GE CF6-6D

Service difficulty reports · 1,051

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 = '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 FDEA201006162031Relief Valve · leakingON CLIMBOUT, GOT HYD 3 ELEV OFF ALERT WITH DECREASING HYD 3 QTY. FOLLOW ON ALERTS HYD 3 OFF AND ON FINAL APPROACH BACK TO DEPARTURE GOT HYD 3 FAIL. LOST ALL HYD 3 QTY. ALTN GEAR EXTENSION USED. LDG WT 343,500LBS. AIRPORT CRASH FIRE RESCUE REPORTED SMOKEJun 16, 2010 · N392FE · Doug MD1010F · Hydraulic System, MainSDR FDEA201006162026Skin · misrepairedLT INBD T/E FLAP LOWER SURFACE FOUND 1 EACH EXISTING REPAIR AT OTBD OF INBD FLAP OTBD HINGE AREA. FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT PER DRAWING ARC2992 REVISION R AND AMM 20-50-02 REVISION 10. E.O. 8-5100-7-5001Jun 16, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006162022Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN AT STA 1159, BETWEEN LONGERON 39R AND 40R. EVALUATED AND FOUND STRAP PN SR10530073-27 AND SHIM PN SR10530073-29 NOT INSTALLED IAW DRAWING SR10530073 SHEET 2, REVISION F. NEW STRAP AND SHIM FABRICATED AND INSTALLED AS PER DRAJun 16, 2010 · N68049 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201006162029Oil System · leakingGOT "LOW OIL QTY" LEVEL NR2 ENGINE FOLLOWED SOON AFTER QTY GOING TO "0". OIL PRESSURE DROPPED TO ABOUT 5 PSI. SHUTDOWN NR 2 ENGINE AND DIVERTED. REMOVED AND REPLACED NR 2 ENGINE IAW WORKCARD 71T1101 & 71T1701, OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Jun 16, 2010 · N68053 · Doug MD1010F · Turbine Engine Oil SystemSDR FDEA201006162033Bracket · corrodedRT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR3 FROM FWD, FOUND UPPER FWD HOLE, BORE CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 16, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006162034Attach Bracket · corrodedRT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR 3 FROM FWD, FOUND LOWER FWD HOLE "BORE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 16, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006162032Attach Fitting · corrodedLT WING INBD FLAP ASSY INBD ACTUATOR LOWER ATTACHMENT FITTING FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140360, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 16, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006141992Stiffener · crackedRT WING L/E STIFFENER IS CRACKED BETWEEN WING STATIONS XORS 560 AND XORS 565. ACCOMPLISHED HFEC IAW NTSPM 06-10-01.001 TO VERIFY AND OF CRACK. REPAIRED CRACKED STRINGER IAW EA 8-5710-136667.Jun 14, 2010 · N357FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201006141993Stiffener · crackedRT WING L/E STIFFENER IS CRACKED BETWEEN WING STATIONS XORS 560 AND XORS 565.Jun 14, 2010 · N357FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201006142007Fitting · chafedCHAFED - LT WING LOAD FITTING. REPAIR CARRIED OUT PER E.A. 8-5750-132416, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 110.Jun 14, 2010 · N560FE · Doug MD1010F · Wing, Attach FittingsSDR FDEA201006142008Fitting · chafedCHAFED - RT WING LOAD FITTING. REMOVED AND REPLACED AS PER AMM 20-50-02 REVISION 10.Jun 14, 2010 · N560FE · Doug MD1010F · Wing, Attach FittingsSDR FDEA201006142009Skin · dentedDENTED LOWER SURFACE INBOARD EDGE OF RT INBOARD AILERON ASSY. DENT AREA MEASURED 0.008" TO 0.060" DEEP, FOUND ACCEPTABLE AS PER SRM 51-80-01 VOLUME II REVISION 96. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 06-10-01.001 ON DENT AREA AND FOUNJun 14, 2010 · N560FE · Doug MD1010F · AileronsSDR FDEA201006131973Skin · misrepairedRT WING FIXED L/E UPPER AREA FOUND 1 EACH EXISTING REPAIR AT NR 3 SLAT INBD VICINITY AREA. FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY SRM REPAIR. EXISTING REPAIR REMOVED AND AND A NEW REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 28 VOLUME I, RJun 13, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006111951Access Panel · damagedRT WING - FUEL TANK ACCESS PANEL NR 634AT CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 8-5710-132418, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Jun 11, 2010 · N560FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006111952Bulkhead · crackedCTR ACCESORY COMPARTMENT AFT PRESSURE BULKHEAD AT STA 1159 "X" = 5 FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5730-140357, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.Jun 11, 2010 · N560FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201006111950Engine · failedNR 1 ENGINE FAILURE AT ROTATION. ACFT SHUTTERED. NO FIRE INDICATION TOWER ADVISED FIREBALL ON LT SIDE OF ACFT. AUS R IN WORK. AUS R PERFORMED VISUAL INSP OF INLET AND EXHAUST AREA(S). NO APPARENT DAMAGE NOTED IN INLET. METAL PARTICLES FOUND IN EXHAUST PIPEJun 11, 2010 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201006101929Spar Cap · crackedDURING HFEC OPEN HOLE INSP AT LT WING REAR SPAR LOWER CAP STA XORS = 345.75 INBD FWD FASTENER HOLE FOUND CRACKED INDICATION ON UPPER LAYER. R & R IAW SRM 51-33-01 VOL II, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Jun 10, 2010 · N560FE · Doug MD1010F · Wing SparSDR FDEA201006101930Skin · scratchedRT WING - NR 5 SLAT ASSY LOWER SURFACE MID AREA FOUND SCRATCHED MARK. REPAIRED IAW EA 8-5740-132420, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Jun 10, 2010 · N560FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201006101947Panel · damagedRT WING - FUEL TANK PANEL NR 631AT CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIR CARRIED OUT IAW EA 8-5710-132418, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Jun 10, 2010 · N560FE · Doug MD1010F · Fuel StorageSDR FDEA201006101948Access Panel · damagedRT WING - FUEL TANK ACCESS PANEL NR 638AB CUT OUT FASTENER HOLE FOUND DAMAGED. REPAIRED IAW EA 8-5710-132419, REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 110.Jun 10, 2010 · N560FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006101949Stiffener · crackedCTR WING TANK FWD UPPER PANEL 01 EACH STIFFENER CRACKED AT STR 21, "X" =30. R & R IAW SRM 51-31-01, VOLUME II, REV 96. NEW STIFFINER FABRICATED IAW DWG NPB6072, REV AL. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100, REV 110.Jun 10, 2010 · N560FE · Doug MD1010F · Fuel StorageSDR FDEA201006101931Hinge Fitting · corrodedLT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) LOWER LUG INBD SIDE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140350, REPAIR CLASSIFIED MINOR PER GMM 6 -2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006101932Hinge Fitting · corrodedLT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) PIVOT POINT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT PER MD10 CMM 57-52-01 REVISION 50. NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-01 REVISION 50. REPAIR CLASSIFIED AS MINOR Jun 10, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006101933Hinge Fitting · corrodedRT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) ACTUATOR ATTACHMENT LUG INBD SURFACE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140351, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006101934Skin · chafedRT WING - NR8 SLAT ASSY OTBD LOWER EDGE FOUND TRIM OFF. REPAIRED AS PER SRM 57-00-01 VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201006101935Skin · chafedRT WING - NR 7 SLAT ASSY LOWER MID SURFACE FOUND TRIM OFF. REPAIRED PER SRM 57-00-01 VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201006091874Floor Panel · delaminatedCTR PIT FLOOR PANEL 183 WF IS DELAMINATED FROM STA 1521 TO 1601, RBL 48. FABRICATED NEW FLOOR PANEL 183 WF IAW DWG SRZ 25-005, REV "H".Jun 9, 2010 · N357FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201006091875Floor Panel · delaminatedCTR PIT FLOOR PANEL 183 XF IS DELAMINATED FROM STA 1601 TO 1701, RBL 48. FABRICATED NEW FLOOR PANEL 183 XF IAW DWG SRZ 25-005, REV "H".Jun 9, 2010 · N357FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201006091879Floor Panel · delaminatedFWD PIT FLOOR PANEL 123 DF IS DELAMINATED FROM STA 735 TO 795, RBL 48. FABRICATED NEW FLOOR PANEL 123 DF IAW DWG SRZ 25-005, REV "H".Jun 9, 2010 · N357FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201006081860Floorbeam · crackedMAIN DECK CARGO - FLOORBEAM FOUND CRACKED AT STA 1305, X = 107. REPAIRED IAW SRM 53-00-01 FIG 9, VOL I, REV 96 AND EA 8-5310-140346, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Jun 8, 2010 · N560FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201006081862Support Fitting · chafedLT WING - INBD FLAP INBD TRACK MOST FWD SUPPORT FITTING FOUND CHAFED. REPAIRED AS PER E.A. 1-5740-140356, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 110.Jun 8, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006081863Skin · damagedRT WING - INBD FLAP ASSY LOWER SURFACE FOUND MULTIPLE DENT AND SCRATCHES. REPAIRED SRM 57-10-00, FIG 3 VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAWGMM 6-2-100, REV 110.Jun 8, 2010 · N560FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201006081864Skin · crackedREPAIRED HORIZ STAB UPPER LT AFT SKIN PLANK IAW EA 8-5510-123540.Jun 8, 2010 · N357FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR FDEA201006071855Plate · crackedLT WING L/E CAVITY UPPER JOINT PLATE IS CRACKED AT XFS 669. R & R JOINT PLATE AT LT WING L/E STA XFS 669 IAW SRM 51-33-01, VOL II AND SRM 51-35-01, VOL II.Jun 7, 2010 · N357FE · Doug MD1010F · Wing Main, Frame StructureSDR FDEA201006071857Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT IS CORRODED TOP & BOTTOM FROM BS 1868 TO BS 1871; LBL 56. REMOVED CORROSION IAW SRM 51-21-01, PG 28A, VOL II. 100% MATERIAL LOSS - OUT OF LIMITS IAW SRM 53-00-01, FIG 1-B, VOL I. REMOVED FLOOR SUPPORT FROM FS 1853 TO Jun 7, 2010 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201006051830Skin · scratchedLT WING - SLAT NR 5 LOWER SURFACE FOUND SCRATCHED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 31 VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Jun 5, 2010 · N560FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201006041813Panel Support · crackedLT WING L/E LOWER PANEL SUPPORT IS CRACKED AT XORS 98. R & R PANEL SUPPORT AT XORS 98 IAW SRM 51-33-01 AND 51-35-01, VOL II.Jun 4, 2010 · N357FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201006041815Fitting · crackedNR 3 SPOOL FITTING LOCATION HAS CRACK INDICATIONS AT HOLES "C" AND "D". R & R NR 3 SPOOL FITTING IAW SRM 51-31-01, VOL I, SRM 51-33-01, VOL II, SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123543.Jun 4, 2010 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201006041816Fitting · crackedNR 4 SPOOL FITTING LOCATION HAS CRACK INDICATIONS AT HOLES "A", AND "C". R & R NR 4 SPOOL FITTING IAW SRM 51-31-01, VOL I, SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123543.Jun 4, 2010 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201006041817Fitting · crackedNR 5 SPOOL FITTING LOCATION HAS CRACK INDICATIONS AT HOLES "C" AND "D". R & R NR 5 SPOOL FITTING IAW SRM 51-31-01, VOL I, SRM 51-10-00, VOL I, SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123543.Jun 4, 2010 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201006041818Fitting · crackedMCD NR 7 SPOOL FITTING LOCATION HAS CRACK INDICATIONS AT HOLES "A", "B", "C", "D". R & R NR 7 SPOOL FITTING IAW SRM 51-31-01, VOL I, SRM 51-35-01, VOL II, SRM 51-10-00, VOL I, SRM 53-50-00, FIG 17, VOL I AND EA 8-5310-123543.Jun 4, 2010 · N357FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201006041827Fitting · crackedLT WING - INBD FLAP WELL, FLAP SIDE LOAD FITTING FOUND CRACKED. LT WING INBD FLAP WELL AREA FLAP ROLLER FITTING R & R IAW SRM 51-31-01 VOL II REV 96. NEW FLAP ROLLER FITTING FABRICATED IAW DWG ANB7394 REVISION AA. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 1Jun 4, 2010 · N560FE · Doug MD1010F · Wing, Attach FittingsSDR FDEA201006041832Sensor · malfunctionedAFTER LANDING RECEIVED CABIN SMOKE ALERT. NO SMOKE OR FUMES SEEN. EVACUATED THE ACFT AFTER BLOWING L1 SLIDE. AFTER APPLYING ELECTRICAL POWER THERE WAS NO CABIN SMOKE INDICATION ON OVERHEAD SMOKE DETECTION PANEL. ACCESSED VIA AND AIU NO FAULTS IN CURRENT FJun 4, 2010 · N550FE · Doug MD1010F · Fire DetectionSDR FDEA201006031781Skin · crackedLT WING - INBD ASSY UPPER SURFACE OTBD AREA FOUND CRACKED. REPAIRED IAW SRM 57-10-00 VOL I, REVISION 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Jun 3, 2010 · N560FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006031782Beam · crackedMAIN DECK CARGO COMPARTMENT - LT 3 DOOR ASSY, BEAM NR 2 FROM LOWER FOUND CRACKED. CRACKED NR 2 BEAM AT MAIN DECK CARGO COMPARTMENT LT NR3 DOOR ASSY. REPAIRED IAW SRM 51-31-01, VOLUME II AND EA NR 8-5210-139247, REPAIR CLASSIFIED MAJOR GMM 6-2-100 REV 110.Jun 3, 2010 · N560FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201006031783Beam · crackedMAIN DECK CARGO COMPARTMENT - RT 3 DOOR ASSY, BEAM NR 1 FROM UPPER FOUND CRACKED. CRACKED BEAM AT MAIN DECK CARGO COMPARTMENT RT NR3 DOOR ASSY, NR1 FROM UPPER R & R IAW SRM 51-31-01 VOL II, REV 110.Jun 3, 2010 · N560FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201006031803Stiffener · crackedRT WING L/E LOWER PANEL SUPPORT STIFFENER IS CRACKED AT WING STA XORS 940, AFT SIDE. STOP DRILLED CRACK IN FORMER IAW SRM 57-00-01, FIG 3, SHEET 2, VOL I. FORMED REPAIR DOUBLERS IAW SRM 57-00-01, FIG 3, SHEET 2, VOL I. HEAT TREATED REPAIR DOUBLERS IAW SJun 3, 2010 · N357FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201006031804Skin · crackedRT WING L/E INNER SKIN IS CRACKED AT WING STA XORS 560. RECEIVED MATERIAL ID 0.020 6AL-4Y TITANIUM AMD FABRICATED DOUBLER IAW SRM 57-10-00, PG 222, VOL I. PRIMED IAW SRM 51-21-01, VOL II. INSTALLED DOUBLER IAW SRM 57-10-00, PG 222, VOL I.Jun 3, 2010 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006031805Skin · crackedLT WING L/E CAVITY UPPER SKIN IS CRACKED AT AT XFS 672. FABRICATED DOUBLER IAW SRM 57-10-00, FIG 71, PG 222, VOL I. PRIMED DOUBLER IAW SRM 51-21-01, VOL II. INSTALLED DOUBLER IAW SRM 57-10-00, FIG 71, PG 222, VOL I.Jun 3, 2010 · N357FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201006031806Rib · crackedLT WING L/E RIB IS CRACKED AT XORS 270; UPPER FRONT SPAR AREA. REPAIRED CRACKED RIB IAW E.A. 8-5710-123546.Jun 3, 2010 · N357FE · Doug MD1010F · Wing, Rib/Bulkhead
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