Boeing 747-47UF

Service difficulty reports · 3,116

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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 aircraft_model_key = '74747UF'
  ORDER BY difficulty_date DESC"

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SDR UIEA201000191Nozzle · dentedDURING MX WALKAROUND, FOUND A DENT ON THE EXHAUST NOZZLE OUTER SLEEVE AT APPROX THE 6:00 POSITION ON THE NR1 ENGINE. THE DENT IS APPROX 2" LONG AND 0.05 INCHES WIDE AND IS APPROX 42 INCHES FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS.Mar 23, 2010 · N409MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR UIEA201000040Tension Tie · crackedLEFT BS 1140 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1140 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 2.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000039Tension Tie · crackedRIGHT BS 1160 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1160 TENSION TIE HOLES OVERSIZED REPAIRED AS PER EO4453A197 AND SB 747-53A2507 REV 1.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000038Tension Tie · crackedRIGHT BS 1160 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT ANGLE CLIP. BS 1160 TENSION TIE ANGLE CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000037Tension Tie · crackedLEFT BS 1180 TENSION TIE AREA 2 FASTENER HOLES CRACKED AT FRAME WEB. BS 1180 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 4.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000036Tension Tie · crackedLEFT BS 1220 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FRAME. BS 1220 ENTIRE FRAME REPLACED FROM PRODUCTION SPLICE STR 4 TO STR 11.5 PRODUCTION SPLICE PER EO 4453A216 PART 7 POINT 6.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000035Tension Tie · crackedLEFT BS 1200 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-11 FIG 1 AND EO 4453A216.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000034Tension Tie · crackedRIGHT BS 1140 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-12-2R AND EO 4453A216.Mar 23, 2010 · N429MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000031Tire · separatedON WALKAROUND FOUND NR 4 TIRE RECAP SEPARATED FROM TIRE. PERFORMED AIRCRAFT INSPECTION PER CHAP 5-51-34-201. REPLACED TIRE PER AMM 34-45-01. AIRCRAFT INSPECTION REVEALED SEVERAL DENTS TO LEFT I/B LOWER SURFACES OF FORE, MID AND AFT FLAPS AND TRAILING EDGE PMar 19, 2010 · N499MC · Boeing 74747UF · TireSDR UIEA201000190Fastener · missingA RIVET WAS MISSING AND WAS NOTED ON THE LT WING L/E RIB, OTBD LOF LANDING LIGHT. PERFORMED A TIME LIMITED REPAIR BY INSTALLING A BLIND FASTENER IN LIEU OF A SOLID RIVET. SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AFTER PART 1 AND PERMANENT REPAIR PRIOR TO ORMar 16, 2010 · N409MC · Boeing 74747UF · Wing, Rib/BulkheadSDR UIEA201000025Support · crackedLT WING LOWER SURFACE ADJACENT TO NR 5 SPOILER OTBD AREA UPPER SURFACE FIXED PANEL SUPPORT STRUCTURE CRACKED. UPPER SURFACE SUPPORT FITTING REPLACED IAW SRM 51-10-02, 51-40-02 AND AMM 57-22-01.Mar 1, 2010 · N499MC · Boeing 74747UF · Wing Miscellaneous StructureSDR UIEA201000024Fitting · crackedLT WING INBD MIS FLAP TRACK CARRIAGE FITTING SAFE LINK ATTACH BOLT BORE HOLE CRACKED. LT WING INBD MID FLAP REPLACED IAW 27-51-01.Mar 1, 2010 · N499MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000023Angle · crackedRT OTBD ELEVATOR L/E INBD BALANCE WEIGHT BOX ANGLE CRACKED. ELEVATOR STA 227.65 SUPPORT WEB AND WEB ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW 51-40-02.Mar 1, 2010 · N499MC · Boeing 74747UF · Elevator Miscellaneous StructureSDR UIEA201000022Rib · crackedLT INBD ELEVATOR L/E MOST INBD RIB ANGLE CRACKED. INBD RIB UPPER MOST UPPER RIB ANGLE BRACKET REPLACED IAW SRM 51-00-02 AND 51-40-02.Mar 1, 2010 · N499MC · Boeing 74747UF · Elevator, Spar/RibSDR UIEA201000017Tire · separatedTIRE TREAD SEPARATED FROM NR 8 POSITION ON T/O FROM SCL, DISCOVERED AFTER LANDING AT MIA. A/C INSPECTED, FOUND 5 LOWER AFT BODY PANELS WITH DENT DAMAGE. REPAIRED PANELS PER ATLAS EO 4453A335. REPLACED TIRES NR 7 AND NR 8 POSITION PER AMM 32.45.01.Feb 24, 2010 · N498MC · Boeing 74747UF · TireSDR UIEA201000159Access Panel · crackedCRACKS WERE FOUND IN THE NR 3 PYLON INBD ACCESS PANEL 472FL AS SHOWN IN FIGURE 1. NR 3 PYLON ACCESS PANEL 452FL CRACKED AREA REPAIRED IAW EO 4454A095.Feb 9, 2010 · N412MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA201000008Rib · crackedCRACKING WAS FOUND IN THE LT/RT HST LEADING EDGE RIBS BETWEEN LE STA 131.946 AND LE STA 527.190. REPAIRED THE 5EA CRACK AREA IAW EI NO T2010A55B-175 REV 00 AND T2010P55B-165 REV 00. CONDITION CHECK NORMAL.Jan 30, 2010 · N408MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA201000007Shim · migratedSHIM MIGRATION WAS FOUND BETWEEN RT LONGERON FITTING AND FUSELAGE SKIN AT STA 1241, RBL 128, WL 175. REPAIR IN IAW EI NR T2010A53B-137 REV 00. CHECK CONDITION NORMAL AND JOB COMPLETED. INITIAL AND REPEAT INSPECTION AT EVERY C-CHECK NOT TO EXCEED 24 MONTHS PJan 30, 2010 · N408MC · Boeing 74747UF · Fuselage Main, Longeron/StringerSDR UIEA201000006Skin · dentedDENT - SKIN UPPER SURFACE OF FWD CARGO BELOW SKIN STA. 695, S46R-S47R. REPAIRED THE DAMAGED AREA IAW 747-400F SRM 53-00-01 REPAIR 6 REV 53 REPEAT INSPECTION ON THE FOLLOWING METHOD EXTERNAL HFEC INTERVAL 6.000 FLIGHT CYCLES PER EO NR 4453A326. CONDITION CHECJan 30, 2010 · N408MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA201000005Frame · brokenFOUND FUSELAGE STRUCTURE FRAME BROKEN AT STA 1800 S-10R. REPAIRED THE FRAME BROKEN AREA IAW EI NR T2010A53B-166. FOLLOWED UP INSPECTION PRIOR TO 25,000 TOTAL FLIGHT CYCLES PER EO NR 4453A327.Jan 30, 2010 · N408MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA201000004Skin · wornPART 1-4 FOUND DAMAGE WEAR ON LT AND RT SIDE VERTICAL STAB SEAL INTERFACE SKIN AREA BETWEEN BS 2360-2390 AND BS 2521-2598 AND BS 2280- 2360. BLEND OUT DAMAGE AREA IAW SRM 53-00-01 REV 53 RESIDUAL MATERIAL THICKNESS WITHIN ALLOWABLE DAMAGE, APPLY PROTECTIVE COJan 30, 2010 · N408MC · Boeing 74747UF · Vertical Stabilizer, Plate/SkinSDR UIEA201000003Sleeve · dentedA DENT WAS FOUND ON THE NR 4 ENG LT EXHAUST SLEEVE, AT THE 9 O'CLOCK LOCATION NEAR NAC STA 349-236. MANUFACTURER PROVIDED INSPECTION TIMELINE OF REF/D/AND PERFORM FPI INSPECTION PER BAC 5423 TO ENSURE NO CRACKS ARE PRESENT ON NOTED DENT. REPEAT INSPECTION EVJan 30, 2010 · N408MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR UIEA201000088Skin · delaminatedLT WING UPPER SURFACE OTBD, ALL OTBD AREA FOUND DELAMINATED. RT WING OTBD AIL UPPER SURFACE DELAMINATED AT SEVERAL LOCATION AS MARKED. LT WING UPPER SURFACE OTBD AILERON REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 507013-1. Jan 6, 2010 · N409MC · Boeing 74747UF · AileronsSDR UIEA201000090Skin · delaminatedRT WING OTBD AFT FLAP L/E MID AREA FOUND DELAMINATED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-07 FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU506866-1. EO 4457A224RA, 4457A225RA.Jan 5, 2010 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000095Skin · delaminatedRT WING T/E INBD FORE FLAP L/E FOUND DELAMINATION AS MARKED. RT WING - INBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504747-1. EO 4457A224RA, 4457A225RA.Jan 1, 2010 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000091Skin · dentedRT WING T/E OTBD AFT FLAP LWR SURFACE FOUND DENT AS MARKED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-10, REPAIR NR 4, FIG 201 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU505223. EO 4457A224RA, 4457A225RA.Jan 1, 2010 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000087Skin · delaminatedLT WING UPPER SURFACE OTBB AIL INBD AREA DELAMINATED AT SEVERAL LOCATIONS AS MARKED. RT WING - OTBD AILERON UPPER SURFACE REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NT: DJU 504200-1, EO 4457A224RA AND 4457A225RA.Jan 1, 2010 · N409MC · Boeing 74747UF · AileronsSDR UIEA201000086Floor Support · deformedBULK CARGO FLOOR PANEL SUPPORT DEFORMED AT RBL 38" STA 2100. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.Jan 1, 2010 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000085Floor Support · deformedBULK CARGO FLOOR PANEL SUPPORT DEFORMED AT RBL 38" AT STA 2080. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.Jan 1, 2010 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000084Floor Support · deformedBULK CARGO - FLOOR PANEL SUPPORT DEFORMED AT RBL 38" STA 2060. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.Jan 1, 2010 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000083Floor Support · deformedBULK CARGO - FLOOR PANEL SUPPORT DEFORMED AT RBL 7" STA 2020. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.Jan 1, 2010 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000094Skin · delaminatedRT WING INBD AFT FLAP LWR SURFACE 1 LOCATION FOUND DELAMINATED AS MARKED. RT WING - INBD AFT FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU504176-1. EO 4457A224RA , 4457A225RA.Dec 31, 2009 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000092Skin · delaminatedLT WING T/E OTBD FORE FLAP L/E FOUND DELAMINATION AT SEVERAL LOCATION AS MARKED. LT WING -OTBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503665-1. EO 4457A224RA, 4457A225RA.Dec 31, 2009 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000093Skin · delaminatedEO 4457A224RA, 4457A225RA: RT WING INBD MID FLAP UPPER SURFACE 2 LOCATION FOUND DELAMINATED AS MARKED. RT WING INBD MID FLAP LWR SURFACE OTBD AFT CORNER SCRATCH AS MARKED. RT WING - INBD MID FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTDec 31, 2009 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000096Flap Track · erodedNR 7 FIX FLAP TRACK FAIRING L/E AREA ERODED. NR 7 FIX FAIRING RESIN REPAIRED IAW SRM 51-70-06, PARA 5.0, EO 4457A224RA, 4457A225RA.Dec 31, 2009 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000089Aileron · delaminatedLEFT WING I/B AILERON O/B TRAILING EDGE CORNER FOUND DELAMINATION AS MARKED. LEFT WING - I/B AILERON REPAIRED AS PER SRM 51-70-06, FIG 9 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503673-1. EO 4457A224RA 4457A225RA.Dec 31, 2009 · N409MC · Boeing 74747UF · AileronsSDR UIEA201000082Skin · gougedRT WING LOWER SURFACE HAS 2 AREAS WITH GOUGES ON SKIN EDGES STN 1551 & STN 1558. BOTH WITHIN SRM LIMITS. SRM 57-20-01-1A-1 DETAIL 1. GOUGE MARK SMOOTHED OUT IAW SRM 51-10-02. EO 4457A218, REV B.Dec 27, 2009 · N409MC · Boeing 74747UF · Wing, Plate/SkinSDR 2010FA0000019Valve · leakingDURING FUELING NOTED FUEL COMING FROM RT WING JETTISON TUBE. JETTISON VALVE LEAKING. FUELING STOPPED AND JETTISON NOZZLE CYCLED IAW MM TASK 28-31-00-715-068. LEAK STOPPED Dec 18, 2009 · N492MC · Boeing 74747UF · Fuel Dump SystemSDR P5CA2009110501609Depressor · damagedFOUND LWR AFT CARGO DOOR REAR SIDE UPPER DEPRESSOR SEAL DAMAGED 1/2 X 1/2. REMOVED/SMOOTH DAMAGED AREA AND APPLIED 2 LAYERS OF SPEED TAPE APPLIED IAW PART 1 OF EO 4453A303 IN ADDITION TO FAA 8110-3 ISSUED 5 NOV 2009. VISUAL INSP IS REQUIRED AT EVERY FLIGHT LNov 5, 2009 · N416MC · Boeing 74747UF · Cargo/Baggage DoorsSDR UIEA200900061AStructure · damagedLT THRUST REVERSER CORE COWL ON ENG 2 WERE DAMAGED DUE TO WRONG COWL CLOSING SEQUENCE. COWL REPAIRED IAW EO 4478A100 AND 4471A044.Nov 4, 2009 · N418MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2009110300004Structure · damagedEO 4471A044, DURING THE A-CHECK INSP ON 11/3/2009, MX FOUND DAMAGE TO THE NR 2 ENG LT CORE COWL UPPER FWD CORNER. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND Nov 3, 2009 · N418MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR UIEA2009102200002Floorboard · damagedMX FOUND DAMAGE/DELAMINATION TO THE MAIN DECK FLOORBOARD BS395 AND BS410 RBL 75 & RBL 78 (REF FIGURE 1)(INITIATE REPETITIVE DVIS AT EVERY A CHECK AND PERFORM PERMANENT REPAIR PRIOR TO OR AT THE NEXT C-CHECK AFTER PART 1 IAW THE SRM 53-00-50, REPAIR 1.)Oct 22, 2009 · N418MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA200900057Fire Detector · false activationAIR TURN BACK. EICAS MESSAGE AFT MAIN DECK FIRE . UPON INSPECTION NO IDICATION OF FIRE SUSPECT VISABLE MOISTURE . INSPECTED CABIN AREA FOR POSSIBLE FIRE OR SMOKE DAMAGE AND FOUND NONE PRESENT. SUSPECT HEAVY CONDISATION OF RAIN WATER ON MAIN DECK CARGO AREA.Oct 8, 2009 · N497MC · Boeing 74747UF · Fire DetectionSDR UIEA201000158Fairing · damagedTRAILING EDGE I/B MID FLAP LEADING EDGE FAIRING UPPER MID AREA FOUND DAMAGED (DIMENSION 15 X 4.5 INCHES). LT WING - TRAILING EDGE I/B MID FLAP LEADING EDGE FAIRING UPPER MID AREA COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5.0 FIG 6.Oct 4, 2009 · N408MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200900062Structure · damagedLT WING INBD MID FLAP L/E FOUND DAMAGED AT MOST INBD AREA. PERMANENT REPAIR PERFORMED IN ACFT WITH THE SRM 41-70-07 AND SRM 57-53-01 FIG 201, TABLE 1.Sep 22, 2009 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000178Conduit · damagedFLEXIBLE ELECTRICAL CONDUIT AT THE LT WING GEAR DAMAGED. "PERFORMED A TIME LIMITED REPAIR IAW THE SWPM 20-10-91".Sep 2, 2009 · N499MC · Boeing 74747UF · Electrical Power SystemSDR UIEA200900053Unknown · unknownFLYING WITH AUTOPILOT OFF, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, ACFT ROLLED HARD LEFT, INTERMITTENT. WITH AUTOPILOT ENGAGED, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, YOKE MOVES RIGHT APPROX 2 UNITS TO MAINT WING LEVEL, ALSO INTERMITTENT. ACCOMPLISHED VISUAL ISep 2, 2009 · N496MC · Boeing 74747UF · Flight Control SystemSDR UIEA201000163Insulation · damagedUPON REMOVAL OF THE NR 2 ENGINE FOR REPLACEMENT PURPOSES THE NR 2 STRUT LOWER WEB INSULATION BLANKET ("HEAT SHIELD") WAS FOUND DAMAGED WITH MISSING MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR BY INSTALLING A REPAIR DOUBLER MADE FROM SS 301Aug 15, 2009 · N418MC · Boeing 74747UF · Nacelle/Pylon Miscellaneous StructureSDR UIEA200900050Skin · crackedRT NR3 CORE COWL UPPER AFT AREA FAIRING OUTER SKIN AT NAC STATION 296.25 TO 304.5 HAS A 8.250 INCH CRACK. TIME LIMITED REPAIR WAS ACCOMPLISHED IAW SRM 51-40-02-06-0 AND EO 4471A043. TO INSPECT OR ACCOMPLISH PERMANENT REPAIR NEXT A-CHECK.Aug 14, 2009 · N496MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA200900049Seat Track · crackedMAIN DECK SIDE DOOR AREA AT LT, FS 1806.95 TO 1809.95, LBL99 SEAT TRACK CROWN LUG HAS A 3.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52-2R-6 REPAIR 6 AND EO 4453A271.Aug 14, 2009 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
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