JASC 2410
Service difficulty reports · 891
Reports filed under 2410 · Alternator-Generator Drive, 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 = '2410' 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 = '2410' 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 ABXA20260921415Idg · faultedDURING ENGINE START AND TAXI, L ENG GEN DRIVE & DISC. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED LT ENGINE IDG IAW MEL 24-00-1-1. MBCB 09/24/26. REF ITEM 2, GEN DRIVE LIGHT INOP. MBCB 09/24/26. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.SDR SWI2025F00066Electrical Sys · power lossCOMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333) REFERENCE AML 1512638, AML 1512639, AML 1512641, AML 1512642, AMLSDR SWAA2024120473111Idg · slowN1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE )<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENGSDR SWAA2024120473951Hmu · slowN1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE )<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENGSDR SWAA2024120473952Pump · slowN1 & N2 SLOW TO REDUCE BELOW 45% N1 WHEN RETARDING THRUST LEVER. TAKES APPROX 30 SECS TO REDUCE TO IDLE. ( #1 ENGINE )<[01] R&R #1 ENG IDG PER [AMM 24-11-11-401-NG (INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION - PERMANENT)]. NO HELP.;[02] R&R #1 ENGSDR 2024FA0000827Trans Rectifier · groundedBOTH TRANSFORMER RECTIFIERS (TRUS) WENT OFFLINE (CIRCUIT BREAKERS POPPED) DURING AN AERIAL FIREFIGHTING MISSION. THIS ACTIVATED EMERGENCY ELECTRICAL SYSTEMS AND THE PILOTS WERE ABLE TO RETURN TO THE POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. UPON INSPECTIONSDR IXXA202407086048Trans Rectifier · faultedUPON POWER APPLICATION ON TAXI STRONG ELECTRICAL SMOKE AND FUMES, MULTIPLE DISCRETE LIGHTS HALF LIT, INDICATOR LIGHT 1 BREAKER POPPED. AIRCRAFT RETURNED TO BLOCKS. RANG OUT WIRING FROM LEFT GENERATOR CONTROL UNIT TO LEFT INTEGRATED DRIVE UNIT AND RANG OUT WIRISDR IXXA20240803055Generator · faultedENROUTE FROM KCLT TO KSBD R GEN DRIVE MESSAGE DISPLAYED ON EICAS FL340. APU INOPERATIVE DUE TO SYSTEM ACTIVELY IN DEFERRED MAINTENANCE STATUS. PER ATI MINIMUM EQUIPMENT LIST 49-11-01-01 BOTH ENGINE GENERATORS MUST BE OPERATIVE IF APU IS INOPERATIVE FOR CURRESDR 2023FA0000845Volt Regulator · failedVOLTAGE REGULATOR FAIL AFTER 66.2 HOURS OF OPERATION. AFTER REMOVAL FROM AIRCRAFT NOTICED TWO PART NUMBER STICKERS OVERLAPPING EACH OTHER. EACH STICKER HAD DIFFERENT SERIAL NUMBERS TOP S/N 80Y66728 BOTTOM 80X66735SDR 2023FA0000812Tensioner · destroyedDURING FLIGHT THE PILOTS RECEIVED AN ALTERNATOR FAILURE FOR THE RH ALTERNATOR. UPON INSPECTION I NOTICED THE TENSIONER PULLEY FOR THE BELT DRIVEN ITEMS ON THE ENGINE WAS DESTROYED.SDR ASAA2023102845898Valve · leaking#2 ENGINE IDG HAS HISTORY OF FREQUENT OIL SERVICING. (#PRI2/ETOPS). GROUNDED - YES. (RESOLVED ON W/O: 1975026 TASKCARD: N/R-00001 ) ACCOMPLISHED TSR LEAK CHECK ACCOMPLISHED IAW AMM 24-11-00-700-801 NO LEAKS FOUND. INTEGRATED AIR/OIL COOLERS INSPECTED FOR LEAKSSDR ASAA2023103045855Idg · faulted#1 GENERATOR CAME OFF LINE DURING DESCENT AND WOULDNT RESET. SOURCE OFF LIGHT GEN OFF. BUS LIGHT. GROUNDED - YES. PERFORMED BITE TEST ON #1 IDG PER FIM 24-21 TASK 801. NO FURTHER FAULTS NOTED. INITIAL EVALUATION REVEALED IDG FAULT LIGHT ON GCU 1. PERFORMED WIRSDR ASAA2023101245641Unknown · unknown#1 DRIVE LIGHT NOT ILLUMINATED WITH ENGINE SHUT DOWN. LIGHT ILLUMINATES DURING LIGHT TEST. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023092845423Cooler · leakingTECH SERVICES FOLLOW-UP TO IDG #2 CONTINUED FREQUENT SERVICING---(#PR2)--- *** ETOPS SIGNIFICANT SYSTEM ***. GROUNDED - YES. (RESOLVED ON W/O: 1971410 TASKCARD: N/R-00002 ) INSPECTED IDG #2, NO EVIDENCE OF LEAKING FOUND.INSPECTED IDG #2 OIL COOLER. FOUND EVIDESDR ASAA2023092745582Idg · leakingFOLLOW-UP TO #2 IDG FREQUENT SERVICING----(#PRI2)-----ETOPS SIGNIFICANT SYSTEM----. GROUNDED - YES. #2 ENG IDG WAS REMOVED REPLACED AND TESTED ON AAR N/R 1021781-4000-0002 SN OK360555.SDR ASAA2023092245276Unknown · unknown#2 IDG DRIVE LIGHT NOT ILLUMINATED WITH ENGINE NOT RUNNING WORKS WITH LIGHT TEST. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023091345197Valve · leakingFOLLOW-UP TO #2 IDG FREQUENT SERVICING----(#PRI2)-----ETOPS SIGNIFICANT SYSTEM----. GROUNDED - YES. (RESOLVED ON W/O: 1969651 TASKCARD: N/R-00001 ) ACCOMPLISHED LEAK CHECK IN REF AMM 71-00-00. NO LEAKS NOTED. R&R IDG VENT VALVE REF AMM 24-11-00-700-804R&R IDGSDR ASAA2023082244733Unknown · unknown#2 IDG DRIVE LIGHT DOES NOT ILLUMINATE WITH THE #2 ENGINE SHUTDOWN. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023072344164Unknown · unknownLT ENGINE DRIVE LIGHT INTERMITTENT. GROUNDED - YES. (RESOLVED ON W/O: 1962955 TASKCARD: N/R-00001 ) RESISTANCE CKS FOR CHARGE PRESSURE SWITCH AT DP1206 PIN 5&6, NO DEFECTS NOTED REF FIM 24-11 TASK 804 & WDM 24-11-11. RAN ENGINE, VERIFIED DRIVE LT NORMAL OPS, NSDR ASAA2023072144163Unknown · unknownENG 2 DRIVE LIGHT NOT ILLUMINATED. GROUNDED - YES. PERFORMED #2 IDG OPS CHECK IAW AMM 24-11-00 OPS CK GOOD SEAMC DAVE NOTIFIED. NON ASA EMP KYLE WALEN A&P N9VR0841.SDR ASAA2023062543755Unknown · unknown#2 GEN DRIVE WILL INTERMITTANTLY NOT ILLUMINATE WITH ENGINE OFF(PRI 2). GROUNDED - YES. REF IFIM TASK 24-11-00-810-804 PERFORMED GCU BITE TEST, BITE TEST PASSED.PERFORMED WIRE CHECK BETWEEN PIN-61 OF CONNECTOR D10892A AND PIN-16 OF CONNECTOR D636 WIRE TEST GOOSDR ASAA2023062443714Unknown · unknownENG #2 DRIVE LIGHT DID NOT ILLUMINATE EXCEPT IN TEST. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023062143676Unknown · unknown#2 DRIVE LIGHT NOT ILLUMINATED EXCEPT DURING LIGHT TEST. GROUNDED - YES. PERFORMED GCU #2 BITE TEST . REF AMM 24-21-81. BITE TEST GOOD. #2 DRIVE LIGHT ILLUMINATED. AIRCRAFT IS RELEASED FROM MEL 24-11-02. PLACARD REMOVED.SDR 2023FA0000279Alternator · unknownEN ROUTE THE CREW BEGAN TO NOTICE AN ALTERNATOR FAILURE WARNING SIGNALS WENT OFF. CREW NOTIFIED ATC TO BEGIN HEADING BACK OR TO LAND THE AIRCRAFT AT THE NEAREST AIRPORT. SHORTLY AFTER THE PIC AND COPILOT BEGAN TO SMELL WHAT THEY BELIEVED WAS A FIRE. PILOT TURNSDR 2023FA0000305Alternator · failedN4678Q, C210, DECLARED AN EMERGENCY DUE TO POSSIBLE ELECTRICAL ISSUE. THE FLIGHT LANDED SAFELY WITHOUT ISSUE.SDR DALA2023051503798Unknown · unknownSHIP 3250 - ATO - AT APPROXIMATELY 40 KNOTS DUE TO ELEC IDG 1 LO OIL PR ECAM MSG. CORRECTIVE ACTION: FOUND IDG #1 OIL LOW. SERVICED IDG. NO LEAKS NOTED. OK TO CONTINUE. (9415372)SDR ASAA2023050343095Filter · cloggedFOUND #1 IDG DPI POPPED DURING WALK AROUND. GROUNDED - YES. INSPECTED AND REPLACED IDG SCAVENGE AND CHARGE FILTERS, NO DEBRIS FOUND. REF B737-9 AMM 24-11-41, LEAK CHECK GOOD, OPS CHECK GOOD.SDR ASAA2023042743048Idg · failedGEN NO.1 CAME OFF LINE DURING DESCENT AND WOULD NOT RECONNECT TO THE BUS. APU WAS STARTED IAW QRH AND WAS CONNECTED TO THE L BUS. GROUNDED - YES. REMOVED AND REPLACED #1 ENG IDG IAW BOEING 737-800 AMM 24-11-11.SDR VNAA202304121112Unknown · unknownSPARKS COMING ELECTRICAL POWER CONTROL PANEL / INSTALLED ELECTRICAL CONTROL PANEL IAW CRJ 700 AMM 24-13-01-400-800-A01. OPS CHECK GOODSDR ASAA2023040142721Idg · unknownON WALK AROUND FOUND #1 ENG IDG NO OIL IN SIGHT GLASS. GROUNDED - YES. REMOVE AND INSTALLED #1 IDG REF AMM 24-11-11.SDR DALA2023032902405Unknown · unknownSHIP 3017 - ATO - AT 100KTS DUE TO NBR 1 ENGINE IDG LOW OIL PRESSURE FAULT MESSAGE. CORRECTIVE ACTION: DEFERRED #1 IDG PER MEL 24-20-01A; R/R IDG. (LP# 4073536)SDR DALA2023032102153Idg · inoperativeSHIP 3861 -ATB- DUE TO BIRD STRIKE ON DEPARTURE. LEFT ENGINE GENERATOR INOP. CORRECTIVE ACTION: PERFORMED GCU BITE CHECK. NO FAULTS. FOUND DPI EXTENDED. INSPECTED SCAVENGE FILTER. REPLACED THE #1 IDG PER B737 AMM 24-11. OPS CHECK OK.SDR DALA2023032002086Unknown · unknownSHIP 8115 - DIV - TO LAS DUE TO "L GEN FAIL" CATION MESSAGE FOLLOWED BY "APU FAIL" WARNING MESSAGE. CORRECTIVE ACTION: REPLACED VARIABLE FREQUENCY GENERATOR (VFG) AND GENERATOR CONTROL UNIT (GCU). (LP# 9493830)SDR ASAA2023031642381Unknown · unknownON PREFIGHT THE #2 IDG CONTROL CB POPPED. GROUNDED - YES. PERFORMED C/B RESET REF B737-9 AMM 20-60-01 C/B DID NOT REOPEN.SDR ASAA2023031542457Unknown · faulty#2 IDG "DRIVE" LIGHT EXTINGUISHED WITH ENGINE STOPPED, WORKS ON LIGHT TEST NORMALLY. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE IDG REF B737-9 AMM 24-11-11-400-801.SDR ASAA2023030842262Idg · leakingOIL RESIDUE ON #1 ENGINE COWLING AND SMALL OIL PUDDLE ON GROUND BENEATH #1 ENGINE. GROUNDED - YES. PERFORMED B737-900 AMM TASK 71-71-00-200-801-F00. FOUND ENG 1 IDG PAD DRAIN LEAKING 6 DROPS /MIN AFTER ENGINE SHUTDOWN. REMOVED AND REPLACED #1 ENGINE IDG REF AMSDR ASAA2023030642208Idg · faulty#2 ENG SOURCE OFF LIGHT FOLLOWED BY DRIVE LIGHT ILLUMINATED DURING TAXI. DRIVE QRC ACCOMPLISHED. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE IDG IAW B737-900 AMM 24-11-11-401.SDR ASAA2023022842119Idg · failedAFTER START GEN 2 WOULD NOT CONNECT TO TRANSFER BUS. GROUNDED - YES. REMOVED AND REPLACED #2 ENG IDG REF B737-800 AMM 24-11-11.SDR ASAA2023022342065Idg · leaking#1 ENGINE LEAKING HYDRALIC FLUID. GROUNDED - YES. PERFORMED #1 ENGINE IDG OIL SYSTEM STATIC LEAK PER B737-800 AMM 24-11-00. FOUND LEAK AT PORT DIRECTLY BELOW DISCONNECT RING. #1 IDG REMOVED & REPLACED PER AMM 24-11-11.SDR DALA2023022201313None · noneSHIP 1606 -ATO- DUE TO LT GEN OFF INDICATION. CORRECTIVE ACTION: MEL APPLIED. IDG R/R NEXT MTC OPPORTUNITY. COOLER R/R ON MCC FOLLOW UP LOG. A/C RTS. (9916676)SDR ASAA2023020741859Idg · leakingFOLLOW-UP TO #1 IDG FREQUENT SERVICING, ACCOMPLISHED STATIC LEAK TEST REF B737-800 AMM 24-11-00-700-801. FOUND LEAK COMING FROM VALVE CAP (REF CMM FOR IDG, ITEM 160). GROUNDED - YES. REMOVED AND REPLACED #1 IDG, REF B737-800 AMM 24-11-11/401.SDR ASAA2023012941751Idg · faulty#1 GEN DRIVE LIGHT IS GOING OUT AND COMING BACK ON CAUSING MASTER CAUTION ELEC LIGHT WITH #1 ENG OFF. GROUNDED - YES. REMOVED AND REPLACED #1 IDG REF 737-800 AMM 24-11-11.SDR CALA2022122803504Receptacle · damagedPRY EXT POWER PINS WITH SIGNS OF OVERHEAT AFTER GPU CABLE FAILURE. REMOVED AND REPLACED PRIMARRY EXTERNAL POWER RECEPTICAL.SDR DALA2022110707200None · noneSHIP 0699 - DIV - INTO CVG DUE TO THE LOSS OF THE RIGHT GENERATOR WHILE THE APU WAS ON MEL. CORRECTIVE ACTION: REPLACED RT GCU AND IDG.SDR ABXA20221019116Control Unit · noneAFTER PUSH LH GENERATOR DISCONNECTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET LEFT HAND GENERATOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AALA202210185155Idg · noneAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED AN ELECTRICAL GENERATOR 2 FAULT MESSAGE AND 10 MINUTES LATER REPORTED THAT THE APU AUTO SHUT DOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PHX WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANSDR SWAA2022101057920Generator · faulty#1 IDG LIGHT ILLUMINATED ON TOUCHDOWN; EXTINGUISHED AFTER SLOWING BELOW 60 KIAS. 02OCT: SERVICED IDG PER AMM 12-13-21.PERFORMED ENGINE RUN PER AMM 71-00-00 / [01] OK TO CONTINUE PER MEL 24-1-02 SP1<BR>AUTH#: 95448;[02] R&R #1 IDG IAW AMM 24-11-11. OPS CHECK GOSDR ASAA2022092940082Idg · faulty#2 DRIVE LIGHT ILLUMINATED ON CLIMB OUT. GROUNDED - YES. REMOVED AND REPLACED #2 IDG REF B737-800 AMM 24-11-11.SDR ASAA2022092840090Seal · leaking#1 ENGINE OIL TREND DATA SHOWS OIL CONSUMPTION TO GREATER THAN EXPECTED. ENGINE POWER RUN REQUIRED. GROUNDED - YES. FOUND EVIDENCE OF OIL LEAKING FROM IDG PAD DRAIN LINE. PERFORMED IDLE ENGINE RUN AND FOUND ACTIVE LEAK FROM IDG PAD DRAIN OF 7 DROPS PER MINUTE,SDR DALA2022092606299None · noneSHIP 675 - DIV - TO CVG DUE TO LOSS OF RIGHT ENGINE GENERATOR WITH APU ON MEL. CORRECTIVE ACTION: REPLACED GCU AND RT IDG, LK CK AND OPS CHECK GOOD. APU REPLACED.
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