GE CF6-50E2

Service difficulty reports · 401

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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 = 'CF650E2'
  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 P5CA0401105Manifold · leakingFUEL DRAINING FROM DRAIN MAST NR 3 ENGINE PORT ON ENGINE START. REPLACED NR 3 ENGINE VBR FUEL MANIFOLD ASSY AS PER MM 75-32-00. OPS & LEAK CHECK OK AS PER MM 71-00-00 TEST NR 3.Jun 20, 2004 · N505MC · Boeing 7472D3B · Engine Fuel DistributionSDR UIEA200400114Acm · unserviceableAFTER TAKEOFF, NR 3 AIR CONDITIONING PACK STARTED MAKING LOW RUMBLING SOUND. SMELLED BURNING ODOR, TURNED NR 3 PACK OFF FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 3 AIR CYCLE MACHINE. GROUND OPERATION CHECK NORMAL IAW MM.Jun 17, 2004 · N517MC · Boeing 747243B · Cabin Cooling SystemSDR UIEA200400113Fuel Filter · contaminatedNR 1 ENGINE FAILED DURING CRUISE, FLIGHT LEVEL 350, .84 MACH, NORMAL FLIGHT. FOLLOWED PROCEDURES AND ATTEMPTED TO RESTART ENGINE WITH NO SUCCESS. ACCOMPLISHED ENGINE INLET AND EXHAUST INSPECTION ALL NORMAL. REPLACED NR 1 ENGINE FUEL FILTER IAW MM, LEAK CHECKJun 16, 2004 · N518MC · Boeing 747243B · Aircraft Fuel Filter/StrainerSDR P5CA0401101Line · looseDURING CLIMBOUT NR 4 ENGINE FIRE LIGHT ILLUMINATION AND FIRE BELL SOUNDED. ENGINE SHUT DOWN, BOTTLES NOT FIRED. FOUND SENSE LINE OFF PRV. SECURED LINE & CHANGED UNION PER MM 36-11-19. OPERATIONAL CHECK OK.Jun 9, 2004 · N355MC · Boeing 747341 · Pneumatic Distribution SystemSDR P5CA0401102Relief Valve · leakingDURING A/C CLIMBOUT AT 23,000 FT, NR 4 ENGINE NACELLE TEMPERATURE WAS INDICATING 8 UNITS. ACCOMPLISHED PROCEDURE FOR ABNORMAL NACELLE TEMPERATURE RETURNED TO NORMAL. NACELLE TEMPERATURE FLUCTUATED WITH THROTTLE MOVEMENT. REMOVED AND REPLACED PRESSURE REGULAJun 9, 2004 · N355MC · Boeing 747341 · Pneumatic Distribution SystemSDR UIEA200400111Handle · malfunctionedDUE TO GEAR DOOR OPEN INDICATION: AFTER GEAR RETRACTION, RED DOOR OPEN LIGHT REMAINED ILLUMINATED. RAN SECTION 3 PROCEDURES, LT WING GEAR DOOR OPEN LIGHT ILLUMINATES WITH PRIMARY AND ALTERNATE DOOR SELECTION SWITCHES. DOOR IS OPEN WITH AIRCRAFT RUMBLE. UP OJun 7, 2004 · N517MC · Boeing 747243B · Landing Gear SelectorSDR UIEA200400102Bulkhead · crackedD-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L. 146.5, ALSO THE STRUT SKIN ASSEMBLY AT THE AFT LOWER ACCESS CUT OUT EDGE ADJACENT TO THE STRAP CRACK LOCATION WAS FOUND WITH CHAFING DAMAGJun 4, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Bulkhead/FirewallSDR UIEA200400103Bulkhead · crackedD-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACCESS CUT OUT EDGE CHAJun 4, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Bulkhead/FirewallSDR P5CA0401100Mec · failedAFTER ENGINE START, NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT, IDLE PARAMETERS NORMAL. REPLACED MEC PER AMM 73-21-01.Jun 3, 2004 · N509MC · Boeing 747230B · Fuel Control/Turbine EnginesSDR UIEA200400110Antenna · inoperativeATB DUE TO BOTH RADARS INOPERATIVE: AFTER LEVEL OFF, BOTH RADAR SCREENS INOPERATIVE. SHOWED BLUE AZIMUTH LINES, BUT NO RANGE OR SWEEP. REPLACED RADAR ANTENNA. OPERATION CK IAW MM, ALL NORMAL. NOTE: NO FUEL DUMPED.Jun 3, 2004 · N540MC · Boeing 747243B · Independent Position Determining SystemSDR UIEA200400108Precooler · cracked(D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN Jun 2, 2004 · N808MC · Boeing 747212B · Pneumatic Distribution SystemSDR UIEA200400109Skin · crackedD-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TJun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR UIEA200400107Skin · cracked(D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOJun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR UIEA200400105Skin · crackedD-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE, Jun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR UIEA200400104Frame · damagedD CHECK, DURING MAINT INSP FOUND COCKPIT EMERGENCY EXIT DOOR CUTOUT FRAME AND CHORDS DAMAGED BETWEEN STA 360 AND 380 WITH MISDRILLED HOLES BETWEEN STRINGER 2L AND 2AL. SEVERAL MISDRILLED HOLES AND DRILL STARTS WERE REPAIRED AS FOLLOWS. FOR BS 360, WEB DAMAGEJun 2, 2004 · N808MC · Boeing 747212B · Fuselage Main, FrameSDR UIEA200400096Fitting · crackedD-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TERMINATING ACTION, DAMAGE WAS FOUND AT THE UPPER MOST FASTENER HOLE ON THE RIGHT SIDE OF THE FITTING AFT VERTICAL FLANGE. THE DEFECT WAS COMMay 25, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Main FrameSDR UIEA200400097Skin · wrinkledD CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC STA 286. THE DAMAGES ARE JUS AFT OF THE STRUT LARGE TITANIUM DOUBLER. SUBJECT SKIN ASSEMBLY WASMay 25, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR P5CA0401088Connector · damagedAFTER PUSH BACK ON ENGINE START, NR 2 ENGINE EGT GAUGE HAD FLAG IN VIEW. T/S FOUND BROKEN PIN IN CONNECTOR, REPLACED, ALL INDICATIONS NORMAL.May 7, 2004 · N534MC · Boeing 7472F6B · Electrical ConnectorsSDR P5CA0401089Wire Harness · damagedDURING ENGINE NR 2 START AT GATE, CREW REPORT THAT ENGINE NR 2 EGT NO INDICATION & FLAG IN VIEW. TROUBLE SHOT, FOUND RT UPPER HARNESS AT FAULT. REMOVED AND REPLACE ENGINE HARNESS, ENGINE RUN OPS CHECK OK.May 6, 2004 · N534MC · Boeing 7472F6B · Engine Indicating System WiringSDR UIEA200400089Engine · malfunctionedPRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM OF ABOUT 10-15 PERCENMay 4, 2004 · N536MC · Boeing 747228F · Engine (Turbine/Turboprop)SDR UIEA200400068Valve · inoperativeAZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USEDApr 22, 2004 · N536MC · Boeing 747228F · Pneumatic Distribution SystemSDR UIEA200400051Bushing · worn(D) CHECK, DURING SCHEDULE MAINTENANCE, NR 8 MOVEABLE CANOE AFT SECTION SECONDARY DOOR ASSEMBLY LOWER BEARING FOUND MIGRATED. THE LUG BORES ARE OVERSIZED TO 0.7827 INCH DIAMETER TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE. AN ALUMINUM REApr 15, 2004 · N522MC · Boeing 7472D7B · Wing, Control SurfacesSDR UIEA200400047Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 1 PYLON PERCOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. Apr 13, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400048Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 2 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. Apr 13, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400049Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 3 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. Apr 13, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400050Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 4 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSEMBLY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITIOApr 13, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400044Stiffener · crackedD CHECK, DURING SCHEDULE MAINTENANCE OF NR 1 PYLON, THE LHS NR 5 STIFFENER END WAS FOUND CRACKED AT NAC STA 288.0 WL 146.5. TRIMMED OFF THE CRACKED STIFFENER END. FABRICATED A REPAIR PLATE TO MATCH THE TRIMMED OFF PORTION OF THE STIFFENER ATTACHING FLANGE. Apr 8, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon Miscellaneous StructureSDR UIEA200400045Beam · crackedD CHECK, CRACKS WERE FOUND AT RT WING LE LOWER OUTBOARD BEAM LOCATIONS AT ILES 414.50 AND 543.93. TRIMMED OUT CRACKED PORTIONS OF BEAM NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICED IN REPLACEMENT SECTIONS OF BEAM BETWEEN TRIM LINES AND PROApr 8, 2004 · N522MC · Boeing 7472D7B · Wing Main, Frame StructureSDR UIEA200400046Slide · malfunctionedUPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, SLIDE/RAFT FAILED TO FULLY INFLATE. SEQUENCING MECHANISM RELEASED TO FACILITATE SLIDE RAFT REMOVAL AND DISPATCH TO STOP. NOTE: ACTUAL OR APApr 8, 2004 · N808MC · Boeing 747212B · Escape SlideSDR UIEA200400043Frame · crackedD CHECK, DURING SCHEDULE MAINTENANCE INSPECTION OF NR 3 PYLON, THE BULKHEAD UPPER ASSEMBLY RHS FORWARD ANGLE FRAME FLANGE WAS FOUND CRACKED AT THE END FASTENER HOLE COMMON TO THE FRONT SPAR FITTING AND STRUT CAP SKIN ASSY. FABRICATED A REPAIR ANGLE TO RESTOREApr 7, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Main FrameSDR UIEA200400041Skin · dentedDURING A MAINTENANCE INSPECTION, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 2 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CHORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSPECTION,Apr 7, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400042Skin · dentedD CHECK, DURING A MAINTENANCE INSP, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 3 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSP, INCApr 7, 2004 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200400038Skin · dentedDURING D CHECK, SKIN DENT FOUND ON FWD CARGO DOOR CUTOUT. A SKIN GOUGE ON THE SKIN OF THE FORWARD CARGO DOOR CUTOUT AFT SKIN EDGE, BS670, BETWEEN S-37 AND S-38 WAS REPAIRED BY TRIMMING OUT THE GOUGE. A HFEC AND DETAILED VISUAL INSPECTION WITHIN 20 INCHES WASApr 6, 2004 · N522MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA200400039Floorbeam · damagedDURING D CHECK, FOUND UPPER DECK FLOORBEAM, ONE ELONGATED HOLE WITH A SHORT EDGE MARGIN WAS FOUND COMMON TO STA 360 UPPER DECK FLOORBEAM UPPER CORD. THIS AIRCRAFT WAS MODIFIED TO A SPECIAL FREIGHTER CONFIGURATION. OVERSIZED SME HOLE TO 0.250 INCH DIAMETER (CApr 6, 2004 · N522MC · Boeing 7472D7B · Fuselage Main, Floor BeamSDR UIEA200400037Housing · corrodedDURING D CHECK AT SIN, PITTED CORROSION FOUND OUTBOARD TRAILING EDGE MID-FLAP IB CARRIAGE BRG HOUSING. REMOVED LOCAL SURFACE DAMAGE FROM THE AFFECTED AREA OF HOUSING. NDT INSPECTED TO INSURE CRACK AND DEFECT FREE CONDITION. SMOOTH, BLENDED AND REFINISHED HOApr 5, 2004 · N522MC · Boeing 7472D7B · Trailing Edge FlapsSDR UIEA200400040Fan · inoperativeDURING TAXI IN, SMELL OF SMOKE FROM THE AIR CONDITIONING SYSTEM. FLIGHT DECK FAN SWITCHED OFF WITH NO FURTHER SMELL. AFTER SHUTDOWN, UNABLE TO SWITCH FAN BACK ON. CIRCUIT BREAKER PULLED AND ITEM TRANSFERRED DMI M04-064. REMOVED AND REPLACED FLIGHT COMPARTMApr 4, 2004 · N516MC · Boeing 747243B · Air Distribution FanSDR P5CA0401066Cable · disconnectedNR 1 ENGINE ACCELERATES EXTREMELY SLOW. THE N2, EGT, AND FUEL FLOW ARE NOT ALIGNED WITH OTHER ENGINES. N1 GAUGE REMAINED AT IDLE. CORRECTIVE ACTION: DISCONNECTED MEC VSB/VBV, FEEDBACK CABLES EXERCISED MEC. RECONNECTED VSV/VBV FEEDBACK CABLES. PERFORMED ENApr 3, 2004 · N355MC · Boeing 747341 · Fuel Controlling SystemSDR UIEA200400034Fire Loop · chafedAT APPROXIMATELY 10,000 FT, NR 2 ENIGNE 'A' LOOP WAS INDICATING 7 UNITS, 'B' LOOP INDICATING 2.5. COMPLETED FHB 3.26.10 PROCEDURES NACELLE TEMPERATURE INDICATION ABNORMAL. RETARDED THROTTLE NO CHANGE, 30 SECON LATER 'A' LOOP INDICATES 9 PLUS, 'B' LOOP FLUCTUMar 29, 2004 · N526MC · Boeing 7472D7B · Fire DetectionSDR UIEA200400032Door · missingBIRD STRIKE: VIBRATION OF ENTIRE AIRFRAME ON CLIMB OUT. SUDDEN VIBRATION AT APPROXIMATELY 16,000 FT AND 300K IAS. PERFORMED BIRD STRIKE INSP MM. FOUND DAMAGE TO THE FORWARD NR 1 ACM INLET LEFT SIDE AREA AND NR 1 ACM DOOR MISSING. REPAIRED DAMAGED AREA IAWMar 14, 2004 · N537MC · Boeing 747271C · Air Conditioning DoorsSDR IUEA200400028Connector · dirtyGT8971/5 DNA/BKK ATB AND IFSD DUE TO NR 1 ENGINE FALSE FIRE WARNING: NR 1 ENGINE FIRE INDICATION DURING CLIMB, ALL OTHER SYSTEMS NORMAL EXCEPT (B) LOOP WAS DEFERRED. (A) LOOP WAS INDICATION FAULT AND FIRE. ENGINE SHUTDOWN ACCOMPLISHED AND FUEL JETTISON 28.3Mar 8, 2004 · N506MC · Boeing 7472D3B · Fire DetectionSDR P5CA0401051Relief Valve · illuminatedAT APPROX 6,000 FT NR 4 ENG LOOP FAULT LT ILLUMINATED NACELLE TEMPS A&B OBSERVED RAPIDLY CLIMBING TO 9. REMOVED AND REPLACED HIGH PRESS VLV, HIGH PRESS BLEED VLV HARNESS. REMOVED AND REPLACED PRESSURE RELIEF VLV. ENG OPS CHECKED GOOD, NO DEFECTS NOTED PER MMar 6, 2004 · N505MC · Boeing 7472D3B · Pneumatic Distribution SystemSDR P5CA0401050Connector · looseNR 1 ENG WILL NOT START. MANUAL START UNSUCCESSFUL. FOUND CONNECTOR LOOSE ON NR 1 ENG BLEED AIR VALVE. RECONNECTED PLUG, OPS CHECK OK PER MM 36-11-00.Mar 5, 2004 · N505MC · Boeing 7472D3B · Engine Bleed Air System WiringSDR UIEA200400027Panel · looseMXP/BOM ATB DUE TO SIDE CARGO DOOR OPEN LIGHT ON: SIDE CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF AND REMAINED ON AFTER TAKEOFF. FOUND SECURING PANEL ON LATCH DOOR MECHANISM WITH LOOSE SCREWS. TIGHTENED SCREWS, EXERCISED DOOR AND CHECKED OPERATION, FOUND Mar 4, 2004 · N518MC · Boeing 747243B · Cargo/Baggage DoorsSDR UIEA200400009Skin · corrodedDURING (D) CHECK, WING LOWER SKIN CORROSION FOUND AROUND SURGE TANK SUMP DRAIN VALVE AT WING STA 1487, BETWEEN STRINGERS S-5 AND S-6 LT SIDE. CORROSION DAMAGE IS REPAIRED BY BLEND OUT. REPAIR AREA IS SHOP PEENED AND HFEC INSPECTED. APPLIED ALODINE 1200 AND Feb 2, 2004 · N517MC · Boeing 747243B · Wing, Plate/SkinSDR UIEA200400008Beam · crackedDURING (D) CHECK AT SIN, RT WING LEADING EDGE NOSE BEAM WEB FOUND WITH 4.2500 CRACK AT ILES 1042. REPAIR, TRIM OUT SECTION OF CRACKED WEB TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICE IN REPLACEMENT WEB REPAIR SECTION WITJan 27, 2004 · N517MC · Boeing 747243B · Wing Main, Frame StructureSDR UIEA200400007Duct · misalignedAIR TURNBACK DUE TO NR 3 ENGINE FIRE WARNING. NOTICED EGT AT 850 DEGREES, ON TAKEOFF AT 100 DEGREE HIGHER THAN NR 2 AND NR 4 ENGINES. REMOVED AND REPLACED T/R DRIVE DUCT ASSEMBLY IAW MM, PERFORMED PNEUMATIC LEAK TEST IAW MM, NO LEAKS FOUND. DISCOVERED TURBIJan 26, 2004 · N809MC · Boeing 747228F · Air Distribution SystemSDR P5CA0301003Csd · leakingNR 4 ENGINE CSD LIGHT ON. CSD DISCONNECTED. TRANSFERRED TO DMI 31912 PER MEL 24-1 1A CSD AND GENERAL REMOVED PER MM 24-11-00.Dec 7, 2003 · N354MC · Boeing 747341 · Alternator-Generator DriveSDR P5CA0301000Check Valve · failedNR 1 ENG AT TOP OF DESCENT, FL 380, ENG. STALLED. ENG. RECOVERED AT FL 330 AND STALLED AGAIN. ENGINE SHUT DOWN. REMOVED AND REPLACED 8TH STAGE CHECK VALVE RUN UPPER LEAK CHECK, OK IAW MM 36-11-02 AND 71-00-43.Nov 21, 2003 · N505MC · Boeing 7472D3B · Compressor Bleed ControlSDR UIEA200300066Engine · leakingDOV-RMS - NR 3 ENGINE SHUTDOWN DUE TO ZERO OIL QUANTITY AND PERSSUER BELOW 10 PSI WITH LOW OIL PRESSURE LIGHT ON AT 1509Z. AFTER SHUTDOWN OIL PRESSURE WENT TO ZERO WHILE WINDMILLING. AIRCRAFT DIVERTED TO AMS. REMOVED AND REPLACED ENGINE NR 3 ACCORDING TO MMNov 14, 2003 · N524MC · Boeing 7472D7B · Turbine Engine Oil SystemSDR P5CA0300984Strip · wornNR 1 ENG FAN STATOR ASSY ABRADALE STRIP DAMAGE AT 4 TO 5 O'CLOCK POS. ENG CHANGE REPLACEMENT REQ'D PER ATLAS AIR FORM 01-AA-45. ACCOMPLISH PYLON INSP PER CF6-50E2 R/R WORK CARD OK TO INSTALL. REPAIRED ABRADALE STRIP PER MM 72-31-04.Nov 9, 2003 · N354MC · Boeing 747341 · Turbine Engine Compressor Section
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