GE CF6-80C2B1F
Service difficulty reports · 768
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 = 'CF680C2B1F' 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 = 'CF680C2B1F' 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 U2RA202007090001Skin · crackedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-53A2390, CRACKED FASTENER HOLES WERE NOTED AT SKIN PANEL UNDER LONGERON EXTENSION FITTING 1 EACH BODY STATION 1480 STRINGER S-32L AND 1 EACH AT BODY STATION 1480 BETWEEN STRINGERS S-32R AND S-34R. REPAIR ACSDR U2RA202007090002Exhaust Duct · crackedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-02, A DENT WAS NOTED ON THE OUTER SKIN OF THE NUMBER 2 ENGINE EXHAUST SLEEVE, NACELLE STATION 318 NEAR 7 O`CLOCK POSITION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMSDR U2RA202007090003Skin · crackedDURING ACCOMPLISHMENT OF TASK 57-810-01-01, A CRACK WAS NOTED ON THE SKIN OF THE LEFT WING INBOARD FIXED LEADING EDGE NOSE BEAM CUTOUT, ADJACENT TO THE NUMBER 11 KRUEGER FLAP INBOARD LINK, LEADING EDGE ILES 543.93. REPAIR ACCOMPLISHED, IN ACCORDANCE WITH FLIGSDR U2RA202007080001Skin · deformedDURING ACCOMPLISHMENT OF TASK CARD 32-820-01-01, RIGHT WING LANDING GEAR FORWARD PRIMARY DOOR INNER SKIN WAS NOTED AS DEFORMED. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20289.SDR U2RA202007080004Skin · corrodedDURING ACCOMPLISHMENT OF TASK CARD 55-820-01-01, CORROSION WAS NOTED ON THE SKIN OF THE RIGHT HORIZONTAL STABILIZER UPPER SURFACE AT STABILIZER STATION 385 STRINGER 5. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20322-1.SDR U2RA202007070001Skin · corrodedDURING ACCOMPLISHMENT OF TASK CARD 57-570-00-04, CORROSION WAS DISCOVERED ON THE UPPER FACE OF RIGHT WING OUTBOARD AILERON LEADING EDGE SKIN AT WBL 998 TO WBL 1023. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20320-1.SDR U2RA202007070002Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 57-888-01-01, A CRACK WAS NOTED ON THE UPPER FACE OF RIGHT WING INBOARD FIXED LEADING EDGE NOSE SKIN, ILES 630. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20320-3.SDR U2RA202007070003Strap · corrodedDURING ACCOMPLISHMENT OF TASK CARD 53-630-00-07, CORROSION WAS NOTED ON NUMBER 4 MAIN ENTRY DOOR AREA FRAME STRAP AT BODY STATION 1660 STRINGER S-26L. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20287-1.SDR U2RA202007070004Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-02, CHAFING WAS NOTED ON NUMBER 2 ENGINE RIGHT THRUST REVERSER CORE COWL TRAILING EDGE INNER UPPER SIDE CLOSE OUT PANEL. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-4.SDR U2RA202007070005Torque Box · wornDURING ACCOMPLISHMENT OF TASK CARD 71-812-01-02, NR 2 ENGINE RIGHT THRUST REVERSER TORQUE BOX UPPER CABLE BOLT HOLE WORN WAS NOTED AS WORN. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316-7.SDR U2RA202007070006Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 57-810-01-01, A CRACK WAS NOTED ON THE LEFT WING INBOARD FIXED LEADING EDGE NOSE BEAM CUTOUT, ADJACENT TO THE NUMBER 12 KRUEGER FLAP INBOARD LINK, ILES 445.5. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTINGSDR U2RA202007070007Skin · wornDURING ACCOMPLISHMENT OF TASK CARD 57-808-01-01, 2 EACH FASTENER WERE NOTED AS LOOSE ON THE LEFT WING INBOARD FIXED LEADING EDGE NOSE SKIN, OUTBOARD SIDE, ILES 330. REPAIR ACCOMPLISHED IN ACCORDANCE WITH B747SF STRUCTURAL REPAIR MANUAL 57-41-01-2R-5, WITH DEVSDR U2RA202007070008Skin · wornDURING ACCOMPLISHMENT OF TASK CARD 57-888-01-01, FASTENER NOTED AS LOOSE ON THE RIGHT WING INBOARD FIXED LEADING EDGE NOSE SKIN, OUTBOARD SIDE, ILES 330. - REPAIR ACCOMPLISHED IN ACCORDANCE WITH B747SF STRUCTURAL REPAIR MANUAL 57-41-01-2R-5, WITH DEVIATIONS INSDR U2RA202007070009Skin · deformedDURING ACCOMPLISHMENT OF TASK CARD 57-906-01-01, DEFORMED SKIN WAS NOTED AT INBOARD EDGE OF RIGHT WING NUMBER 18 VARIABLE CAMBER FLAP FOLDING NOSE SKIN. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298.SDR U2RA202009096001Fitting · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-54A2182 POST STRUT MODIFICATION INSPECTIONS OF NUMBER 2 PYLON, CORROSION WAS NOTED ON THE FORWARD UPPER SPAR FITTING AND THE WING FRONT SPAR TO STRUT UPPER LINK FITTING. ACCOMPLISHED REPAIRS IAW STRUCTURAL REPAIR SDR U2RA202009096002Fitting · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-54A2182 POST STRUT MODIFICATION INSPECTIONS OF NUMBER 3 PYLON, CORROSION WAS NOTED ON THE FORWARD UPPER SPAR FITTING AND THE WING FRONT SPAR TO STRUT UPPER LINK FITTING. ACCOMPLISHED REPAIRS IN ACCORDANCE WITH STRSDR U2RA202009086003Web · crackedDURING ACCOMPLISHMENT OF TASK CARD 57-820-01-01, A CRACK WAS NOTED ON LEFT WING CENTER LEADING EDGE NOSE BEAM INBOARD UPPER AT ILES 693.5, UPPER CHORD, LOWER CHORD, AND WEB. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDSDR U2RA202009080604Skin · dentedDURING ACCOMPLISHMENT OF TASK CARD 53-916-01-01, RIGHT APU DOOR EXTERNAL SKIN NOTED AS DENTED, STA 2725, 15 INCHES BELOW APU DOOR HINGE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20309-2.SDR U2RA202009090605Skin · damagedA DENT WITH A NICK WAS NOTED ON THE FUSELAGE SKIN LOCATED APPROXIMATELY BODY STATION 444.5 AT STRINGER S-44L. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING SERVICE REQUEST 4-4843050665 AND ITS ASSOCIATED MESSAGES.SDR U2RA2020090960006Web · crackedA CRACK WAS NOTED IN THE WEB OF THE AFT CARGO COMPARTMENT FLOOR AT BODY STATION 1820 LEFT BUTTOCK LINE 14. ACCOMPLISHED REPAIR IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53-60-07-2R-8 REPAIR 8.SDR U2RA20201016012Fitting · nickedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, NICK NOTED ON NUMBER 2 ENGINE PYLON LFAN COWL AFT SUPPORT BEAM OUTBOARD AREA. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314.SDR U2RA202010160012Link · corrodedDESCRIPTION CORRECTION FOR U2RA202010160012. CORROSION NOTED ON NUMBER 3 PYLON UPPER FORWARD BUSHING. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314-1.SDR U2RA202010190001Bushing · corrodedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-54A2182 REVISION 3, CORROSION NOTED ON NUMBER 3 ENGINE PYLON UPPER LINK FORWARD BUSHING. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314-1.SDR U2RA202010190005Beam · crackedDURING ACCOMPLISHMENT OF TASK CARD 57-820-01-01, A CRACK WAS NOTED ON THE LEFT WING CENTER LEADING EDGE NOSE BEAM INBOARD UPPER AT ILES 693.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 20320-2.SDR U2RA2020070840001Tee Fitting · crackedCRACKS FOUND ON MAIN ENTRY DOOR NR 2 LT/RT SIDE BODY STATION 800 FRAME AFT ANGLE INNER CHORD AND LHS DOOR STOP TEE AT STRINGER S-17 DURING INSPECTIONS PER SERVICE BULLETIN 747-53A2451, REV. 02. ALSO, EXISTING ADDITIONAL FASTENER FOUND ON LT DOOR STOP INTERCOSSDR U2RA2020070840002Skin · dentedDURING ACCOMPLISHMENT OF INSPECTIONS REQUIRED BY TASK CARD 53-804-01-01, A DENT WAS NOTED ON LOWER FUSELAGE EXTERNAL SKIN, AFT CARGO CUTOUT AFT EDGE , BODY STATION 1920, BETWEEN STRINGERS S-36R S-37R. DENT WAS REPAIRED IN ACCORDANCE WITH FLIGHT VEHICLES CONSUSDR U2RA2020090840003Transfer Sys · damagedDURING ACCOMPLISHMENT OF TASK CARD 25-054-01-01, DAMAGE WAS NOTED ON FORWARD CARGO LOADING SYSTEM BALL TRANSFER UNIT. - ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20287.SDR U2RA2020090874004Transfer Sys · damagedDURING ACCOMPLISHMENT OF TASK CARD 25-054-01-01, DAMAGE WAS NOTED ON AFT CARGO LOADING SYSTEM BALL TRANSFER UNIT. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20287.SDR U2RA2020070840005Skin · corrodedDURING ACCOMPLISHMENT OF TASK CARD 57-710-00-01, CORROSION WAS NOTED ON THE CONDUCTIVE STRIP OF THE LEFT WINGLET TRAILING EDGE WEDGE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBERS 20315 AND 20315-1.SDR U2RA2020090840006Retainer · deformedDURING ACCOMPLISHMENT OF INSPECTION REQUIRED BY TASK CARD 57-830-01-01, LEFT WING OUTER LEADING EDGE LOWER FIXED PANEL LEADING EDGE SEAL RETAINER NOTED AS DEFORMED BETWEEN OLES 1545.50 AND WBL 1241. ACCOMPLISHED REPAIR OF SEAL RETAINER IN ACCORDANCE WITH FLIGSDR U2RA202010160011Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-812-00-04, CRACK NOTED ON NUMBER 4 ENGINE PYLON LEFT AFT FAIRING DOOR INNER SURFACE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-9A.SDR U2RA2020101612Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-812-00-01, CRACK NOTED ON NUMBER 1 ENGINE PYLON LEFT AFT FAIRING DOOR INNER SURFACE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-9B.SDR U2RA202009023001Shim · migratedSHIM MIGRATION NOTED ON LEFT WING MAIN LANDING GEAR GATE SUPPORT FITTING DURING FOLLOW ON INSPECTION FOR PREVIOUS SHIM MIGRATION. ACCOMPLISHED SHIM REPLACEMENT IAW BOEING SERVICE REQUEST NUMBER'S 4-4817985813 AND ASSOCIATED MESSAGES.SDR U2RA202009043001Skin · dentedDURING ACCOMPLISHMENT OF TASK CARD 32-836-01-01, A DENT WAS NOTED ON THE SKIN OF RIGHT BODY LANDING GEAR SHOCK STRUT DOOR. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER EO 20289-1.SDR U2RA2020090170001Skin · crackedDURING ACCOMPLISHMENT OF SB 747-53A2305, SKIN CRACKING WAS DISCOVERED NEAR THE LEFT AND RIGHT HAND AFT CORNERS OF THE NOSE WHEEL WELL. ACCOMPLISHED REPAIRS AS OUTLINED IN SERVICE REQUEST 4-4818744620 AND ITS ASSOCIATED MESSAGES.SDR U2RA20200902002Skin · dentedRIGHT WING INBOARD MID FLAP LOWER SKIN HAS MULTIPLE DENTS. ACCOMPLISHED REPAIR IAW FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER EO 20219.SDR U2RA2020050430001Panel · missingNUMBER 4 ENGINE PYLON OUTBOARD SIDE DOOR PANEL MISSING. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20159.SDR U2RA2020050450001Intercostal · damagedAUXILIARY POWER UNIT COMPARTMENT LNTERCOSTAL DAMAGED. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20152.SDR U2RA2020050450002Intercostal · damagedAUXILIARY POWER UNIT COMPARTMENT LNTERCOSTAL DAMAGED. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20152.SDR U2RA2020050450003Intercostal · damagedAUXILIARY POWER UNIT COMPARTMENT LNTERCOSTAL DAMAGED. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20152.SDR U2RA2020050450004Intercostal · damagedAUXILIARY POWER UNIT COMPARTMENT LNTERCOSTAL DAMAGED. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20152.SDR U2RA2020042540001Relay · inoperativeFLAPS CONTROL EICAS MESSAGE DISPLAYED ON FINAL APPROACH. PERFORMED GO AROUND, COMPLETED CHECKLIST AND LANDED WITHOUT INCIDENT. - CENTRAL MAINTENANCE COMPUTER MESSAGES 27600, 27601, AND 27602 FOUND ACTIVE, FLAP CONTROL UNIT LEFT, RIGHT, AND CENTER FAIL. REMOVSDR U2RA2020041650001Thrust Reverser · damagedNUMBER 4 ENGINE INBOARD THRUST REVERSER DAMAGED - ACCOMPLISHED MAJOR REPAIR OF DAMAGE ON NUMBER 4 ENGINE INBOARD THRUST REVERSER HALF. REPAIR COMPLETED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. ENGINEERING ORDER CONTROL NUMBER 20140 REVISION IR DATESDR U2RA2020042040001Skin · damagedFUSELAGE SKIN DAMAGED SECTION 48, BODY STATION 2655 TO 2689, STRINGER 5L TO 11L - ACCOMPLISHED MAJOR REPAIR OF DAMAGE IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. ENGINEERING ORDER CONTROL NUMBER 20138 REVISION A
DATED APRIL 15, 2020, DATA APPROVED ON SDR SAJF2020031609013Turbine Blades · damagedCREW SATCOM INFO AROUND 10,000 FEET A/C FEEL VIBRATION AND CHECK ENGINE-3 LPT VIBRATION SHOW 5.0 AT N2 98% N1 66%. CREW MANUAL SHUT DOWN ENG-3 PER QRH PROCEDURE AND ATB. 1.AFTER LANDING, VISUAL CHECK THE ENGINE EXHAUST AREA FOUND METAL CHIPS AND LPT 5TH BLADESSDR IPXA2020021452120Oil System · leakingDIVERTED NR 3 ENG OIL QUANTITY DROPPED DOWN TO 2 QTS IN FLIGHT. REF LOG PAGE 232822, ITEM 1 ALERT K189826 #3 ENG (S/N 706878) SCHEDULE TO BE REMOVE.REPLACED # 3 ENGINE PER UPS TC 71-000-00-01 & EO M-7320-44176 & E-7900-62890 APPENDIX B. NEW ESN 704393. THIS CSDR SAJF2020024108034Blade · crackedCI-5224 TPE-ANC ENG2 VIBRATION DURING CLIMB, GROUND CHECK FOUND 1 EA LPT 5 BLADE GOT A NICK AND METAL CHIPS AT ENGINE EXHAUST. FURTHER BSI FOUND LPT 3 VANE BROKEN AND SEVERAL LPT 3 BLADE DAMAGED OVER AMM LIMIT. ENGINE NEED TO BE REPLACED. CI MOC FURTHER SENT ASDR P5CA2019122740233Scavenge Pump · contaminatedSHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL QUANTITY. MAINTENANCE NOTED THAT UPON ARRIVAL, OIL QUANTITY RETURNED TO 18 QUARTS. NO LEAKS FOUND. PERFORMED AN INSPECTION OF THE SCAVENGE SYSTEM FILTERS, FOUND DEBRIS IN THE TRANSFER GEARBOX INLET SCREEN TO THE SSDR P5CA2019122300229Engine · failedNR 1 ENGINE FAILED AT 3500 FT MESSAGE ON APPROACH IN RAIN WITH NAI ON ENGINE RESTARTED AUTOMATICALLY. FOLLOWED FIM 71-00 FIGURE 114 FOR AUTO SHUTDOWN EVENT. ALSO FOLLOWED POWERPLANT ENGINEERING GUIDANCE TO ACCOMPLISH BORESCOPE / INSPECTION FOR INTERNAL DAMAGESDR P5CA2019121320227Compressor · stalledAT 20,000 FT, NR 1 ENGINE COMPRESSOR STALLED. ENGINE WAS SHUT DOWN. ATB. REMOVED AND REPLACED THE NR 1 ENGINE IAW AMM 71-00-02. PERFORMED IDLE RUN AND LEAK TESTS IAW AMM 71-00-00, OPS CHECKED SATISFACTORY.
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