JASC 7100
Service difficulty reports · 635
Reports filed under 7100 · Powerplant 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 = '7100' 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 = '7100' 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 2022FA0000457Cylinder · leakingOVERHAULED RH ENGINE WAS INSTALLED ON THE AIRCRAFT. AFTER TEST FLIGHT, AN OIL LEAK WAS NOTED FROM THE #6 CYLINDER BASE. THE CRS THAT OVERHAULED THE ENGINE INSTRUCTED US TO REMOVE THE #6 CYLINDER TO CHECK FOR ISSUES. DURING THE REMOVAL OF THE CYLINDER, IT WASSDR CALA2022071301729Engine · failedLEFT ENGINE LOUD BANG AT 27000FT. ENG FAIL NO N2 THIS IS FOR LEFT ENGINE SN. 222128 (TSI= 11297, CSI= 1351).
INSTALLED NEW ENGINESDR 2022FA0000352Exhaust Valve · brokenNUMBER ONE CYLINDER EXHAUST VALVE STEM BROKE RELEASING VALVE INTO CYLINDER.SDR TIMA202207130008Engine · shutdownPS NORMAL THROUGH 10,000 FT. CLIMBING THROUGH ABOUT 10500 FT THE PILOT NOTICED THE RH TORQUE GAUGE BEGIN TO FALL, THEN THE RH OIL PRESSURE LIGHT CAME ON. PILOT FELT A YAW, WAITED ABOUT THIRTY SECONDS TO CONFIRM FAILURE, SECURED THE ENGINE AND RETURNED BACK TO SDR NACA2022071000002Blades · abnormalRH ENGINE #4 AND #6 BLADES WITH A NICK NEAR THE TIP. BLENDED RH ENGINE BLADE #6 BLADE WITHIN LIMITS IAW B767 AMM 72-31-02. DEFERRED DMI 72-31-02 ROUTINE SLIP TO MOC ACCOMPLISHMENT OF FPI WITHIN 50 FLIGHT HOURS, DUE TAT 107288@1447 7-10-22SDR DALA2022071204843None · noneSHIP 3271 #1 ENGINE FAILURE ON TAKEOFF. CORRECTIVE ACTION: REPLACED NUMBER ONE ENGINE PER A320 AMM 71-00. OK FOR SERVICE. (2306883)SDR TIMA20220705007Engine · shutdownLIGHT WAS FROM KHDN TO KCYS THEN KDEN. PILOT PICKED UP CLEARANCE FOR KCYS AT THE END OF THE TAXIWAY. PILOT DID A REDUCED POWER TAKEOFF FROM RWY 10. UPON REACHING 1,500' AGL PILOT RAISED THE FLAPS REDUCED TORQUE A FEW 1000"/LBS THEN HE BROUGHT THE PROPS BACK TOSDR 4DPA2020070400001Engine · overtempCREW REPORTED-THERMAL RUNAWAY SHORTLY AFTER LEVELING AT FL370. ITT BEGAN CLIMBING. PULLED BACK #2 THRUST LEVER AND ITT CLIMBED ABOVE 1000. ELECTED TO SHUT DOWN ENGINE #2 AS IT GAVE UP THE GHOST AS WELL. ENGINE SHUT DOWN WITHOUT ISSUE. BEFORE SHUTDOWN OIL SDR JIKA202206301Oil Cooler · leakingWHILE IN ROUTE TO KMLI, THE FLIGHT CREW REPORTED RIGHT ENGINE OIL PRESSURE DECREASED AND THE AIRCRAFT YAWED RIGHT. THE RIGHT ENGINE WAS SHUT DOWN AND SECURED AND EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KBMI. MAINTENANCE INSPECTED AND FSDR IPXA2022062783544Engine · abnormalINSPECTION TYPE:NADURING #2 ENGINE START AT MAX MOTOR (23%) #2 FUEL LEVER WOULD NOT MOVE OUT OF CUTOFF POSITION. FUEL WAS NEVER ADDED AND START WAS ABORTEDPERFROMED 3 ENGINE STARTS / STOPS CYCLES IAW AMM 71-00-00-0501. ALL OPS CHECK GOOD. RUNS WERE PERFROMED ASDR QXEA2022062400231Fadec · abnormalON LANDING ROLLOUT ENG1 NO DISPATCH AND ENG 1 FADEC FAULT ILLUMINATED. REMOVED FROM SERVICE. R&R #1 ENG FADEC IAW CF34-8 LMM 73-00-00-800-801 #1 ENG OPS TEST GOOD NO MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE.SDR 2022F00269None · none#2 ENGINE SHUTDOWN DURING CRUISE, TAIL PUMPS LO, ALT PUMPS LOSDR CALA2022061501513Nozzle · missingPDA 3 AFT #2 ENG COMMON NOZZLE ASSY.PIECE MISSING ON INTERIOR OF C.N.A.12 O-CLOCK POSITION.10 INCHES FORWARD. ADDED PICTURE. ADDED MORE PICTURES.ONE WILL BE A CLOSER VIEW.ONE WILL BE WHAT SUPERVISOR ON DUTY EWR AND CENTER DESK LINE CONTROL EWR NOTIFIED IS INSTSDR CALA2022061501510None · noneFOUND LIGHTNING STRIKE DAMAGE TO THE RH ENGINE INNER COWL FIN (PLACARDED WITH NO GRAB) IAW AMM 05-51-18 REMOVED THE #2 ENGINE STRAKE PER REF AMM 71-13-19-000-010-B.SDR IXXA2022061403Pad · wornREMOVED AND REPLACED # 2 ENGINE LOUVRED DOOR , AFT LATCH STOP PAD SEE PARTIAL 1-4 FOR FAB OF STOP PAD IAW B767 SRM 51-40-02 PARA 4SDR SCNA20220608068Engine · low pressureDEFECT: PRECAUTIONARY SHUTDOWN OF ENGINE #1 DUE TO OIL PRESSURE FLICKERING YELLOW TO RED. OIL QUANTITY AT SHUTDOWN WAS ZERO. RESOLUTION: (IN PROGRESS)SDR UIEA2022052300502Frame · chipped#3 ENG R/H CORE COWL NO.5 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED. FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG. 201 REV 94, DATE: 20 FEB 2022</P>)SDR UIEA2022052300503Cowling · gouged#3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022</P>)SDR UIEA2022052300504Frame · chipped#4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022SDR ABXA202252759Eicas · false indicationDURING RIGHT ENGINE START - WHEN TO GND, RIGHT ENGINE SHOWED EGT EXCEEDANCE. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE CLEARED MX MESSAGES ON EICAS BIT EEC MONITOR, NO FAULTS NOTED. ACCOMPLISHED MES OF #2 ENGINE IAW 71-00-00, ALL SDR I5PA2022052575702Engine · defectiveRIGHT ENGINE WAS REPLACED DUE TO A HIGH OIL CONSUMPTION.SDR I5PA2022052575701Bleed Valve · inoperativeLEFT ENGINE HOT START OCCURED DURING THE ATTEMPT. FURTHER INSPECTION FOUND DISCREPANCIES IN THE 2.5 BLEED VALVE SYSTEM. ENGINE WAS REMOVED AND SENT FOR REPAIR. ONCE REPAIRED, ENGINE WAS RE-INSTALLED ON THE AIRCRAFT.SDR GTIA2022052636435None · noneFUME EVENT OBSERVED AT TOP OF DESCENT. APPLIED PROCEDURE FOR ELIMINATION OF ODOR/FUMES. TURNED OFF PACK 1 AND SMELL DISCIPATTED.-T/S IAW TSM 71-00-00-810-847-A. NO FAULTS OR ODORS AT THIS TIME.SDR 2022F00238Frequency Gen · damagedIN FLIGHT A GEN 1 FAIL WARNING MESSAGE APPEARED ON THE CAS, AFTER INSPECTION IT WAS DISCOVERED THAT THE CAUSE WAS A CATASTROPHIC FAILURE OF THE #1 VFG LEADING TO DAMAGE OF SURROUNDING PARTS/COMPONENTS, DEBRIS FROM THE FAILURE WAS FOUND WITHIN THE LH ENGINE COWSDR QR9R20220523001Engine · fault messageDURING FLIGHT, #2 ENGINE CHIP CAUTION ILLUMINATED ON CAD. THIS WAS THE 3RD LIGHT EVENT AND 3RD TIME METAL PARTICLES WERE FOUND ON CHIP DETECTOR. REMOVED AND REPLACED MODULE 05 ASSEMBLY IAW ARRIEL 1E2, 72-00-15-900-801-B01. TEST FLIGHT SUCCESSFULLY COMPLETED IASDR I5PA2022052268803Sense Line · cloggedEVENT - MGE 880 AIR RETURN DUE TO NO EPR VALUES ON PRIMARY AND STANDBY ON LH ENG. MX PURGED LH ENG SENSE LINES, LH ENG RUN UP. OPS CHECK NORMAL PER FIM 71-01 TABLE 308, AMM 71-00-00.SDR GTIA2022052336434None · noneFUME EVENT AFT CABIN WHEN GEAR CAME DOWN-RUN #1 AND #2 ENG IAW AMM 71-00-00. NO FUME OR ANY SMELL ON AFT CABIN AC OK FOR SERVICESDR HALA2022052300103None · noneETOPS - #1 ENGINE HIGH VIB - ENGINE REPLACED PER ENGINEERING REQUEST // REMOVED AND REPLACED #1 ENGINE PER HAL TASKCARD J321-72-WHI-02SDR UIEA2022051400470Engine · installedREINSTALL ALL REMOVED HYDRAULIC, PNEMAUTIC AND ELECTRIAL CONNECTORS AND LINKS DUE TO #1 ENGINE CHANGE CANCELATION. REINSTALLED ALL; HYDRAULIC; PNEUMATIC AND ELECTRICAL CONNECTORS AS PER 71-00-02. PENDING ENGINE RUN UP LEAK CHECK .PERFORMED IDLE ;LEAK CHSDR 2022FA0000459Crankcase · destroyedAFTER CLIMBING TO 12000 FT FROM KCYS, THE AIRCRAFT TRANSITIONED TO CRUISE TO PREPARE FOR AERIAL SURVEY WORK. SHORTLY THEREAFTER, THE RE HAD A VIBRATION, POWER LOSS, AND STOPPAGE. THE AIRCRAFT WAS LANDING BACK AT KCYS WITHOUT INCIDENT. AFTER THE COWLING WAS RSDR NACA2022051200001None · noneMECHANICAL INTERRUPTION (SIC) FLUID LEAK ON #1 ENGINE DURING STARTUP @ 1417Z IN KMIA. ACCOMPLISHED LEFT ENGINE DRY MOTORING AND WET MOTORING IAW AMM 71-00-00, NO LEAKS NOTED AT THIS TIME. AFTER ENGINE RUN AT IDLE POWER TO REMOVE REMAINING FUEL ALL NORMAL.SDR IPMALJ1805050822Regulator Valve · erraticIN CRUISE FLIGHT LEFT ENGINE OIL TEMPERATURE CLIMBED TO RED LINE REDUCTION IN POWER DID NOT PREVENT POWER FROM INCREASING TO APPROXIMATELY 120 DEGREES C. POWER WAS REDUCED FURTHER AND IN DESCENT THE OIL TEMP RETURNED TO NORMAL RANGE. WHEN POWER WAS INCREASE INSDR UIEA2022050600446Vane · unserviceable#2 ESN 704757 HAS 1EA HPT VANE AT 5 O'CLOCK POSITION WITH CONVEX SIDE MISSING AND LIFTING MATERIAL. CONDITION IS NOT PERMITTED. REPLACED ENGINE. REMOVED #2 ENG PER B767-300 AMM 71-00-02. OK TO INSTALL SERVICIABLE ENG. / INSTALLED NEW SERVICIABSDR CALA2022050601160Window · noneEECM MESSAGE INDEX BIRD STRIKE PROBLEM WAS ENCOUNTERED BY THE FL IGHT CREW WHICH WAS NOT COVERED IN THE FAULT CODE DIAGRAMS (REF FAULT CODE DIAGRAM FOR FLIGHT CREW ACTION) BIRDSTRIKE ON FO FRONT W INDSCREEN CLEANED F/O WINDOW IAW AMM TASK 12-25-04-102-001 AND SDR DALA2022050503143Compressor · stalledSHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 103 KNOTS FOLLOWING THE #2 ENGINE COMPRESSOR STALL AFTER INGESTING A MYLAR BALLOON FLOATING OVER THE RUNWAY. CORRECTIVE ACTION: MAINTENANCE FOUND BALLOON DEBRIS IN THE TAIL PIPE. INSPECTION PERFORMED BORESCOPE PER ASDR GTIA2022050536407None · noneAIRCRAFT HAD A NORMAL ENGINE PARAMETERS BUT NO PERFORMANCE ON THE CLIMB-PERFORMED HIGH POWER ASSURANCE TEST ALL PARAMETERS FOR ENG 1 & 2 SATISFACTORY IAW AMM 71-00-00-710-806-ASDR IXXA2022050304Sleeve · deteriorated#1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.SDR IXXA2022050303Sleeve · worn#1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITIONSDR 2022FA0000243None · faulted"OPEN"- DURING MAINTENANCE CHECK FLIGHT, THE #1 ENGINE EXPERIENCED A HIGH VIBRATION AND SHUTDOWN WITH SUDDEN STOPPAGE. AIRCRAFT RETURNED TO BASE. SDR UIEA2022042000342None · noneNO.1 ENG R/H CORE COWL EXHAUST DUCT INLET EDGE AREA FOUND CHAFING ( P/N 224-2302-545 )(<P>NO.1 ENG R/H CORE COWL ( P/N : 224-2302-545 S/N : 325001 ) EXHAUST DUCT INLET EDGE CHAFING AREA WELD REPAIRED AND DOUBLER ( P/N : 224M4762-3 ) REPLACED IAW EO 1971A278-1SDR 2022FA0000242None · none"OPEN" - DURING MAINTENANCE CHECK FLIGHT, THE #1 ENGINE EXPERIENCED A HIGH VIBRATION AND SHUTDOWN WITH SUDDEN STOPPAGE .AIRCRAFT RETURNED TO BASE.SDR KCSA2022042308Engine · stalledRIGHT ENGINE COMPRESSOR STALL, FOLLOWED BY EXHAUST GAS TEMPERATURE INCREASE, RIGHT ENGINE UNRESPONSIVE. RIGHT ENGINE LEFT AT IDLE FOR REMAINDER OF FLIGHT, EMERGENCY DECLARED.SDR TAMF20220426021None · noneDURING T/O THRUST SET, ENG THRUST LOSS ABNORM BLEED OR PACK APPEARED ON ECAM DISPLAY, THE PILOT DECIDED TO INTERRUPT THE TAKEOFF AND AFTER PERFORM THE CABIN PROCEDURES, THE FAILURE DISAPPEARED AND FINALLY THE TAKE OFF WAS NORMAL.
AS A MAINTENANCE ACTION, AT TSDR QMLA2022042220026None · unserviceableWHILE ON A FLIGHT TO A PR, PILOT NOTICED AN AMBER GOV LIGHT IN FLIGHT FOLLOWED BY A DECREASE IN ENGINE POWER AND ROTOR SPEED. PILOT ABORTED THE LANDING AND LANDED AT A NEARBY AIRPORT BEING THE SAFFORD AIRPORT.SDR CALA2022041801004Engine · vibratesR ENG VIBRATION TO 8.0 A/C TRIMMED TO 2.5 UNITS VERY PRONOUNCED REFER TO FIM TASK DMC-B787-A-G71-00-00-31A-280A-A,ENGINE OVER IMAGES FROM FLT DECK AND MY BOING IMAGE FROM MY BOEING MAXIMUM VIBRATION - INSPECTION. TOMC-EMC BORRELLI. REF AMM.71-00-00-31A-280A-ASDR IPXA2022041581183Engine · noneINSPECTION TYPE:NA**SUPPLEMENTAL SDR**IFSD** DIVERSION**EMERGENCY DECL'D**DURING CRUISE FL370, LH ENG SURGE & LOST THRUST. THRUST LEVER MOVEMENT RESULTED IN NO RESPONSE. AUDIBLE BANG SHUT DOWN ENG/ WITH FUEL CONTROL SWITCH. RAN ENG QRH.PERFORMED FIM TASK AMM 7SDR SCNA20220414030None · noneDEFECT: AT FL 370 ENGINE #2 ROLLED BACK THRUST LEVER DID NOT RESPOND "RED EGT " BOX ILLUMINATED. RESOLUTION: PERFORMED FIM TASK 73-06 TASK 812 “AUTO DECELERATION” AND FIM TASK 71-06 TASK 805 “OVERTEMP NOT DURING START”. DURING FIM 71-06 TASK 805 FOUND ONLSDR ABXA2022041141None · noneR/H ENGINE EGT EXCEEDANCE ON START 542 DEGREES FOR 3 SECONDS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE T/S IAW FIM 71-08-00-990-816-P00. PERFORMED #2 ENG START WITH FLT CREW IAW AMM 71-00-00. SECOND ENG START WITHIN LIMITS. AIRCRAFT RETSDR 2022F00186Engine · damagedENGINE #1 AT 90 KTS WE HAD ENGINE SURGE OR STALL (TWICE) RTO RWY 14 TOW 46.7. BOROSCOPE INSPECTION DAMAGE OUT OF LIMITS.SDR I5PA2022040975702Egt Indication · abnormalAIRCRAFT AIR RETURN DUE TO RIGHT ENGINE EGT EXCEEDING LIMITATIONS DURING CLIMB.
(DISCREPANCY IS CURRENTLY OPEN)
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