GE CF6-6D

Service difficulty reports · 1,051

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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 = 'CF66D'
  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.

SDR FDEA201010114005Skin · crackedRT WING TIP UPPER SURFACE APPROX 13 INCH FROM TIP AND 41 INCH FROM AFT, FOUND CRACKED. SKIN SURFACE TRIMMED AND REPAIR CARRIED OUT AS PER EA 8-5730-143465. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Oct 11, 2010 · N385FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201010093979Engine · failedON POWER UP FOR TAKEOFF HEARD 3 TO 4 LOUD THUMPS FROM RIGHT SIDE OF ACFT. IMMEDIATELY REJECTED T/O AT NO MORE THAN 15TO20 KNOTS. NO ABNORMAL ENGINE INDICATIONS NOTED HOWEVER ANOTHER AIRCRAFT REPORTED FLAMES SHOT OUT OF NR 3 ENGINE. CLEARED RWY AND SECUREDOct 9, 2010 · N368FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201010073969Tube · crackedNR1 ENG LT THRUST REVERSER GREEN COOLING TUBE IS CRACKED. R & R NR1 ENG LT THRUST REVERSER COOLING TUBE IAW AMM70-00-00; AMM 78-32-14; 70-32-01; SRM 51-21-01 AND SRM 51-41-01.Oct 7, 2010 · N370FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA201010054019Structure · damagedCTR ACCESSORY COMPARTMENT, INBD SLAT DRIVE CONTROL RETENTION MECHANISM (LT SIDE) HAS 2 SHEARED MECHANICAL FUSES.Oct 5, 2010 · N389FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201010013851Skin · crackedTHE LT WING OTBD FLAP , SECOND FROM INBD WEDGE SEGMENT UPPER SKIN, HAS AN APPROX 2" LONG CRACK IN THE FWD MID SECTION AT APPROX STA OF 565.Oct 1, 2010 · N359FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201009293781Floorboard · delaminatedCENTER CARGO BAY FLOORBOARD 183HF DELAMINATED. FABRICATED FLOORBOARD 183 HF IAW DWG SRZ 25-005, REV "H".Sep 29, 2010 · N389FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009293782Floorboard · delaminatedCENTER CARGO BAY FLOORBOARD 183GF DELAMINATED. FABRICATED FLOORBOARD 183 GF IAW DWG SRZ 25-005, REV "H".Sep 29, 2010 · N389FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009293783Floorboard · delaminatedCENTER CARGO BAY FLOORBOARD 183PF IS DELAMINATED. FABRICATED CENTER CARGO BAY FLOORBOARD 183 PF IAW DWG SRZ 25-005, REV "H".Sep 29, 2010 · N389FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009293784Floor Panel · debondedCTR ACCESSORY COMPARTMENT LT STEP IS DEBONDED. REMOVED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW SRM 51-31-01, VOL II. FABRICATED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW DWG SRZ 25-005, REV "H". INSTALLED NEW PANEL IAW SRM 51-31-01, VOL II.Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009293795Seat Track · damagedMAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 775 RBL 8. REMOVED AND RE-INSTALLED FLOOR BOARD PANEL LBL 0 TO RBL 27 AT STA 615 - 775. MATERIAL ID NEW SEAT TRACK 49291150-12000, PO 617966.1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. VOL I. OK TO PRIME, Sep 29, 2010 · N370FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009273753Skin · crackedLT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACK AT 2 LOCATIONS. TRIMMED AND REPAIR CARRIED OUT IAW EA 8-5710-143751, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Sep 27, 2010 · N390FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201009273754Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. CARRIED OUT IAW EA NR8-5710-143754, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Sep 27, 2010 · N390FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201009253712Seat Track · gougedSEAT TRACK LBL 48 BETWEEN FS 1688 HAS A GOUGE ON CROWN AREA. FABRICATED SEGMENT OF SEAT TRACK ON TRAVELER T10/853974 AND REPAIR PARTS ON TRAVELER T10/853972. INSTALLED SEAT TRACK AND REPAIR IAW SRM 53-70-00. CLASSIFED AS A MAJOR REPAIR.Sep 25, 2010 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009243701Fuel Control · flamed outNR 1 ENG RPM FLUCTUATED FROM IDLE & 90 % WITH CONCURRENT NR 1 THROTTLE MOVEMENT. NR 2 & 3 ENG VIA AUTOTHROTTLE SYS RESPONDED IN OPPOSITE DIRECTION TO COMPENSATE SPEED ERRORS. AUTOTHROTTLES SWITCHED TO OTHER SYS WITH NO CORRECTION NOTED. AUTOTHROTTLE SYS DISCOSep 24, 2010 · N358FE · Doug MD1010F · Fuel Control/Turbine EnginesSDR FDEA201009243703Stop Fitting · shearedL-1 DOOR; FWD SIDE; 5TH DOOR STOP UP; IS SHEARED OFF. R & R THE L-1 STOP FITTING (5TH UP FROM THE BOTTOM) IAW SRM 51-31-01, VOL I. REMOVED AND RE-INSTALLED THE L-1 DOOR SLIDE AND ADJUSTED THE L-1 DOOR STOPS IAW AMM 52-11-03-2, AMM 25-61-01 AND AMM 52-11-00-Sep 24, 2010 · N389FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201009243704Seat Track · wornSEAT TRACK LBL 48 AT FS 1389 HAS SHARP EDGES ON BOTTOM PORTION OF CROWN. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-70-00. FABRICATED NEW SEAT TRACK SECTION ON TRAVELER T10/853975 AND REPAIR Sep 24, 2010 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009233662Fitting · misinstalledNR 1 PYLON AFT BULKHEAD FITTING HAS 12 EA FASTENERS ALONG THE UPPER FLANGE SPINNING. ACCOMPLISHED EA 8-5450-123559.Sep 23, 2010 · N389FE · Doug MD1010F · Nacelle/Pylon, Attach FittingsSDR FDEA201009233688Bracket · corrodedCTR CARGO PIT FRAME AND CLIP (LWR SIDE) HAS CORROSION FROM BS 1701 TO BS 1702; LONGERON 44R. REMOVED BRACKET IAW SRM 51-35-01, VOL II. FOUND TO BE OUT OF LIMITS. FABRICATED NEW BRACKET IAW DWG AFA0043. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTASep 23, 2010 · N370FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201009233689Gusset · crackedMAIN CABIN INTERNAL FRAME GUSSET IS CRACKED BETWEEN BS 1480 AND BS 1482, STRINGER 16R - STRINGER 17R. FABRICATED NEW CHANNEL IAW DWG 88277. HEAT TREATED CHANNEL FROM 7075-0 TO 7075-T6 PER DWG AWE 7017, REV "AH" AND IAW DPS 7.0. LOCATED AND DRILLED NEW CHASep 23, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201009233778Wedge · corrodedRT OTBD FLAP SEC WEDGE PANEL, INBD TOP SKIN REQUIRES REPLACEMENT BECAUSE OF CORROSION. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II. FABRICATED 1 EA DOUBLER IAW DWG ARC 1953, REV "J". FABRICATED -34 AND -35 TEE CAPS IAW DWG ARC 1953Sep 23, 2010 · N370FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201009213601Channel · corrodedCTR CARGO COMPARTMENT CHANNEL IS CORRODED BELOW THE CARGO FLOOR AT BS 1521, RBL 56. REMOVED DAMAGED J-CHANNEL IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. MATERIAL ID FOR REPAIR ANGLE AND ZEE ANGLE IS 7075-T6511Sep 21, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201009213602Support · corrodedAFT CARGO COMPARTMENT AREA SEAT TRACK SUPPORT IS CORRODED AT THE TRACK ATTACH POINT; BS 1840, RBL 20. REMOVED CORROSION ON THE SEAT TRACK SUPPORT IN THE AFT CARGO COMPARTMENT AT THE TRACK ATTACH POINT BS 1841, RBL 20. FOUND TO BE OUT OF LIMITS IAW SRM 53-0Sep 21, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201009213597Hinge Fitting · crackedFOUND 1 EA CRACK EMANATING FROM FASTENER HOLE ON THE LT WING, OTBD FLAP, INBD FWD FLAP TO WING FITTING. HFEC INSP VERIFIED INDICATION OF CRACK. REMOVED CRACKED LT OB FLAP IB HINGE WING FITTING ARB2431 TRANSFERED HOLES TO NEW SERVICABLE FITTINGS PER NRB601Sep 21, 2010 · N566FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009203545Rib · misrepairedEXISTING REPAIR - RT WING LOWER SURFACE L/E CAVITY OTBD OF SLAT TRACK NR 8 SUPPORT RIB. EVALUATED AND FOUND ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW RIB FABRICATED PER DRAWING NR ARB1286 REVISION K. RIB REMOVED AND REPLACED PER SRM 51-31-01Sep 20, 2010 · N562FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201009203546Longeron · corrodedAFTER REMOVAL OF SKIN TO FACILITATE REPAIR (REF SNRM N00362) FOUND CORROSION ON LONGERON 50L BETWEEN STA 765 TO STA 824. CORRODED LONGERON 50L BETWEEN STA 765 TO STA 824 PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFSep 20, 2010 · N562FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201009203547Longeron · corrodedCORROSION ON LONGERON 51L BETWEEN STA 765 TO 824. FOUND AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111. REPAIR CLASSIFIED AS Sep 20, 2010 · N562FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201009203548Longeron · corrodedCORROSION ON LONGERON 51R BETWEEN STA765 TO 824 FOUND AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. PERFORMED SPLICE REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111. REPAIR CLASSIFIED AS CATSep 20, 2010 · N562FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201009203550Longeron · misinstalledLONGERON 52 BETWEEN STA 765 TO STA 791.75 FOUND NOT IAW BLUEPRINT DWG NDA6214, AFTER REMOVAL OF SKIN TO FACILITATE REPAIR. DISCREPANT LONGERON 52 BETWEEN STA 765 TO STA 859 PERFORMED SPLICE REPAIR IAW SRM 53-10-00 FIG 1 AND FIG 2, VOL I, REV 96. REPAIR CLASSISep 20, 2010 · N562FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201009203563Floor Support · damagedAFT CARGO COMPARTMENT AREA FLOOR PANEL SUPPORT FRAME HAS A DOUBLE DRILLED HOLES AT BS 1801, RBL 40. MATERIAL ID'S ANGLE PO NR 456452.1, STRAP PO NR652554.2 & FILLER PO NR652554.2 IAW SRM 53-00-01, FIG 9, VOL I. REMOVED DAMAGE AND FABBED REPAIR PARTS IAW SRM 5Sep 20, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201009203564Duct · corrodedNR2 ENGINE INLET DUCT INTERIOR SKIN IS CORRODED; FASTENERS SHEARED AND IS CORRODED INSIDE PANEL 362 DOOR (RT), STA 222. REMOVED AND REPLACED INLET SKIN IAW MD/DC10 SRM 51-31-01, VOL II AND DWG AJC7288, REV "D".Sep 20, 2010 · N370FE · Doug MD1010F · Engine Air Intake SystemSDR FDEA201009173519Pan · corrodedAT APPROX FS 383 LAV SERVICE PANEL. THE LAV PAN HAS CORROSION AND CRACKED FLANGE. R & R PAN AND DOUBLER. REF SRM 51-35-01Sep 17, 2010 · N387FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201009173530Skin · wornRT WING NR 6 LEADING SLAT LOWER SURFACE HAS WORN SPOTS. REMOVED DAMAGE AND EVALUATED AREA IAW SRM 57-00-01, VOL I. AREA WAS FOUND OUT OF LIMITS. REMOVED DAMAGE IAW SRM 51-71-00, VOL II. FABRICATED AND INSTALLED REPAIR IAW SRM 57-00-01, VOL I, AND SRM 51-31Sep 17, 2010 · N389FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201009163510Bulkhead · corrodedLT WHEEL WELL FWD BULKHEAD SLANT PANEL LWR OTBD CORNER HAS CORROSION. REPAIRED SLANT PANEL TO REAR SPAR CAP ANGLE. REF SRM 53-40-00Sep 16, 2010 · N387FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201009153490Spar Cap · crackedLT WING REAR SPAR AT STA XORS 345.750, 3 EA FASTENER HOLES ON THE OTBD SIDE HAS CRACK INDICATIONS. REPAIRED CRACKED HOLES IAW EA 8-5710-123557.Sep 15, 2010 · N389FE · Doug MD1010F · Wing SparSDR FDEA201009153491Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA LOWER TEAR STRAP N AND SKIN HAS CORROSION AT FRAME 824; LONGERON 50R - LONGERON 50L. FABRICATED AND INSTALLED NEW LONGERONS IAW DAC DWG ADA 3064 AND NDA 6014. LOCATED AND DRILLED NEW SHEAR TIES IAW DAC DWG NDA 6014; SRM 51-23Sep 15, 2010 · N370FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201009153492Skin · bulgedFUSELAGE SKIN BULGED AT STA 824, LONGERON 52. REMOVED DAMAGED SKIN AND TEAR STRAPS. FABBED NEW SKIN SECTION, TEAR STRAPS AND END SPLICE IAWDWG NDA 6014 AND SRM 53-20-00, FIG 17, VOL I. ALODINED, PRIMED AND PAINTED PARTS IAW SRM 51-21-01, VOL II. INSTALLEDSep 15, 2010 · N370FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201009153427Hinge Fitting · corrodedRT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 3 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153438Hinge Fitting · wornRT WING OTBD FLAP; INBD HINGE; LOCATION NR 6 OTBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153439Hinge Fitting · corrodedRT WING OTBD FLAP; INBD HINGE; LOCATION NR6 OTBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153440Hinge Fitting · corrodedRT WING OTBD FLAP; INBD HINGE; SIDE LOAD FITTING; FWD BOLT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153442Hinge Fitting · corrodedRT WING OTBD FLAP; INBD HINGE; SIDE LOAD FITTING; MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153443Hinge Fitting · corrodedRT WING OTBD FLAP; INBD HINGE; BARREL NUT HOLE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153444Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 2 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153445Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3; INBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153446Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3, OTBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153447Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 3; MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153448Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 4; INBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153449Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR4; OTBD LUG FACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153450Hinge Fitting · wornRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5; INBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153451Hinge Fitting · wornRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5 OTBD BUSHING IS WORN. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach Fittings
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