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 HALA2011022000109Warning Message · false activationETOPS SIGNIFICANT SYS - EICAS MESSAGE AILERON LOCKOUT ILLUMINATED AT HIGH SPEED (270KTS ACCELERATING) FOR 2 MIN THEN EXTINGUISHED. OTBD AILERONS INDICATED NORMAL-LOCKED OUT. TROUBLESHOT IAW FIM 27-11-00-1, FIG 104, FOUND TO BE OK FOR SERVICE.Feb 20, 2011 · N597HA · Boeing 767332 · Central WarningSDR UIEA2011021800090Skin · delaminatedMAJOR REPAIR. DURING WALK-AROUND INSP. MX FOUND THE NR 4 RT THRUST REVERSER TRANSLATING COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN, LOCATED APPROX AT THE 3 O'CLOCK POSITION (REF FIG 1 AND 2). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESFeb 18, 2011 · N409MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2011021600140Bolt · wrong partFWD NR 1, NR 8 BOLT TOO SHORT REF EGAT EI NR T2011A27B-349, REV 00. REPLACED NEW BOLT.Feb 16, 2011 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR FDEA201102140556Seat Track · corrodedMAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 & FRAME 76; LBL 43. REPAIRED MAIN DECK SEAT TRACK BETWEEN FRAME 74 TO FRAME 76 WITH 35 INCHES OF SEAT TRACK SECTION AND SPLICE IAW SRM 53-10-16, FIG 208, SHEET 1, LBL 43.Feb 14, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011021400093Indicator · failedETOPS SIGNIFICANT SYS- DURING CRUISE AND DESCENT IN TURBULENCE, CAPT ALTIMETER VACILATED +- 200 TO 500' WHILE F/O ALTIMETER STEADY AND IVSI ALSO STEADY. REPLACED CAPT'S ALTIMETER INDICATOR. OPS CHECK OK IAW MM 34-13-01.Feb 14, 2011 · N594HA · Boeing 767332 · Altimeter, Barometric/EncoderSDR DALA1110950129Light · inoperativeEMERGENCY LIGHTS AT L1 CLOSET DOOR ARE INOPERATIVE. MX RE-SECURED THE LIGHT ASSY. SYS OPS IS NORMAL.Feb 14, 2011 · N129DL · Boeing 767332 · Emergency LightingSDR UIEA2011021400139Access Door · wornWORN ON NR 1 PYLON RT ACCESS DOOR ASSY. REPAIRED DAMAGE AREA IAW T2011A54B-34, REV 00.Feb 14, 2011 · N409MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR HALA2011021300090Probe · malfunctionedLT FUEL QUANTITY & TOTAL QTY INTERMITTENT EICAS MSG FUEL QTY IND DISPLAYED FUEL QTY TEST NOT CHECKED. BITE CHECKED FQIS PROCESSOR SHOWS FAULT CODE C4. REPLACED NR 4, 9 & 14 LT TANK PROBES & LT MAIN TANK COMPENSATOR. FQIS CAPACITANCE & INSULATION RESISTANCE TFeb 13, 2011 · N598HA · Boeing 767332 · Fuel Quantity IndicatorSDR FDEA201102030466Blades · damagedDURING INITIAL CLIMBOUT, FELT MODERATE VIBRATION (FELT LIKE NOSE GEAR SPINNING). AFTER INITIAL LEVEL OFF AT 9000 FT, VIBRATION LESSENED. DURING CLIMB TO 15000 FT, VIBRATION CONTINUED TO REVERSE WITH HIGH EVM READING. RAN QRH & WITH HIGH EVM & VIBRATION AFeb 3, 2011 · N599FE · Doug MD11F · Turbine Engine Compressor SectionSDR HALA2011020100070A/C Pack · malfunctionedETOPS SIGNIFICANT SYS - AFTER START UP, LT PACK WOULD NOT OPERATE WITH NORMAL PNEU PRESS. RECYCLED SWITCH TO NO AVAIL, CLOSE APU VALVE AND REOPENED AND PACK OPERATED NORMALLY. GROUND RUN CHECK OK AFTER ENG START PNEU PRESS AND OPS OF LT PACK CHECK OK WITHOUTFeb 1, 2011 · N598HA · Boeing 767332 · Cabin Cooling SystemSDR FDEA201101310424Skin · damaged.5" X .5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITTING IAW SRM 55-41-12 PARA 30 WET LAYUP REPAIR. NO CORE DAMAGE EXIST AT 22" AFT OF NR4 ATTACH FITTIJan 31, 2011 · N423FE · Airbus A310203 · Rudder, Plate/SkinSDR FDEA201101310426Lamp · inoperativeDURING TRANSIT CHECK FOUND SLIDE PRESSURE PRESS-TO-TEST LIGHT INOP. RELEASED FOR SERVICE IAW MEL: 25-61-02. RELAMPED LT PRESSURE INDICATOR AND FUNCTION CHECKED PER MM 25-61-04-5-0. FOUND NORMAL. CLEARED DMI.Jan 31, 2011 · N612FE · Doug MD11F · Escape SlideSDR FDEA201101300411Cable · wornWHILE PERFORMING AFT DOOR CHECKS, R4 DOOR FWD CABLE JUMPED PULLEY AND IS DAMAGED. DEPRESSURIZED DOOR ASSIST BOTTLE. REMOVED PULLEY FOR R4 DOOR LOWER CABLE DRIVE UNIT, R4 DOOR LOWERING CABLE HAS 4 STRANDS BROKEN IN A 1" AREA. IAW AMM 20-20-06-2 THE NYLONJan 30, 2011 · N583FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201101290410Line · looseAFTER EXTENDING LANDING GEAR, RECEIVED A "HYD 3 QTY LO" ALERT. QTY STABILIZED AT 1.7 ON ARRIVAL FOUND NR 3 HYD SYS QTY IND READ 2.8 AFTER ENG SHUTDOWN. FOUND STAB COMP DOOR AREA & NR 3 LEFT EDP SUCTION HOSE ELBOW AREA HYD STAIN. SERVICED NR 3 HYD SYS TO 7.5 IJan 29, 2011 · N589FE · Doug MD11F · Hydraulic System, MainSDR FDEA201101290409Skin · damagedFOUND SKIN DAMAGED. CARGO DOOR AFT CUTOUT SKIN AT STATION 1781 LONGERON 39 CARRIED OUT REPAIR AS PER SRM 53-00-15 REPAIR 8 FIGURE 201 REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Jan 29, 2011 · N596FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201101290407Seat Track · corrodedMAIN DECK STA 1663 "X" = -75.25 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.Jan 29, 2011 · N614FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011012800052Adc · malfunctionedETOPS SIGNIFICANT SYS - ABOUT 45 MIN FROM DESTINATION, F/O'S AIRSPEED INDICATOR JUMPED FROM 260 TO 285 & ALTIMETER WENT FROM 38,000 TO 38,200, VSI DOWN 1000' IAW MIN. CAPT'S INSTRUMENTS NORMAL. EICAS MESSAGES: OVERSPEED IAS DISAGREE, ALT DISAGREE, RUDDER RATJan 28, 2011 · N597HA · Boeing 767332 · Air Data ComputerSDR SAJFCALS100005Engine · failed(ACFT/B-18317) DURING CLIMB AT 10,500FT, ENG 1 SPOOLED DOWN AND ENGINE FAIL MESSAGE OCCURED. CREW ATTEMPTED TO RELIGHT BUT IN VAIN. ENGINE 1 WAS THEN SHUTDOWN AND ACFT RETURNED TO DEPARTURE. GROUND INSP FOUND METAL CHIPS IN TAIL PIPE. ENGINE WAS REPLACED DJan 24, 2011 · N18317 · Airbus A330300 · Engine (Turbine/Turboprop)SDR SAJFCALS100005R1Engine · failed(ACFT/B-18317)THIS IS TO CORRECT THE INFORMATION PREVIOUSLY REPORTED AS SAJFCALS100005. DURING CLIMB AT 10,500 FT, ENGINE 1 SPOOLED DOWN AND ENGINE FAIL MESSAGE OCCURED. CREW ATTEMPTED TO RELIGHT BUT IN VAIN. ENGINE 1 WAS THEN SHUTDOWN AND ACFT RETURNED TO Jan 24, 2011 · N18317 · Airbus A330300 · Engine (Turbine/Turboprop)SDR FDEA201101220333Mount · corrodedDURING NR 2 ENGINE PYLON MOUNT AFT HOLE CORROSION REMOVAL FOUND LOWER MATING FACE WITH CORROSION NEAR TO THE HOLE. REPAIRED IAW EA 6-5450-143832. DEEPEST REWORKED SURFACE: 0.019" AND MAXIMUM ALLOWABLE DEPTH: 0.0138" IAW SRM 54-51-81 CONFIGURATION 2, FIG 104,Jan 22, 2011 · N663FE · Airbus A300F4605R · Engine Mount SectionSDR UIEA2011012200035Web · brokenBROKEN WEB AFT LWR CARGO STRUCTURE AT STA 1760 BETWEEN STRINGER S43R TO S44R (REPAIR DAMAGE AREA IAW SRM 51-70-13, REV 58)Jan 22, 2011 · N412MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR FDEA201101210324Skin · damagedLT WING - WING TIP T/E SEVERAL RIVET HOLES ELONGATED. REMOVED AS PER SRM 51-40-21 REVISION 19. ELONGATED HOLES REWORKED AS PER DRAWING A57247017 ISSUE M AND NEW RIVETS INSTALLED AS PER SRM 51-40-21 REVISION 19. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISJan 21, 2011 · N663FE · Airbus A300F4605R · Wing, Plate/SkinSDR UIEA2011012100017Frame · crackedREPAIR NR 4 ENG RT FAN REVERSER TORQUE BOX FWD FRAME CRACK. (REPAIR IAW EI NO T2011 A78B-208 REV 00)Jan 21, 2011 · N412MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2011012000006Structure · dentedDURING WALK-AROUND INSP, DAMAGE WAS FOUND TO THE LOWER LOBE - BS 1820, WL 188 - LOWER AFT CARGO DOOR CONSISTING OF A DENT. LENGTH: 10 IN. WIDTH: 2.0 IN. DEPTH:0.175 (REF. FIG 1). THE DAMAGE IS OUT OF THE SRM 52-30-01, FIG 101, ALLOWABLE DAMAGE 1, DETAILS XI AJan 20, 2011 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR DALA1104731605Floorbeam · corrodedCORROSION ON FLOORBEAM AT FS 865 AND LBL 33. REPAIRED ON NRC 154.Jan 20, 2011 · N1605 · Boeing 767332 · Fuselage Main, Floor BeamSDR FDEA201101190287Jackscrew · inoperativeFLAP SYSTEM 1, 2, FAULT ON OVERHEAD PANEL ON ECAM. ATTEMPTED TO CYCLE FLAP HANDLE BUT PROBLEM REMAINED. FOLLOWED QRH RETURNED TO DEPARTURE. HAPPENED WHEN FLAPS 15 SELECTED. FLAPS APPEARED STUCK APPROX 13-14 DEG, WOULD NOT MOVE PAST THAT. ACFT BELOW MAX LJan 19, 2011 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR UIEA2011011900015Cowling · chafedCHAFING FOUND NR 1 ENG LT CORE COWL HAD CHAFING ON INTERIOR FRAME AREA AT ABOUT 3:00. (REPAIR DAMAGE AREA IAW SRM 54-45, FIG 201, REPAIR 1. REV 58.)Jan 19, 2011 · N412MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR IPXA11664546Angle · crackedINSPECTION TYPE:C, BULK CARGO COMPT STA 1581, RT INBD CABIN LWR SPLICE ANGLE FOUND CRACKED. BULK CARGO COMPT STA 1581 RT INBD CABIN LWR SPLICE ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 49.Jan 18, 2011 · N304UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR HALA2011011700056Floor Support · corrodedLEVEL 2 CORROSION FOUND OUTSIDE SRM LIMITS, SECT 43 FLOOR STRUCTURE TRUSS STA 654+105, LBL 95 IAW SRM 53-00-51-1A-1, REV 84. SECT 43 FLOOR STRUCTURE TRUSS STA 654+105 LBL 95 REPLACED IAW SRM 51-40-02 REV 84.Jan 17, 2011 · N594HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA2011011500033Engine · malfunctionedETOPS SIGNIFICANT SYS - DURING START LT ENGINE STOPPED ACCELERATING AT 55.7 PERCENT AND 744 DEGREES C, TERMINATED START AFTER N2 RPM 0. MOTORED ENGINE FOR 1 MIN ATTEMPTED 2ND START ENGINE STARTED NORMALLY MAX EGT 640. CW B, FIM 71-06-00, FIG 101, SHEET 1 RANJan 15, 2011 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR FDEA201101150181Apu · smokeAPU SMOKE (BOTTLE DISCHARGED, IAW SMF THERE IS OIL LEAKING FROM APU AND APU OIL QTY IS ZERO. IAW FLIGHT CREW DISCHARGED BOTTLE, NO FIRE WARNING INDICATION WAS PRESENT. NOTIFIED BY MX POSSIBLE APU FIRE. DISCHARGED ON BOTTLE. REMOVED AND REPLACED OUTBD. FIREJan 15, 2011 · N574FE · Doug MD11F · APU Core EngineSDR HALA2011011400027Probe · malfunctionedETOPS SIGNIFICANT SYS - TAT PROBE EICAS LT ON. REPLACED TAT PROBE IAW MM 34-12-02. OPS CK OK IAW M/M 30-33-00.Jan 14, 2011 · N580HA · Boeing 767332 · Pitot/Static Anti-Ice SystemSDR FDEA201101130129Skin · crackedRT WING LOWER SKIN PANEL INBD OF RIB 9 JUST INBD OF STIFFENER, FOUND WITH SUPPORT CRACK. REPAIR CARRIED OUT AS PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.Jan 13, 2011 · N663FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201101120106Skin · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON RT WING LOWER BOTTOM SKIN PANEL INBD OF RIB NR 9. REPAIR CARRIED OUT PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.Jan 12, 2011 · N663FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201101120107Frame · crackedMAIN DECK CARGO COMPARTMENT, WITH REF TO EO 6-5310-7-5006A1 PART 1, PAGE 21 OF 48 STEP 79, FRAME 44 HOLE B ABOVE STRINGER 26, CRACK INDICATION FOUND. REPAIR CARRIED OUT PER EO NR 6-5310-7-5006 A1 PART 1. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISIJan 12, 2011 · N663FE · Airbus A300F4605R · Fuselage Main, FrameSDR WRLA20110112464Frame · crackedTAIL CONE FRAME CANTED STA 2165.062 CRACKED. TEMPORARY REPAIR PER SRT ENGINEERING INSTRUCTIONS 53-EI-268842.Jan 12, 2011 · N382WA · Doug MD11F · Aerodynamic FairingsSDR DALA1102330124Skin · delaminatedRT WING OTBD FLAP LWR SURFACE MID INSPAR PANEL SKIN DELAMINATED AT APPROX 66"FROM INBD AND 24" FRM BOTTOM; CA: REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 57-53-01 OTIS. REPAIR PARTS BONDED IAW SRM 51-70-10 OTIS. DECAL INSTALLED ADJ TO REPAIR IAW PS 900-5-Jan 11, 2011 · N124DE · Boeing 767332 · Trailing Edge FlapsSDR FDEA201101100096Attach Fitting · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON FWD CARGO DOOR ACTUATOR ATTACH FITTING AT FRAME 22A. REMOVED IAW SRM 51-40-21, REV 19 AND REPLACED WITH NEW FRAME SECTION IAW SRM 51-40-21, REV 19 AND EA 6-5230-143830. THIS REPAIR IS CLASSIFIED AS MAJOR Jan 10, 2011 · N663FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR HALA2011010800023Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - DURING GEAR RETRACTION ON TAKE OFF, GEAR HORN & CONFIG LIGHT CAME ON WHEN GEAR HANDLE PLACED IN UP POSITION. BOTH DISAPPEARED WHEN HANDLE PLACED IN OFF POSITION. R & R LDG CONFIG WARNING MODULE CARD IAW AMM 31-51-04. OPS CK GOOD IAW AJan 8, 2011 · N596HA · Boeing 767332 · Landing Gear Position and WarningSDR HALA2011010800024Actuator · failedETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS CAME ON DURING DESCENT APPROX 10,OOO FT. T/S IAW FIM 27-11-00/101 NO FAULTS ON BOTH SAM IAW FIG 104A, CKD ALL CONNECTION FOUND NO FAULTS. DURING AILERON LOCKOUT TEST LT ACTUATOR APPEARS TO STALL. REPLACED SAME AJan 8, 2011 · N597HA · Boeing 767332 · Aileron Control SystemSDR FDEA201101060022Fitting · corrodedUPON REMOVAL OF LOWER WEB AT VERTICAL STAB FOUND CORROSION ON AFT FITTING AT LT ATTACH POINT. REMOVED CORROSION ON AFT TRAVERSE FITTING ON VERT STAB AT REAR SPAR IAW SRM 51-74-10, PG 5. BEFORE THICKNESS 0.557, AFTER 0.448. LOSS OF 0.069 IS OUT OF LIMITS IAWJan 6, 2011 · N443FE · Airbus A310203 · Vertical StabilizerSDR FDEA201101060023Rib · corrodedVERTICAL STABILIZER INTERIOR DIAGONAL ANGLE AT RT JOINT OF RIB 9 AND STR 2 HAS CORROSION ABOUT 4 SQ INCHES. REMOVED DIAGONAL BRACE AT RIB 10 AND REAR SPAR ON VERTICAL STABILIZER IAW SRM 51-72-10, PG 1-3. REMOVED CORROSION IAW SRM 51-76-10, PG 205, PARA 6. Jan 6, 2011 · N443FE · Airbus A310203 · Vertical Stabilizer, Spar/RibSDR FDEA201101060024Stiffener · corrodedVERTICAL STABILIZER INTERIOR REAR SPAR HORIZ STIFFENER BETWEEN RIB 9 AND RIB 10 HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZ STIFFNER AND DIAGONAL STIFFNER BETWEEN RIB 9 AND 10 AT VERT STAB REAR SPAR. REMOVED CORROSION ON HORIZ STIFFNER, NOMINAL 0.050, REJan 6, 2011 · N443FE · Airbus A310203 · Vertical Stabilizer Miscellaneous StructureSDR FDEA201101060025Angle · corrodedVERTICAL STABILIZER REAR SPAR FWD FACE RIB 9, HORIZ ANGLE HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZONTAL ANGLE AT FWD FACE OF RIB 9 IAW SRM 51-40-21, PG 22 PARA 7. REMOVED CORROSION IAW SRM 51-74-10, PG 205, PARA 3. NOMINAL THICKNESS IS 0.063, REMAINJan 6, 2011 · N443FE · Airbus A310203 · Vertical Stabilizer, Spar/RibSDR FDEA201101060026Structure · corrodedVERTICAL STABILIZER REAR SPAR LT CHORD, RIB 10 TO RIB 16 HAS CORROSION AT 11 EA NUT PLATES LOCATIONS. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145551.Jan 6, 2011 · N443FE · Airbus A310203 · Vertical StabilizerSDR FDEA201101060027Structure · corrodedVERTICAL STABILIZER RT CHORD BETWEEN RIB 18 AND RIB 25 HAS SURFACE CORROSION AROUND NUTPLATES, 3 PLACES, APPROX 3 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145551.Jan 6, 2011 · N443FE · Airbus A310203 · Vertical StabilizerSDR FDEA201101060031Fitting · corrodedVERTICAL STABILIZER LT AFT FITTING HAS CORROSION ON OTBD FACE, 2 LOCALIZED AREAS ABOUT 3 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145557.Jan 6, 2011 · N443FE · Airbus A310203 · Vertical Stabilizer, Attach FittingsSDR FDEA201101060033Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS SURFACE CORROSION BETWEEN FR 85 AND FR 86, BETWEEN STR 5 LT AND STR 6 LT. CLEANED FUSELAGE TAIL SECTION EXTERNAL SKIN BETWEEN FR 85 AND FR 86 BETWEEN STR 5L AND 6L IAW AMM 12-21-12. UPON FURTHER INSPECTION NO CORROSIONJan 6, 2011 · N443FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201101060035Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL FUSELAGE SKIN HAS SURFACE CORROSION AT FR 84, STR 5 LT ABOUT 7 SQ INCHES. CLEANED FUSELAGE TAIL SEC EXTERNAL SKIN BETWEEN FR 85 AND FR 86 AND STR 5R AND 6R IAW AMM 12-21-12. AFTER FURTHER INSP, NO CORROSION NOTED. REPROTECTEDJan 6, 2011 · N443FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201101060045Spar · crackedCRACK AT FRONT SPAR CONNECTING SECTION AT RIB 1,2.5 INCH LONG. REMOVED TRANSVERSE FITTING AT VERTICAL STAB FWD SPAR RIB 1 AND REMOVED CONNECTION SECTION AT RIB 1 IAW SRM 51-72-10 PG 1-3. CLEANED AREA IAW AMM 12-21-11. REPROTECTED AREA IAW SRM 51-75-10 PG 3Jan 6, 2011 · N443FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
Back to GE CF6-80 series