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 U2RA2023011000001Fire Warning · false activationMAIN DECK FIRE WARNING, MASTER WARNING AND FIRE BELL ON TAKEOFF ROLL. REJECTED TAKEOFF. FIRE BELL CONTINUED TO SOUND AFTER SILENCED. - NO FIRE PRESENT. DISCOVERED MOISTURE IN CARD FILE M5206 CAUSED BY PALLETS BEING LOADED WET AND WATER DRIPPING INTO THE ELESDR U2RA2023011000002Fire Warning · false activationMAIN DECK FIRE WARNING ACTIVATED AFTER LANDING. NO STATUS OR EICAS MESSAGE SHOWN. - NO FIRE PRESENT. PERFORMED GROUND TEST PER AIRCRAFT MAINTENANCE MANUAL 26-14-00. SYSTEM OPS CHECKS GOOD.SDR U2RA2022122300063Sign · inoperativeLEFT UPPER DECK DOOR EXIT SIGNS INOPERATIVE.SDR U2RA2022122300064Light · inoperative2 EACH UPPER DECK EMERGENCY CEILING LIGHTS INOPERATIVE.SDR U2RA2022121400057Battery Pack · inoperativeLEFT UPPER DECK EMERGENCY DOOR BATTERY OK TEST LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK PER AIRCRAFT MAINTENANCE MANUAL 52-23-14. OPS NORMALSDR U2RA2022120500056Skin · gouged1.125" X 1.0" GOUGE DISCOVERED ON LOWER FUSELAGE SKIN BETWEEN BODY STATION 480 AND 500, BETWEEN STRINGERS 38R AND 39R. - ACCOMPLISHED INTERIM REPAIR PER FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 22204-1 REVISION IR, APPROVED ON FORM 8110-3 DATED 11/25/SDR U2RA2022100400049None · noneLEFT UPPER DECK DOOR BATTERY OK LIGHT WILL NOT ILLUMINATE. TESTED LIGHT PER AIRCRAFT MAINTENANCE MANUAL 52-34-14 AND UNABLE TO DUPLICATE.SDR U2RA2022091600048None · noneLOWER AFT CARGO DOOR LOWER FORWARD CORNER SUSTAINED GROUND DAMAGE - ACCOMPLISHED CATEGORY B MAJOR REPAIR IN ACCORDANCE WITH B747-400SF STRUCTURAL REPAIR MANUAL 52-30-01 REPAIR 2.SDR U2RA2022082300045Battery · no testRIGHT UPPER DECK DOOR ASSIST BATTERY OK TEST LIGHT DID NOT ILLUMINATE - DEFERRED PER MEL 52-23-07-01.SDR U2RA2022080300039Powerpack · inoperativeRIGHT UPPER DECK DOOR ASSIST BOTTLE POWER PACK DOES NOT TEST - REMOVED AND REPLACED POWER PACK IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR U2RA2022061700020None · noneGROUND EQUIPMENT DAMAGE TO NUMBER 1 ENGINE INLET COWLING - ACCOMPLISHED TIME LIMITED MAJOR REPAIR OF COWLING PER FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER 220092-1 REVISION IR DATED 6/14/2022.SDR U2RA2022061300019Switch · inoperativeDURING REFUEL, FUEL SPILLED FROM THE RIGHT WING OVERBOARD VENT. - OVERFILL PROTECTION FOUND FAULTY. REPLACED RIGHT SURGE TANK FLOAT SWITCH PER AIRCRAFT MAINTENANCE MANUAL 28-21-12.SDR U2RA2022060900018None · noneDURING REFUEL, FUEL SPILLED FROM THE RIGHT WING OVERBOARD VENT. - SUMPED RIGHT WING SURGE TANK AND CONTINUED REFUEL OF AIRCRAFT PER AIRCRAFT MAINTENANCE MANUAL 12-11-10 WITHOUT INCIDENT. NO DEFECTS NOTED PER AIRCRAFT MAINTENANCE MANUAL 28-21-00SDR 9WGA2022050535601Control Unit · brokenTHRUST LEVERS NON-RESPONSIVE WHEN MANUALLY INCREASED WITH AUTO THROTTLES ENGAGED. AP FAIL / AUTO THROTTLES FAIL. R & R #2 BCU IAW MM 24-23-01. AUTO LAND/AUTO THROTTLES NOW SATIS. OPS TEST OF FCC, L,C,R IAW MM 22-10-00 PASS TEST SATIS. TEST OF FMC AND FMC SERSDR P5CA2022030800088Duct · noneNO.4 ENG R/H C-DUCT OPEN ACTUATOR ATT FITTING BOLT HOLE FOUND ELONGATED.(<P>NO.4 ENG R/H C-DUCT REPLACED IAW AMM 78-31-01. T/R COWL P/N 683L177G13 CONVERSION TO P/N 683L179G09 REF TO CARD NO. CR.636372</P>)SDR U2RA202121400070Panel · puncturedREFERENCE NATIONAL AIRLINES AIRCRAFT MAINTENANCE LOG PAGE 52103, FORWARD LOWER CARGO COMPARTMENT FLOOR PANEL PUNCTURED AT STATION 680, BETWEEN STRINGERS 45R AND 46R. ACCOMPLISHED TIME LIMITED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERISDR U2RA2021112400068None · noneRIGHT EMERGENCY ESCAPE DOOR BATTERY TEST FUNCTION INOPERATIVE - RESEATED CONNECTOR ON THE BATTERY PACK AND SYSTEM FUNCTIONS NORMAL PER AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR 2022F00129Shaft · crackedCF6-80C2B1F, FAN FWD SHAFT WITH 6 EA FPI INDICATIONS ON AREA FB NEAR THE VENT HOLES. 1 EA INDICATION CONFIRMED AS A CRACK. PER THE GEK92451 TASK 72-21-05-230-001-051 A.(2) INDICATIONS IN AREA FA AND FB ARE NOT PERMITTED. PART IS UNSALVAGEABLE.SDR U2RA2021101100064Thrust Reverser · gouged#1 ENGINE OTBD T/R FORWARD UPPER FAN COWL LANDING (RING TORQUE BOX RETAINER) GOUGED.
ACCOMPLISHED MAJOR REPAIR OF THE #1 ENGINE (LH) THRUST REVERSER RING TORQUE BOX RETAINER GOUGE IAW VT-SAA EA 747-7831-56-A9241 REV. I/R. 8110-3 APPROVED BY ROBERT M. MANASHI SDR U2RA2021101100059Thrust Reverser · gougedWHILE ACCOMPLISHING TC ACCESS 400 FOUND #4 ENG. I/B SIDE TR SUPPORT WEB BENT AND GOUGED P/N 315U2028-23J, S/N R649-291.
ACCOMPLISHED MAJOR REPAIR OF THE #4 ENGINE INBD SIDE T/R SUPPORT WEB FLANGE P/N 315U2028-23J, S/N R649-291 BEND AND GOUGED EDGE IAW VT-SAA SDR UIEA2021062301404Manifold · separatedAFTER TAKEOFF RECEIVED A OVHT ENG 2 NAC EICAS MESSAGE FOLLOWED BY FIRE ENG 2 EICAS AND ALARMS(<P>INSPECTION FOUND 14TH STAGE HIGH PRESS MANIFOLD AT 3 O'CLOCK SEPARATED CAUSING HEAT DAMAGES TO NUMEROUS WIRES, HARNESS AND INSIDE OF RH TR COWL. REMOVED AND REPLACSDR U2RA2021060200018Power Supply · inoperativeUPPER DECK RIGHT DOOR EMERGENCY BOTTLE SQUIB BATTERY TEST INOPERATIVE. - REMOVED AND REPLACED UPPER DECK DOOR BOTTLE SQUIB BATTERY IAW B747-400 AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR KCSA2021032809Engine · stalled#3 ENGINE STALL NO LIMITS EXCEEDED. #3 ENGINE PRECAUTIONARY SHUTDOWN. PERFORMED BORESCOPE OF #3 ENGINE IAW B747 AMM 72-00-00. FOUND SEVERE DAMAGE TO BLADES IN B1-12 & B1-13 PARTS. REMOVED AND REPLACED #3 POWERPLANT SYSTEM LEAK AND OP'S CHECKS GOOD IAW KA 747-SDR P5CA2021031500070Compressor · damagedDEPARTING KLAX ENG #1 COMPRESSOR STALLED 4 TIMES CLIMING OUT OF APPROX 1000'. QRH PROCEDURES FOLLOWED RESULTING IN NORMAL ENGINE OPERATION.(<P>PERFORMED STALL INSPECTION WITH BOROSCOPE AT HPC 1,6,12,13,14. FOUND DAMAGE AT 12,13,14 BLADES SO DECIDED ENGINE REPLSDR 9WGA2020121234401Compressor · stalledENGINE NR 1 HIGH EGT, COMPRESSOR STALL, VIBRATION. RAN ENGINE LIMIT SURGE/STALL CHECKLIST. SHUTDOWN ENGINE AND RETURNED TO SHV.SDR P5CA2020083170290Relay · malfunctionedREJECTED TAKEOFF AT 35 KNOTS FOR ENGINE 2 REV STATUS MESSAGE REMAINED.DMI 133482 RAISED, MEL 78-31-01A APPLIED, CAT 'C'. MAINT PROCEDURES CARRIED OUT. R/R RELAY IAW AMM 78-36-07. OPS CHECK GOOD.SDR U2RA202008040001Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-153-01-04, ENLARGED BOLT HOLE NOTED ON NUMBER 4 PYLON PANEL NUMBER 482EL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202008040002Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-153-01-01, ENLARGED BOLT HOLES NOTED ON NUMBER 1 PYLON PANEL NUMBER 452EL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202010160001Stanchion · crackedDURING ACCOMPLISHMENT OF TASK CARD 53-510-00-01, 1 EACH CRACK NOTED ON STANCHION AT FORWARD CARGO DOOR CUTOUT AREA AT BODY STATION 560 STRINGER S-35R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20307.SDR U2RA202010160002Angle · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-814-00-02, 1 EACH CRACK NOTED ON SKATE ANGLE OF NUMBER 3 PYLON INBOARD FAIRING AT NACELLE STATION 457. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20305.SDR U2RA202010160003Angle · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-814-00-02, 1 EACH CRACK NOTED ON ANGLE OF NUMBER 2 PYLON PANEL 464B INBOARD UPPER FORWARD SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20305-1.SDR U2RA202010160004Fitting · nickedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, A NICK WAS NOTED ON THE NUMBER 2 PYLON FAN COWL AFT SUPPORT BEAM OUTBOARD AREA. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314.SDR U2RA202010160005Panel · crackedCRACK NOTED ON NUMBER 4 PYLON LEFT UPPER SIDE SKIN. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-1.SDR U2RA20201016006Skin · deformedDEFORMATION NOTED ON SKIN OF NUMBER 4 PYLON LEFT UPPER FAIRING DOOR FORWARD SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-2.SDR U2RA202010150001Strap · crackedDURING ACCOMPLISHMENT OF SB 747-53A2450 REV 8, 2 EACH CRACKED FASTENER HOLES WERE NOTED, 1 EACH AT BODY STATION 2231 STRINGER S-16L AND 1 EACH AT BODY STATION 2231 STRINGER S-19L. REPAIRS ACCOMPLISHED IN ACCORDANCE WITH B747-400SF STRUCTURAL REPAIR MANUAL 53-SDR U2RA202010150002Door Frame · crackedDURING ACCOMPLISHMENT OF SB 747-53A2450 REV 8, 2 EACH CRACKED FASTENER HOLE NOTED AT NR 5 RIGHT MAIN ENTRY DOOR CUTOUT, 1 EACH AT BODY STATION 2231 STRINGER S-19R. REPAIR ACCOMPLISHED IN ACCORDANCE WITH B747-400SF STRUCTURAL REPAIR MANUAL 53-60-15-2R-2, WITH SDR U2RA202010160010Skin · gougedGOUGE NOTED ON NUMBER 1 PYLON UNDERWING FAIRING SKIN PANEL AT NACELLE STATION 332. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-5.SDR U2RA202010190004Stiffener · crackedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-53A2465 REVISION 5, FOUND NOSE WHEEL WELL SIDE PANEL STIFFENER CRACKED AT BODY STATION 265-STA 280 WATERLINE 170, LEFT BUTTOCK LINE 30. FABRICATED STIFFENER IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INCSDR U2RA202007110001Skin · corrodedDURING ACCOMPLISHMENT OF DAMAGE TOLERANCE INSPECTION FOR SATELITE COMMUNICATION SYSTEM ANTENNA DOUBLER, CORROSION WAS NOTED ON THE SKIN INTERIOR AT BODY STATION 1480 FROM STRINGER S-10L TO STRINGER S-11L. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLESSDR U2RA202007110002Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-03, ENLARGED BOLT HOLE NOTED ON NUMBER 3 PYLON PANEL NUMBER 472ER. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202007110003Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-04, CHAFING WAS NOTED ON SKIN OF NUMBER 4 PYLON PANEL NUMBER 482FR. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20319-1.SDR U2RA202007110004Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, CRACKS WERE NOTED ON THE EXTERNAL SURFACE OF NUMBER 2 PYLON PANEL NUMBER 462GL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316.SDR U2RA202007110005Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-03, CRACKS WERE NOTED ON THE EXTERNAL SURFACE OF NUMBER 3 PYLON PANEL NUMBER 472FL. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20316-8.SDR U2RA202010190003Bracket · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-806-00-01, A CRACK WAS NOTED ON A PNEUMATIC TUBE SUPPORT BRACKET, INSIDE NUMBER 1 PYLON PANEL 451B. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 20293-4.SDR U2RA202007100001Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 53-804-01-01, EXISTING BLEND REPAIR NOTED ON SKIN AT LOWER FUSELAGE STA 1801 S-38R TO S-39R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC, ENGINEERING ORDER NUMBER 20288.SDR U2RA202007100002Structure · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING WAS NOTED ON THE SKIN OF NUMBER 1 ENGINE RIGHT THRUST REVERSER COWL INNER SURFACE FORWARD SIDE, NAC STA 131.78. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUSDR U2RA202007100003Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-810-01-01, CHAFING NOTED ON THE SKIN OF THE NUMBER 1 ENGINE LEFT THRUST REVERSER COWL INNER FACE LOWER BIFURCATION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20319-2.SDR U2RA202007100004Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-814-01-01, CHAFING WAS NOTED ON DOUBLER OF NUMBER 1 ENGINE LEFT CORE COWL INNER FACE AFT SIDE FRAME. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER 20316-10.SDR U2RA202010160006Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-04, DENT WITH GOUGES WAS NOTED ON THE SKIN OF NUMBER 4 ENGINE LEFT CORE COWL OUTER SURFACE AT NACELLE STATION 182.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20SDR U2RA202010160007Skin · dentedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-04, DENT WITH GOUGES WAS NOTED ON THE SKIN OF NUMBER 4 ENGINE LEFT CORE COWL OUTER SURFACE AT NACELLE STATION 182.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20
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