JASC 2897
Service difficulty reports · 656
Reports filed under 2897 · Fuel System Wiring, 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 = '2897' 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 = '2897' 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 UALA2011110906101Receptacle · dirtyLEFT MAIN FUEL QTY BLANK AT LAX. TROUBLESHOOTING NEW FUEL QTY PROCESSOR, NO HELP. NEW FUEL QTY PROCESSOR INSTALLED BY MECHANIC. NO HELP. PROCESSOR SHOWS PRESENT FAULTS (LM HI Z SHIELD OPEN AT SPAR G01). ACP TROUBLESHOOTING PER MM. RANG OUT WIRES FROM FUESDR UALA2011101705623Circuit Breaker · faultedFUEL CROSSFEED LIGHT REMAINED ON WHEN OPEN-CLOSE SELECTED. RESET BREAKER AND RECONNECTED CONNECTOR TO AFT FUEL CROSSFEED ACTUATOR, AFT FUEL CROSSFEED CHECKED OKAY PER MM.SDR UALA2011092605188Circuit Breaker · trippedACFT WILL NOT TAKE FUEL, FOUND C-B OUT A9 FUELING VALVES ON THE P34 PANEL MAIN E&E BAY. FLT DECK. P6-1 PANEL C-B E6 FOR FUELING VALVES POPPED.SDR 3PRA201109070001Switch · burnedWHILE PERFORMING "BEFORE START" CHECKS WITH GPU CONNECTED AND POWERING SYS, A HEAVY ELECTRICAL BURNING ODOR AND SMOKE CAME FROM OVERHEAD ELECTRICAL PANEL. CREW THEN SHUTDOWN SYSTEMS IAW COMPANY SOP'S AND ALERTED MX. MX FOUND RT AUXILLIARY FUEL PUMP QA8 SWITCSDR CA110901003Conduit · damaged(CAN) LT FUEL BOOST PUMP CONDUIT FOUND LEAKING AND FOUND TO HAVE A PIN HOLE THROUGH THE CONDUIT ALLOWING FUEL TO RUN INSIDE THE CONDUIT, IPC REF 28-20-00-01 ITEM 15B.SDR FDEA201108243457Connector · inoperativeTANK 2 RAFT PUMP INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 28-22-01-02-A. REMOVED PUMP AND FOUND ELECTRICAL CONNECTOR R5-1103 BURNED AND PINS BURNED OFF THE PUMP. REMOVED NR 2 RT/AFT BOOST PUMP HARNESS, BOOST PUMP AND CAP. OPS CHECKED GOOD, LEAK CHECKED GOSDR IXXA1100520Wire Harness · damagedDURING CLIMBOUT, NR 3 MAIN TANK BOOST PUMP C/B`S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MASDR IXXA110052OWire Harness · damagedDURING CLIMB OUT, NR 3 MAIN TANK BOOST PUMP C/B'S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTUE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MASDR UALA2011070703364Wire · chafedWHEN FUELING BOTH DC FUEL CONTROL AND FUEL PANEL CB POPPED. RESET AND POPPED WHEN FUEL DOOR OPENED. REMOVED FUELING PANEL AND REPAIRED CHAFING WIRING BEHIND PANEL. REINSTALLED AND OPS CHECK GOOD.SDR QMLA2011070711073Bonding Strap · brokenARRIVED AT HELICOPTER, THE FUEL QUANTITY INDICATION WENT FROM 50 PERCENT TO 0 PERCENT. AN UNUSUAL ODOR FOLLOWED DURING FLIGHT. TROUBLESHOT SYS, FOUND WITH A/C ELECTRIC POWER ON, AND BOOST PUMPS ON. FLUCTUATING FUEL INDICATION, LOW FUEL PRESSURE, AND INOP FUSDR CA110628009Connector · burnedDURING TROUBLESHOOTING FOR LOW VOLTAGE AT LT AUX FUEL PUMP (15VDC), FOUND SPDA2 CONNECTOR P4, PIN H BURNED ON BOTH CONNECTORS (SPDA AND CONNECTOR SOCKET). SPDA AND DAMAGED CONNECTORS PIN AND SOCKET WERE REPLACED. NOTE: FOUND REDISH BROWN DEPOSITS ON PUMP CONSDR CA110527006Wire · damagedDURING A TRAINING FLIGHT, A PUMP 1 FORWARD PRESSURE AMBER (CAUTION LEVEL) CAS MESSAGE APPEARED. SUBSEQUENT INVESTIGATION BY MX REVEALED EVIDENCE OF ELECTRICAL ARCING AND BURNING IN THE FUEL GALLERY. THE WIRE LEADING FROM THE RF (RADIO FREQUENCY) FILTER ON THESDR A8JA20110504001Connector · dirtyACFT DEPARTED. WHILE CLIMBING THROUGH, CREW NOTED AN AMBER CAS MESSAGE OF "RT FUEL BOOST". THIS INDICATES A LOW FUEL PRESSURE DETECTION AND ALERTS THE CREW THAT THE BOOST PUMP WAS AUTOMATICALLY ACTIVATED. THE CREW PERFORMED THE ACTIONS FROM THE EMERGENCY CHSDR UALA2011040101572Wire Harness · faultyFWD LAV TANK GAUGE READS FULL WHEN EMPTY. CHECKED J3 CABLE FOR CONTINUITY, CABLE CHECKS GOOD. CHECKED AUTO ZERO ADJUSTMENT, NO HELP. PERFORMED TROUBLESHOOTING PER AMM, FOUND LCM SENSOR INDICATOR LIGHT ON FOR CONTINUOUS LEVEL SENSOR J3. ATTEMPTED TO RESET, NSDR CA110408004Wire · damaged(CAN) LEFT OUTER TANK BOOST PUMP 1 & 2 INDICATE LOW PRESS & LT INNER TANK BOOST PUMP NR 2 INDICATES LOW PRESS. FOUND WIRING DAMAGED IN LT WW JUST ON TOP OF GREEN HYD HP MANIFOLD AT FEED THROUGH NR 31VP, 6 WIRES FOUND DAMAGED & SHORTED & CUT AT SPLICE 116VS & SDR UALA2011031401230Wire Harness · chafedFUELER REPORTS WIRE BUNDLE CHAFING IN SIDE FUEL PANEL DOOR, FWD SIDE. FOUND WIRE W1500-0068-20 WORN THRU INSULATION. NO STRANDS OF WIRE BROKEN. REPAIRED WIRE PER SWPM. OPS CHECKED GOOD.SDR MYWA110032Connector · unsecureETOPS SIGNIFICANT SYSTEM: CENTER RIGHT FUEL LOW PRESSURE LIGHT DOESN'T ILLUMINATE WHEN LOW OR NO PRESSURE. FOUND RT CTR FUEL LOW PRESSURE SWITCH CONNECTOR NOT FULLY SECURED. RE-SECURED CONNECTOR IAW AMM 28-42-11, OPS CHECK OK.SDR UALA2011030401056Wire · brokenFUELER REPORTS THAT AUTO PRERELT DOES NOT WORK. FOUND WIRE OPEN BETWEEN D40324J -PIN 22 OF FUELING PANEL DISCONNECT P28 AND D2440A -PIN D8 OF M121 FUEL QTY PRO UNIT. ISOLATED PROBLEM TO BETWEEN D40328P-PIN 22 AND D42344P-PIN 22. FOUND WIRE W3484-4002Y-18 BRSDR HALA2011021700103Wire Harness · damagedETOPS SIGNIFICANT SYS - DUE TO HISTORY OF LT FUEL QUANITITY BLANKING/ TOTALIZER. REPLACE LT FUEL TANK WIRING HARNESS. R & R LT WING QTY HARNESS IAW AMM 28-41-09 THRU STEP E29, THRU STEP E33. ALL WING PANELS LEAK CHECKED ON ITEM 39, LOG PAGE 384767 COMPLETED SDR 2011FA0000123Connector · burnedPREFLIGHT FOUND RT BOOST PUMP INOP. TROUBLESHOOTING FOUND WIRE CONNECTORS AND TERMINAL BLOCK AT TB-AA IN DA PANEL OVERHEATED AND BURNED DUE TO IMPROPER TORQUE OF NUTS ON TERMINAL STUDS REQUIRING REPLACEMENT OF TERMINAL BLOCK AA, AND WIRES FROM AA1L AND AA2L TOSDR UALA2011021400762Connector · dirtyRT ENG SPAR VALVE ON, STAYED ON, ENG STARTED THEN FLAMED OUT. CYCLED ACTUATOR, CKD GROUND IAW MM. CLEANED CONNECTOR, STARTED NORMAL 2 TIMES AT GATE.SDR 2011FA0000134Connector · damagedDURING FUEL TANK INSPECTIONS, FINDING ELECTRICAL BLANKING PINS IN WING ROOT OF FUEL TANKS. PINS FALLING OUT OF PLUGS PREVIOUSLY INSTALLED DURING ACFT MFG.SDR UALA2011012800488Wire · shortedGROUND TEST MESSAGE REPORT SHOWS TANK WIRING-MAIN 3, PROBE 4, SHORT LO-Z GROUND. REMOVED NR 4 PROBE FROM NR 3 MAIN F138. REPLACED 3 MAIN TANK UNIT F138. REMOVED FUEL PLATE 645AB. INSTALLED 3 MAIN FUEL PLATE 645AB, CLEARED AND CLOSED.SDR MASA2011012201763Harness · faultyRT FUEL LOW PRESS CAUTION IN FLT. MX REPLACED THE VIOLET HARNESS.SDR 2011FA0000090Connector · damagedWHILE PERFORMING THE 2B INTERNAL WING INSP, FOUND THAT THE LT AND RT ELECTRICAL CONNECTOR BLANKING PINS WERE FALLING OUT BECOMING FOD IN THE CTR FUEL TANK. CONNECOTRS ARE LOCATED IN FUEL ACCESS PANELS 175AB AND 176AB, ON THE FWD WALL.SDR 2011FA0000089Connector · damagedWHILE PERFORMING THE 2B INTERNAL WING INSP, FOUND THAT THE LT & RT ELECTRICAL CONNECTOR BLANKING PINS WERE FALLING OUT, BECOMING FOD IN THE CTR FUEL TANK. CONNECTORS ARE LOCATED IN THE FUEL BAYS OF PANEL 175AB AND 176AB, ON THE FWD WALL.SDR UALA2010123004776Connector · looseRT AFT FUEL PUMP EICAS. REPLACED RT AFT BOOST PUMP CO NTROL RELAY K28242 AND RT AFT BOOST PUMP OVERHEAD SWITCH ASSY, NO HELP.SUSPECT PUMP BAD. REPLACED MAIN FUEL TANK ENGINE FUEL BOOST PUMP MOTOR ASSY, NO HELP. SECURED WD28-22-22. RANG WIRES FROM BOOST PUMP CSDR HALA2010121600588Wire Harness · damagedON CLIMB OUT, RT FUEL QUANTITY INDICATOR AND TOTALIZER WENT BLANK INTERMITTENT. FUEL CONFIG EICAS MESSAGE ILLUMINATED. DE-CLAMPED RT/MAIN TANK HARNESS, INSTALLED RT/MAIN TANK HARNESS FROM HI-Z/LO-Z REC TO PROBES 3,4,5. IAW AMM 28-41-09. INSTALLED HI-Z/LO-Z HASDR HALA2010121400584Wire Harness · damagedETOPS SIGNIFICANT SYSTEM - ON CLIMBOUT RIGHT FUEL QTY INDICATOR AND TOTALIZER WENT BLANK - INTERMITTENT FUEL CONFIG EICAS MESSAGE ILLUMINATED 2. DURING FUEL DUMP "FWD EQUIPMENT COOLING" EICAS AND NO COOLING LIGHT ILLUMINATED. DECLAMPED RT MAIN TANK HARNESS,SDR IPXA10563461Switch · corrodedINSP TYPE:C4, RT WING FUELING CONTROL PANEL SWITCHES HAVE CORROSION. R & R FUELING CONTROL PANEL SWITCHES IAW SRM 20-50-01, AMM 28-41-06-4, AMM 28-41-07-17.SDR UALA2010092003496Connector · damagedFUEL OVERBURN. FLIGHT DIVERTED. NOT ABLE TO CHECK NR1 HYD QTY DUE TO NO INDICATION IN COCKPIT AND AT WHEEL WELL GAUGE. CONNECTOR DT401 REMOVED FROM TRANSMITTER AND SECURED. WIRE W4514-234-20B PIN 3 REMOVED FROM CONNECTOR DT401 AND SECURED WITH BACKSHELL. CONNSDR KNNA251092010KACYWire · brokenAFTER PUSHBACK / DURING ENGING START NR 2 ENGINE STARTED / WHILE STARTING NR 1 ENGINE - NR 2 ENGINE FLAMED OUT. TROUBLESHOT TO A BROKEN WIRE (WDM: 28-21-01 WIRE NR: 388-010-20) ON THE ENGINE FUEL SHUTOFF VALVE AT CANNON PLUG (D790 - PIN: A) REPAIRED REF: (BOSDR UALA2010083103215Wire · damagedBOOSTER PUMP LOW PRESS LIGHT-ON-,SWITCH-ON-,EICAS MESSAGE L-R,FWD-A FT, FUEL PUMP DISPLAYED. POSITION 5 (5=L FWD, 6=L AFT, 9=R FWD, 10=R AFT). CIRCUIT BREAKER POPPED. FOUND SUFFICIENT SLACK IN HARNESS TO RETERMINATE CONDUCTORS BEFORE DAMAGED AREA. RETERMINSDR CA100830006Wire · damagedFUEL CAP ATTACH CHAIN BECAME DISCONNECTED FROM THE TAB ON THE FILLER NECK ALLOWING THE LOOSE END TO FALL INTO THE TANK STILL ATTACHED TO THE CAP. THE LOOSE END OF THE CHAIN WRAPPED AROUND THE FINE WIRE ON THE FUEL SENDING UNIT. THIS CAUSED THE WIRE TO BECOME SDR CA100723005Bonding Jumper · damagedDISCARDED THE FUEL TANK FUEL QTY GAUGING WIRING HARNESS WITHOUT KYNAR SLEEVING (108 MOS FSL INSP), FOUND A BONDING JUMPER DAMAGED AT LT WING (YW 202.000) BY SIGNIFICANT ARCING TO THE FUEL WIRING CONDUIT. JUMPER BRAID HAS BROKEN DOWN, BRITTLE AND FRAYED, THERSDR UALA2010062102167Wire Harness · faultedFUEL QTY IND EICAS. FLIGHT DIVERTED. REPLACED NR 4 CTR TANK FUEL PROBE & FILL VALVE. HIT AGAIN 1ST FLT. REMOVED BULKHEAD PANELS INSIDE CTR TANK 3EA, REPLACE SECTION OF HARNESS FOR NR 1 PROBE, REINSTALLED BULKHEAD PANELS. REPLACED LT CTR TANK HARNESS IAW MM. SDR UALA2010052601818Wire Harness · faultyFQIS. NR 4 FUEL TANK GAUGE WENT BLANK IN FLIGHT. TROUBLESHOOTING FUEL SYS, WILL RPLC 7EA PROBES & HARNESS IN NR 4 RT MAIN TANK. HARNESS ON HAND, 1EA PROBE ON T2350 FRM ORD TANK IS OPENED, VENTING & PREP FOR TANK ENTRY. REPLACED PROBES AND WIRE HARNESS.SDR AALA20100524TUL09Wire Harness · defectiveBNA - INFLIGHT DFW-BWI - CREW REPORTED DURING CRUISE CENTER TANK FUEL PUMP CIRCUIT BREAKER POPPED AND FUEL WOULD NOT TRANSFER FROM CENTER TANK. FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FORWARD CENTER BOOST PUMP HARSDR HALA2010042500185Wire Harness · damagedETOPS SIGNIFICANT SYS - BTB - AFTER ENGINES START RECEIVED EICAS STATUS MSG. FUEL QTY IND AND LOST LT FUEL QTY INDICATION ON LT QTY GAUGE & TOTALIZER. PERFORMED FIM 28-41-00, FIG110 BITE CHECK FQIS FOUND C4 FAULT ACCOMPLISHED FIM 28-41-00/101 TABLE 106 FROMSDR ASAA1057663Wire · chafedC/B SPAR VALVE ENG 2 POPPED. FOUND WIRE W8222 6011 18 CHAFED AND ARCING TO HYD LINE BELOW 'B' SYS EMDP. SPLICED WIRE REF SWPM 20 30 12 & WDM 28 21 11. NR 2 ENG FUEL SPAR VALVE GROUND VERIFICATION SUCCESSFUL REF M/M 28 22 00. P5 2 MODULE OPS NORMAL REF M/M SDR UALA2010022200642Wire · damagedFOUND FUELING CONTROL C/B C1041 P34 L3, POPPED WILL NOT RESET WITH FUELING PANEL DOOR OPEN, WITH K179 REMOVED C/B STAYS IN. ISOLATED FUEL PANEL, M586 CARD, K356,C/B C94 OPEN, NO HELP. FOUND WIRE W427-18-18 WORN THRU SHIELD, WIRES W472-014-20 AND 019-20 WITH SDR 2010FA0000094Connector · loosePILOT REPORTED THAT FLAPS WOULD NOT EXTEND. CONNECTED EXTERNAL POWER AND FOUND THAT FLAPS WORKED PROPERLY. ON POST INSPECTION RUN UP FOUND THAT FUEL BOOST PUMP WOULD NOT OPERATE AND BEACON WOULD NOT FLASH. FOUND THAT THE ABOVE COMPONENTS WERE ON THE SAME ELSDR FDEA201001010002Wire Harness · shortedHAD A TANK 2L AFT PUMP LO ALERT, LEVEL 1 AFTER TAKE OFF FOR ENTIRE FLIGHT. CIRCUIT BREAKER WAS POPPED. FOLLOWED QRH AND KEPT CB OUT. WIRES RUNNING UNDER FLOOR PANELS SHOW SHORT. DISCOVERED DAMAGED AND MELTED WIRE HARNESS UNDER FLOOR PANEL 272CF. ROUTED NESDR MYWA09072Connector · dirtyETOPS SIGNIFICANT SYSTEM - NR 2 FUEL GAUGE AT SINGLE POINT REFUELING PANEL READING 1500 KIL LESS THAN FLIGHT DECK GAUGE.SDR UALA2009121603898Connector · unsecureLT AFT BOOST PUMP LOW PRESS LIGHT ON, EICAS MSG L AFT FUEL PUMP DISPLAYED. LT AFT BOOST PUMP CB (C366) TRIP AT P6 PANEL. FOUND PIN 1 AT CONNECTOR D1746 SHORTED TO GND OR SHIELD GND WITH CONNECTOR D41704P DISCONNECTED AT P33 PANEL POSITION 24. CONNECTOR D4170SDR CA091102008Wire Harness · failed(CAN) FUEL QTY INDICATION REPORTED AS UNDER-READING. TROUBLESHOOTING DETERMINED A FAILED WIRING HARNESS ASSY IN THE WET WING TANK. THIS IS THE THIRD FAILURE OF THIS HARNESS ON 2 COMPANY ACFT, IN EITHER LT OR RT WINGS. INSTALLING A NEW HARNESS HAS RECITIFED THESDR UALA2009102903382Connector · corrodedLT MAIN FQIS CONNECTOR M1944 ASSY IS CORRODED. INSTALLED NEW FQIS CONNECTOR M1944. OPS CHECKS GOOD. REF FUEL BITE.SDR UALA2009101903254Connector · corrodedLEFT MAIN FUEL QUANTITY CONNECTOR M1944 BADLY CORRODED AT BACKSHELL. REMOVED AND REPLACED M1944 FQIS CONNECTOR BACKSHELL PER MFG CINCH SB CN1156-28-02. LOOP RESISTANCE CHECKS GOOD PER MM 20-55-54 AND FUEL QTY BITE CHECK GOOD.SDR CA091021012Wire Harness · chafed(CAN) DURING TROUBLESHOOTING CONCERNING A FAULTY LT AUX PUMP INDICATION. IT WAS FOUND THAT A WIRING BUNDLE WAS CHAFFED. DURING MAINTENANCE FUNCTION CHECKS OF THE SYSTEM THE WIRE BUNDLE BEGAN TO ARC AND BURN. THIS CAUSED AN IGNITION OF THE VAPORS FROM LPS CONTASDR UALA2009101203212Wire Harness · failedRIGHT FUEL QTY INDICATION ISSUE. REMOVED HARNESS FROM RIB 30 TO RIB 18. REMOVED HARNESS FROM INBOARD TO PYLON. INSTALLED SUMMING PLUGS AND SEALED AT 1900 WITH B1-2. STARTED TO ROUTE HARNESS FROM PLUGS INBOARD AND OUTBOARD. NEED TO BE SECURED. SECURED WIR
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