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 AU510001653Vent Line · leakingRT FUEL VENT LEAKING. INVESTIGATION FOUND THAT THE SEALANT AROUND THE VENT TUBE IN THE RT WET WING FUEL TANK HAD DETERIORATED ALLOWING FUEL TO LEAK INTO THE VENT LINE.Dec 12, 2005 · Beech 58SDR AU510001608Line · crackedLINE LOCATED IN RT WING ROOT CRACKED. LIMITED INFORMATION PROVIDED.Dec 12, 2005 · Cessna 402CSDR AU510002175Line · damaged(AUS) FUEL PIPES LEAKING. FUEL WAS FOUND TO HAVE BEEN LEAKING FROM THE BLANKED T-FITTINGS THAT WERE INSTALLED IN THE FUEL SELECTOR TO FIREWALL SUPPLY LINE PN 11443-005 AND THE RETURN LINE PN 11444-005. ON REMOVAL THE FUEL LINES WERE FOUND TO HAVE VERY POOR/DADec 10, 2005 · Cirrus SR22SDR AALA20050802O-Ring · cutDFW - REPORTS OF SMOKE AND FUEL STREAMING OUT OF LEFT HAND ENGINE DURING LANDING, REVERSE, AND ROLL OUT. FUEL CONTINUED TO LEAK FOR 20 MINUTES AFTER ALL POWER REMOVED. FOUND LEFT HAND ENGINE FILTER BOWL LEAKING. O-RING CUT. REPLACED O-RING. SYSTEM GROUNDDec 5, 2005 · N513AA · Doug DC982SDR 2005FA0001620Tube · chafedWHILE RETRACTING AND EXTUENDING LANDING GEAR FOR ADJUSTMENT OF DROOPING IB MAIN WHEEL DOOR NOTED ABNORMAL NOISE AND VIBRATION DURING APPROXIAMTE MID-TRAVEL. INVESTIGATED FURTHER, FOUND RT MLG RETRACT ROD ASSY. CHAFING ON PN 002-920000-49 AND PN 002-920000-51Dec 2, 2005 · N200KH · Beech 58SDR CA051202006Line · chafedFUEL PIPE BETWEEN STAINER AND UNION WORN ALMOST THROUGH BY NOSE STEERING ROD. PART REPLACED WITH CLEARANCE TO ROD.Nov 28, 2005 · Cessna 172MSDR 2005FA0001585Line · leakingPILOT REPORTED FUEL LEAKING FROM THE IB WING ROOT AREA AFTER AIRCRAFT WAS FUELED. UPON INSPECTION, RUBBER FUEL HOSES AT WING ROOT WERE FOUND TO BE HARD, SPLIT LENGTHWISE AND LEAKING THROUGH WALL OF HOSE. (K)Nov 21, 2005 · N544SP · Cessna 172SSDR 2006FA0000011Valve · leakingPART WAS RECEIVED TO REPLACE EXISTING PART DUE TIME CHANGE. WHEN PART WAS INSTALLED, PART FUNCTIONED FINE. WHEN FUEL WAS INTRODUCED TO SYSTEM FOR LEAK CHECK, UNIT WAS FOUND TO NOT HOLD SEAL. THIS IS THE FIRST OF 2 VALVES FROM THE SAME FACILITY THAT HAVE LEANov 15, 2005SDR AU510001782Fuel Sys · faultyUNCOMMANDED INFLIGHT FUEL TRANSFER. INVESTIGATION COULD NOT FIND ANY MECHANICAL CAUSE FOR THE DEFECT.Nov 8, 2005 · Boeing 767338SDR CA051109003Check Valve · contaminated(CAN) WE HAVE RECEIVED A REPORT CONCERNING A PROBLEM WITH THE FUEL SYSTEM. THE FUEL CHECK VALVE P/N: 222-366-687-101 WAS FOUND COMING APART. THEY FOUND THAT THE NUT HAD COME OFF OF THE POPPET ASSEMBLY AND CONTAMINATING THE FUEL FILTER, THE FUEL PUMP AND THENov 7, 2005 · Bell 430SDR 11112005ATube · leakingDURING LINE CHECK AFTER STRUCTURAL INSPECTION FOUND FUEL LEAKING FROM RIGHT INBOARD DRY BAY DRAIN HOLE. FURTHER INSPECTION REVEALED TO BE A SMALL PIN HOLE IN THE RIGHT STANDBY FUEL PUMP WIRE CONDUIT (TUBE ASSEMBLY). REMOVED AND REPLACED RT STANDBY FUEL PUMP Nov 3, 2005 · N356CJ · Saab 340BSDR QXEA200501383O-Ring · leakingDEN - MAINTENANCE FOUND POSSIBLE FUEL LEAK AT BOTTOM OF AIRCRAFT FUSELAGE. REPLACED 2 O-RINGS AT THE REFUEL/DEFUEL HOUSING ADAPTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 21, 2005 · N601QX · Cndair CL6002C10SDR AALA20050653Valve · inoperativeORD - INFLIGHT DURING CLIMB RECEIVED FUEL INBALANCE EICAS MESSAGE. FUEL WAS 2500 POUNDS HEAVIER IN RIGHT HAND MAIN TANK. FUEL WAS THEN BALANCED. ON LANDING RIGHT HAND MAIN TANK SHOWED 1500 POUNDS LESS THAN LEFT HAND MAIN TANK. REPLACED RIGHT HAND MAIN TANKOct 5, 2005 · N354AA · Boeing 767323SDR UPS05145522Actuator · inoperativeFUEL IMBALANCE BETWEEN LT AND RT INNER TANKS. EMERGENCY DECLARED. R & R LT ISOLATION VALVE ACTUATOR IAW AMM 28-22-52-4. R&R'D LEFT ISOLATION VALVE PB SW. SYSTEM CKS GOOD.Sep 28, 2005 · N139UP · Airbus A300F4622RSDR CA050915005Fitting · loose(CAN) DURING SERVICING A STRONG ODOR OF JET FUEL WAS NOTICED IN THE AFT EQUIPMENT BAY. AFTER INVESTIGATION, THE TRANSFER FUEL LINE FROM THE TAIL TANK TO THE FUSELAGE AUXILIARY TANK WAS FOUND TO BE LEAKING. THE WIGGINS FITTING ON THE TRANSFER ROTOR BURST FUELSep 15, 2005 · Cndair CL604SDR QXEA200501248Warning Light · illuminatedPDX - ON FLIGHT 2507, DURING TAXI OUT, RECEIVED A AUTO CROSSFLOW INHIBIT CAUTION MESSAGE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET PER THE SERVICE LETTER 28-007C. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.Sep 15, 2005 · N615QX · Cndair CL6002C10SDR SIMA200525704Valve · brokenFUEL STREAMING FROM RIGHT WING. REPLACED RIGHT FUEL TANK OUTBOARD FLAPPER VALVE IAW 28-11-04. PERFORMED A FUNCTIONAL CHECK FLIGHT WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Sep 13, 2005 · N618AE · Emb EMB145LRSDR P5CA0501397Actuator · malfunctionedAFTER ENGINE START, NR 1 ENGINE RAN FOR APPROX 3 MINUTES THEN SHUT DOWN. REPLACED NR 1 ENGINE SPAR VALVE ACTUATOR, MM 28-22-01.Sep 8, 2005 · N858FT · Boeing 747123SDR 2005FA0001232Line · chafedMAIN FUEL SUPPLY LINE FROM FUEL SELECTOR TO FIREWALL HAD HOLE CHAFED IN IT. THE WIRE BUNDLE TO THE CB PANEL WAS CHAFING LINE. (K)Aug 19, 2005 · N2354B · Cirrus SR22SDR UPS05245526Fitting · leakingINSPECTION TYPE: C+SI, FUEL LEAK FROM UNDERNEATH LT LANDING GEAR FWD TRUNNION SUPPORT SITTING SEEMS TO BE COMING FROM LWR LARGE BOLTS. LWR I/B FASTENERS (X2) REMOVED IAW TRUNNION REMOVED AND CORROSION FOUND SRM 51-30-02 AND BOTH HOLES REAMED TO 1ST OVERSIZE Aug 17, 2005 · N922UP · Boeing 72731CSDR DXTA200500892Pipe · chafedMCC REQUEST TO INSPECT LINE ASSY, (REFUEL/DEFUEL FLOW) P/N 6516311-55 (IPC 28-22-00 ITEM #156) FOR CHAFING BY FLAP CROSS OVER CABLE. REMOVED PANELS 171BB AND 172BB FOR VISUAL ACCESS NR FOUND CHAFING IN ACCESS PNL 172BB ON SP FUELING LINE. MEASURED CHAFFING TAug 8, 2005 · N800QS · Cessna 560CESSNASDR DXTA200500891Pipe · chafedPERFORM VISUAL INSPECTION OF THE RT LINE ASSY P/N 6516311-19 (REFUEL/DEFUEL FLOW) FOR SIGNS OF CHAFFING BY FLAP CROSS OVER CABLE BEHIND PANEL 172BB. (CHAPT. 6 ACCESS PLATES AND PANELS INDENTIFICATION. CE-560E MM 6-20-02 FIG 2 PG 12 OF 14). GAINED ACCESS FOR IAug 8, 2005 · N825QS · Cessna 560CESSNASDR CQWR20005006Line · damagedDURING PHASE 1 THRU 5 INSPECTION, FOUND REFUEL/DEFUEL FLOW LINE ASSY (P/N 6516311-55) SAWED BY THE FORWARD FLAP CROSS-OVER CABLE. THIS LINE ASSY HAD BEEN DAMAGED MORE THAN 50 PERCENT OF THE WALL THICKNESS, AND IS LOCATED IN THE LEFT WING ROOT DRY BAY AREA FORAug 5, 2005 · N808Q · Cessna 560CESSNASDR PJM2005F00000Line · leakingINFLIGHT FIRE RESULTED FROM SMALL PIN HOLE IN FUEL PRESSURE LINE MOUNTED TO AFT FACE OF FIREWALL, SPRAYED FUEL ONTO BACK OF INSTRUMENTS IN PILOTS INSTRUMENT PANEL. UNABLE TO DETERMINE IGNITION SOURCE. AC MADE EMERG LANDING, FIRE WAS EXTINGUISHED WITH ONBOARDAug 5, 2005 · N6868B · Dhav DHC3SDR A6WA200540259Sensor · inoperativeRT FUEL HIGH LEVEL SENSOR INOPERATIVE PLACARD AND PLACED ON MEL. CODE ON COMPUTER SHOWS 140 (LT TANK HIGH LEVEL SENSOR). REMOVED AND REPLACED RT FUEL LEVEL SENSOR IAW AMM. OPS AND LEAK CHECK GOOD. (K)Jul 19, 2005 · N459AW · Cndair CL6002B19SDR CA050815002Line · corroded(CAN) DURING TROUBLESHOOTING, FOUND FUEL CROSS-FEED LINE ROUTED THROUGH RT DOOR POST WEEPING FUEL. PORTION OF LINE REMOVED AND UPON FURTHER EXAMINATION A PIN-HOLE CAUSED BY CORROSION WAS FOUND UNDER PLASTIC ANTI-CHAFE MATERIAL. SUSPECT CONDENSATION OVER MANY YJul 14, 2005 · Cessna A185FSDR P5CA0501375Line · leakingNR 2 ENGINE FUEL LEAK. REPLACED NR 2 ENGINE FUEL LINE (DRY BAY AREA). LEAK CHECK OK PER MM 28-22-00.Jul 11, 2005 · N858FT · Boeing 747123SDR CA050712007Line · brokenDURING INSPECTION OF THE LT WING TIP FUEL TANK THE INTERNAL FUEL DELIVERY LINE WAS FOUND TO BE BROKEN AT THE INBOARD BULKHEAD ATTACH POINT (TACKWELD). THIS CONDITION IF RETURNED TO SERVICE WOULD NOT ALLOW THE FULL CONTENTS OF THE WING TANK TO BE TRANSFERED TOJun 13, 2005 · Dhav DHC2*SDR 2005FA0000994Line · corrodedDURING ANNUAL INSPECTION FOUND FUEL STAINS ON CROSSFEED LINE UNDER CABIN FLOOR PANEL. FOUND CROSSFEED LINE CORRODED THROUGH. LINE WAS LEAKING AT A CORRODED AREA. THERE WAS NOTHING TOUCHING FUEL LINE. (GL21200502745) (K)Jun 9, 2005 · N98560 · Cessna 340ASDR DL76S050304Switch · burnedRIGHT FWD FUEL BOOST PUMP SWITCH REMOVED AND EVIDENCE OF BURNING NOTED AND PLASTIC MELTED. REPLACED SWITCH AND REPAIRED WIRING.Jun 3, 2005 · N132DN · Boeing 767332SDR CA050516010Fitting · mismanufactured(CAN) DURING INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE FWD ENGINE FIREWALL FITTINGDURING A LEAK/PRESSURE CHECK. UPON INVESTIGATION IT WAS DISCOVERED THAT THE FIREWALL FITTING HAD A FACTORY MANUFACTUINGDEFECT (SCORE MARK) THAT EXTENDED FROM THE HEX NUT PORTMay 13, 2005 · Airtrc AT802ASDR 2005FA0000711Fitting · crackedFUEL LINE FITTING CRACKED AT THE INLET TO THE FUEL PUMP. CRACK WAS LOCATED IN THE BEND RADIUS (45 DEGREE FITTING)OF A STRATOFLEX HOSE ASSEMBLY. FUEL WAS SPRAYING FROM THE FITTING AFT TOWARDS THE TURBO AND CAUSED AN ENGINE FIRE IN FLIGHT, LT ENGINE.May 12, 2005 · N975DC · Piper PA31SDR DJFA2005092Transfer Tube · malfunctionedCREW FOUND FUEL CROSSFEED NOT MAINTAINING A BALANCED CONDITION AS RT WING TANK CONTINUED TO DEPLETE. CROSSFEED SWITCHES CYCLED & CIRCUIT BREAKERS CHKD. REPORTED FUSELAGE FUEL NOT TRANSFERRING TO WING TANKS. ACFT PREVIOUSLY ISSUED MEL 28-2-2 FOR DISCREPANCY May 11, 2005 · N799TA · Beech 400ASDR CA050516007Tube · leaking(CAN) WHILE LANDING,ONE OF THE PASSENGERS IN THE CABIN NOTICED FLUID RUNNING DOWN THE RIGHT HAND SIDE OF THE AIRCRAFT. AFTER AIRCRAFT SHUT DOWN THE ENGINEER INSPECTEDTHE RIGHT HAND ENGINE AND FOUND A TUBE ASSY FROM THE MAIN FUEL SUPPLY LINE HADLOOSENED, CAUSINMay 10, 2005 · Carson S61LSKRSKYSDR CA050509003Line · cracked(CAN) PILOT REPORTED (TAIL TANK AUTO INHIBIT LIGHT ON) BEFORE DEPARTURE. UPON INVESTIGATION, A CRACK ON THE TAIL TANK PRESSURE FUEL LINE WAS FOUND. IPC 28-13-22 ITEM 115.May 9, 2005 · Cndair CL604SDR CA050503006Line · leaking(CAN) DURING PREFLIGHT CHECK, NOTICED FUEL SEEPING FROM LT FLEXIBLE FUEL TRANSFER HOSE LOCATED IN LT WHEEL WELL AREA. SEEPAGE APPEARS TO BE FROM HOSE MATERIAL AND NOT THE FITTING. HOSE ASSY WILL BE SENT TO MFG FOR INSPECTION. NEW HOSE WAS INSTALLED AND LEAKMay 2, 2005 · Lear 45LEARSDR P5CA0501345Line · leakingFUEL MIGRATING INTO NR 1 MAIN FUEL TANK. FOUND CROSS FEED LINE LEAKING AT FWD BULKHEAD COUPLING. RESEALED AND RETORQUED COUPLING OPS AND LEAK CK OK PER MM 28-22-07 AND 28-11-02.Apr 26, 2005 · N355MC · Boeing 747341SDR P5CA0501344Check Valve · malfunctionedDURING CROSS FEED FROM CENTER WING AND NR 2 AND NR 3 MAIN TANKS, ALL CROSS FEED VALVES OPEN AND NR 1 AND NR 4 TANKS BOOST PUMP OFF. NR 1 MAIN TANK QTY INCREASES 1000 KGS PER HOUR. REPLACED CHECK VALVE AT AFT BOOST PUMP NR 1. VERIFIED OPERATION OF DISCHARGE Apr 25, 2005 · N355MC · Boeing 747341SDR CA050422006Line · crackedDURING FUELING, FUEL BEGAN LEAKING ALMOST IMMEDIATELY, APPROX 300 LITRES IN TANK. UPON INVESTIGATION BY MAINTENANCE CREW, 2 INCH CRACK DISCOVERED IN FUEL INTECONNECT AT WELDED SEAM. NO SIGNS OF CORROSION. MAY HAVE BEEN CAUSED BY TRAPPED WATER, HOWEVER NO TApr 20, 2005 · Cndair CL2151A10SDR CA050417001Ejector · cracked(CAN) FUEL QUANTITY ON THE CENTER TANK INCREASES (SUSPECT FUEL LEAKAGE FROM LEFT MAINTANK). MX FOUND LEFT PRIMARY EJECTOR TO BE CRACKED. REMOVED AND REPLACED LEFT AND RIGHT EJECTORS IAW CRJ AMM 28020-01 AND S/B 670BA-28-027. PERFORMED OPS CHECK OF LEFT AND Apr 12, 2005 · Cndair CL6002C10SDR CA050418004Line · worn(CAN) DURING 200 HOURS INSPECTION, FUEL LINE ASSEMBLY FROM UNION TO FUEL STRAINER FOUND WORN (DAMAGED) BY NOSE STEERING PUSH/PULL ROD ASSY. NOTE: SAME DAMAGED FOUND PREVIOUSLY WHICH SDR WAS PRODUCED IN FEBRUARY 11, 2005. NEW FUEL LINE ASSY SUPPLY BY MFG SEEM Apr 11, 2005 · Cessna 172PSDR DXTA200500656Flapper Valve · leakingWING TANK O-FILL-R CAS MESSAGE ILLUMINATED IN FLIGHT. FUEL VENTED OVERBOARD, THEN STOPPED. CAS MESSAGE WENT OUT BUT CAME ON AGAIN SHORTLY THEREAFTER, CAS MESSAGE THEN WENT OUT. REMOVED FLAPPER VALVE DUE TO MALFUNCTION. INSTALLED NEW FLAPPER VALVE IAW CE750Apr 1, 2005 · N958QS · Cessna 750SDR 2005FA0000570Line · crackedFOUND FUEL BYPASS TUBE ASSY CRACKED WHERE TUBE WELDED TO FLARE END OF B-NUT FITTING. TUBE APPEARS TO BE MFG WITH SMALLER RADIUS TO FIT INSIDE FLARE, CAUSING WEAK POINT. SUGGEST CLOSER INSPECTION AT THIS AREA DURING ROUTINE INSPECTION AND PRESSURE CHECK WITH Mar 7, 2005 · N24AN · Emb EMB110P2SDR CA050314003Line · worn(CAN) DURING THE ACCOMPLISHMENT OF MFG SB 550-28-14 WING FUEL BOOST PUMP WIRING IMPROVEMENT, LINE ASSEMBLY P/N 6526355-37 FOUND DAMAGED, WHICH THE ELECTRIC FUEL PUMP HARNESS CUT THROUGH THE WALL OF TUBING. NO DAMAGED FOUND ON ELECTRICAL HARNESS.Mar 7, 2005 · Cessna 550SDR CA050223001Filter · open(CAN) ENGINE FLAME OUT ON LANDING, 200 POUNDS ON BOARD. SENT AME ON SITE CHECK FUEL SYSTEM. IN-LINE FUEL FILTER STUCK OPEN. CLEAN ALL FUEL SYSTEMS AND GROUND RUN IAW MM PROCEDURE. FLEW THE A/C BACK TO THE HANGAR AND CLEANED FUEL SYSTEMS AGAIN. CHECK FOR LOFeb 16, 2005 · Bell 206L1SDR CA050218005Line · chafed(CAN) DURING INSPECTION OF NOSE GEAR STEERING TUBE ASSEMBLY ON RT SIDE. THE MAIN FUEL LINE ASSEMBLY (UNION TO FUEL STRAINER) FOUND BADLY CHAFED THROUGH SIDEWALL OF L INE ASSEMBLY CAUSED BY POOR CLEARANCE BETWEEN FUEL LINE ASSEMBLY AND NOSE GEAR STEERING TUBE. Feb 14, 2005 · Cessna 172MSDR RAIA00502017Actuator · inoperativePIT - RIGHT FUEL SOV WILL NOT OPEN. MAINTENANCE REMOVED AND REPLACED RT FUEL SOV ACTUATOR.Feb 12, 2005 · N558HK · Jetair JETSTM4101SDR CA050213004Tube · worn(CAN) PRIOR TO TAKEOFF, ENGINE POWER REDUCED ACCOMPANIED BY AN INCREASE IN FUEL FLOW. THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED A DISLODGED FUEL MANIFOLD TUBE WITH A WORN RETAINING PLATE COLLAR.Feb 5, 2005 · Skrsky S76BSDR CA050207001Tube · corroded(CAN) INVESTIGATION OF A (FUEL SMELL IN THE CABIN) AND A MINOR EXTERNAL FUEL LEAK REVEALED THAT WELDED FUEL TUBE ASSY BETWEEN FUEL TANK AND FLEX HOSE TO THE WING STRUT WAS LEAKING. REMOVAL OF ADEL CLAMP REVEALED CORROSION PITS UNDERNEATH WITH ASSOCIATED FUEL Feb 5, 2005 · Dhav DHC6100SDR 2005FA0000300Line · chafedWHILE PERFORMING AN ANNUAL INSPECTION IN THE CABIN SUBFLOOR AREAS, NOTED A FUEL LEAK AT THE PORT 90 DEGREE RIDGID FUEL LINE LINKING THE WING TANK, VIA THE PORT DOOR PILLAR, TO SUBFLOOR LINE THAT CONNECTS TO THE SELECTOR VALVE. IT WAS INSTALLED BACKWARD. THIS Jan 30, 2005 · Cessna 206CESSNA
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