GE CF6-50E2

Service difficulty reports · 401

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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 = '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 P5CA0601445Starter · failedABORTED START ON NR 1 ENGINE, DUE TO SLOW ACCELERATION AND SPARKS FROM STARTER EXHAUST. REMOVED AND REPLACED NR 1 ENGINE STARTER PER MM 80-40-07. FUNCTION CHECKS NORMAL.Feb 15, 2006 · N509MC · Boeing 747230B · Engine StarterSDR CA060104006Manifold · failedOPERATOR REPORTED N1 VIBRATION AND METAL CONTAMINATION OF A SUMP SCAVENGE SCREEN AND MASTER CHIP DETECTOR. THE ENGINE WAS REMOVED FOR FURTHER INVESTIGATION. DURING INITIAL TROUBLESHOOTING, LOOSE MATERIAL WAS HEARD TUMBLING IN THE SPINNER CONE AND EVIDENCE OFDec 28, 2005 · Turbine Engine Oil SystemSDR P5CA0501415Wire · looseFLIGHT CREW REPORTED NR 3 ENGINE EGT INOP. FOUND LOOSE WIRE AT HARNESS END (PYLON CONNECTION). SECURED WIRE, ALL OPS AND INDICATIONS NORMAL IAW MM 77-00-00.Nov 25, 2005 · N355MC · Boeing 747341 · Engine Indicating System WiringSDR P5CA0501416Metering Tube · leakingNR1 ENGINE FUEL LEAK AT FUEL METERING UNIT VBV ROD END TUBE. VBV ACTUATOR FUEL TUBE REPLACED AT FUEL CONTROL AND PERFORMED ENGINE RUN AND LEAK CHECK IAW MM 73-21-01.Nov 20, 2005 · N508MC · Boeing 747230B · Fuel Controlling SystemSDR P5CA0501414Coupler · defectiveFO'S HEADING, FLIGHT DIRECTOR, AND BOTH VOR FLAGS IN RMI CAME INTO VIEW WITH HEADING FLAG IN HSI. REMOVED AND REPLACED NR 2 COMPASS COUPLER IAW AMM 34-21-00.Nov 2, 2005 · N508MC · Boeing 747230B · Magnetic CompassSDR UIEA200500166Switch · defectiveAT APPROX FL 280, AFT CARGO LIGHT ON FE`S PANEL AND CARGO DOOR LIGHT ON PILOTS PANEL BEGAN FLICKERING, SHORTLY IT CAME ON STEADY. DESCENDED AC TO FL250 AND ACCOMPLISHED FHB PROCEDURES FOR DOOR OPEN LIGHT. AT NO TIME EXPERIENCED PRESSURIZATION PROBLEMS PRIOR Oct 18, 2005 · N506MC · Boeing 7472D3B · Door Warning SystemSDR P5CA0501398Check Valve · failedAT FL 37.0 NR 3 ENGINE COMPRESSOR STALLED, ALL PARAMETERS NORMAL. OPS OK AT LOWER ALTITUDE. BORESCOPE PER MM 72-00-00 PG 680P, NO FINDINGS. FOUND 8TH STAGE CHECK VALVE FAILED. REPLACED SAME, OPS NORMAL PER 36-11-02.Sep 9, 2005 · N508MC · Boeing 747230B · Engine Bleed Air SystemSDR UIEA200500124Support · crackedD-CHECK, NR 2 PYLON, RT LWR AFT SKIRT FAIRING LOWER STIFFENER CRACKED. STOPPED DRILLED THE CRACK. NDT AND HFEC INSPECTED ALL AFFECTED FASTENER HOLES AND REPAIR AREA TO ENSURE CRACKS AND DAMAGE FREE CONDITION. FABRICATED AND INSTALLED 0.050 INCH THICK REPAIRAug 31, 2005 · N524MC · Boeing 7472D7B · Nacelle/Pylon Miscellaneous StructureSDR UIEA200500121Angle · out of limitsD-CHECK, NR 4 PYLON SIDE COWL HINGE SUPPORT ANGLE BRACE, ONE HOLE EXCEEDING LIMITS. THE HOLE WAS OVERSIZED TO 0.484 INCHES DIAMETER INCLUDING A .0312 DIAMETER INSURANCE CUT. THE HOLE WAS NDT INSPECTED TO ENSURE A CRACK AND DAMAGE FREE CONDITION. A REPAIR STAug 30, 2005 · N524MC · Boeing 7472D7B · Nacelle/Pylon, Main FrameSDR UIEA200500122Pressure Panel · crackedD-CHECK, FUSELAGE STA 1241 SLOPING PRESSURE DECK WEB WAS FOUND WITH CRACK AT DUCT CUTOUT. THE CRACKED AREA REPAIRED BY CUTTING EXISTING WEB SECTIONS BETWEEN UPPER EDGE OF THE SLOPING DECK AND REAR SPAR AND FROM BL 0 TO TRIM LINE. HFEC INSPECTED THE EDGE OF TAug 30, 2005 · N524MC · Boeing 7472D7B · Fuselage Floor PanelSDR UIEA200500123Skin · chafedD-CHECK, DURING MAINTENANCE INSPECTION, THE NR 2 STRUT RT SIDE SKIN ASSEMBLY INTERNAL BONDED DOUBLER WAS FOUND CHAFED AT THE 463AR ACCESS PANEL CUTOUT. THE INTERNAL DOUBLER AND SKIN WERE TRIMMED BACK PAST THE EXISTING CUTOUT IN THE OUTER SKIN. THE REPAIR AREAug 30, 2005 · N524MC · Boeing 7472D7B · Nacelle/Pylon, Plate/SkinSDR UIEA200500120Trunnion · chafedD-CHECK, RECESSED MARK ON RT BODY GEAR IB TRUNNION SUPPORT FITTING. THE RECESSED MARK WAS BLENDED OUT WITH A MINIMUM 63 RHR SURFACE FINISH. 10X VISUALLY AND HFEC INSPECTED TO ENSURE CRACK AND CORROSION FREE CONDITION. ALODINED AND REINSTATED THE FINISH. FIAug 29, 2005 · N524MC · Boeing 7472D7B · Landing Gear Retraction/Extension SystemSDR 0820200501Engine · leakingABOUT (1) HR AFTER DEPARTURE FROM (ORD), AT CRUISE FLT, NR 3 ENGINE LOSS OIL QTY AND OIL PRESSURE (TO ZERO) ACCOMPANIED BY ENGINE OIL PRESSURE NR 3 LIGHT. ACCOMPLISHED AOM PROCEDURE AND ENGINE FAILURE/SHUTDOWN CKLIST. AIRCRAFT RETURNED TO (ORD) WITHOUT FURTHAug 28, 2005 · N354MC · Boeing 747341 · Engine (Turbine/Turboprop)SDR UIEA200500119Wire Harness · shortedDAILY CHECK, IB PICKUP ITEM BY MAINTENANCE. UNABLE TO POWER CGO HANDLING BUSSES. REMOVED AND REPLACED BPCU NR 1 AND NR 2. ALSO, FOUND WIRE HARNESS W124, 12 WIRES SHORTED OUT. REPAIRED IAW SWPM ACCOMPLISHED, CARGO HANDLING SYSTEM CHECKS NORMAL. (K)Aug 25, 2005 · N537MC · Boeing 747271C · AC Power Distribution SystemSDR UIEA200500117Brake · leakingAFTER TAKEOFF, NR 4 HYD LOW QUANTITY LIGHT CAME ON. NR 4 SYSTEM WAS 1.5 GAL. SYSTEM WAS SHUTDOWN AND USED ONLY FOR LANDING. FOUND NR 8 BRAKE ASSY BLANKING PLATE MISSING AND LEAKING BAD. REMOVED AND REPLACED NR 8 BRAKE ASSY IAW MM. LEAK CHECK, OK. REPLACEAug 24, 2005 · N537MC · Boeing 747271C · Landing Gear Brake SystemSDR P5CA0501367Valve · stuckON TAKEOFF NR 1 ENGINE A-FIRE LOOP WENT TO 4.0. B-FIRE LOOP WENT TO 5.0 AND STAYED THERE UNTIL THROTTLES WERE RETARDED FOR DESCENT. FOUND NR 1 ENGINE HIGH STAGE VALVE STUCK OPEN, LOCKED CLOSED, OPENED MEL 36-01-3B.Jun 24, 2005 · N355MC · Boeing 747341 · Pneumatic Distribution SystemSDR P5CA0501373Engine · failedAFTER TAKEOFF NR 1 ENGINE FAILED. SHUT DOWN ENGINE AND JETTISON FUEL IAW CHECK LIST. AFTER SHUT DOWN OIL PRESSURE ZERO. NR 1 ENGINE REPLACED PER ENGINE CHANGE FORM 00-AA-45. RUN UP OK PER MM 71-00-00 TEST NR 3, 8 AND 9.Jun 14, 2005 · N508MC · Boeing 747230B · Engine (Turbine/Turboprop)SDR UIEA200500079Shear Tie · crackedFRAME 440, RT SIDE BETWEEN STRINGERS 10A AND 11 TOP HOLE OF FRAME TO FUSELAGE SKIN ATTACHMENT ANGLE HAS .2500 INCH CRACK GOING UPWARD AND .0625 INCH CRACK GOING DOWNWARD. CUTOUT CRACKED SECTION OF ATTACHMENT ANGLE IAW SRM. ACCOMPLISHED HFEC INSP OF CUTOUT OFMay 24, 2005 · N536MC · Boeing 747271C · Fuselage Internal Mounting StructureSDR UIEA200500078Servo Valve · leakingDURING CRUISE, NR 2 HYD QUANTITY WENT FROM 6.1 TO 2.2, 5 HOURS INTO FLIGHT. SUSPECT HYD LEAK. RAN PROCEDURES TO SHUTDOWN HYD SYSTEM NR 2 IAW FLIGHT HAND BOOK. REPLACED LOWER RUDDER POWER PACKAGE SERVO VALVE IAW MM. PRESSURIZED HYD SYSTEM IAW MM. LEAD CHECMay 20, 2005 · N534MC · Boeing 7472F6B · Hydraulic System, MainSDR P5CA0501348Valve · leakingNR 2 ENGINE HYDRAULIC SUPPLY C/B POP’S. REPLACED SUPPLY VALVE, OPS AND LEAK CHECK OK PER MM 29-11-04.May 1, 2005 · N355MC · Boeing 747341 · Hydraulic System, MainSDR P5CA0501347Nozzle · damagedON WALK AROUND, FOUND A HOLE APPROXIMATELY 1.5 INCH IN DIAMETER ON NR 3 ENGINE LONG FIXED CORE EXHAUST NOZZLE AT 8:00 O’CLOCK POSITION. REPAIRED NR 3 ENGINE LONG FIXED CORE COWL EXHAUST NOZZLE AS PER GE ENGINE MANUAL 78-11-01, REPAIR 010.Apr 27, 2005 · N509MC · Boeing 747230B · Engine Collector/Tailpipe/NozzleSDR UIEA200500063Bulkhead · crackedBS 400 BULKHEAD WEB CUT OUT FOR NOSE GEAR RETRACT ACTUATOR PAN FOUND BOTH LOWER CORNERS CRACKED. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, BulkheadSDR UIEA200500064Pylon · crackedNR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Nacelle/Pylon, Bulkhead/FirewallSDR UIEA200500065Pylon · crackedLT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Nacelle/Pylon, Plate/SkinSDR UIEA200500066Precooler · crackedPYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Pneumatic SystemSDR UIEA200500067Pressure Panel · corrodedBS 1408, LBL 78 WHEEL WELL PRESSURE DECK CORRODED AT FASTENERS LOCATIONS. PRESSURE DECK REPAIRED IAW MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, BulkheadSDR UIEA200500068Frame · crackedNOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, FrameSDR UIEA200500069Skin · crackedNR 1 PYLON LT ACCESS DOOR 452BL CUT OUT LOWER EDGE CRACKED. REPAIRED ACCOMPLISHED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, Plate/SkinSDR UIEA200500070Pan · crackedLT SIDE CANTED BULKHEAD AT BS 1245, LBL 60 CLOSURE PAN FOR AILERON CONTROL CABLE FEED THROUGH TO PRESSURE DECK FOUND WITH (2) CRACKED LINES. CLOSURE PAN REPAIRED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Miscellaneous StructureSDR UIEA200500056Control System · intermittentAFTER ROLLING OUT 360 DEGREES, VOR COURSE INBOUND, ALL NAV INDICATIONS, OK. AFTER DESCENDING TO FL 10.0 JUST PRIOR TO CROSSING THE VOR SELECTED ILS FREQ ON CAPT AND FO MCP, BOTH HIS SELECTOR SWITCHES WERE SET TO ILS AND NAV MODE ON ILS. CPT HAD COURSE AND G/Apr 25, 2005 · N523MC · Boeing 7472D7B · Landing and Taxi AidsSDR UIEA200500057Computer · inoperativeAUTOPILOT WILL NOT ENGAGE. AUTOPILOT PUT AIRPLANE IN A 45 DEGREE BANK LT AND RT. DISENGAGED AUTOPILOT, STABILIZED AIRCRAFT AND RE-ENGAGED AUTOPILOT, AIRCRAFT STARTED ROLLING AGAIN. THE AIRCRAFT DIVERTED. RE-RACKED THE AUTOPILOT ROLL COMPUTER IAW MM, AUTOApr 24, 2005 · N537MC · Boeing 747271C · Autopilot SystemSDR UIEA200500055Gearbox · seizedDURING CRUISE ENGINE NR 2 FUEL FLOW BEGAN FLUCTUATING FOR 30 SECONDS, THEN THE ENGINE SHUTDOWN WITH THE FOLLOWING INDICATIONS. N1=26.1 PERCENT, EGT 0.0, N2 0.0, OIL PRESSURE 0.0, OIL QUANTITY 3.7 GALLONS, AND FUEL FLOW WAS 1.095. ENGINE WAS WINDMILLING 3 HOUApr 22, 2005 · N505MC · Boeing 7472D3B · Turbine Engine Reduction GearSDR P5CA0501337Clamp · looseON TAKEOFF GROUND ROLL & SETTING TAKEOFF THRUST AT 105.4 DEGREES. SET ROLLING APPROXIMATELY 90 KNOTS. NR 2 ENGINE FIRE LIGHT CAME ON, ABORTED TAKEOFF WITH THROTTLES BACK AT IDLE & SHUT DOWN NR 2 ENGINE. BOTH A & B LOOPS READING 8 UNITS. BRAKE TEMPS ALL GREApr 17, 2005 · N508MC · Boeing 747230B · Pneumatic Distribution SystemSDR P5CA0501336Shutoff Valve · failedDURING CLIMBOUT, NR 1 ENGINE NACELLE LOOPS A & B WENT INTO RED, SET WARNING BELLS OFF. ENGINE SHUTDOWN. OIL PRESSURE 45 PSI. REPLACED NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE PER MM 36-11-05. LEAK CHECK OIL, OPS CHECK NORMAL ON HIGH POWER RUN UP PER MM 71-0Apr 14, 2005 · N508MC · Boeing 747230B · Pneumatic SystemSDR P5CA0501341Regulator Valve · malfunctionedDURING CLIMBOUT NR 1 ENGINE NACELLE LOOPS A & B WENT INTO THE RED - SET BELL OFF - ENGINE SHUT DOWN OIL PRESSURE 45 PSI. REPLACED ENGINE PRESSURE REGULATING VALVE, LEAK CHECK OK. OPS CHECKED OK DURING ENGINE HIGH POWER ASSURANCE RUN, MM 36-11-19 & MM 36-11-0Apr 14, 2005 · N508MC · Boeing 747230B · Pneumatic Distribution SystemSDR UIEA200500049Panel · crackedD-CHECK, DURING SCHEDULED INSPECTION, CRACKS WERE FOUND AT THE LOWER CORNERS OF STA 400 BULKHEAD WEB PRESSURE PANEL CUTOUT. ANOTHER CRACK WAS FOUND ON THE LOWER IB SIDE OF THE PRESSURE PANEL ASSY. THE CRACKS ON THE STA 400 WERE TRIMMED OUT. REPAIRED DOUBLERApr 6, 2005 · N537MC · Boeing 747271C · Fuselage Main, BulkheadSDR UIEA200500048Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION, CRACK DAMAGE WAS FOUND IN THE SKIN ASSY AND THE ADJACENT NR 3 STIFFENER AT PRE-COOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STA 248 ON THE RT SIDE. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. Apr 5, 2005 · N537MC · Boeing 747271C · Nacelle/Pylon, Plate/SkinSDR UIEA200500046Drain Mast · damagedA FIRM LANDING ON TOUCH DOWN, ON WALK AROUND, AFTER PARKING, NOTICED NR 3 ENGINE IAW MM. NO FURTHER DAMAGE NOTED. ALSO ALIGNMENT MARKS ON STRUT DOORS ARE ALIGNED AND NO DAMAGE TO CANOES OR TAIL SECTION OF AIRCRAFT FOUND. REPLACEMENT COWLS OR SLEEVES IS NOT Apr 4, 2005 · N506MC · Boeing 7472D3B · Turbine Engine Accessory DriveSDR UIEA200500047Relay · failedAFTER TAKE OFF, LEADING EDGE FLAPS NR 1 AND NR 3 WOULD NOT RETRACT. PRIMARY LEADING EDGE C/B OPEN. REPLACED R1102 RELAY IAW WDM 27-81-01. INSPECTED PDU`S DAMAGE, NONE FOUND. CLEANED ALL CONNECTORS AND RESEATED C/B. OPS CHECK CARRIED OUT SEVERAL TIMES IAW Apr 4, 2005 · N809MC · Boeing 747228F · Leading Edge Slat Control SystemSDR UIEA200500045Structure · crackedLOUD AIR LEAK FROM AROUND DOOR ON MAIN CARGO DECK. AREA BY PALLET POSITION LR-MR. AFT OBSERVATION WINDOW DOOR. REMOVED AND INSTALLED NR 4 MAIN ENTRY DOOR IAW AMM. LEAK CHECK IAW AMM. NO LEAK NOTED. CABIN PRESSURIZATION LEAKAGE TEST ACCOMPLISHED IAW MM. Mar 31, 2005 · N522MC · Boeing 7472D7B · Passenger/Crew DoorsSDR UIEA200500043Beam · crackedD-CHECK, DURING SCHEDULED INSPECTION, CRACKS WERE FOUND AT THE NOSE GEAR WELL ON THE VERTICAL BEAM WEBS AT LHS BS 280L, 300L, 320L AND 320R. DAMAGED PORTION OF THE VERTICAL BEAM WEB WAS TRIMMED OUT AND A NEW SECTION OF THE WEB WAS SPLICED IN. NOTE: THESE RMar 30, 2005 · N537MC · Boeing 747271C · Fuselage Main, StructureSDR UIEA200500042Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION, NR 3 PYLON, A 2.25 INCH CRACK WAS FOUND AT THE TOP EDGE OF SKIN ASSY AT NAC WL147.8, JUST FORWARD OF THE NAC STA 286. CRACK IN THE SKIN ASSY WAS CONTAINED WITH A 1.0 INCH DIAMETER HOLE AT THE CRACK TIP. REPAIR AREA WAS NDMar 29, 2005 · N537MC · Boeing 747271C · Nacelle/Pylon, Plate/SkinSDR UIEA200500041Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION. THE STRUT SKIN ASSY EDGE ADJACENT TO THE PRECOOLER EXHAUST CUTOUT WAS FOUND CRACKED. SKIN ASSY INSPECTION CONFIRMED THAT CRACKS TERMINATED IN EXISTING FASTENER HOLES. NR3 STIFFENER WAS REINFORCED WITH A STEEL LOWER REPAIMar 28, 2005 · N537MC · Boeing 747271C · Nacelle/Pylon, Plate/SkinSDR P5CA0501319Actuator · inoperativeDURING ENGINE START NR 3 ENGINE WOULD NOT LIGHT OFF. TROUBLESHOT, FOUND FUEL CONDITION ACTUATOR INOP. REMOVED & REPLACED CONDITION ACTUATOR PER MM 76-11-00. OPS NORMAL.Feb 9, 2005 · N509MC · Boeing 747230B · Fuel Controlling SystemSDR UIEA200500006Control Panel · failedAIRCRAFT DIVERTED DUE TO (ILS LOC AND GS NOT RECEIVABLE) ON BOTH CAPTAIN AND FO HSI, ALL FLAGS VISIBLE ON BOTH SIDES INDICATING COMPLETE FAILURE OF THE ILS NAV CONTROL PANEL. REPLACED ILS CONTROL PANEL IAW MM 34-31-01 PERFORMED OPS CHECK ON ILS SYSTEM OK IAW Feb 3, 2005 · N526MC · Boeing 7472D7B · Landing and Taxi AidsSDR P5CAO501312Engine · stalledDURING CRUISE AT FL 310, NR 3 ENGINE COMPRESSOR STALLED, EGT WENT TO 500 DEGREES, N1 50 PERCENT, N2 40 PERCENT. PERFORMED RESTART THE ENGINE WOULD NOT START PAST 30 PERCENT N1, 40 PERCENT N2, WITH EGT AT 625 DEGREES & F/F AT 400 PPH. THROTTLE MOVEMENT HAD NOFeb 1, 2005 · N508MC · Boeing 747230B · Engine (Turbine/Turboprop)SDR UIEA200500005Pump · leakingNR 1 HYDRAULIC CONTENTS RAPIDLY DEPLETED DURING FLIGHT. APPROPRIATE DRILLS CARRIED OUT. REMOVED AND REPLACED NR 1 ENGINE EDP IAW MM 29-11-05. NO EVIDENCE OF LEAKS AFTERWARDS. SERVICED NR 1 HYDRAULIC SYSTEM TO FULL. INSPECTED PRESS AND CASE DRAIN FILTERS. Jan 27, 2005 · N512MC · Boeing 747230B · Hydraulic Pump (Electric/Engine), MainSDR UIEA200500004Slide · failedUPPER DECK EMERGENCY ESCAPE SLIDE DID NOT PROPERLY DEPLOY WHEN ACTIVATED. (EA15200503933)Jan 26, 2005 · N808MC · Boeing 747212B · Escape SlideSDR UIEA200400209Rheostat · burnedHOT SMELL (ELECTRICAL) DETECTED IN CRUSE. C/B PILOT PANEL ENDER FLIGHT DECK LIGHTS WAS PULLED ON P6 PANEL. SMELL STOPPED, SHORTLY AFTER. PANEL BELOW CAPTAIN CUP HOLDER FELT HOT. ON T/S FOUND T77 DIMMER BURNED. REMOVED AND REPLACED DIMMER. OPS CHECK NORMADec 29, 2004 · N505MC · Boeing 7472D3B · Flight Compartment LightingSDR UIEA200400205Fairing · missingON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED REPAIR WORK TO BE DONE PRIOR TO FURTHER FLIGHT. FABRICATED A TIME LIMITED REPLACEMENT FAIRING FROM 0.040 INCH THICK 2024-T3 CLAD SHEET. PERDec 27, 2004 · N536MC · Boeing 747228F · Horizontal Stabilizer, Plate/Skin
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