JASC 2497
Service difficulty reports · 2,202
Reports filed under 2497 · Electrical Power 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 = '2497' 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 = '2497' 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 UALA2011110405996Wire · damagedGEN 2 FAULT DISPLAYED ON UPPER ECAM. NR 2 ENG IDG WILL NOT COME ONLINE UNTIL MANUALLY SELECTED, ALL PARAMETERS NORMAL AFTER SELECTION. RMV'D NR 2 ENG IDG. REMOVED MR24212-40978. BREAKERS T27 AND T25 PULLED AND COLLARED. RPLC'D IDG AGAIN, STILL NO HELP. FOSDR CA111104009Wire · chafed(CAN) SMOKE ODOR OBSERVED IN THE FLIGHT COMPARTMENT DURING MX VISIT. DURING TROUBLESHOOTING, FOUND SMOKE COMING OUT FROM TROM PANEL BEHIND F/O`S SEAT WHEN OBSERVERS LIGHT SWITCH TURNED "ON". UPON REMOVING TRIM PANEL FOUND WIRE 3316-2A22-2 CHAFING TO FRAME SDR HALA2011102500492Connector · dirtyETOPS SIGNIFICANT SYS - RT ENG IDG VALVE CB POOPED IN FLT (M31). INSPECTED RT IDG VALVE WIRING, CLEANED CONNECTOR TO IDG VALVE. T/S IAW FIM 24-20-00. RESET C/B, RAN ENGINE OPS CHECKED GOOD. OK FOR SERVICE.SDR YENA20111024373Wire · chafedFLT 787 JFK-SXM, AIR TURNBACK DUE TO MULTIPLE CIRCUIT BREAKER / RELAY CYCLES (HEARD AUDIBLY) FOLLOWED BY MULTIPLE ECAM WARNINGS. AUTOMATION FAILURES AND LOSS OF CAPT AND F/O PFD AND ND. ALL SYSTEMS RESTORED AFTER RELAYS STOPPED CYCLING. FOUND WIRE INSULATIOSDR CA111021007Wire · shorted(CAN) DURING TAXI OUT, THE CREW NOTICED A STRONG BURNING ODOR IN THE CABIN AND COCKPIT. THE CREW ELECTED TO STOP IN THE CENTRAL DEICE FACILITY AND EVACUATE THE ACFT. DURING MX T/S THE FOLLOWING ADDITIONAL DEFECTS WERE NOTED: THE NR 2 CARGO SMOKE DETECTOR FAISDR HNAA2011102700340Connector · dirtyRIGHT AC BUSS CAUTION LIGHT ILLUMINATED ALONG WITH STALL WARNING AND RT TRU CAUTION LIGHT. CHECKED NR 2 ENGINE BRUSH BLOCK AND CLEANED. CHECKED WIRING IN NR 2 NACELLE AND CLEANED CONNECTOR ON AC GENERATOR. CHECKED AC CONTACTOR BOX. NO DEFECTS NOTED. RAN ASDR UALA2011100305326Terminal Block · damagedTERMINAL BLOCK 7200 VT NR 11 ABOVE G4 GALLEY HAS THE THREADED STUD PULLED OUT OF THE BLOCK AND THE BLOCK IS BURNED. REPLACED BLOCK & TERMINALS ON BLOCK NR 11. OPS CHECKED SYSTEMS PER AWM 25-33-04 AND ESPM 20-44-51. OVEN R41 INOPERATIVE AND DEFERRED DF0960. SDR HNAA2011100700322Terminal · burnedHOT ELECTRIC ODOR IN COCKPIT. POWERED DOWN ACFT. ODOR REDUCED. R & R APU GEN CABLE FROM 2445-K62 TO 2442-TB1 AND TERMINAL STUD 2445-TB1. OPS CHECKED GOOD.SDR FDEA201109234075Connector · failedABORTED TAKE OFF DUE TO GENERATOR FAULT, NOTICED IDG NR 2 FAULT LIGHT FLICKERING. DISCONNECTED NR 2 IDG. R & R CONNECTOR DG13B IAW CMM 71-51-00. SECURED WIRING AND RETAPED. RAN NR 2 ENGINE REF JRH AT T/O POWER; NO FLICKERING LIGHT. OPS CHECKED NORMAL.SDR 2011FA0000659Wire · burnedDURING TAXI AFTER LANDING, PILOTS REPORTED ELECTRICAL ODOR, UPON INVESTGATING FOUND WIRE TERMINAL LUG IN THE RT POWER J BOX ON THE RT GEN ERATOR BUSS TO BE LOSS AND BURN. REPLACED WITH NEW WIRE ASSY AND HARDWARE SUPPLY FROM MFG.SDR UALA2011092105097Wire · shortedR GENERATOR DRIVE LIGHT ILLUMINATED. DISCONNECTED RIGHT ENGINE GEN PER FLT MANUAL. SEE PREVIOUS HIST. SAMC TEXT: R-GEN DRIVE EICAS ADV MSG AND RT 'DRIVE' AMBER LIGHT ILLUMINATED ON OVERHEAD PANEL. FOUND WIRES W3538-003-18 AND W3538-004-18 SHORTING TO BACKSSDR CALA2011090600574Connector · damagedON TAKEOFF AT 40 KTS, LEFT AC BUS OFF, BUSTIE, L GEN CTL ILLUMINATED. CAPTAINS INSTRUMENT FAILED, EQUIPMENT COOLING OVERHEAT ALARM SOUNDED. REJECTED TAKEOFF. REF N/R 4486695 AND 4486716. RAN ENGS, TRANSFER BUS. NO FAULTS NOTED.SDR CA110909010Connector · shorted(CAN) FLIGHT CONTROL MALFUNCTION INCIDENT DETAILS: DURING THE ILS APPROACH FOR RUNWAY, SELECTED FLAP AT 3 AND RECEIVED 2 ECAM MESSAGES "F/CTRL FLAPS FAULT" AND "F/CTRL FLAP SENSOR" WITH FLAPS INDICATING AMBER. RECYCLED FLAP LEVER IAW ECAM, NIL FIX. FLAPS LOSDR CA110829002Buss Bar · loose(CAN) IN FLIGHT, CBP2-L8 DC 2 FEED CIRCUIT BREAKER TRIPPED. BURNED ODOR AND FUMES REPORTED. ACFT LANDED AS SCHEDULED. MX FOUND TWO BURNED BUSS BARS CONNECTED TO CBP2-L8 DC 2 FEED DUE TO A LOOSE SCREW.SDR CA110826007Power Cable · damaged(CAN) COMPLETION INSTALLED, INTERIOR IN BAGGAGE BAY HAD A UPPER INTERCOSTAL INSTALLED THAT IS USED TO SUPPORT BAGGAGE BAY HEADLINER GROSS POINT PANELING. THE INTERCOSTAL INSTALLED WAS FOUND WITH EXCESSIVELY LONG SCREW/BOLT AND THIS WAS CHAFING INTO THE GENERATSDR CA110829016Circuit Breaker · burned(CAN) THE UNDER WIRE OF THE SKEET HOSE WORE THROUGH AND CAME INTO CONTACT WITH THE UNDERSIDE OF THE RT ESSENTIAL BUS CIRCUIT BREAKERS AND CAUSED SMOKE IN COCKPIT WHEN PLANE WAS LANDING - PLANE LANDED WITHOUT INCIDENT.SDR ASOA201101499Wire Harness · arcedWHILE COMPLYING WITH REO 601R-24-60-002 , FOUND ON MAIN WIRE BUNDLE TO CB PANEL WIRE DAMAGED BY ARCING AND BURNING. R & R WIRES IAW AMM 24-31-01. OPS CHECKED IAW AMM 24-31-01.SDR CA110802004Relay · failedRELAY FAILED CAUSING TORQUE DROP BY 35 PERCENT AND CAUSED PILOT TO ABORT TAKEOFF - PART REPLACED AND ACFT RETURNED TO SERVICE.SDR IPXA1M68335Wire · damagedEMERGENCY DECLARED - RECEIVED LEVEL 3 CABIN SMOKE, LEVEL 2 SEL FADEC OFF AND SEVERAL LEVEL 1 ALERTS. SMOKE IN THE COCKPIT. ACFT OUT OF SERVICE. INSPECTION FOUND THE WIRES DAMAGED ABOVE R1 DOOR DROP CEILING PANEL. REPAIR OF THOSE WIRES C/O. COMPLIED WITSDR DXTA2011072604673Circuit Card · burnedAFTER TAKEOFF, NOTICED A VERY SLIGHT ELECTRICAL SMOKE ODOR. AFTER CLIMBING THROUGH 24000', ODOR STRONGER & "LT & RT ICE DETECT FAIL" EICAS CAUTIONS CAME ON SIMULTANEOUSLY. LIGHTS ON FOR ABOUT 30 SECS & THEN DISSAPPEARED. ANNUCIATORS APPEARED ABOUT 30 SECS SDR CA100722001Wire · damaged(CAN) CUSTOMER CALLED WITH ELECTRICAL SYSTEM FAIL/ELECTRICAL SYSTEM FAULT. CAIMS REPORTING SPDA1 RX EMSCDU2 FAULT. FOUND WIRING TO SPDA NR 1 HEAT DAMAGED. FOUND TRU 2 FEED WIRE TO THE DCPC IS THE ROUTE CAUSE OF DAMAGE. CABLE PB189A4 HAD COME LOOSE FROM THE FSDR CA110715002Wire Harness · faulted"APU RELAY ENGAGED" LIGHT CAME ON AND STAYED ON ANYTIME THE APU MASTER SWITCH WAS SELECTED ON. THIS LIGHT IS SUPPOSED TO INDICATE TO THE CREW ANY TIME EITHER THE APU STARTER OR GENERATOR RELAYS HAVE BEEN ACTIVATED. WITH THIS FAILURE, IT WAS NOT POSSIBLE TO VSDR UALA2011071303531Connector · damagedNR 2 ENG IDG INBOARD BACKSHELL (DM24001A) LOOSE. SECURED LOOSE BACKSHELL.SDR KY7A17733Wire · burnedENROUTE, PILOT BECAME AWARE OF SMOKE FROM AROUND RT SIDE CB PANEL AND IN CABIN. PILOT DECLARED EMERGENCY AND LANDED. ACFT WAS INSPECTED AND FERRIED WITH NO ISSUES. UPON INSPECTION AND TEST: FWD COAT CLOSET DIRECTLY BEHIND COPILOTS SEAT EVAPORATOR SHROUD WASDR CA110711015Circuit Breaker · inoperativeCIRCUIT BREAKER WON`T RESET.SDR CA110627020Ground Stud · meltedON JUNE 25TH, LATE EVENING, DURING ENGINE START, RT ENGINE WOULD NOT START. DISCOVERED THAT A GROUND STUD HAS MELTED & CAUSED A HOLE APPROX DIA .900", IN RT NACELLE FRAME PN 215T16511-15 (REF. IPC 54-10-00 P016-17 F004 ITEM 600). THIS GROUND STUD IS THE RT GENSDR QXEA2011062700466Wire · chafedFAA REPORT CHAFED WIRE NR 1 NACELLE NEAR A/C CONTACTOR BOX. CHAFE IS LOCATED 8" FROM PLUG J2 OF A/C CONTACTOR BOX, PHASE 'C' WIRE. C/W TEMPORARY REPAIR OF CHAFED WIRE IAW R/D 8/4-24-011. PLACED ON DMI FOR PERMANENT REPAIR. RETURNED TO SERVICE.SDR UALA2011061702981Control Unit · inoperativeGALLEY POWER COACH INOPERATIVE FEEDER 2 NO POWER. REPLACED M227 PER MM. AFT GALLEY POWER CHECKS GOOD FOLLOWING TRANSFER.SDR CA110701001Relay · wrong partAFTER STARTING THE NR2 ENGINE, ELECTRICAL SMOKE FUMES DETECTED IN THE COCKPIT. SMOKE CONTINUED TO BUILD. ELECTRICAL FIRE SUSPECTED. THE CREW SHUTDOWN ACFT POWER AND ENGINES. DC BATTERY DISCONNECTED. AFTER SHUTDOWN SMOKE STOPPED. CREW INVESTIGATED SOURCE ASDR 2011FA0000369Buss Bar · crackedON DOING A COMPRESSOR/POWER RECOVERY WASH AT MAINTENANCE SHOP. THE GPU PLUG, GROUNDING SHUNT BURNED AND BROKEN IN HALF. THIS IS THE SECOND TIME THIS HAS HAPPENED. THERE IS NO LIMITAION ON GPU USE.SDR UALA2011061302882Wire · brokenAFTER T-S FOUND BROKEN WIRE IN FWD EE PANEL P-32. WIRE IS MARKED AA AND W1132. IT LOOKS LIKE IT IS GOING ON THE RT UTIL BUS CB AT TOP OF P-32 PANEL. BROKEN WIRE REPAIR ON PTT 8322002 SECURED RT UTILITY BUS CB ON P32 PANEL REF 24-51-24.SDR UALA2011061302915Wire · brokenCREW REPORTED SMOKE IN CABIN. FA DESCRIBED ELECRICAL ODOR IN 1ST CLASS ON DESCENT. NO DEFINITE LOCATION. NO ODORS NOTED IN COCKPIT OR COACH, OR FWD GALLEY. EMERGENCY PROCEDURES CLEARED HAZY SMOKE AT 10,000'. IN P32 PANEL FOUND 0058 WIRE C1 LUG BROKEN OFF AT SDR CA110613012Ground Wire · corrodedTHE GROUND TERMINAL OF THE ALTERNATOR WAS CORRODED/DIRTY MAKING BAD CONTACT. THE OIL TEMPERATURE GAUGE WAS "BACK READING" OFF THIS WHICH CAUSED THE GAUGE TO READ HIGH. CESSNA TECH REP WAS ADVISED OF THE PROBLEM AND RECOMMENDED THIS TO CHECK AS A SOLUTION WHICHSDR CA110611003Buss Bar · looseWHEN SELECTING NR 2 BATTERY MASTER SWITCH ON, NO POWER WAS AVAILABLE TO THE ACFT. WHEN BOTH BATTERY SWITCHES WERE TURNED ON THERE WAS NO POWER INDICATION ON THE DC VOLT METER AND THE CO-PILOTS EFIS SCREENS DID NOT POWER UP. EVERYTHING WORKED FINE WHEN EXTERNASDR CA110609004Wire · arcedACFT WAS UNDERGOING ROUTINE INSPECTION AND WIRING REPAIR AT RT ENGINE ALTERNATOR. DURING WIRING INSPECTION WITH POWER `ON`, SMOKE WAS NOTICED COMING FROM THE AFT ENGINE AREA. FURTHER INSPECTION REVEALED, THROUGH THE RT ALTERNATOR FILTER CASE INSPECTION HOLE,SDR UALA2011060802831Terminal Block · corrodedFOUND CORRODED TERMINAL BLOCK IN AFT PIT. PICS ON RVI. REPLACED GROUND BLOCK GB46008B, NORMAL OPERATION RESTORED TO AFT CARGO LOADING SYSTEM, CKS OKAY.SDR CA110608006Terminal · brokenALTERNATOR FAILURE IN FLIGHT, UNSCHEDULED LANDING, ON T/S SYS FOUND THE ALTERNATOR B & WIRE TERMINAL END BROKEN OFF AT THE B+ CONNECTION AT ALTERNATOR. TIME ON THE ACFT IS 5662, UNKNOWN IF TERMINAL END HAS BEEN CHANGED IN THE PAST.SDR CA110607014Contactor · looseRELAY FAILED IN FLIGHT CAUSING SEVERAL SYS FAILURES. PART WAS REPLACED ON SPEC. IT WAS NOTED THAT SEVERAL OF THE CONNECTING POSTS WERE LOOSE, ALMOST IF THE BONDING MATERIAL OR SOLDER HAD FAILED.SDR CA110531008Wire · burnedACFT LOST RADIO COMMUNICATIONS IN FLIGHT. RETURNED TO DEPARTURE AIRPORT. MX FOUND A BURNED WIRE ON THE ALTERNATOR AND REPAIRED. ALTERNATOR REPLACED.SDR WRLA20110529486Wire Harness · burnedNR 3 ENG FIRE IN FLIGHT. THE RELATED FIRE WARNING SYSTEM FUNCTIONED PROPERLY AND THE NR 1 FIRE BOTTLE WAS BLOWN. FOUND IDG HARNESS BURNT.SDR SIMA201114701Wire Harness · chafedON FLIGHT 4243 THE CREW REPORTED SMOKE IN THE COCKPIT AND THE SMELL OF BURNING WIRE. THE SMOKE SEEMED TO ORIGINATE FROM THE GLARESHIELD AND BY BOTH SETS OF RUDDER PEDALS. THE ODOR WAS A SULFUR SMELL THEN WIRE BURNING. THE CAPTAIN DECLARED AN EMERGENCY AND DSDR 2011FA0000372Terminal · meltedTHE POSITIVE STUD MELTED OUT FROM THE ARMMETER AND THE ACFT LOST POWER TO THE BUSS BAR.SDR UALA2011051702429Feeder Cable · damagedNR 1 ENGINE IDG FEEDER CABLE PROTECTIVE SLEEVES ARE DAMAGED AT THE IDG END. REPLACED SLEEVES.SDR 2011FA0000292Wire · shortedWHILE IN FLIGHT THE RT ALTERNATOR FIELD HOT WIRE SHORTED TO GROUND IN THE ALTERNATOR. MAIN VOLTAGE REGUALTOR BREAKER TRIPED. A RESET ALSO RESULTED IN A TRIP. SWITCHING TO THE AUX VOLTAGE REGULATOR GAVE THE SAME RESULTS. A COMPLETE LOSS OF ELECTRICAL POWER SDR UALA2011050402191Feeder Cable · burnedGALLEY POWER FEEDER CABLES BURNED AND BROKEN AT PREVIOUS SPLICE STA 1600-1620, STR 3R. REPAIRED THE AMP COPPER, ALUMINUM SPLICE OF THE POWER FEEDER WIRES FOR GALLEY G4A.SDR CA110728006Wire Harness · chafedACFT EXPERIENCED A WING TIP BRAKE FAIL - MESSG - WHICH AFTER TROUBLESHOOTING FOUND BROKEN, CHAFED AND BURNED WIRES AT THE LT WING T/E - AFT SPAR RACEWAY. AFTER FURTHER INVESTIGATION - THERE WAS A SB (AD) THAT WAS COMPLETED ON THIS ACFT WITH A COMPLIANCE DATESDR CA110530010Wire · misinstalledTHE DC POWER EMERGENCY OVERRIDE TEST HAS REVEALED THAT THE RMU NR 1 WAS NOT SHOWING ANY DASHES WHEN TRANSFERRED IN DC POWER EMERGENCY OVERIDE MODE. AFTER SEARCHING FOR THE FAILURE, DISCOVERED THAT THE SPDA DC ESS LOADS AND SPDA DC 2 LOAD WIRES WERE INVERT WHISDR QXEA2011050200299Wire Harness · burnedUNDER FLOOR AREA AFT OF THE COCKPIT FOUND WIRE BUNDLE W10 HAS 11 BURNED WIRES AND WIRE BUMDLE W17 HAS 2 BURNED WIRES. REPAIRED WIRES BY SPLICING OUT BURNED SECTIONS IAW WIRING DIAGRAM 20-16-10 AND 20-16-20. WIRES AFFECTED WERE : 2800-T11A-20-1, 2800-T14A-20-1,SDR CA110510004Buss Bar · burnedDURING RETURN FLIGHT, CREW EXPERIENCED A FAILED LT ENGINE ANTI-ICE INDICATION. UPON INVESTIGATION BY MX, ARCING AND EVIDENCE OF BURNING WAS FOUND IN AFT MOUNTED ELECTRICAL JUNCTION BOX. LT ANTI-ICE BUS BAR PN 6538342-7, FUSE LIMITER PN ANL175, FUSE LIMITER BASDR CA110414010Grounding Strap · cracked(CAN) AIRCRAFT EXPERIENCED INTERMITTENT ELECTRICAL FAILURE DURING FLIGHT. ALTERNATOR INSPECTED AND GROUNDING STRAP, PN 10-1025 ON REAR CASE FROM THE F2 TERMINAL TO CASE GROUND WAS FOUND TO BE CRACKED THROUGH. THE GROUND STRAP WAS STILL IN CONTACT WITH THE CAS
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