GE CF6-80C2B7F
Service difficulty reports · 405
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 = 'CF680C2B7F' 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 = 'CF680C2B7F' 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 P5CA2021020800038Warning Message · false activationR OIL FILTER STATUS MESSAGE DISPLAYED(<P>PERFORMED R ENG OIL FILTER BYPASS WARNING TEST IAW B767 AMM 79-35-00.OPS CHECK GOOD.NO DEFECTS NOTED AT THIS TIME. PERFORMED VISAUL INSPECTION ON R ENG OIL FILTER. NO DEFECTS NOTED AT THIS TIME.<BR /></P>)SDR UIEA2021020500233Pressure Switch · malfunctionedRIGHT ENG TAI EICAS MESSAGE.(<P>TRANSFERRED TO MEL 30-21-01-04-02, MDDR 141976, CAT "C". DUE DATE 15FEB21. T&I TJ: 21:42Z.</P><P>05JAN, RIV, LP 1246922, ITEM M3: REMOVED AND REPLACED RT ENGINE ANTI-ICE VALVE IAW AMM 30-21-03. OPS CHECK IS GOOD AT THIS TIME. ITSDR P5CA2021012800029Connector · looseRT ENGINE FIRE LOOP 1 STATUS MESSAGE DISPLAYED ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120). TRANSFERED TO MDDR 141557, IAW DDG 26-11-01-01, CAT C, DD 07FEB21. FOUND LOOSE CONNECTOR AT LOWER LOOP RT SIDE, SECURED CONNECTOR. OPERATIONS SDR UIEA2021012400112Switch · failedREV DISPLAYED ABOVE LEFT ENGINE N1 GAUGE NORMAL REVERSE WORKED ON LANDING. TRANSFERED TO MDDR 141401, IAW MEL 78-31-01 CAT C, DUE 04FEB21 PLACARD INSTALLED MX PROCEDURE C/W. REMOVED NR 1 TR OUTBOARD SWITCH, PER B767 AMM 78-36-01 AND REPLACED W/78-36-01. OPESDR UIEA2021012500121Filter · failed"RT ENGINE FUEL FILT" MESSAGE ON EICAS. REMOVED AND INSPECTED RT ENGINE FUEL FILTER, IAW B767 AMM 73-11-02, NO VISIBLE CONTAMINATION FOUND. INSTALLED NEW FILTER, IAW B767 AMM 73-11-02-404-008. LEAK CHECK GOOD, WET MOTOR NR 2 ENGINE PERFORMED, IAW AMM 71-00-SDR UIEA2021011500059Igniter · wornDURING BORO INSPECTION FOUND NR 2 ENGINE UPPER IGNITER WITH EXCESSIVE TIP WEAR. REMOVED AND REPLACED NR 2 ENGINE UPPER IGNITER PLUG, IAW AMM 74-11-01.SDR IPXA2020123063959Shutoff Valve · malfunctionedINSPECTION TYPE: N/A ATB, LANDED UNEVENTFUL. NO EMEGENCY DECLARED. AFTER T/O THROUGH 5,000 LT ENGINE HPSOV EICAS L/BLEED LIGHT ILLUMINATED RAN QRH AIR TURNBACK SDF DUE TO ICING AT MCI. EICAS/BLEED REILLUMINATED AT FL 340 AND REMAINED AFTER QRH PROCEDURE, FOSDR IPXA2020123063945Shutoff Valve · malfunctionedINSPECTION TYPE: N/A ATB. LANDED UNEVENTFUL, NO EMERGENCY DECLARED. LT ENGINE HPSOV EICAS MESSAGE DISPLAYED AT B6000 FT BLEED LIGHT REILLUMINATED AFTER BLEED LIGHT REILLUMINATED AFTER QRH PROCEDURE COMPLETED. AVOIDED ICING CONDITION, PER QRH. REMOVED AND RSDR IPXA2020122963918Warning Message · false activationINSPECTION TYPE: N/A, DIVERSION, NO EMERGENCY DECLARED. DURING ARRIVAL BOTH "LT & RT ENGINE AI VALVE" MESSAGES OCCURED. MESSAGES CLEARED BY THEMSELVES BUT RE-APPEARED. DIVERTER DENVER TO PHOENIX DUE TO ICING IN DENVER TERMINAL AREA. T/S PER FIM 30-11-00-99SDR UIEA2020121502584Engine · damagedNR 1 ENGINE REQUIRES TO REMOVE BLADES FOR FACILITATE REPAIR AND RE-INSTALL AS REQUIRED. REMOVED NR 1 ENGINE BLADES 8EA ,IAW B767 AMM 72-31-02. RE-INSTALLED 8 BLADES, AS PER AMM 72-31-02 ON ENGINE NR 1. PENDING RE-TORQUE POST ENGINE RUN. PERFORMED SPINNER RSDR UIEA2020121502576Packing · leakingENGINE NR 1 WITH EVIDENCE OF OIL LEAK COMING FROM NR 1 BEARING MANIFOLD. REMOVED AND REPLACED PACKINGS AT ENGINE NR 1 MANIFOLD BEARING, IAW 767 AMM 72-31-03, PENDING LEAK CHECK. PERFORMED ENGINE IDLE RUN, IAW 767- AMM 71-00-00, NO LEAKS NOTED.SDR UIEA2020121502572Rod · wornNR 1 ENGINE AFT STRUT OUTBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD SUPPORTING HARDWARE IS WORN AND HAS TOO MUCH PLAY. REMOVED AND REPLACED DAMAGED HOLD OPEN ROD AT NR 1 ENGINE AFT STRUT OUTBOARD ACCESS PANEL DOOR, PER B767-300 AMM 20-11-00-910-802.SDR UIEA2020121502571Rod · damagedNR 2 ENGINE AFT STRUT INBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD DAMAGED. REMOVED AND REPLACED DAMAGED HOLD OPEN ROD AT NR 2 ENGINE AFT STRUT INBOARD SIDE ACCESS PANEL, PER B767-300 AMM 20-11-00-910-802.SDR UIEA2020121502570Rod · missingNR 1 ENGINE AFT STRUT INBOARD HYDRAULIC ACCESS PANEL HOLD OPEN ROD IS MISSING. LOCATED AND INSTALLED NEW HOLD OPEN ROD AT NR 1 ENGINE AFT STRUT INBOARD ACCESS PANEL DOOR, PER B767-300 AMM 20-11-00-910-802.SDR UIEA2020121502569Liner · delaminatedNR 1 ENGINE INLET AT POSITION 4 O'CLOCK ACOUSTIC PANEL FOUND DELAMINATED. REMOVED AND REPLACED DAMAGED ACOUSTIC PANEL LINER AT NR 1 ENGINE INLET AT POSITION 4 O'CLOCK, PER B767-300 AMM 72-33-01-004-001-H00 AMM 72-33-01-004-011-H00.SDR IPXA2020121463392Engine · failedINSPECTION TYPE: NA ATB-EMERGENCY DECLARED, NO EQUIPMENT USED. A/C WAS TAKEN OUT OF SERVICE. ON DEPARTURE AT 1500' AGL AFTER SELECTING VNAV RT ENGINE N1 ROLLED BACK TO 27% LOUD S RUMBLE IN AIRCRAFT W/POWER LOSS IN RT ENGINE. ENGINE RAN AT IDLE LEFT UNTIL CLSDR UIEA2020121402565Channel · damagedENGINE PYLON NR 1 AND NR 2 INBOARD AND OUTBOARD DOORS HOLD OPEN RODS CHANNEL DAMAGED. REMOVED AND REPLACED 4 EA DAMAGED CHANNEL AT ENGINE PYLON NR 1 AND NR 2 INBOARD AND OUTBOARD DOORS BY HOLD OPEN ROD, PER B767-300 SRM 51-40-02-0G-0.SDR UIEA2020121402559Gasket · leakingNR 2 ENGINE FUEL LEAK IN IDG FUEL/OIL COOLER LOCATED IN PORT OF FUEL IN. REMOVED AND REPLACED NR 2 ENGINE IDG FUEL/OIL HEAT EXCHANGER "FUEL IN " TUBE GASKET, IAW AMM 24-11-10 PENDING LEAK CHECK. ACCOMPLISHED ENGINE IDLE RUN, IAW 767 AMM 71-00-00, NO LEAKS NOSDR UIEA2020121402553Start Valve · slowL START VALVE SLOW TO OPEN. PERFORMED ENGINE RUN OF LT ENGINE, IAW AMM 71-00-00 AND AMM 80-11-00/501 STARTER VALVE IN TRANSIT FOR APPROXIMATELY 4 SECONDS. ALL SYSTEM OPERATIONS NORMAL. NO DEFECTS NOTED AT THIS TIME.SDR UIEA2020113002474Engine · power lossBELOW 5000 ON ARRIVAL AMBER IDLE DISAGREE MESSAGE DISRUPTED LT ENGINE WAS 28% WHEN RT ENGINE WAS 40%. PERFORMED LT & RT ENGINE PIMU BITE PROCEDURE 71-01-01 FT 810. NO FAULTS ON EITHER PIMU BITE. NO IDLE DISAGREE MESSAGE DISPLAYED NO FAULTS AT THIS TIME.SDR UIEA2020112302450Acoustic Liner · damagedRT ENGINE ACOUSTIC PANEL AFT OF FAN BLADE AT 08:00 POSITION HAS DAMAGE 18" L X 6" W, AT 11:00 POSITION HAS DAMAGE 12" L X 3.5" W, AT 04:00 POSITION HAS DAMAGE 7" L X 8" W, AT 02:00 POSITION HAS DAMAGE 3.5" L X 8" W, AT 06:00 POSITION HAS DAMAGE 9.5" L X 3" W. SDR UIEA2020111202386Seal · debondedSEALANT DISBONDED ON NR 1 ENGINE FWD OUTER ACOUSTIC PANEL 2 O`CLOCK POSITION. TRANSFERRED TO NON MEL 137644, PER AMM 72-00-00 TABLE 640, GOOD FOR 10F/C. APPLIED SEALANT TO ACOUSTIC LINER SEGMENT ON NR 1 ENGINE 2 O`CLOCK POSITION, IAW AMM 72-33-01. THIS CLEASDR UIEA2020110902374None · noneLEFT ENGINE APPEARS TO BE STRUCK BY BIRD. DUE TO BIRD STRIKE ON NR 1 ENGINE CONDITIONAL INSPECTION REQUIRED. INSPECTED NR 1 ESN 702640 FOR BIRD STRIKE, IAW B767 AMM 72-00-00. FOUND NO DAMAGE BY BIRDSTRIKE WITHIN THE LPC OR HPC. C/W CONDITIONAL BIRD STRIKE SDR UIEA2020110902365Acoustic Liner · damagedFOUND DAMAGE ON ACOUSTIC LINER ON NR 1 ENGINE 2 O'CLOCK POSITION. CONTINUES OPERATIONS LIMIT, IAW 72-00-00. 10 FLT CYCLES. EXAMINED THE LINE SEGMENT AND FOUND MISSING PIECES. NO MISSING PIECES ARE PERMITTED, IAW AMM 72-32-00. TRANSFERED TO NON MEL 137410.SDR UIEA2020110602358Starter · failedRT ENGINE STARTER WOULD NOT ACCEPT OIL DURING STARTER OIL CHANGE, WC A-80-301-00-02 AS PART OF WO 72732. REMOVED AND REPLACED RT STARTER ASSEMBLY, IAW 80-11-01. STARTER OIL SERVICED, IDLE LEAK TEST GOOD, REF 71-00-00.SDR UIEA2020110102342None · noneIN FLIGHT, FL 370 1700Z SAT -50 DEG C, LEFT ENGINE VIBE MONITOR INDICATED "FAN" 5.0 (FULL SCALE DEFLECT). TRANSFERRED TO MDDR NR 137066, IAW MEL 77-31-01, CAT C DUE DATE 11NOV20. MCC NOTIFIED EH. PLACARDS INSTALLED. T+I 2108Z CW. PERFORMED LT ENGINE VIBRASDR UIEA2020102902334Accelerometer · malfunctionedIN FLIGHT LEFT VIB INDICATOR ERRATIC INDICATIONS FROM .5-5.0 NO ACTUAL VIB FELT. ALL OTHER INDICATIONS NORMAL. TRANSFERRED TO MDDR 136877, IAW DDG 77-31-01 CAT "C", DUE 08NOV20. INSTALLED ALTERNATE/EXTERNAL NR 1 ACCELEROMETER, IAW AMM 77-31-01 (LT ENGINE). SDR UIEA2020102902336Skin · delaminatedRIGHT ENGINE INBOARD IN COWL HAS DELAMINATED SKIN (UNDERNEATH) ABOUT 52 INCHES BY 17 INCHES. REMOVED AND REPLACED RT ENGINE INBOARD FAN COWL, PER AMM 71-11-04/401. LATCHES ADJUSTED, PER AMM 71-11-05. OPERATIONS CHECK OK.SDR UIEA2020102602306Fastener · looseRIGHT ENGINE VIBRATION INDICATOR SHOWING 0.2-3.1 FOR 30 SECONDS DURING CLIMB. OSCILLATING, NO VIBRATIONS FELT. PERFORMED EXTERNAL ENGINE INSPECTION, IAW AMM 72-00-00. FOUND LOOSE FASTENERS ON INNER ACOUSTIC PANELS, SECURED FASTENERS, IAW AMM 72-53-01.SDR UIEA2020102402293Ecu · malfunctionedRT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REMOVED AND REPLACED ECU. OPERATIONS CHECKS NORMAL, IAW AMM 73-21-15. PERFORMED ENGINE RUN-UP, OPERATIONS CHECKS NORMAL. NO FAULTS NOTED, IAW AMM 71-00-00.SDR UIEA2020102302292Connector · damagedIN CRUISE AT FL370 LEFT ENGINE FAN VIB INDICATIONS RANGED ERRATICALLY FROM 0.4-5.0 FOR APPROXIMATELY THREE MINUTES. NO ACTUAL VIBRATION FELT. TRANSFERRED TO MDDR 136585 MEL 77-31-01, CAT C DUE DATE 01NOV20. RS 2107Z 25OCT, ILN MX. REMOVED AND REPLACED ENGISDR UIEA2020101902277Warning Light · false activationRT ENGINE ANTI ICE VALVE LIGHT ON SHUT DOWN. C/W OPERATIONS CHECK OF RT ENGINE ANTI ICE SYSTEM, IAW AMM 30-21-00. OPERATIONS CHECK GOOD, NO FAULTS NOTED. OK FOR SERVICE.SDR UIEA2020101502260Cable · damagedLT ENGINE W11 AND W12 CABLE ASSEMBLYS HAVE HEAT DAMAGE IN THE AREA NEAR BOTH COUPLING SEAT OF 8TH STAGE MANIFOLD. REMOVED AND REPLACED W11 CABLE, IAW B767 AMM 73-21-18-804-099-H00, 73-21-18-004-088-H00, 73-21-18-404-92-H00, NO FAULTS NOTED. REMOVED AND REPLASDR UIEA2020100802195Sensor · fluctuatesRT ENG OIL TEMP FLUCTUATING IN FLIGHT TO 0 DEG C, ALWAYS SHOWED LESS THAN LT ENGINE ON START. RT ENGINE OIL TEMP FLUCTUATING UP TO -17 DEG C. REMOVED AND REPLACED RIGHT ENGINE OIL TEMP SENSOR. OPS CHECKS GOOD, IAW AMM 79-34-01.SDR UIEA2020092542063Fuel Line · leakingON POST FLIGHT WALK AROUND FOUND FUEL LEAK RT ENGINE. ON RIGHT ENG RETORQUED & "FUEL IN" TUBE ON IDG FUEL OIL HEAT EXCHANGER, IAW 24-11-10. RAN ENG, PER 71-00-00, LEAK CK GOOD.SDR P5CA2020092540321Warning System · false indicationUPON START NR 1 ENGINE (LEFT SIDE) THE EGT INITIALLY ACCELERATED ABNORMALLY QUICKLY AND STABILIZED AROUND 430 F EGT. INSPECTED NR 1 ENG'S INLET & EXHAUST AREA AND NO TROUBLE FOUND. NO EGT EXCEEDANCE MSG FOUND ON ENG EXCD PAGE. PERFORMED PIMU BITE PROCEDURE SDR UIEA2020092512027Sealant · deterioratedNR 2 ENGINE INBOARD AND OUTBOARD T/R COWLING INNER SIDE PROTECTOR HEAT SEALANT IS DETERIORATED, MISSING IN SEVERAL AREAS. PREPARED, CLEANED, AND REPAIRED PROTECTOR HEAT SEALANT NR 2 ENG INBOARD AND OUTBOARD T/R COWLING INNER SIDE, PER B767-300 AMM 78-31-00-30SDR UIEA2020092212041Acoustic Liner · damagedRIGHT ENGINE ACOUSTIC LINER DAMAGED AFT OF FAN BLADES 6 O'CLOCK POSITION. OK TO CONTINUE, IAW AMM 72-00-00-206-167-H00 FOR UP TO 10 FLIGHT CYCLES OR 100 FLIGHT HOURS, WHICHEVER COMES FIRST. TRANSFERRED TO MDDR 134661 NON MEL, IAW AMM 72-00-00-206-167-H0. RESDR UIEA2020091702016Manifold · damagedLEFT ENGINE TCC DUCT IS DAMAGED. ITEM TRANSFERRED TO MDDR 134586, IAW DDG 75-24-01, CAT C DUE 27SEP20. LT ENGINE TURBINE COOLING SYSTEM INOPERABLE. REMOVED DAMAGED INLET MANIFOLD AND INSTALLED NEW INLET MANIFOLD, IAW AMM 75-24-03-404-037-H00; 75-24-03-004-0SDR UIEA2020091001974Seal · leakingNR 2 ENGINE 1ST STAGE ROTO DISK FAN SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 2 ENGINE FAN HUB MANIFOLD SEAL, PER MM 72-31-03-404-005-H00. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.SDR UIEA2020091441975Packing · leakingNR 1 ENGINE 1ST STAGE ROTO DISK SHAFT HAS OIL LEAKS. REMOVED AND REPLACED NR 1 BEARING MANIFOLD PACKING ON NR 1 ENGINE, IAW 767 AMM 72-31-03. PENDING ENGINE IDLE, RUN LEAK TEST. OPERATED ENGINE PER MM 71-00-00-862-053-H03. NO LEAKS NOTED.SDR P5CA2020091070303Transmitter · malfunctionedLT ENG AFTER START 160 PSI (TOP OF SCALE), ALL OTHER INDICATIONS NORMAL. LEFT ENGINE OIL PRESSURE TRANSMITTER REPLACED, AS PER AMM 79-32-21. ENGINE SPIN CHECK OK, INDICATION NORMAL.SDR UIEA2020091101978Blade · chippedNR 2 ENG NR 6 BLADE LEADING ENGINE IS CHIPPED. PERFORMED BLEND REPAIR ON RT ENG NR 6 BLADE, IAW AMM 72-31-02. NO FURTHER DEFECTS NOTED.SDR UIEA2020090101910Start Valve · malfunctionedRIGHT STARTER CUTOUT AND RT ENG STARTER EICAS CAUTION INTERMITTENT INFLIGHT. FL 350. PREVIOUS WRITE UP PAGE 1160322. REMOVED AND REPLACED RH ENG. START VALVE IAW AMM 80-11-02 OPS CHECK GOOD</P>)SDR UIEA2020082871878Computer · faultedRT STARTER CUT OUT MSG CAUTION INTERMITTENT AT 31,000 FT. MSG CAUSED BY FAULTY L EICAS COMPUTER. REF ITEM #3 FOR REPLACEMENT OF EICAS COMPUTER, RAN RT ENGINE IAW AMM 71-00-00. OPS CHECK GOOD. RT STARTER CUTOUT MSG DID NOT RETURN. ITEM 3: REMOVED AND REPLACEDSDR UIEA2020082401862Blade · damagedL/H ENG ACOUSTICAL PANEL SHOWING HONEY COMB AT 8 O'CLOCK POSITION EVALUATED LH ENG, FOUND PANEL OUT OF LIMITS. REMOVED SPINNER BLADES 1-7 AND ACOUSTIC PANELS IAW B767 AMM 72-33-01. PANELS, BLADES AND SPINNER INSTALLATION STILL REQ. M4 ENTRY CONTINUED ON LOG PASDR UIEA2020082491815Shutoff Valve · malfunctionedUPON ENG START, "R ENG BLEED OFF" CAUTION MSG APPEARED AND REMAINED ILLUMINATED TRANSFERRED TO MDDR # 133090 PER MEL 36-11-01-02A, CAT C, DUE 29AUG20. PLACARD INSTALLED. LP 1279625 ITEMS 7,8,9: REMOVED RH PRSOV IAW AMM 36-11-09. PRSOV IN PYLON BUT NOT INSTALLESDR UIEA2020081901817Circuit Card · malfunctionedSTATUS MSG L ENG FIRE LOOP 1(<P>ISSUED MDDR 133103 IAW MEL 26-11-01-01, CAT C, DUE 29AUG20.</P><P>LP 1297199: PERFORMED VISUAL INSPECTION ON LOWER FWD ENG #1 FIRE DETECTOR. FOUND DETECTOR ELEMENT TOUCHING THE SUPPORT TUBE IAW FIM 26-11 FT 802. READJUSTED ELEMESDR IPXA2020081859189Actuator · damagedFOUND DAMAGE ON THE NR 1 ENGINE THRUST REVERSER UPPER ACTUATOR CLEVIS FITTING REF DEFERRAL M 716678. EO B767-7830-77544A C/W. PLACED ON DEFERRAL PER EO B767-7830-77544-A. REMOVED TRANS NR 1 ENG OUTBOARD TRANSCOWL, IAW AMM 78-1-10-401. INSTALLED TRANSCOWL UPSDR UIEA2020082171792Drain Mast · missingON WALK AROUND FOUND # 2 ENG DRAIN MAST MISSING(<P>IAW AMM 71-71-01 INSTALLED DRAIN MAST ON #2 ENG. OPS NORMAL AT THIS TIME.<BR /></P>)
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