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.

SDR UIEA2010110900176Sleeve · crackedDURING MX WALKAROUND OF MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX THE 2 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 2.25" LONG AND IS NEAR THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS WITHIN LNov 9, 2010 · N415MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR FDEA201011094294Rib · crackedLT WING T/E AREA 1EA RIB CRACKED POSITION UNDER NR3 SPOILER INBD SIDE. FABRICATE NEW PART IAW DWG A-57240194. REPLACED NEW PART IAW SRM 51-72-10 AND 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 9, 2010 · N665FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201011094288Skin · crackedWHILE CARRYING OUT WALKAROUND CHECK, FOUND LOWER CTR CARGO DOOR WITH 01 EACH EDGE CRACK AT FWD LOWER CORNER. REPAIRED AS PER SRM 52-30-16 FIGURE 201 REVISION 44.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.Nov 9, 2010 · N616FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201011094291Shim · migratedLT WING NR 6 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE SHIM MIGRATED. EA6-2750-141649 REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011094292Shim · misalignedLT WING NR4 FLAP TRACK FRONT CARRIAGE UPPER SHIM MIGRATED IAW EA6-2750-141649 REPAIR ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011094293Shim · migratedLT WING NR3 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE SHIM MIGRATED, IAW EA6-2750-141649 REPAIR ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011084285Frame · deformedMAIN DECK CARGO - FRAME AT STA 1721, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO STATION 1721 LONGERON 12LH FRAME AREA CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 1Nov 8, 2010 · N618FE · Doug MD11F · Fuselage Main, FrameSDR UIEA2010110700174Sleeve · crackedDURING MX WALKAROUND OF MX FOUND 3EA CRACKS ON THE EXHAUST NOZZLE OUTER SLEEVE, THE FIRST CRACK STARTING AT APPROX THE 12 O'CLOCK POSITION AND ENDING AT THE 2 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 19" LONG AND IS APPROX 13" FNov 7, 2010 · N493MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR IPXA10663562Floor Panel · damagedREF D 434408, POSITION 2L HAS 1 X 1 HOLE IN FLOOR PANEL. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693G AND INSTALLED IAW AMM 51-01-01.Nov 6, 2010 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR UIEA201000239Engine · shutdownSHORTLY AFTER TAKEOFF NR1 ENGINE OIL FILTER ILLUMINATED. SHUTDOWN ENGINE. ON ARRIVAL FOUND EICAS SHOWN OIL QTY READING 1 FOR NR1 ENGINE. ON INSP FOUND OIL IN THE TAIL PIPE. CHECKED MAIN CHIP DETECTOR AND "B" SUMP FOUND HEAVY METAL DEPOSIT ON CHIP DETECTORS. Nov 2, 2010 · N409MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR FDEA201011014203Warning Light · illuminatedON DEPARTURE RECEIVED LEVEL 1 "ANTI ICE SENSOR FAIL" REMAINED ON UNTIL SHUTDOWN IN CHOCKS.Nov 1, 2010 · N596FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA201011014200Longeron · crackedCTR CARGO COMPARTMENT RT TUNNEL STRUCTURE FOUND LONGERON L-29 CRACKED AT STA 1676. LONGERON AT STATION 1676 L-29RH CENTER CARGO COMPARTMENT TUNNEL TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-05 FIGURE 202 REVISION 44. THIS REPAIR IS CLASSIFIED AS MNov 1, 2010 · N618FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201011014201Skin · cracked08 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA 713.6.Nov 1, 2010 · N618FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201011014202Skin · cracked10 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.6. REPAIR CARRIED OUT AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= Nov 1, 2010 · N618FE · Doug MD11F · Wing, Plate/SkinSDR UIEA201000238Structure · delaminatedDURING WALKAROUND INSP, MX FOUND THE LT WING GEAR DOOR - LOWER EDGE DELAMINATION, MEASURING 9.0 IN. X 0.500 IN. (REF. FIG 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY Oct 31, 2010 · N497MC · Boeing 74747UF · Landing Gear DoorsSDR IPXA10663424Connector · brokenINSPECTION TYPE:ETOP DIVERSION - "CARGO DET AIR" EICAS MESSAGE. M438137. R & R SMOKE DETECTOR VACUUM SWITCH IAW AMM 26-16- 04-4. FOUND CONNECTOR BROKEN ON SWITCH.Oct 29, 2010 · N302UP · Boeing 76734AF · Fire Protection System WiringSDR HALA2010102700501Syncronizer · out of adjustETOPS SIGNIFICANT SYS - AT LOW TO MID RANGE POWER SETTING ENGINES ARE OUT OF SYNC BY ABOUT 1 PERCENT, AS OF 10/27/10, NR1 ENG HAS 61,562 TSO. NR 2 ENG HAS 14,934 TSO. ALL ENG "EPR" LIMITS NORMAL. OK FOR SERVICE.Oct 27, 2010 · N598HA · Boeing 767332 · Engine SynchronizingSDR FDEA201010274175Wire Harness · failedRTO AT 70 KTS DUE TO LEVEL 1 "FIRE DET 3 FAIL" INDICATION. INSPECTED NR 3 ENG FIRE LOOP HARNESS . FOUND WIRE AT CONNECTOR (TB2) ,WIRE (A) BROKEN AT TERMINAL END. PERFORMED RESISTANCE CHECKS FOR (B) LOOP FIRE DETECTORS, FOUND BROKEN RESPONDER AT UPPER LT(B)Oct 27, 2010 · N574FE · Doug MD11F · Fire Protection System WiringSDR HALA2010102600499Projector · smokeF/A RPT SMOKE IN CABIN. SMOKE MAY HAVE COME FROM VIDEO EQUIP FRONT OF MID CABIN. PAX REPORTED SEEING SPARKS SCREEN WARM TO TOUCH DOWN POWERED ALL PAX ENTR EQUIP PULLED CB'S T8 & U32 DOWNPWD UTILITY BUSSES, TEAC EQUIP PWR ON LT STILL SHOWS PWR. SMOKE DISSAPAOct 26, 2010 · N594HA · Boeing 767332 · Entertainment SystemSDR HALA2010102500497A/C Pack · malfunctionedETOPS SIGNIFICANT SYS - RT PACK DOES NOT OPERATE ON GROUND. PERFORMED RT PACK BITE. RESET PACK RT PACK NOW OPS NORMAL, OK FOR SERVICE.Oct 25, 2010 · N596HA · Boeing 767332 · Cabin Cooling SystemSDR UIEA201000237Nose Cowl · dentedMX FOUND NR 3 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 2 O' CLOCK POSITION MEASURING 12.0 INCHES IN LENGTH X 5.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO SHARP CREASES AND/OR CRACK CONDITION EXOct 24, 2010 · N408MC · Boeing 74747UF · Engine Air Intake SystemSDR HALA2010102300488Pump · leakingETOPS SIGNIFICANT SYS - LT QTY HYD AT ,65 RF. FOUND NR1 ENGINE DRIVEN PUMP HSG LEAKING. R & R NR1 EDP IAW AMM 29-11-05. LEAK AND OPS CHECK OK. RESERVICED LT HYD SYS AS REQUIRED NO LEAKS NOTED. OK FOR SERVICE.Oct 23, 2010 · N596HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), MainSDR UIEA201000236Skin · damagedDURING WALK-AROUND , MX FOUND DAMAGE TO THE RT WING OTBD FORE AND AFT FLAPS (REF FIG 1-3).DIMENSIONS AND DETAILS: RT OTBD FORE FLAP WBL793 - L/E PUNCTURE - 2.250 IN. X 2.0 IN. (REF FIG 1). RT OTBD FORE FLAP WBL810 - L/E PUNCTURE - 5.0 IN. X 2.5 IN. (REF FIG 2)Oct 22, 2010 · N499MC · Boeing 74747UF · Trailing Edge FlapsSDR FDEA201010224151Switch · faultedKRUGER FLAP WOULD NOT RETRACT AFTER TAKEOFF OR EXTEND FOR LANDING. FOUND EXTEND SWITCH FAULTING IAW TSM 27-80-12. R & R SWITCH IAW AMM 27-89-11-04-0. OPS CKD GOOD.Oct 22, 2010 · N428FE · Airbus A310203 · Leading Edge Slat Control SystemSDR UIEA201000234Skin · damagedDURING A3 CHECK INSP OF ACFT, MX FOUND 4 EA CHAFE MARKS ON THE RT INBD AFT FLAP UPPER EXTERNAL SKIN CAUSED BY BOTTOM OF SCREWS THAT SECURE AFT SECTION OF COVE PANEL. AFTER BLENDOUT AREAS 1-4 FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01, FIG 101, DETAIOct 18, 2010 · N498MC · Boeing 74747UF · Trailing Edge FlapsSDR FDEA201010164085Line · leakingHYD 1 OFF ALERT IN CRUISE 2.7 G REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. FOLLOWED QRH PROCEDURES LANDED WITHOUT INCIDENT. REPLACED LT INBD FLAP ACTUATOR PRESSURE LINE IAW AOct 16, 2010 · N617FE · Doug MD11F · Hydraulic System, MainSDR UIEA201000231Cam · crackedDURING A-CHECK AND INSP IAW EO 4452A068, WEAR WAS FOUND IN THE MAIN DECK SIDE CARGO DOOR MIDSPAN LATCH CAM THAT IS OUTSIDE OF WEAR LIMITS IAW THE AMM 52-32-01-206. FWD MID SPAN LATCH CAM ID= 1.1740 , ALLOWED WEAR LIMITS IAW AMM IS 1.1240 (0.05). AFT MID SPAN Oct 10, 2010 · N499MC · Boeing 74747UF · Cargo/Baggage DoorsSDR DALA1026051521Skin · crackedFOUND DURING PSV13 THE INBD SIDE SKIN OF THE NR2 ENG PYLON WAS FOUND CRACKED AT THE OVAL CUTOUT AT APPROX NAC STA 235 AND RAN FROM THE UPPER AFT CORNER APPROX 2.5 IN AND TERMINATES AT A FASTENER. REPAIRED IAW ERA 486275-14 REV ORIG.Oct 8, 2010 · N394DL · Boeing 767324 · Nacelle/Pylon, Plate/SkinSDR FDEA201010063961Seat Track · crackedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1521 X=75 FOUND CRACKED. TRIMMED OUT IAW SRM 53-00-52, FIG 201, REVISION 44. CRACK SEAT TRACK REMOVED IAW SRM 51-33-01 REV 44. REPAIR SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201, REV 44.Oct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010063962Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-0 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1 REV B EXISITING SPLICE REMOVED AND RE-ISTALLED IAW SRM 51-33-01, REV 44. REPAIR COct 6, 2010 · N585FE · Doug MD11 · Fuselage Miscellaneous StructureSDR FDEA201010063963Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-53 TO STA 5-83 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1, REV B. EXISTING SPLICE REMOVED AND RE-INSTALLED IAW SRM 51-33-01, REVOct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010063964Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK FLANGE AT STATION 5-0 TO STATION 5-53 X= 8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK REMOVED AND AND NEW SEAT TRACK INSTALLED IAW SRM 51-33-01 REV 44. NEW SEAT TRACK FABRICATED IAW DWG REV B. EXISTING SPLICE REMOVED AND RE-Oct 6, 2010 · N585FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1025741802Oven · fireTHIRTY MINUTES AFTER DEPARTURE, F/A REPORTED THE ODOR OF SMOKE IN THE AFT GALLEY. CREW STATED THAT AFT GALLEY NR 4 OVEN EMITTED ODOR AND FLAMES. AFTER THEY PULLED C/B THE SMOKE AND FLAME EXTINGUISHED. SOURCE WAS CONFIRMED. FLT CONTINUED REMOVED OVENS 3 AND 4 IOct 5, 2010 · N826MH · Boeing 767432ER · Buffet/GalleysSDR HALA2010100300437Fuel Filter · cloggedETOPS SIGNIFICANT SYS- ON T/O RT-ENG FUEL FILTER LIGHT CAME ON, NO OTHER INDICATIONS OBSERVED. R & R RT ENG FUEL FILTER IAW AMM 73-11-02 ACCOMPLISHED TEST 2 MOTOR THE ENG IAW AMM 71-00-00 NO LEAKS, NO FAULTS NOTED. OK FOR SVC.Oct 3, 2010 · N598HA · Boeing 767332 · Engine Fuel DistributionSDR HALA2010100200438Altimeter · inoperativeETOPS SIGNIFICANT SYS - CAPT ALTIMETER DISPLAYS OFF FLAG. REPLACED ALT IAW MM 34-13-01, CHECKS OK.Oct 2, 2010 · N594HA · Boeing 767332 · Altimeter, Barometric/EncoderSDR HALA2010100100436Fire Loop · brokenETOPS SIGNIFICANT SYS - WHILE PERFORMING OVERNIGHT/ETOPS EICAS DISPLAYED RT ENG OH LP2. FOUND UPPER FWD OVERHEAT LOOP WITH BROKEN FITTING AT RESOLVER. R & R IAW AMM 26-11-02/401 CONFIG 2. FOUND UPPER AFT OVHEAT LOOP WITH BROKEN FITTING. R & R IAW AMM ABOVE.Oct 1, 2010 · N598HA · Boeing 767332 · Fire DetectionSDR UIEA2010092800167Panel · damagedEO 4425A197; DURING MX WALKAROUND, MX FOUND THE MAIN DECK - RT BS1250, WL 248 SIDEWALL PANEL DAMAGED; HOLE 2.5 IN. LONG X 1.5 IN. WIDE. (IAW AMM 25-52-01-308-062, THE DAMAGE/HOLE IS OUT OF LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCSep 28, 2010 · N499MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR IPXA10662816Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662817Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662844Floor Panel · dentedAFT PANEL AT POSITION 5 CTR HAS A DENT, FULL LENGTH OF THE PANEL AND THROUGH A PREVIOUS REPAIR. MARKED. REMOVED FLOOR PANEL 14315876-58 IAW AMM 53-01-05-4. REFERENCE L/P 450341 ITEM 2 FOR PNL INSTALL. ITEM IS A MAJOR REPAIR TRANSFERRED TO NRC 355068. COMPLETSep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662845Floor Panel · dented2ND FROM AFT PANEL AT POSITION 5 CTR IN MCD HAS DENT RUNNING APPROX 2 FT LONG AT AFT EDGE GOING FWD AND THROUGH 2 PREVIOUS REPAIRS. (MARKED) REMOVED PANEL IAW AMM 53-01-05-4. SEE LP 450338/1 REF D413473 AND REF L/P 450342/1 FOR REMOVAL AND REINSTALL. ITEM IS Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662846Floor Panel · dentedCTR FLOORBOARD PANEL AT POS 10/11 HAS 3 HOLES ALONG WITH SEVERAL OTHER HOLES ON DEFERRAL REF D413492, D426407. REMOVED PANEL IAW AMM 53-01-05-4. REF L/P 450341/3 FOR PANEL INSTALLATION. THIS IS AS MAJOR REPAIR TRANSFERRED TO NRC 355067. ALL WORK COMPLETED ONSep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662847Floorboard · dentedPREVIOUS REPAIR FAILED ON MCD CNTR FLOORBOARD POS 9/10. REQUIRES NEW REPAIR PANEL. REPAIR IS A MAJOR REPAIR TRANSFERRED TO NRC 355064. SEE LOG PAGE 450344 FOR REMOVAL ITEM NR1.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UIEA2010092600163Fairing · damagedDURING WALK-AROUND INSPECTION, MX REPORTED THE NR 8 FLAP TRACK FAIRING 'CANOE' DAMAGED WITH A CRACK AND 2 DENTS (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, DVI INSPECTIONS AFTER EVERY 5 FLIGHT Sep 26, 2010 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR IPXA10662794Floor Panel · puncturedFLOOR PANEL AT POS 9L HAS SMALL PUNCTURE. REPAIRED IAW SRM 53-00-50-2R.Sep 26, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR UIEA2010092500165Support · damagedDURING WALK-AROUND INSP, MX REPORTED THE RBG - BRAKE TORQUE LIMITER NR 11 - LOAD SENSOR RING SUPPORT; CABLE DAMAGE LOAD SENSOR RING SUPPORT AND CABLE ASSY DAMAGED. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONSSep 25, 2010 · N492MC · Boeing 74747UF · Main Landing Gear Attach SectionSDR FDEA201009243697Skin · corrodedFWD CARGO COMPT- 136AR ACCESS DOOR SURROUNDING CUTOUT SKIN INTERIOR SURFACE FOUND CORROSION (FR38.1-38.2 , STGR49R-54L) REMOVED CORROSION IAW SRM 51-74-10 THE REMAINING THICKNESS IS 0.040" PER NTM 51-10-04 NO CRACK FOUND IAW NTM 51-10-08 AND NTM 51-10-18 Sep 24, 2010 · N410FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201009243699Frame · crackedUPPER AFT FUSELAGE FRAME CLIP AT CANT STA Y = 2069 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01, REVISION 44. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201009233691Seat Track · wornMAIN DECK CARGO COMPARTMENT - SEAT TRACK 5R AT FRAME 61 HAS ONE EACH ELONGATED SCALLOP MEASURED AT .985. R & R DAMAGED SEAT TRACK SECTION FRAME 58 TO 62 SEAT TRACK 5R IAW SRM 53-10-16, PARA 10 AND 51-72-10.Sep 23, 2010 · N445FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009233692Skin · delaminatedRT ELEVATOR LOWER SURFACE HAS 3 SPOTS BULGED PAINT WITH LIGHT SURFACE CORROSION AT STA 622 AND 2 SPOTS OF BULGED PAINT, LIGHT SURFACE CORROSION AT STA 472. REMOVED CORROSION IAW SRM 51-74-10, NDT CHECK COMPLIED FOUND SKIN DELAMINATED. REPAIRED RT ELEVATOR Sep 23, 2010 · N445FE · Airbus A310203 · Elevator, Plate/Skin
Back to GE CF6-80 series