GE CF6-80C2B6F
Service difficulty reports · 1,456
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'CF680C2B6F' 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 engine_model_key = 'CF680C2B6F' 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 P5CA2021042800156None · noneDURING WALK AROUND FOUND EVIDENCE OF BIRD STRIKE ON RH ENGINE INLET. PERFORMED HPC BOROSCOPE THROUGH PLUGS B1-0, B1-1, B1-6 AND B1-12 IAW AMM 72-00-00-706-146-110. NO DAMAGE NOTED.SDR UIEA2021042600999Indicator · dimSTANDBY ENGINE INSTRUMENTS VERY DIM AND HARD TO READ WHEN TURNED ON(<P>REMOVED AND REPLACED ENGINE STANDBY INDICATOR IAW AMM 77-41-01. OPS CHECK GOOD AT THIS TIME<BR /></P>)SDR UIEA2021042200976Brake · malfunctioned# 1 ENG. OUTBD T/R ELECTRICAL MECHANICAL BRAKE DOES NOT STAY IN THE UNLOCK POSITION(<P>REMOVED AND REPLACED 3 1 ENG. OUTBD THRUST REV ELECTRO MECHANICAL BRAKE IAW AMM 78-34-07.</P><P>PENDING OPS CHK . ACCOMPLISHED ELECTRO MECH. BRAKE CHECK PER MM 78-30-00-505SDR UIEA2021042200975Brake · malfunctioned#1 ENG INBD T/R ELECTRICAL MECHANICAL BRAKE DOES NOT STAY IN THE UNLOCK ED POSITION. REMOVED & REPLACED #1 ENGINE INBD THRUST REV. ELECTRO MECHANICAL BRAKE IAW AMM 78-34-07.</P><P>PENDING OPS CHK . ACCOMPLISHED ELECTRO MECH BRAKE CHECK PER MM 78-30-00-705-001SDR UIEA2021042200974Connector · loose# 1 ENG PDV ELECTRICAL CONNECTOR BACK SHELL LOOSE(<P>ASSEMBLED STRAIN RELIEF & BACKSHELL CONNECTOR # 1 ENG DPV P5 PER SWPM 20-60-09 REV 76 & W/D 78-34-11 REV 32.</P>)SDR UIEA2021042200973Bolt · loose# 1 ENG HAS WIRE BUNDLE CLAMP NOT SECURED (BOLT MISSING) @ 11 O' CLOCK POS. JUST FWD OF MAIN HYD. LINE .(<P>REMOVED AND REPLACED MISSING BOLT PER MM 20-11-00.</P>)SDR UIEA2021042200966Clamp · brokenENG # 1 (D) SUMP LINE HAS BROKEN CLAMP .(<P>REMOVED AND REPLACED D SUMP BROKEN LINE CLAMP PER MM 79-21-09-400-801-H00.</P>)SDR UIEA2021042200965Clamp · brokenENG #2 (D) SUMP LINE HAS 1EA BROKEN CLAMP(<P>REMOVED AND REPLACED D SUMP BROKEN LINE CLAMP PER 79-21-09-400-501-H00</P>)SDR P5CA2021042300153Igniter · failedR ENG IGNITOR 2 STATUS. RIGHT ENGINE WOULD NOT LIGHT IN SINGLE(<P>PLACED ON MEL 74-00-01B, MDDR 145735, CAT C - DUE 02 MAY 2021. PLACARD INSTALLED.</P><P>REMOVED AND REPLACED #2 IGNITOR PLUG REF B767 AMM 74-21-02/401. PERFORMED IGNITION SYSTEM AUDIBLE TEST PERSDR 2021F00054Blade · damaged71 02 59 01 (VIBRATION DURING DESCENT ENGINE 1). DURING BOROSCOPE INSPECTION 31 BALDES DAMAGED IN HPC 4TH STAGE; 16 BLADES DAMAGED IN HPC 5TH STAGE, BLADES DAMAGED IN HPC 6TH STAGE, BLADES DEMAGED IN HPC 7TH STAGE, BLADES DAMAGED IN HPC 13TH STAGE, NGV TE OUTESDR UIEA2021041400890Engine · unknownINFO ONLY, DURING ENGINE START IN ILN, THE LEFT ENGINE HAD NO EGT RISE WHEN FUEL CONTROL SWITCH IN RUN. WHEN ENGINE START SELECTOR MOVED FROM SINGLE TO BOTH, LEFT ENGINE START NORMAL. PERFORMED IGNITION AUDIBLE CHECK OF LEFT ENGINE. OPS CHECK OKAY AT THIS TIMSDR UIEA2021041400888Isolation Valve · malfunctioned"L BLD ISLN VAL" EICAS DURING PREFLIGHT.(<P>REMOVED AND REPLACED L ISO VALVE IAW AMM 36-11-04, OPS AND LEAK CHECKS GOOD AT THIS TIME.</P>)SDR UIEA2021041300880Engine · not reportedR GENERATOR OFF EICAS MESSAGE DISPLAY. TRANSFERED TO DMI # 145249, CAT B, DUE DATE 16 APR 21 IAW DDG 24-00-01-01. LOG PAGE 1465065: REMOVED AND REPLACED #2 ENGINE IAW AMM 71-00-00. OPS CK GOOD. THIS CLEARS MDDR 145249.SDR 2LCF20210412Hmu · malfunctionedON APRIL 12TH, IN FLIGHT UC-1407 SCHEDULED ON THE ROUTE MIA TO VCP AT CRUISE LEVEL, A DIFFERENCE OF 400 KILOS WAS DETECTED BETWEEN THE TOTALIZED AND CALCULATED FUEL, AND ALSO A DIFFERENCE OF 300 KILOS WAS FOUND COMPARED WITH THE FUEL ESTABLISHED IN THE FLIGHT SDR UIEA2021040800860Filter · warning messageRT ENG FUEL FILTER ILLUMINATED IN CLIMBOUT W/FF ABOVE 10K PPH EXTINGUISHED ON POWER REDUCTION(<P>REMOVED AND REPLACED RH ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKS GOOD. OPS CHECKS NORMAL. NO DEFECTS NOTED.</P>)SDR UIEA2021040900868Filter · faultedRT ENGINE FUEL FILTER ILLUMINATED IN CLIMBOUT WITH FF ABOVE 10KPPH. EXTINGUISHED ON POWER REDUCTION.(<P>R/R R/H ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKS GOOD. OPS CHECKS NORMAL, NO DEFECTS NOTED</P>)SDR DALA2021041402192Acoustic Panel · damagedSHIP 1705 #1 ENGINE AFT BY PASS DAMAGED ACOUSTICAL PANEL AFT OF FAN BLADES. REPAIRED PER ERA 469315-14. (LP 7591294)SDR UIEA2021040800862Anti-Ice Valve · failedSTATUS MESSAGE: L ENG TAI VALVE(<P>R/R ENG INLET TAI VALVE LH IAW AMM 30-21-03. PERFORMED OPS CHECK. OPS CHECKS GOOD</P>)SDR UIEA2021040500838Igniter · faultedR ENGINE NO LIGHT OFF FIRST ATTEMPT WITH ENG START IN "SINGLE". SECOND START NORMAL WITH SWITCH IN "BOTH". DISCOVERED EICAS MESSAGE R ENG IGNITOR 2, CONFIRMED FAULT ON R PIMU. REMOVED R ENG NR 2 IGNITER AND INSTALLED NEW IGNITER IAW AMM 74-21-02. OPS CHECK GOSDR UIEA2021040500835Igniter · faultedITEM #1 INFO ONLY: R ENG NO LIGHT OFF FIRST ATTEMPT W/ENG START IN "SINGLE". SECOND ATTEMPT NORMAL START W/ SWITCH IN "BOTH".(<P>NOTED BY MX. PERFORMED IGNITION SYSTEM AUDIBLE TEST OF RH ENGINE IAW AMM 74-00-00. OPS CHECK GOOD AUDIBLE HEARD ON BOTH IGNITERS ONSDR UIEA2021040500836Engine · unknownDURING #1 ENG START ENG DID NOT LIGHT OFF. SUBSEQUENTLY SELECTED THE "ENG START" SELECTOR TO BOTH. ENG STARTED NORMALLY ON SEC ATTEMPT.(<P>PERFORMED IGNITION SYS AUDIBLE TEST IAW AMM 74-00-00.OPS CHK OK.RAN #1 ENG PER AMM 71-00-00. ENG START 1ST ATTEMPT.<BR /SDR UIEA2021040300817Seal · leaking#2 ENG PRVC LOCATIONS E AND K FOUND TO HAVE LEAKS(<P>REMOVED AND REPLACED SEALS AT BOTH LOCATION "E AND K". ACCOMPLISHED RECHECK FOR LEAKS PER TALLY ENG PNEU LEAK CHECK. NO LEAK NOTED AMM 36-11-19.</P>)SDR UIEA2021040300816Blade · dented#2 ENG HAS ONE FAN BLADE WITH A DENT ON THE LEADING EDGE.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;">CLEANED DENTED AREA OF # 2 ENG FAN BLADE FOUND WITHIN LIMITS AT LEADING EDGE PER B767-300 AMM 72-31-02-226-012-H00. PERFORMED NDT SPOT FLOURESCENT PENETRASDR UIEA2021032700724Engine · vibrationLH ENGINE @ CLIMB POWER 104.2 N1 A VIB 3.5(<P>ENGINE VIB WITHIN LIMITS IAW AMM 71-00-00. TEST 6. ALSO PERFORMED GVI INSPECTION IAW AMM 72-00-00</P>)SDR UIEA2021032100666Lead · damagedENG #2 UPPER HI TENSION LEAD DAMAGED(<P>REMOVED AND REPLACED #2 ENG UPPER HI TENSION LEAD IAW B767-300 AMM 74-21-01 NOTE. OPS CHK GOOD.</P>)SDR UIEA2021031400550Lead · cracked#2 ENGINE LOWER IGNITER LEAD END SHIELD IS CRACKED(<P>REMOVED AND REPLACED #2 ENGINE LOWER IGNITION LEAD IAW AMM 74-21-01. PENDING OPS CHECK.</P><P>PERFORMED OPS CHECK, GOOD.</P>)SDR UIEA2021031600600Liner · crackedENGINE # 2 S/N 702954 COMBUSTION CHAMBER OUTER LINER BETWEEN 7 TO 8 O'CLOCK POSITION HAS A TWO PANEL CRACK BETWEEN PANEL # 1 AND PANEL # 2. REQUIRES RE-INSPECTION EVERY 200 CYCLES PER W/C # A-72-307-C1-2 TABLE 3(<P>TRANSFERRED ITEM TO MCI A-001</P>)SDR UIEA2021031200524Igniter · failedNO LIGHT OFF ON #2 ENGINE, PLACED ENGINE START SELECTOR TO BOTH. SUCCESSFUL START ON 2ND ATTEMPT.(<P>REMOVED AND REPLACED IGNITER RIGHT UPPER PLUG REF AMM 74-21-02-004-005-H00 AMM 74-21-02-404-006-H00. OPS CHECK GOOD.</P>)SDR UIEA2021030800488Filter · warning messageON CLIMB OUT RECEIVED "R ENG FUEL FILT" EICAS MSG. COMPLIED W/ QRH. ALL ENGINE INDICATIONS NORMAL.(<P>REMOVED AND REPLACED RH ENG FUEL FILTER IAW AMM 73-11-02. PERFORMED IDLE RUN OF RH ENG IAW AMM 71-00-00. NO MESSAGES NOTED AT THIS TIME. NO LEAKS NOTED OPS CHSDR UIEA2021030800486Pressure Switch · malfunctionedDURING PRE-FLIGHT CHECKLIST FOUND LH ENG PRESSURE WARNING LIGHT NOT EMITTING.(<P>REMOVED AND REPLACED LH ENG LOW OIL PRESSURE WARNING SWITCH IAW AMM 79-33-01. OPS CHECK GOOD. LIGHT EMITTS.</P>)SDR UIEA2021030300467Seal · exposed#1 ENGINE INLET PROBE SEAL EXPOSED (TRIMMED). TRIMMED #1 ENGINE INLET COWL SEAL IAW SRM 51-00-00 AND GMM 3.2.39. OPS CHECK GOOD AT THIS TIME AND PLACED ON NON MEL. REF GMM 3.2.39 AND 3.2.40. DATE 3 MAR 21- LP 1312700 ITEM 5 - SCK - ITEM TO BE REPLACED WITHIN SDR 2LCF20210227Adi · odorON FEBRUARY 27, AIRCRAFT N542LA DURING THE CRUISE PHASE ON THE MIA - CJC ROUTE (UC-1307) MOMENTARILY TURNED OFF THE ADI OF THE CAPTAIN'S POSITION AND FOLLOWED BY A SHORT-CIRCUIT NOISE AND SMELL OF SMOKE IN THE CABIN; THE CREW MADE THE DECISION DIVERT TO PTY’S SDR UIEA2021022200391Anti-Ice Valve · inoperativeBTB RT ENG A/I VALVE WOULD NOT OPEN. PERFORMED FIM 30-21TASK 806. FOUND A/I CONTROL TO CHECK OK. VERIFIED A/I VALVE POSITION OF NR 2 ENGINE AND PERFORMED VALVE OPS CHECK IAW AMM 30-21-03 AND 36-11-09. OPS CHECK GOOD AT THIS TIME.SDR UIEA2021020400229Engine · vibrationABOVE FL 250 KIAS AIRFRAME VIBRATION WITH LOW TONE HUMMING, OCCURS CONTINUOUSLY THROUGHOUT THE FLIGHT DURING CLIMB. N1 (R) AT 1.4 UNITS VIBRATION.(C/W AIRFRAME VIBRATION CONDITIONAL INSPECTION PART 2 77-31-02 FOR ENG 2. LOCKS AND RING SECURE. PERFORMED VISUSDR P5CA2021012900032Fire Loop · false activationSTATUS MESSAGE "RT ENGINE FIRE L1" AFTER ROTATION GOES AWAY AT THE TOP OF DESCENT. HAPPENED LAST TWO FLIGHT LEGS. DUE TO HISTORY AND PREV ACTIONS/TS TAKEN. RESET FIRE DETECT. CARD M689. NO PRESENT LEG FAULT, IAW AMM 26-11-00.SDR UIEA2021012900149Card · warning messageRT ENGINE SPEED CARD MESSAGE. PERFORMED ENG SPEED CARD TEST, PER FIM 73-21 FAULT TREE 871. OPERATIONS CHECK GOOD. PERFORMED ENGINE RUN ON NR 2 ENGINE, PER AMM 71-00-00-862-053-H03. OPERATIONS CHECK GOOD. VERIFIED NO FAULTS WERE FOUND DURING OPERATIONS CHESDR UIEA2021012800143Igniter · failedRT ENGINE WOULD NOT LIGHT OFF ON SINGLE IGNITOR. NORMAL START WITH IGNITOR IN BOTH. STATUS MESSAGE R ENG IGNITOR 2. REMOVED AND REPLACED NR 2 ENGINE IGNITOR PLUG. OPERATIONS CHECK GOOD, IAW AMM 74-21-02 & 74-00-00.SDR UIEA2021020100169Sensor · failedRIGHT ENGINE SPEED CARD STS MSG. R & R RT ENGINE N2 SPEED CARD OFF PN 285T0458-303, SN D04761. OPS CHECK NORMAL IAW AMM 73-21-54. MSG CLEARED. 28JAN21 LOG PG 1271503 ITM 5 MIA; R & R RIGHT ENGINE N2 SPEED SENSOR. OPS CHECK NORMAL IAW AMM 77-12-02. PERFORMSDR UIEA2021012700137Eec · fault messageRT ENGINE EEC MSG AFTER START. RESET EEC (RT). OPERATIONS CHECK GOOD, IAW 71-00-00.SDR UIEA2021020100174Tail Cone · oil consumptionREF 74069-NR-0023 RIGHT NR 2 ENG HAS OIL IN TAIL CONE. AFTER FURTHER EVALUATION AND BORESCOPE OF NR 2 ENG CRF IAW B767 AMM 72-00-00-206-175-H00 FOUND OIL WETTING ON SUMP SCAVENGE TUBE AND AT JOINT BETWEEN THE SUMP OUTER WALL AND THE CRF, 6 O'CLOCK POS, WITH TSDR P5CA2021012500025Idg · failedDURING TAKEOFF ROLL, INITIATED A LOW SPEED AT 55 KTS, REJECTED TAKEOFF FOR RT GEN OFF AND RT GEN DRIVE EICAS MESSAGES. TRANSFERED TO MDDR 141408, REF POLAR DDG 24-00-01-01, CAT B, DUE 28 JAN21. MCC NOTIFIED, PLACARDS INSTALLED. MX ACTION C/W. REMOVED AND RSDR UIEA2021012700133Line · leakingUPON ARRIVAL, RIGHT ENGINE OIL QUANTITY LOW. PERFORMED HI-POWER ENGINE RUN LEAK CHECK, PER MCC REQUEST IAW 767 AMM. TWO LEAKS NOTED ON D-SUMP SUPPLY LINE. REMOVED, INSPECTED, AND CLEANED SCAVENGE INLET SCREEN ASSEMBLYS, LUBE FILTER, AND MAGNETIC ISOLATOR PLSDR P5CA2021012300024Circuit Card · malfunctionedRT ENGINE FIRE LP 2 EICAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CARD FILE, PRINTED CIRCUIT BOARD, IAW AMM 26-10-01. OPERATIONS CHECKS GOOD. EICAS MESSAGE NO LONGER VISIBLE.SDR P5CA2021012300023Circuit Card · malfunctionedRT ENGINE FIRE LP 1 EICAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CARD FILE, PRINTED CIRCUIT BOARD, IAW AMM 26-10-01. OPERATIONS CHECKS GOOD. EICAS MESSAGE NO LONGER VISIBLE.SDR UIEA2021012500119Module · not seatedIDLE DISAGREE EICAS MESSAGE ON LT ENGINE AFTER START. RE-RACKED THE PIMU MODULE. RAN LT ENG AT IDLE PER 71-01-02. OPERATIONS CHECK GOOD. NO EICAS MESSAGES AT THIS TIME. PIMU RE-RAKED, IAW AMM 77-35-02, MESSAGE CLEARED, PER AMM 31-41-00.SDR P5CA2021012200018Oil System · lowRT GEN OFF ON TAKEOFF. DEFERRED PER MEL 24-00-01-01, DMI 141247, 25JAN21, CAT B. PLACARD INSTALLED. UPON VISUAL INSPECTION FOUND THE NR 2 IDG LOW ON OIL, SERVICED IDG WITH 3 QTS, IAW AMM 12-13-03. THIS CLEARS DMI 141247. MCC NOTIFIED AND PLACARD REMOVED.SDR P5CA2021012200020Engine · damagedOIL FOUND IN RT EXHAUST CONE AND SPINNER DAMAGED. RT ENGINE CHANGE COMPLETE, IAW WORK CARD A-71-999-09-02. ENGINE RUNS ARE GOOD AT THIS TIME.SDR DALA2021011900333Eec · faultedDUE TO AUTO-THROTTLE INOPERATIVE ALONG WITH VNAV DATA ISSUES AND SPEED RESTRICTED. CORRECTIVE ACTION: FOUND LEFT ENGINE EEC FAULT, REPLACED LEFT ENGINE EEC AND FMC PER B767AMM. DURING OPERATIONAL CHECK, FOUND LEFT ENGINE CHANNEL A BLANK. PIMU FAULTS CHANNELSDR UIEA2021011900086Skin · dentedNR 1 ENGINE INLET HAS SEVERAL DENTS ON INNER BARREL SLEEVE. REMOVED AND REPLACED NR 1 ENGINE INLET COWL ASSEMBLY, IAW B767 AMM 72-33-02.SDR UIEA2021011900090Filter · unknownLT FUEL FILTER EICAS MESSAGE. REMOVED AND REPLACED LT ENGINE FUEL FILTER ELEMENT, PER AMM 73-11-02. MESSAGE CLEARED. LEAK CHECK GOOD.
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