Boeing 747-47UF

Service difficulty reports · 3,116

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 aircraft_model_key = '74747UF'
  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 UIEA2022042800413None · noneCORROSION DAMAGES ON RH HST CENTER SECTION UPPER SKIN TOP SURFACE BETWEEN STAB STA 143.6 AND 172.4, STRINGER 3 TO 12(<P>1) REMOVE THE AFFECTED FASTENERS IAW SRM 51.40.02 REV 94 2) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94 3) PFM NOT INSP REFER TO JOBApr 30, 2022 · N477MC · Boeing 74747UF · Horizontal Stabilizer, Tab StructureSDR UIEA2022042800412Bearing · noneFND L1 DR GUIDE ARM ROD END BEARING DAMAGE(<P>1) IAW AMM TASK 52-11-04-004-001 REV 103 AND AMM TASK 52-11-04-404-006 REV 103 REPLACE L1 DOOR GUIDE ARM ROD END BEARING 2_ COND CHK NML</P>)Apr 30, 2022 · N477MC · Boeing 74747UF · DoorsSDR UIEA2022042800414None · noneCORROSION DAMAGE ON LH HST CENTER SECTION UPPER SKIN TOP SURFACE BETWEEN STAB STA 165.64 AND 172.4, STRINGER 3(<P>1) REMOVER THE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94. 3) PFM NDT INSP REFER TO JOB CAApr 30, 2022 · N477MC · Boeing 74747UF · Horizontal Stabilizer, Plate/SkinSDR UIEA2022040700265Seat Track · crackedF/O'S AFT INBOARD SEAT TRACK FOUND CRACKED AT FORWARD END.(<P>F/O'S SEAT REMOVED AND INSTALLED IAW AMM 25-11-01-404-031. SEAT TRACK REPLACED IAW AMM 25-11-01-824-127. SEAT OPERATIONAL TEST OK IAW AMM 25-11-00/201.</P>)Apr 7, 2022 · N499MC · Boeing 74747UF · Flight Compartment EquipmentSDR UIEA2022032600242Aoa · failedCREW REPORTED AUTOPILOT FAILURES, SINGLE IRU MODE, MULTIPLE ADC ISSUES, WHICH WERE CONFIRMED IN AHM.(<P ><SPAN>REPLACED LEFT AIR DATA COMPUTER. DURING OPS CHECK, LEFT ANGLE OF ATTACK SENSOR FAILED. REMOVED AND REPLACED LEFT ANGLE OF ATTACK SENSOR IAW AMM 34-12Mar 26, 2022 · N492MC · Boeing 74747UF · Outside Air Temperature Indicator/SensorSDR UIEA2022032400236Skid Shoe · corrodedCORROSION - MD CGO FUSELAGE SKIN AREA AT STA 1000 FWD S-16R TO S-17R(<P>ACCOMPLISHED <SPAN>EI # T2022A53M-636 REV 2. ATTACHED TO W/O 6828148. JOB COMPLETED.</SPAN></P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2022032300221Skin · corrodedCORROSION DAMAGES ON INNER SURFACE OF FUSELAGE SKIN DURING PERFORMING INSP PER SB 747-53A2878(<P>REPAIR DAMAGE AREA IAW EI NO. T2022A53M-636 REV 2. JOB COMPLETED</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2022032300222Web · crackedCRACK ON THE WEB OF STA 1480 BULKHEAD FRAME AT RBL 110 AND WL 150(<P>REMOVE FASTENERS IAW SRM 51-40-02 REV 94. PERFORM WEB REPAIR IAW EI # T2022A53M-716 REV 1. COND CHK NORMAL AND JOB COMPLETED. </P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2022032300223Web · crackedCRACK ON THE WEB OF STA 1480 BULKHEAD FRAME AT LBL 80 AND WL 120(<P>REPAIRED DAMAGED AREA IAW EI #T2022A53M-710 REV 1. CONDITION NORMAL AND JOB COMPLETED</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2022032300224Floorbeam · corrodedFOUND MD FLOOR BEAM CORROSION AT STA 1500, RBL 90(<P>ACCOMPLISHED EI #T2022A53M-734 REV 2 AND DWG #65B38075 SHEET 11. JOB COMPLETED</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, Floor BeamSDR UIEA2022032300225Floorbeam · corrodedREPAIR CORROSION ON FLOOR BEAM UPPER CAP AT STA 2240 BETWEEN LBL 67.01 & LBL 90(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND <SPAN>EI # T2022A53M-727 REV 1. INSTALLED FASTENERMar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, Floor BeamSDR UIEA2022032300226Skin · corrodedCORROSION - SKIN SURFACE LWR FUESLAGE INSIDE OF WING TO BODY FAIRING AT STA 840, S-44L & S-45L(<P>REM0VE DAMAGE AREA FASTENERS IAW SRM 51-40-02 REV 94. ACCOMPLISH <SPAN>EI # T2022A53M-746 REV 1 & DWG #142A3544 SHEET 7 REV B AND DWG #142A3784 SHEET 12 REV F. JOMar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2022032300227Seat Track · corrodedCORROSION ON MD SEAT TRACK BETWEEN STA 960 AND 980, LBL 11.33(<P>PERFORMED SEAT TRACK REPAIR IAW<SPAN>EI # T2022A53M-788 REV 1. INSTALL REPAIR IAW SRM 51-40-02 REV 94 AND DWG #65B38252 SHEET 14 REV . JOB COMPLETED & COND CHK NORMAL.</SPAN></P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2022032300228Seat Track · corrodedCORROSION DAMAGE ON THE SEAT TRACK OF MD BETWEEN STA 2060 & STA 2110.45 AT LBL 98.58.(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. ACCOMPLISHED <SPAN>EI # T2022A53M-704 REV 2 AND SRM 53-02-52-2R-6 DETAIL III REV 94. REINSTALLED FASTENERMar 21, 2022 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2022032300229Seat Track · crackedFOUND CRACK DAMAGE ON CROWN OF SEAR TRACK OF MD AT STA 2268, LBL 33.99(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-6 REPAIR 6 REV 94 & <SPAN>EI # T2022A53M-720 REV 1. INSTALLED FASTENERS IAW SRMar 21, 2022 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2022032300230None · noneMISSING RECORD OF EXISTING REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN STA 460 & STA 480, S-37R & S-39R(<P>PERFORMED FUSELAGE SKIN REPAUR DOUBLER IAW SRM 51-40-02 REV 94 & <SPAN>EI # T2022A53M-841 REV 1. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA2022032300231Strap · crackedCRACK DAMAGES ON THE STRAP AND INNER CORD OD STA 2231 FRAME AT S-16L & S-17L(<P>ACCOMPLISHED THE REPAIR IAW <SPAN>EI # T2022A53M-748 REV 1 AND SRM 53-60-15-2R-2 REPAIR 2 REV 94 AND DWG #65B0500 SH 19 REV D. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2022032400232Floorbeam · not reportedDEVIATION FOUND DURING PERFORMING SB 4453A087 PART 2 ON UPPER DECK FLOOR BEAM(<P>ACCOMPLISHED JOB IAW EI # T2022A53M-820 REV 1. JOB COMPLETED AND COND CHK NML.</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2022032400233Track · crackedCRACK - SUBSTITURE TRACK, MID CGO COMPT UNDER FLOOR AT B.S 995, LBL 75.92(<P>ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAIR 13 REV 94 & DWG # 65B38250 SH 9 REV B. & 65B16004 SH 4 REV A. COND CHK NML & JOB COMPLETED.</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2022032400234Track · corrodedFOUND MD SUBSTITUTE TRACK CORROSION AT STA 720 LBL 75.92(<P>ACCOMPLISHED THE REPAIR IAW SRM 53-00-52-2R-13 REPAIR 13 REV 94, DWG# 65B38250 SH 17 REV A & SH 9 REV B. COND CHK NML AND JOB COMPLETED.</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2022032400235Skin · dentedDENT - RH WING INBD #8 SPOILER UPPER SKIN(<P>CUT OUT THE DAMAGE MATERIAL AND CLEAN.MEASURE THE DAMAGE SIZE L=2.6", W=1.5", 2/3" FROM INBD EDGE, 2" FROM AFT EDGE. BOND REPAIR FILLER AND DOUBLER WITH FILM ADHESIVE. CURE AT 250 DEGREES F FOR 120 MINS. MAINTAIN MIMar 21, 2022 · N496MC · Boeing 74747UF · SpoilersSDR UIEA2022032400237Intercostal · corrodedFOUND BULK CGO SLOPING SIDEWALL STRUCTURE INTERCOSTAL CORROSION AT STA 1960 - 1980, S-38R(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALL NEW INTERCOSTAL IAW SRM 51-40-02 REV 94 AND DWG #65B04652 SH 2 & DWG #65B04153 SH 13 REV B & 146U3009 SH 4 REV D. Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2022032400238Angle · corrodedCORROSION - ANGLE, LOWER FUSELAGE INSIDE OF WING TO BODY FAIRING NO. 191DAL AT STA 960 TO STA 985, LBL 4(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALL NEW PART IAW SRM 51-40-02 REV 94 ANF DWG # 65B06976 SH 2 REV G. JOB COMPLETED AND COND CHK NML.</P>Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2022032400239Support · corrodedFOUND MD FLOOR STRUCTURE SUPPORT CORROSION AT STA 2376, RBL 16(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. INSTALLED NEW PART IAW SRM 51-40-02 REV 94 AND DWG #65B38754 SH 8 REV A. JOB COMPLETED AND COND CHK NML.</P>)Mar 21, 2022 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2022031100199Metering Valve · looseAFTER TAKEOFF HYD QTY LOW 1 EICAS(<P>INSPECTED AND FOUND NOSE STEERING METERING VALVE SUPPLY AND RETURN LINES LOOSE. RESECURED LINES. OPS CHECK LEAK CHECK GOOD PER AMM 20-11-18. SERVICED #1 HYD. SYSTEM PER AMM 12-12-01.</P>)Mar 10, 2022 · N475MC · Boeing 74747UF · Hydraulic System, MainSDR UIEA2022021500135Skin · cracked#3 ENG RH CORE COWL EXHAUST LWR RIVETS HOLES FOUND CRACKED(<P>#3 ENG RH CORE COWL PRECOOLER LOWER SKIN CRACK AREA EXTERNAL DOUBLER REPAIRED</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2022021600139Doubler · crackedM/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWEEN STR 21L AND STR 22L FOUND CRACKED(<P>M/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWEEN STR 21L AND STR 22L CRACK AREA EXTERNAL DOUBLERS REPAIRED.</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022021700144Frame · chafed#1 ENG L/H CORE COWL INNER NO.4 FRAME MID AREA FOUND CHAFING DAMAGE(<P>#1 ENG LH CORE COWL INNER NO.4 FRAME MID CHAFING DAMAGE AREA EXTERNAL PATCH REPAIRED</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Engine Exhaust SystemSDR UIEA2022021700145Skin · dentedRHW #18 VC-FLAP BALLNOSE SKIN LWR MID AREA FOUND DENT(<P>RHW #18 VC-FLAP BALLNOSE SKIN LWR MID OUT OF LIMITS DENT AREA EXTERNAL DOUBLER REPAIRED</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022100151Battery · failedEMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5169 FAILED(<P>REPLACED POWER SUPPLY BATT M5169 IAW AMM 33-51-04 AND TEST PASS</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Lighting SystemSDR UIEA2022022100152Battery · failedEMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5170 FAILED(<P>REPLACED POWER SUPPLY BATT M5170 IAW AMM 33-51-04 AND TEST PASS</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Lighting SystemSDR UIEA2022022200153Flap · delaminatedRHW O/B MID FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200154Flap · delaminatedRHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200155Flap · delaminatedLHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200156Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200157Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Wing StructureSDR UIEA2022022200158Flap · delaminatedRHW O/B AFT FLAP AFT O/B CORNER FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5G</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200159Flap · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Wing StructureSDR UIEA2022022200160Flap · delaminatedRHW O/B FORE FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200161Flap · delaminatedLHW O/B AFT FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200162Flap · delaminatedRHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Flight Control SystemSDR UIEA2022022200163Rib · crackedRHW I/B MID FLAP O/B RIB AFT ANGLE (CLIP) FOUND CRACKED(<P>FABRICATE THE REPLACEMENT ANGLE (CLIP) FROM 70757651 BARD PLATE. AND REPLACED AND INSTALLED.</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Wing StructureSDR UIEA2022022300164Shear Tie · crackedSTA 1000 FRONT SPAR UPPER RBL 33.99" ATTACH SHEAR TIE FOUND CRACKED(<P>USING 69B14267U11 SHEAR TIP IN LIEU OF 69B14267U9 SHEAR TIE REPLACED AND INSTALLED</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Wing StructureSDR UIEA2022022300165Access Panel · elongated#2 PYLON VALVE ACCESS PNL #462EL 1EA BOLT HOLE ELONGATED(<P>#2 PYLON VALVE ACCESS PNL #462EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15404 REV.A</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Nacelle/Pylon StructureSDR UIEA2022022300166Access Panel · elongated#3 PYLON VALVE ACCESS PNL #472EL 2EA BOLT HOLES ELONGATED(<P>#3 PYLON VALVE ACCESS PNL #472EL 2EA ELONGATED BOLT HOLES AREA DOUBLER REPAIRED AS PER RI-54-50-15403 REV.A</P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Nacelle/Pylon StructureSDR UIEA2022022300167Access Panel · elongated#1 PYLON VALVE ACCESS PNL #452EL 1EA BOLT HOLE ELONGATED(<P>#1 PYLON VALVE ACCESS PNL #452EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15405 REV.A </P>)Mar 1, 2022 · N415MC · Boeing 74747UF · Nacelle/Pylon StructureSDR UIEA2022021400107None · noneREPAIR - CORROSION DAMAGES ON INNER SURFACED OF FUSELAGE SKIN DURING PERFORMING INSPECTION PER SB 747-53A2878(<P>ACCOMPLISHED THE EI NO T2022A53M-199 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 14, 2022 · N408MC · Boeing 74747UF · Fuselage, Wing Attach FittingsSDR UIEA2022021400108None · noneCRACK ON SIDE ANGLES OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300 AND STA 320, RBL 30, WL 190.(<P>ACCOMPLISHED EI NO T2022A53M-088, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022021400109None · noneCRACK ON SIDE ANGLES OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30, WL 190.(<P>ACCOMPLISHED EI NO T2022A53M-087 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2022021400110None · noneFOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 500 - STA 520, S-26L - S-28L.(<P>EXISTING REPAIR DOUBLER WAS COVERED BY EO NO 4453B133 REV 1 AND EI NO T2022A53M-351 REV 1. REFER RAM FORM N408MC-22-22. JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UF · Fuselage Structure (General)
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