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 UIEA2022052200497Skin · crackedL/H BLG I/B STRUT DOOR SKIN FOUND CRACK. SKIN CRACK AREA REPAIRED AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201 REV 94 DATE 20FEB 2022Jun 2, 2022 · N416MC · Boeing 74747UF · DoorsSDR UIEA2022052200498Attach Angle · crackedM/D LHS STA 960 S-7 FRAME FWD/ CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED AND P/N NO.65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052300499Beam · elongatedAFT CGO STA 1820-1840 MOST RH HORIZ TORQUE TUBE R/H SUPPORT BEARING ATTACHED BEAM FOUND HOLE ELONGATED. HOLE ELONGATED INTERCOSTAL LOCAL FABRICATED AS PER BOEING DWG: 65B06061 & RPL AND INSTALLED AS PER SRM 51-40-02Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052300500Panel · crackedLHW TE CAVITY LWR FIXED PANEL CHORD FOUND CRACKED AT WS 1470 CHORD LOCAL FABRICATED AS PER BOEING DWG : 65B08175 AND PART LIST AND CHORD INSTALLED AS PER SRM 51-40-02Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052300501Curtain · tornBULK CARGO STA 2160 CURTAIN FOUND LWR AREA TORN. PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-15628 REV.A</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Cargo CompartmentsSDR UIEA2022052300502Frame · chipped#3 ENG R/H CORE COWL NO.5 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED. FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG. 201 REV 94, DATE: 20 FEB 2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant SystemSDR UIEA2022052300503Cowling · gouged#3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant SystemSDR UIEA2022052300504Frame · chipped#4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant SystemSDR UIEA2022052300528Flap · chafedLHW O/B FORE FLAP T/E UPR SURFACE O/B AREA FOUND CHAFING AS MARKED (3" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB 20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400529Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (125" TO I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400530Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (22" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400531Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION (145" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400532Flap · chafedLHW O/B AFT FLAP T/E FOUND CHAFING (95" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400533Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (140" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400534Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (107" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400535Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (55" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400536Skin · delaminatedLHW I/B FORE FLAP AFTER WEDGE UPPER SURFACE O/B AREA FOUND DELAMINATION (26" TO O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052400537Skin · delaminatedRHW O/B T/E MID FLAP UPR SURFACE AT AFT AREA 135" FROM O/B EDGE FOUND DELAMINATED. PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052500540Attach Bolt · elongatedAFT CARGO STA 1820-1840 RBL 30" MOST R/H HORIZONTAL TORQUE TUBE L/H SUPPORT BEARING ATT BEAM FOUND BOLT HOLE ELONGATED. LOCAL FABRICATE INTERCOSTAL AS PER BOEING DWG 65B06201 & PART LIST AND DOUBLER AS PER BOEING DWG 69B02959 PL AND NEW PARTS INSTALLED AS PERJun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052500541Frame · chafedAPU COMPARTMENT STA 2685 L/H FRAME MID SECTION FOUND CHAFING. FRAME CHAFING AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94, DATE: 20 FEB 2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052500542Frame · chafedAPU COMPARTMENT STA 2690 L/H FRAME MID SECTION FOUND CHAFING, FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94 DATE 20 FEB 2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052500543Spoiler · dentedRHW #12 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 2 AND FIGURE - 203 REV 94 ,FEB 20/2022</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · SpoilersSDR UIEA2022052500544Spoiler · dentedLHW #4 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 AND FIGURE - 201 REV94 ,FEB20/2022Jun 2, 2022 · N416MC · Boeing 74747UF · SpoilersSDR UIEA2022052600546Bushing · elongated#3 PYLON TORQUE BOX INNER AREA NAC STA 298.93 BLEED AIR DUCT R/H SUPPORT ROD LWR DUCT SIDE ATTACHED BOLT HOLE FOUND ELONGATION LINE REAM 2EA AFFECTED BUSHING HOLES AND FABRICATE 2 EACH BUSHING AS PER HX RI-36-11-15646 REV A</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Nacelle/Pylon StructureSDR UIEA2022052600547Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 57.5 SHEAR TIE AS MARKED APPROX 13/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH AT O/B SIDE. CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV 1 PART5</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052600548Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 75.92 SHEAR TIE AS MARKED APPROX 1 3/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH TO O/B SIDE(<P>CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV. 1 PART 6</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052600549Skin Panel · installedFUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052600550Fitting · damagedFUSELAGE - LONGERON EXTENSION FITTING - BODY STATION 1480 TO BODY STATION 1540 - STRINGERS S-32 TO S-33 (EO4453A818 5& 6). L/R STA 1480 - STA 1540 LONGERON EXTENSION FITTINGS REPLACEMENT AS PER ATLAS AIR EO4453A818 PART 3 4 AND RI NO. RI-53-00-15644 REV.AJun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052700551Fastener · crackedEO 4453A821-1 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) (L/H FASTENERS & WASHERS DEVIATIONS; DOUBLER S.E.M AND R/H FASTENERS & WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOJun 2, 2022 · N416MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052900555Housing · crackedRHW I/B FORE FLAP TO MID FLAP MOST O/B LEVER HOUSING FOUND CRACK. LEVER HOUSING REPLACED AS PER SRM 51-10-01 AND NEW HOUSING INSTALLED AS PER SRM 51-40-02Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052900556Web · crackedRHW I/B FORE FLAP MOST O/B WBL 410.25 O/B RIB ASSY UPPER CHORD & WEB FOUND CRACKED(<P>LOCAL FABRICATE WEB AS PER RI NO.RI-57-00-15623 REV.A AND REPLACED UPPER CHORD AS PER SRM 51-10-02 AND NEW WEB AND UPPER CHORD INSTALLED AS PER SRM 51-40-02</P>)Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022052900557Structure · crackedREFER WO.790016 RI-57-00-15623 REV A HFEC OPEN HOLE INSPECTION FOUND R/H I/B FORE FLAP O/B RIB ASSY AT WBL 410.25 AT I/B WEB, I/B LOWER CHORD & O/B LOWER CHORD CRACKED. LOCAL FABRICATE I/B LOWER CHORD AND O/B LOWER CHORD AS PER BOEING DWG: 65B39038 AND PART Jun 2, 2022 · N416MC · Boeing 74747UF · Wing StructureSDR UIEA2022053000558Drive Assy · failedBOTH L & R WEATHER RADARS FAILED AT CRUISE. REMOVED AND REPLACED WEATHER RADAR DRIVE MOUNT ASSEMBLY.May 30, 2022 · N418MC · Boeing 74747UF · Doppler SystemSDR UIEA2022052400538Rod End Bearing · elongatedNO.4 ENG LH C-DUCT OPEN ACTUATOR ROD END BOLT HOLE FOUND ELONGATED. NO.4 ENG L/H C-DUCT REPLACED IAW 78-31-01May 25, 2022 · N418MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2022051600482Fitting · crackedFUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 RBL 33.99. FUSE - CENTER SECTION - STA 1000 RBL 33.99" FRONT SPAR SHEAR TIE LUG FTG P/N 69B14267U9 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024 May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022051600483Fitting · crackedFUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 LBL 57.5. FUSE - CENTER SECTION - STA 1000 LBL 57.5" FRONT SPAR SHEAR TIE LUG FTG P/N: 69B14267U7 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024 PMay 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022051800487Cargo Track · crackedAFT CARGO STA 1860 AND STA 1880 LBL 24" CARGO TRACK FOUND CRACKED. AFT CARGO STA 1830.45 TO STA 1890.45 LBL 24.75 CARGO TRACK REPAIRED IAW RI-53-00-15595 REV.AMay 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022051800488Skin · crackedEO 4453A516 PART 1 AND PART 2 - FUSE SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL INSPECTION FOUND LH SKIN CRACKED. FUSE - STA 400 L/H AND R/H SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND PART 4 AND RI-53-10-15613 REV.A<May 25, 2022 · N418MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022052400539Latch · elongatedAPU DOOR RH NO.5 LATCH CUTOUT FOUND ELONGATED. APU DOOR ASSY RH P/N: 65B02771-204 S/N: TLS28220 REPLACED AND INSTALLED IAW AMM 52-48-02May 25, 2022 · N418MC · Boeing 74747UF · Tail Cone DoorsSDR UIEA2022052600545Latch · elongatedAPU DOOR RH NO.5 LATCH CUTOUT FOUND ELONGATED. APU DOOR ASSY RH P/N: 65B02771-204 S/N TLS28220 REPLACED AND INSTALLED IAW AMM 52-48-02May 25, 2022 · N418MC · Boeing 74747UF · Tail Cone DoorsSDR UIEA2022051900492Strap · displacedFLAPPING AND RUSHING AIR SOUND COMING FROM UPPER DECK SERVICE DOOR AT 10,500 FT(<P>FOUND DOOR STRAP INHIBITING DOOR SEAL, REMOVED DOOR STRAP, DOOR CLOSED PROPERLY.</P>)May 19, 2022 · N415MC · Boeing 74747UF · Service DoorsSDR 9WGA2022050925801Actuator · lockedDISCREPANCY: EICAS GEAR DISAGREE UNABLE TO RETRACT LEFT BODY GEAR AFTER TAKEOFF. CORRECTIVE ACTION: REPLACED LH BODY GEAR RETRACT ACTUATOR, LEAK CHECKS GOOD. REF AMM 32-33-01-004-001/404-009.May 9, 2022 · N258SN · Boeing 74747UF · Landing Gear ActuatorSDR UIEA2022050300429Switch · fault messageBLEED 2 EICAS MESSAGE(<P>CMC # 36227 PER FIM TASK # 36-11/940. REMOVED AND REPLACED #2 ENG BLEED AIR OVERPRESSURE SWITCH PER AMM 36-21-03/401. THEN OPERATIONAL TEST WITH ENG RAN, OK PER AMM 71-00-00/501. NO MSG FOUND. A/C OK FOR SVC.<SPAN STYLE="WHITE-SPACE: PMay 3, 2022 · N477MC · Boeing 74747UF · Pneumatic Indicating SystemSDR UIEA2022042800405None · noneCHAFING -SKIN, L/H WING INBD ALLERON OUTBD UPPER SKIN AND TE END CAP(<P>1) PERFORM THE REPAIR IAW B747-400F SRM 57-60-01-ZR-1 REFER TO SRM 51-70-07-0G-0 REV 94 REFER TO THE JOB CARD ATTACHING SHEET FOR THE REPAIR PROCESS DETAILS 2) CONDITION CHECK IS SATISFACTApr 30, 2022 · N477MC · Boeing 74747UF · Wing StructureSDR UIEA2022042800406None · noneRH WING INBOARD AILERON, OUTBD TE WEDGE SKIN CHAFING WORN(<P>1) PERFORM RH WING INBD AILERON OUTB TE WEDGE SKIN REPAIR REFER TO J/C ATTACHING SHEET NO 0342653 2) CONDITION CHECK IS SATISFACTORY</P>)Apr 30, 2022 · N477MC · Boeing 74747UF · Wing StructureSDR UIEA2022042800407None · noneFOUND M/D SUBSTITUTE TRACK CRACK STA 980 RBL 75.92(<P>1) ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAI 13 REV 94 AND DWG NO 65B16004 SH4 REV A, 65B38250 SH 17 REV A, 65B 38250 SH 9 REV B. 2) JOB COMPLETED AND CONDITION CHECK NORMAL </P>)Apr 30, 2022 · N477MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022042800408None · noneFOUND M/D SUBSTITUTE TRACK CRACK STA 1600 AND 1640 AND STA 1492 LBL 75.92(<P>1) ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAIR 13 REV 94 AND DWG NO 144U0802 SH 3 REV B, 65B38251 SH 62 REV A, 65B38251 SH 75 REV, 65B38251 SH 32 REV. 2) JOB COMPLETED AND CApr 30, 2022 · N477MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022042800409None · noneFOUND M/D EMERGENCY LIGHT INOP(<P>IAW AMM 33-51-04-902-001-001 REV 104 REPLACED THE BATTERY PACK AND PERFORMED THE FUNCTIONAL TEST, THE RESULT WAS SATISFACTORY</P>)Apr 30, 2022 · N477MC · Boeing 74747UF · Lighting SystemSDR UIEA2022042800410None · noneFOUND THE EMERGENCY LIGHT BATTERY PACK (M5169) FUNCTIONAL FAIL(<P>1) IAW AMM 33-51-04-902-001-001 REV 103 REPLACED THE EMERGENCY LIGHT BATTERY PACK (M5169). 2) IAW AMM 33-51-04-903-001-001 REV 103 PERFORMED POWER SUPPLY TEST OF M5169, THE RESULT WAS SATISFACTOApr 30, 2022 · N477MC · Boeing 74747UF · Lighting SystemSDR UIEA2022042800411Bearing · noneDAMAGE - L1 DOOR AFT/ UPPER LATCH CAM & DOOR OPEN AFT/ LOWER TORQUE BEARING(<P>1) IAW AMM TASK 52-11-19-001-001 REV 103 AND 52-11-19-404-008 REV 103 REPLACE L1 DOOR FWD LOWER LATCH TORQUE TUBE BEARING. 2) IAW AMM 52-11-01-735-080 REV 103 RPL AND ADT L1 DOOR AFApr 30, 2022 · N477MC · Boeing 74747UF · Doors
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