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 FDEA201009153452Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR 5 INBD LUG FACE OUTER SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153457Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR7 MOUNTING SURFACE IS CORRODED. NON-ROUTINE N01018 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153458Hinge Fitting · corrodedLT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR3; INBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153459Hinge Fitting · corrodedLT WING OTBD FLAP; OTBD HINGE FITTING; LOCATION NR3; OTBD BORE CHAMFER IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153481Hinge Fitting · wornLT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 5; OTBD BUSHING IS WORN. REPLACED THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009153482Hinge Fitting · corrodedLEFT WING OTBD FLAP; INBD HINGE FITTING; LOCATION NR 5; INBD LUG FACE INNER SURFACE IS CORRODED. NON-ROUTINE N01019 IS REPLACING THE HINGE ASSEMBLY.Sep 15, 2010 · N370FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201009143371Floor Panel · damagedCENTER CARGO BAY FLOOR PANEL, NR 183DF HAS SEVERAL DAMAGED INSERTS. FABRICATED CENTER CARGO BAY FLOOR PANEL 183 DF IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143372Floor Panel · damagedAFT CARGO BAY FLOOR PANEL NR 187DF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED AFT CARGO BAY FLOOR PANEL 187 DF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143374Floor Panel · damagedFWD CARGO BAY FLOOR PANEL 123DF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED FLOOR PANEL 123 DF IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143378Floor Panel · damagedCENTER PIT FLOOR PANEL 183 XF HAS EDGE DAMAGE AND FASTENER HOLE DAMAGE. FABRICATED CENTER PIT PANEL 183 XF IAW FEDEX DWG SRZ 25-005, REV "H".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143377Floorboard · damagedFWD PIT FLOORBOARD AT STA 1059-1089 LT, INBD HAS DAMAGE AROUND FASTENER HOLE ON THE EDGE. FABRICATED FWD PIT PANEL 127 UF; STA 1059 TO STA 1089 IAW SRZ 25-005, REV "H".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143379Floor Panel · crackedTAIL CONE LT UPPER FLOOR PANEL IS CRACKED. FABRICATED PANEL FOR TAIL CONE LT UPPER IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143380Floor Panel · puncturedTAIL CONE LWR CTR FLOOR PANEL IS PUNCTURED IN SEVERAL PLACES. FABRICATED TAILCONE LT LOWER CENTER PANEL IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143381Floor Panel · wornTAIL CONE; AFT PATIO DOOR HAS HONEYCOMB EXPOSED. FABRICATED TAIL CONE AFT ACCESS DOOR IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143382Floor Panel · crackedTAIL CONE; RIGHT PATIO DOOR FLOOR PANEL IS CRACKED. FABRICATED TAIL CONE RIGHT PATIO DOOR PANEL IAW DWG SRZ 25-005, REV "H". REMOVED FLOORBOARD PER SRM 51-31-01, VOL II. INSTALLED NEW FLOORBOARD PER SRM 51-31-01, VOL II.Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009143375Floor Panel · damagedFWD PIT FLOOR PANEL 123GF HAS EDGE DAMAGE IN SEVERAL PLACES. FABRICATED FLOOR PANEL 123 GF IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N370FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201009123347Seat Track · damagedCABIN - LT STA 930 - 935 X=47.5 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 929 TO STATION 989 X=47.5 AS PER SRM 53-70-00 FIG 1 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Sep 12, 2010 · N40061 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009123350Skin · dentedRT WING OTBD FLAP LOWER SURFACE OTBD OF INBD HINGE FOUND DENT. REPAIRED AS PER SRM 57-10-00 FIG 7 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 12, 2010 · N40061 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201009123348Skin · damagedRT WING NR4 SLAT LOWER SURFACE INBD AFT EDGE FOUND DAMAGED. DAMAGED SKIN AT LOWER SURFACE OF RT WING NR4 SLAT INBD AFT EDGE, TRIMMED AND CARRIED OUT REPAIR IAW SRM 57-10-00, FIG 31, VOLUME I, REV 96. SLAT OPS AND GAP CHECK CARRIED OUT FOUND SATISFACTORY IAW Sep 12, 2010 · N40061 · Doug MD1010F · Leading Edge DevicesSDR FDEA201009123349Skin · dentedRT WING OTBD FLAP LOWER SURFACE AREA JUST INBD OF OTBD HINGE FOUND DENT. RT WING OTBD FLAP LOWER SURFACE AREA JUST INBD OF OTBD HINGE DENT AREA REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 7, VOLUME I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111Sep 12, 2010 · N40061 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201009103339Fitting · crackedMCD NR2 SPOOL HAS A CRACK INDICATION AT HOLE "C". REMOVED SPOOL FITTING NR 2 IAW SRM 51-31-01, VOL II. MATERIAL ID IAW MD/DC10 SRM 53-50-00, FIG 17, VOL I. INSTALLED NEW SPOOL FITTING IAW SRM 51-33-01, VOL II, PERFORMED HFEC IAW NATSPM 06-10-01.003 ON 4 ESep 10, 2010 · N370FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201009103340Fitting · crackedMCD NR 5 SPOOL HAS A CRACK INDICATION AT HOLE "D". REMOVED AND REPLACED THE NR 5 SPOOL FITTING IAW SRM 51-31-01, VOL II AND SRM 51-33-01, VOL II. MACHINED AND INSTALLED BUSHING IN HOLE "D" IAW SRM 53-50-00, VOL I.Sep 10, 2010 · N370FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201009093331Beam · crackedCRACK INDICATION FOUND ON 1ST LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE A. REPAIRED AS PER EA 8-5310-143730. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Sep 9, 2010 · N40061 · Doug MD1010F · Fuselage Main, StructureSDR FDEA201009053279Support Bracket · crackedCABIN - L3 MED PLUG NR 6 DOOR BEAM SUPPORT BRACKET FOUND CRACKED. DAMAGED SUPPORT BRACKET AT CABIN L3 MED PLUG NR6 DOOR BEAM REMOVED IAW SRM 51-31-01 VOLUME II, REV 96. NEW SUPPORT BRACKET FABRICATED IAW DWG ADA3754 REV F AND INSTALLED IAW EA 8-5210-132476. Sep 5, 2010 · N40061 · Doug MD1010F · Service DoorsSDR FDEA201009053281Attach Fitting · unknownEXISTING REPAIR AT MLG LT WING TRUNNION FITTING AFT UPPER ATTACHMENT HOLE. REPAIRED AS PER EA 8-5740-143417. (MAJOR REPAIR)Sep 5, 2010 · N562FE · Doug MD1010F · Wing, Landing Gear Attach FittingsSDR FDEA201009053285Skin · misrepairedLT WING SLAT NR 7 INNER SURFACE FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN-ACCORDANCE-WITH ANY APPROVED DATA. EXISTING REPAIR REMOVED AS PER SRM 51-35-02, VOLUME II, REVISION 96. NEW REPAIR ACCOMPLISHED AS PER SRM 57-10-00Sep 5, 2010 · N562FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201009053287Skin · misrepairedEXISTING REPAIR ON LT WING INBD FLAP ASSY, UPPER SURFACE, LOWER INBD SEGMENT. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AND FOUND NOT IN ACCORDANCE WITH APPROVED DATA. EXISTING REPAIR REMOVED AS PER SRM 51-35-01 VOL. II REVISION 96 AND NEW REPAIR ACCOMPLISSep 5, 2010 · N562FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201009053295Skin · misrepairedRT WING DURING INSTALLATION OF FUEL TANK ACCESS PANEL NR 638AB, FOUND ONE EXTRA FASTENER. RIGHT HAND WING FUEL TANK ACCESS PANEL 638AB CUTOUT 01 EACH EXTRA FASTENER CARRIED OUT REPAIR AS PER EA 8-5710-143726, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVSep 5, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201009053297Skin · misrepairedRIGHT HORIZONTAL STABILIZER DRY BAY, STA XE 228, UPPER STRINGER NR 9 FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR CARRIED PER EA 8-5510-143413, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100,Sep 5, 2010 · N562FE · Doug MD1010F · Horizontal Stabilizer StructureSDR FDEA201009053284Skin · misrepairedLT WING TELESCOPIC DUCT CUTOUT FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED AS PER EA 8-5710-143715, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.Sep 5, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201009053286Skin · misrepairedLT LOWER SURFACE FUELING STATION DOOR CUTOUT FOUND EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 68, VOLUME I, REVISION 96. EO 8-5100-7-5001 A7 PART 2,Sep 5, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201009053293Skin · misrepairedRIGHT HORIZONTAL STAB DRY BAY, STA XE 87, UPPER STRINGER NR 7 FOUND EXISTING REPAIR. EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR ACCOMPLISHED PER EA 8-5510-143416, REPAIR CLASSIFIED AS MASep 5, 2010 · N562FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR FDEA201009023237Coalescer Bag · dirtyAT FL360, AFTER COCKPIT TEMP ADJUSTMENT-STRONG SMOKE ODOR FOLLOWED BY LARGE AMOUNT OF SMOKE IN COCKPIT. FOLLOWED QUICK REF HANDBOOK FOR SMOKE AND FUMES. EMERGENCY DECLARED AND LANDED. REF MM 21-53-00-7 & JRH C/W PACK BURN ON ALL 3 ACFT. PACKS WITH ENG BLESep 2, 2010 · N564FE · Doug MD1010F · Humidity Control SystemSDR FDEA201008303191Panel · misrepairedMAIN DECK CARGO COMPARTMENT - EXISTING REPAIR FOUND ON LT MLG OVERPRESSURE PANEL TOP SURFACE AT STA 1381 TO STA 1401. EXISTING REPAIR ON LT MLG OVERPRESSURE PANEL TOP SURFACE BETWEEN STA 1381 TO STA 1401 LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW Aug 30, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008303192Panel · misrepairedMAIN DECK CARGO COMPARTMENT EXISTING REPAIR FOUND ON LT MLG OVER PRESSURE PANEL TOP SURFACE AT STA 1441 TO STA 1461. EXISTING REPAIR ON LT MLG OVER PRESSURE PANEL TOP SURFACE BETWEEN STA 1441 TO STA 1461. FOUND PREVIOUSLY ACCOMPLISHED AND NOT IAW APPROVED DAug 30, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008293177Angle · gougedLT TAILCONE APPROX AT STA 2230 PATIO DOOR HAS GOUGE ON MAIN FRAME. ACCOMPLISHED TAILCONE LT PATIO DOOR MAIN FRAME REPAIR IAW EA 8-5210-141189, MAJOR REPAIR.Aug 29, 2010 · N10060 · Doug MD1010F · Aerodynamic FairingsSDR FDEA201008293183Seat Track · corrodedAFT CARGO - LT SEAT TRACK STA 1841 LOWER SURFACE CORRODED UNDER ANCHOR NUT. CORROSION AT AFT CARGO LT SEAT TRACK, STA 1841 LOWER SURFACE REMOVED IAW SRM 51-21-01, VOL II, REV 96 AND FOUND WITHIN LIMIT IAW SRM 53-70-00 VOL I, REV 96. ORIGINAL THICKNESS 0.100Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008293184Seat Track · corrodedAFT CARGO - RT SEAT TRACK STA 1841 LOWER SURFACE CORRODED UNDER ANCHOR NUT. AFT CARGO RT SEAT TRACK STA 1841 LOWER SURFACE CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96 AND FOUND WITHIN LIMIT IAW SRM 53-70-00, VOL I, REV 96. ORIGINAL THICKNESS 0.100 INCH,Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008293185Stiffener · crackedLT WING L/E NR1 SLAT LOWER STIFFENER FOUND CRACKED. LT WING L/E NR1 SLAT LOWER CAP PN ARB1588-1, CRACKED AREA TRIMMED AND REPAIRED IAW EA 8-5750-143705. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Aug 29, 2010 · N562FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201008293187Rib · crackedRT WING DROOP L/E BELOW EXTERIOR SKIN TOP EDGE FOUND RIB CRACKED. RT WING DROOP L/E BELOW EXTERIOR SKIN TOP EDGE CRACK RIB REMOVED IAW SRM 51-31-01 VOLUME II, REV 96 AND INSTALLED WITH A FABRICATED RIB SRM 51-35-01, VOL II REV 96. RIB FABRICATED IAW DWG ARB1Aug 29, 2010 · N562FE · Doug MD1010F · Wing, Rib/BulkheadSDR FDEA201008293188Web · corrodedCTR CARGO - AFTER REMOVAL OF STA 1701 TO STA 1781 SUMP PANEL SUPPORT ABOVE LONGERON 45R, WEB BELOW SUPPORT FOUND CORRODED. CORRODED WEB AT CTR CARGO STA 1701 TO STA 1781 LONGERON 45 RT REMOVED IAW SRM 51-31-01, VOL II, REV 96. WEB FABRICATED IAW DWG NR AFA391Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201008293189Skin · chafedRT WING DROOP L/E FWD SURFACE FOUND CHAFED. RT WING DROOP L/E FWD CHAFED SURFACE REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 4, VOL I, REV 96. REPAIR CLASSIFIED IAW GMM 6-2-100, REV 111.Aug 29, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008293181Skin · misrepairedCABIN L3 DOOR FWD JAMB LOWER WEB FOUND EXISTING REPAIR. EXISTING REPAIR AT CABIN L3 DOOR FWD JAMB LOWER WEB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. CABIN L3 DOOR FWD JAMB LOWER WEB REPAIR CARRIED OUT IAW SRM 53-50-00, FIG 19, VOL Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008293182Web · misrepairedCABIN L3 DOOR AFT DOOR JAMB LOWER WEB FOUND EXISTING REPAIR. EXISTING REPAIR AT CABIN L3 DOOR AFT DOOR JAMB LOWER WEB EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW APPROVED DATA. CABIN L3 DOOR, AFT DOOR JAMB LOWER WEB REPAIR CARRIED OUT IAW SRM 53-50-0Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201008293179Skin · misrepairedLT WING DROOP L/E EXTERIOR SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR ON LT WING DROOP L/E EXTERIOR SURFACE FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-10-00 FIG 55, VOL I, REVISION 96 BUT FOUND WITH SHORT EDGE MARGIN. EXISTING REPAIR DOUBLER REMOVED IAW SRM Aug 29, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008293186Floorbeam · misrepairedCTR CARGO - EXISTING REPAIR AT STA 1701 FLOORBEAM WEB AFT SURFACE ABOVE LONGERON 44 RT TO LONGERON, 48 RT. EXISTING REPAIR AT CTR CARGO, STA 1701 FLOORBEAM WEB AFT SURFACE ABOVE LONGERON 44 RT TO LONGERON 48 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT Aug 29, 2010 · N562FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201008273161Hinge · corrodedFWD PIT DOOR HINGE INTERIOR SURFACE HAS CORROSION. REMOVED AND REPLACED HINGE SECTIONS IAW SRM 51-31-01. CLASSIFIED AS A MAJOR REPAIR.Aug 27, 2010 · N10060 · Doug MD1010F · Fuselage, Door HingeSDR FDEA201008253126Skin · crackedRT WING DROOP, L/E UPPER SKIN FOUND CRACKED. RT WING DROOP L/E UPPER SKIN CRACKED AREA REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 55, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Aug 25, 2010 · N562FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201008253127Skin · crackedAFT FUSELAGE COMPARTMENT DOOR 311AB CUT-OUT EXTERIOR SKIN DOUBLER FOUND CRACKED. REPAIRED IAW EA 8-5330-143712, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.Aug 25, 2010 · N562FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201008253125Angle · misrepairedRT WING SLAT NR 2 OTBD EDGE ANGLE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING SLAT NR 2 OTBD EDGE ANGLE EVALUATED AND FOUND ACCOMPLISHED NOT IAW ANY APPROVED DATA. NEW ANGLE FABRICATED IAW DWG NR ARB1647 REV C. ANGLE R & R IAW SRM 51-35-01 VOL II, REV Aug 25, 2010 · N562FE · Doug MD1010F · Leading Edge Devices
Back to GE CF6-6D