVE MALFUNCTION. REPLACED SAME.Mar 17, 2001 · N1501P · Boeing 7673P6SDR AU010195Line · loose(AUS) RT ENGINE MAIN FUEL LINE FLARE NUT DISCONNECTED ON AFT SIDE OFFIREWALL. PERSONNEL/MAINTENANCE ERROR.Mar 14, 2001 · Beech 58SDR CA010404003Fitting · leaking(CAN) THE FLIGHT CREW REPORTED THE NR 1 -FUEL LOW PRESS- CAUTION LIGHT WOULD ILLUMINATE AS SOON AS THE AUXILIARY FUEL PUMP WAS SELECTED OFF, BUT THE LIGHT WOULD GO OUT AT LOW POWER SETTINGS. MAINTENANCE INVESTIGATION REVEALED THAT A FITTING ON THE MOTIVE FLMar 8, 2001 · Dhav DHC8311SDR DHL2001806515Bolt · misinstalledNR 1 ENGINE FUEL LINE BOLTS AT RT SIDE OF PYLON SHOW SAFETY IMPROPER. SAFETIED PROPERLY NR 1 ENGINE FUEL LINE BOLTS (PYLON RT. SIDE) IAW CFMI MM 70-00-40, PAGE 201, PARA 4. STATUS-CLOSED.Mar 7, 2001 · N806DH · Doug DC873FSDR CA010402011Fuel Line · leaking(CAN) STEEL BRAIDED FLEX FUEL SUPPLY LINE, NR 2 ENGINE & APU, IN HYDRAULIC SERVICE CENTER COMPARTMENT LEAKING APPROXIMATELY 3 FEET FROM FORWARD END DUE TO INTERNAL RUPTURE. FUEL LINE IS UNDER INVESTIGATION BY ENGINEERING DEPARTMENT TO DETERMINE THE CAUSE.Feb 28, 2001 · Lkheed 1011385114SDR CA010320018Line · chafed(CAN) LINE ASSEMBLY - FUEL, STRAINER TO ELBOW FOUND CHAFING AGAINST RT NOSE GEAR STEERING BOOT.1.50 INCH X 0/032 INCH TUBING FOUND WORN BY 0/018 INCH ON ONE SIDE. PART HAS BEEN REPLACED WITH A NEW LINE ASSEMBLY - FUEL AND PROTECTED WITH NYLON SPIRAL WRAP.Feb 28, 2001 · Cessna U206GSDR 20010410AP001Needle Valve · separatedOWNER REPORTED ROUGH IDLE AFTER LANDING, ASSUMED THE PROBLEM WAS RELATED TO CARB ICE ON THE GROUND. AIRCRAFT WAS BROUGHT IN FOR ANNUAL INSPECTION AND DURING PRE INSPECTION RUN UP CONFIRMED ROUGH IDLE, BUT SMOOTHED OUT WHEN CARB HEAT WAS APPLIED. DURING INSPFeb 16, 2001 · N3087Q · Cessna 182KSDR AUS20011126Line · misrepaired(AUS) MAIN FUEL SUPPLY LINE CHAFED THROUGH BY COWL FLAP CABLE. NYLONWRAP USED TO PROTECT WORN AREA.Feb 15, 2001 · Cessna 172RGSDR 20010323CW005Valve · inoperativeSERVO WAS CLEANED AND RECERTIFIED, WHICH PARTIALLY IMPROVED ENGINE PERFORMANCE. ENGINE STILL BACKFIRED AT 1300-1500 RPM. CLEANED INJECTORS, WITH NO CHANGE. REMOVED AND INSPECTED FUEL DISTRIBUTION VALVE. FOUND SMALL AMOUNT OF LINT PARTIALLY BLOCKING PASSAFeb 14, 2001 · N74GW · Cessna 172SSDR 20010319CW002Fuel Line · leakingWHILE INVESTIGATING FUEL SMELL INSIDE AIRCRAFT, FOUND FUEL CROSSFEED LINE BELOW FLOOR LEAKING. LINE ATTACHES DIRECTLY TO MAIN FUEL TANK AND RUNS UNDER FLOOR TO OTHER FUEL SOV. LINE FAILED DUE TO CORROSION DUE TO WATER NOT BEING SUMPED FROM FUEL DRAIN POINTS.Feb 8, 2001 · N55RB · Cessna 340ASDR 20010409AP001Adapter · crackedFUEL SMELL IN CABIN, FUEL STAIN LEFT SIDE OF INTERNAL FUSELAGE AT AND BELOW ADAPTER. VISUALLY INSPECTED PART AND FOUND CRACK AT SUMP DRAIN VALVE FITTING. FUEL LEAKED INTO AND WAS STANDING IN THE HULL. LEAK DETECTED DURING REPAIR OF STRUCTURE IN THAT AREA.Feb 5, 2001 · N9WA · Conaer LA4200SDR R7MR33265Valve · leakingFRANGIBLE SELF SEALING VALVE, LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Jan 27, 2001 · N901CF · Doug MD900SDR 20010306AP001Fuel Line · leakingPILOT REPORTED STRONG FUEL ODOR IN CABIN. INVESTIGATION REVEALED FUEL LEAKING FROM FLARELESS FITTING SLEEVE AT BULKHEAD FITTING AFT OF FIREWALL BELOW THE NOSE BAGGAGE AREA FLOOR. FUEL WAS CARRIED BACK INTO THE CABIN AREA INSIDE THE PLASTIC CHAFF SLEEVE COVERINJan 12, 2001 · N81573 · Piper PA32301TSDR 20010206CW001Primer Line · brokenWHILE REPAIRING MASSIVE EXHAUST LEAK ON LEFT ENGINE THE CYLINDER PRIMER LINE WAS FOUND BROKEN IN HALF AND ANOTHER FUEL PRIMER LINE FOUND CHAFED. RAW FUEL AND MASSIVE EXHAUST LEAK COULD CAUSE ENGINE FIRE. NEW LINES INSTALLED. AC HAD RECENT ANNUAL.Dec 12, 2000 · N4048P · Piper PA23160SDR UPS00834556Coupling · leakingINSPECTION TYPE:N/A PIREP-FUEL LEAKING FROM RH WING ***SUPPLEMENTAL MRR*** FOUND GAMA COUPLING LEAKING RT INBD WING REPAIRED COUPLINGDec 8, 2000 · N801UP · Doug DC873FSDR UPS00834536Coupling · leakingINSPECTION TYPE:N/A PIREP-FUEL LEAKING FROM RH WING ***SUPPLEMENTAL MRR*** FOUND GAMA COUPLING LEAKING RT INBD WING REPAIRED COUPLING NOTE: THIS WAS ON THE DAILY EXCP AGAINST 703 WHEN IT SHOULD HAVE BEE N TAIL 801 LOG PAGE ON THIS MRR IS ON 801 VOIDED THISDec 8, 2000 · N703UP · Doug DC871FSDR 20010130CW007Fuel Line · chafedNR1 INLET COWLING CHAFING FUEL INLET LINE, PN3017392, DUE TO INSTALLATION OF SHADIN FUEL FLOW, STC SE1123GL.Dec 7, 2000 · N63177 · Bell 412EPSDR CA001219005Pressure Switch · stuck(CAN) DEC 2,2000 EN ROUTE TO YWG FROM YOW. FL280, MINUS 48 DEGREES C. APPROXIMATELY 1800Z CREW NOTICED TORQUE DECREASE FROM 26.3 TO 24.5. WHILE ATTEMPTING TO RECOVER DECREASED TORQUE WITH PCL, TORQUE FURTHER DECREASED TO APPROXIMATELY 15.4. DURING ROLL BACK ENDec 6, 2000 · Pilats PC1245SDR CA001229017Computer · failed(CAN) DURING CENTRE TO MAIN FUEL TANK TRANSFER, R/H VALVE CLOSED AT 4450+/- 100 LBS, LEFT TANK FUELED TO 4900 LBS. COULD NOT BALANCE FUEL WEIGHT. RETURNED TO SLC.REPLACED FUEL SYSTEM COMPUTER IAW MM 28-41-26. OPS CHECK GOOD.Dec 2, 2000 · Cndair CL6002B19
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