GE CF6-80 series
Service difficulty reports · 1,092
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 = 'CF680' 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 = 'CF680' 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 03FDEA01740Cooling Fan · failedON BLOCKOUT BETWEEN STARTING NR 1 AND NR 2 ENGINES SMOKE STARTED COMING IN TO THE COCKPIT FROM THE EQUIPMENT BAY. PERFORMED VISUAL INSPECTION OF AVIONICS COMPARTMENT, CHECKED ALL BOXES FOR EVIDENCE OF ODOR, REMOVED RELAY PANEL COVERS LOOKING FOR EVIDENCE OF SDR 03FDEA01748Barrel Nut · corrodedHORIZONTAL STAB RT NR 1 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. BLEND OUT CORROSION FOUND EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.SDR 03FDEA01725Fitting · corrodedHORIZONTAL STAB LT NR 26L BORE FOUND BEARING, SIDE WALL & BOTTOM WITH CORROSION. REAMED BORE FOUND CORROSION EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.SDR P5CA0300963Valve · inactiveAT PUSHBACK, NR 3 ENGINE DID NOT START. NO FUEL FLOW. REF DMI 31578. REACTIVATED NR 3 ENG FUEL VALVE. EICAS MESSAGE GROUND. NR 3 ENG STARTS, GROUND STARTS NORMAL, IAWMM 71-00-00. DMI CLEARED, PLACARDS REMOVED.SDR 03FDEA01753Hinge Fitting · corrodedSNRM N0825 - RT WING OB FLAP IB HINGE FITTING (WING SIDE)- LOWER OB ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. ** S/D ** COMINGSDR 03FDEA01754Fitting · corrodedRT WING O/B FLAP I/B HINGE FITTING (WING SIDE) - LOWER I/B ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71748, WINGS - RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.SDR 03FDEA01805Flap Track · chafedSNRM N0776 - LT WING IB FLAP LEADING EDGE OB FLAP VANE TRACK CAVITY FOUND CHAFING MARKS ON FITTING AND SKIN. ** S/D ** COMINGSDR 03FDEA01751Fitting · corrodedRT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- I/B ACTUATOR ATTACH HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.SDR UPS03641380Indicator · inoperativeINSPECTION TYPE: ETOP DIVERSION, CAPTIANS VERTICAL SPEED FLAG IN VIEW ALT AIR DATA DOESN'T CORRECT. (TCAS FLAG IN VSI ALSO IN VIEW) REPLACED CAPTAIN'S VSI PER MM 34-22-06-4 & 34-45-00-5. OPS CHK NORMAL.SDR 03FDEA01652Door · separatedMODERATE SOUNDING BANG AT CRUISE ALT 33,000 FT APPEARED TO BE AROUND FUSELAGE AREA BELOW CAPT. SEAT. NO ABNORMAL ENG/HYD/AIR INDICATIONS. A/C INSPECTED FOR POSSIBLE BIRD STRIKE. THIS WAS NOT A BIRD STRIKE NR 1 RAM AIR SCOOP DOOR CAME OFF IN FLIGHT DOOR ON ORSDR ABXA030369Splice · crackedCRACK INDICATION ON RT UPPER INBOARD HORIZONTAL STABILIZER PIVOT FITTING DURING X-RAY. REMOVED AND REPLACED PLATE IAW REA B655-48039-MR.SDR 03FDEA01606Hinge · corrodedRT OB FLAP IB HINGE (FLAP SIDE) FOUND CORROSION ON INBD AND OB PIVOT BORES AND SPOT FACES. RT OB FLAP IB HINGE (FLAP SIDE) IB AND OB PIVOT BORES AND SPOT FACES CORROSION AREAS REPAIR CARRIED OUT IAW EA NR 1-5750-72686 WINGS, TRAILING EDGE AND TRAILING EDGE DESDR DL764030772Rotary Actuator · faultyFLAP DISAGREE ON T/O OUT OF LAX. CREW FOLLOWED PROCEDURES AND CONTINUED TO OGG. IAW OPERATIONS MANUAL A/C WILL REQUIRE A FLAP 20 LANDING. DISPATCH WILL NOT ALLOW A FLAP 20 LANDING IN OGG DUE TO SHORT RUNWAY SO A/C DIVERTED TO HNL FOR MTC. FOUND NR 3 ROTARY ASDR GK42003F00000Charger · malfunctionedCREW REPORT ON AML: BEFORE START GOT (BATT CHARGER INOP) AND (EMER PWR TST FAIL) ALERTS. TROUBLESHOOTING IAW F/M 24-30-03-00 CARRIED OUT. BOTH MAIN REPLACED IAW AMM 24-32-02 IAW MMDC AD. BATTERY CHARGER REPLACED IAW AMM 24-34-03. EPCU REMOVED AND REPLACED SDR UPS03M41018Slide · deployedR1 DOOR SLIDE DEPLOYED. DEFERRED IAW MEL 52-10-3-2. DOOR IS INOPERATIVE, M263900 ASSIGNED. PLACARD INSTALLED.SDR 03FDEA01179Skin · corrodedRH HOR STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CSDR DL76G030696Spar · crackedPYLON, NR 1 FWD UPPER SPAR WEB, POWER FEEDER CABLE CUTOUT CRACKS. TWO CRACKS WERE FOUND IN THE UPPER SPAR WEB FROM THE POWER FEEDER CUTOUT TO THE NUTPLATE ATTACH HOLES. ERA INSTALLED REPAIR DOUBLER AND FILLER PER S/B 767-54-0090._ERA 385462-14 REVISION ORIGISDR 03FDEA01215Hinge · corrodedLT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE CORRODED. LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE REPAIRED AS PER FEDEX EA 1-5750-71881 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBD FLAP OSDR 03FDEA01122Frame · damagedTEMPORARY REPAIR ON FRAME20A. PERMANENT REPAIR INSTALLED IAW EA 6-5310-60187 A AND DWG SR30-53-001.SDR P5CA0300901Start Valve · malfunctionedENG NR 2 WOULD NOT START EICAS MESSAGE -ENG NR 2 START VLV-. DEFERRED NR 2 ENG PER DDG START VLV REQUIRED MANUAL START.SDR UIEA200300034Sensor · damagedAFTER TAKEOFF DURING CLIMB/CRUISE, FAULT CODE 32 32 03 00 (GEAR DOOR). LEFT BODY GEAR DOOR POSITION INDICATOR SHOWED INTRANSIT IN BOTH GEAR UP AND GEAR DOWN POSITIONS. AIRCRAFT RETURNED TO HKG. FUEL DUMPED 36,500 KGS. FOUND LEFT BODY GEAR ALT SENSOR S428 DSDR 03FDEA01089Barrel Nut · corrodedLT HORIZONTAL STAB NR 3 BORE CORROSION EXCEEDED LIMIT. LT HORIZONTAL STAB NR 3 BORE CORROSION REPAIR CARRIED OUT IAW EA 1-5510-71837, STABILIZERS- HORIZONTAL STAB BARREL NUT BORES- CORROSION REMOVAL- BORE 3 LEFT.SDR DL76G030606Tube · looseON DEPARTURE, RIGHT ENGINE OIL PRESSURE AND QTY WENT TO ZERO. FOUND SHROUD B-NUT ON NBR 6 BEARING SCAV SUPPLY TUBE LOOSE - SECURED SAME - LIMITS FOR LOSS OF OIL PSI NOT EXCEEDED IAW PIREP AND MTC OBSERVANCE - C/W REQD INSPN IAW AMM 72-00-00- LK AND OPS CK GDSDR EA332003B0977Locking Plate · bentDURING AN OPERATIONAL CHECK OF THE INFLATABLE EVACUATION SYSTEM AT THE RT UPPER DECK DOOR ACCORDING MS 23-66-00-040-100 THE RESERVOIR WAS NOT ACTIVATED AND THE SLIDE DID NOT INFLATE. FURTHER INVESTIGATION REVEALED THAT THE PACKBOARD LOCKING PLATE WAS RELEASEDSDR 03FDEA00994Crossbeam · damagedMDIS 658 53-10 0006641 24JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5310-70959 FUSELAGE-MAINFRAME-REWORK OF MAIN DECK CROSSBEAM DAMAGE. FACT 28JUN03 14:23 BFM U COMPLIED WITH EA6-5310-70959 FUSELAGE-MAINFRAME- REWORK OF MAIN DECK CROSSBEAM DAMAGE.SDR 03FDEA00991Panel · crackedNR 1 ENGINE PYLON PRE-COOLER PANEL, CRACK REPAIR. FACT 27JUN03 03:15 BFM R COMPLIED WITH E.A. 6-5452-70948 NACELLES/PYLONS. NR 1 ENGINE PYLON PRE-COOLER PANEL PANEL CRACK REPAIR.SDR 03FDEA00989Flange · gougedREPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE. FACT 27JUN03 06:44 BFMR WORK COMPLIED WITH ON E.A. 6-5310-70955 FUSELAGE-MAINFRAME REPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE.SDR 03FDEA00988Thrust Reverser · damagedTHRUST REVERSER ASSY-REPAIR OF FORMED ZEE ON CORE NACELLE INNER SURFACE. FACT 27JUN03 12:16 BFM R WORK COMPLIED ON EA NR 6-7832-70958_EXHAUST-TR ASSY-REPAIR OF FORMED ZEE ON CORE, COWL INNER SURFACE.SDR 03FDEA00959Panel · crackedNR 593 NE 2 PYLON PRECOOLER PANEL 423 BL CRACKED LT AND RT FWD CORNERS OF SEAL BACKUP PLATE. REMOVED AND REPLACED CRACKED WEB IAW SRM 51-40-21.SDR 03FDEA00958Floor Support · crackedNR 378 MCD FLOORBOARD SUPPORT FRAME 46 CRACKED RBL 35. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-21.SDR 03FDEA00956Channel · gougedMDIS 658 57-10 0006637 21JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z CHANNEL) FACT 23JUN03 17:40 BFM R COMPLIED WITH EA NR 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z-CHANNEL) IAW/SRM 51SDR 03FDEA00946Crossbeam · crackedAFT CARGO CROSSBEAM AT FRAME 59 IS CRACKED APPROX 1 INCH, 4 INCHES RIGHT OF CENTER. REAIRED CROSSBEAM IAW A300-600 SRM 53-10-15 BY CUTTING AND SPLICING IN A NEW SECTION OF BEAM. WORK DOCUMENTED ON M-1805 NR N00080SDR 03FDEA00894Bracket · chafedN 120 NR 1 ENG THRUST REVERSER LOWER AFT CLOSE OUT PANNEL LEADING EDGE, CHAFED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 PG 7 @ MAE.SDR ABXA030193Door Frame · corrodedAFT CARGO DOOR BEAM NR 5, CORROSION WAS FOUND ON THE INNER CHORD P/N 140T2605-3 UNDERNEATH PUMP. AFTER CORROSION REMOVED MINIMUM REMAINING THICKNESS WAS 0.082, WHILE ORIGINAL THICKNESS WAS 0.125 INCH.SDR DHL2003366517Frame · corrodedFOUND CORRODED AT L45. RECEIVED NEW FRAME R5397405421093 FOR A/C 366DH AND FRAME COUPLING R5397405820000, SEGMENT 64 FOUND TO BE OUT OF LIMITS IAW SRM 53-17-00. ORG. THICKNESS .068 REMAINING THICKNESS .0, REMOVED DAMAGE SEGMENT FR. 64 IAW A300 SRM 53-17-00,LOSDR 03FDEA00776Hinge · corrodedLEFT WING- O/B FLAP I/B HINGE (FLAP SIDE) FWD ATTACHING POINT, O/B CTR BOLT, HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.SDR 03FDEA00749Hinge Bracket · corrodedLT WING- IB FLAP OB HINGE (FLAP SIDE) LWR ATTACHING PIVOT OB LUG HOLE FOUND CORRODED. LT WING- I/B FLAP O/B HINGE (FLAP SIDE) LWR ATTACHING PIVOT O/B LUG HOLE. REPAIR CARRIED OUT IAW EA 1-5750-68410 WINGS-LEFT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORROSDR G5S2003F00001Slide · inoperativeINFLATABLE EVACUATION SYSTEM OF THE RIGHT UPPER DECK DOOR DOES NOT INFLATE PROPERLY. THE SLIDE WAS LIFTED AND HAS BEEN FALLEN OUT OF THE DOOR FRAME. SUDDENLY THE SLIDE STOPPED ROTATING AND STUCK. AFTER WAITING SEVERAL SECONDS THE MECHANIC OPENED THE VELCRO SDR AUS20030438Pump · failed(AUS) APU FUEL PUMP FAILED. AFT PUMP HAD THE COVER BLOWN OFF AND FUEL IN THE ELECTRICAL WINDINGS.SDR AUS20030437Motor · failed(AUS) ENGINE STARTER MOTOR FAILED. EXTERNAL DAMAGE TO ENGINE.SDR AUS20030578Motor · failed(AUS) ENGINE STARTER MOTOR FAILED. DAMAGE CAUSED TO ENGINE.SDR 03FDEA00346Sensing Element · damagedAFTER DEPARTURE AT TPE TURNED ON ANTI ICE (ENGINE NR 2 A-ICE), WE WERE IN ICING CONDITION, DESCENDED LOWERED AND RETURNED TO TPE. FACT 23MAR03 22:52 TPE R RECEIVED A/C PARTS AT 2110Z, REPLACED SENSING ELEMENTS D1-90 IAW MM 30-22-11-4, AND PERFORMED ANSDR 03FDEA00345Seat Track · corrodedFORWARD CABIN SEAT TRACK AT STA.487, RIGHT SIDE 27.5 INCHES WITH CORROSION.SDR 03FDEA00347Seat Track · corrodedCABIN SEAT TRACK AT LT X=27.5 STA 420-495 FOUND CORRODED.SDR 03FDEA00230Skin · damagedRT FUSELAGE, AFT, BETWEEN VERTICAL ATTACHMENT BOLTS CENTER AND AFT OB SIDE HAS CORROSION ON SKIN 1 INCH X 4 INCHES. REMOVED FASTENERS FROM AFFECTED AREA. REMOVED CORROSION IAW A310 SRM 51-22-00 C/W UT THICKNESS INSPECTION IAW NTM 51-10-01/401. FOUND TO BE OUSDR 03FDEA00257Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 17R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.SDR 03FDEA00256Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 16R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.SDR 03FDEA00255Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 15R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.SDR 03FDEA00254Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.SDR 03FDEA00253Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.
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