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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2024072200721Skin · delaminatedRHW T/E I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024072200722Skin · delaminatedRHW T/E I/B MID FLAP FOUND DENT(<P>PERFORMED REPAIR AT DENT AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072200723Skin · delaminatedRHW T/E O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072200724Skin · delaminatedRHW T/E O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072200725Skin · delaminatedRHW T/E O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072300726Skin · delaminatedRHW T/E O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072300727Skin · delaminatedRHW T/E O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072300728Skin · delaminatedRHW T/E O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REAPIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072400737Fairing · damaged#2 PYLON UPPER CAVITY FWD L/E FAIRING SEVERAL SCREW HOLE FOUND ELONGATED(<P>#2 PYLON UPPER CAVITY L/E FAIRING FABRICATION AND REPLACEMENT IAW RI-57-31-17019 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024072400738Beam · crackedLHW L/E ILES #690 D BEAM WEB, UPPER CHORD, LOWER CHORD AND UPPER CHORD ATTACH STRAP FOUND CRACK(<P>LHW L/E ILES #690D BEAM WEB, UPPER CHORD, LOWER CHORD AND UPPER CHORD ATTACH STRAP REPAIRED IAW RI NO : RI-57-41-17003 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024072400744Structure · abnormalACCOMPLISH EO 4453A516 PART 3 AND PART 4 NOSE WHEEL WELL AFT CORNER SKIN PNL MOD - SB 747-53A2305 R2 AD 2010-26-07(<P>ACCOMPLISH EO 4453A516 PART 3 AND PART 4 NOSE WHEEL WELL AFT CORNER SKIN PNL MOD SB 747-53A2305 R2 AD 2010-06-07 AND REPAIRED IAW RI-53-18-170SDR UIEA2024072500745Support Bracket · damagedRH WING LDG BEAM MID AREA T/E UPPER SURFACE SUPPORT ROD BRACKET FOUND ELONGATED(<P>RH WING LDG BEAM MID AREA T/E UPPER SURFACE SUPPORT ROD BRACKET REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 AND 69B11994U2 FITTING ASSY FABRICATED AS PER DWG AND PLSDR UIEA2024072800757Actuator · leakingSUSPECTED FUEL LEAK ENGINE 3. SHUTDOWN ENGINE 3 AT FL340. ENGINE 3 SHOWED OIL PRESSURE 11 PSI AFTER SHUTDOWN.(<P>PERFORMED DVI FOR ENG 3 FOR FUEL LEAKS, NO DEFECT NOTED. RAN ENG, NO DEFECTS NOTED, FUEL FLOW IND NORMAL PER AMM 71-00-00. R/R #3 XFEED VALVE ACTUASDR UIEA2024072800758Lamp · inoperativeM/D - EMER LT L5735 NOT ILLUMINATE DURING OPS TEST(<P>M/D - EMER LT L5735 LAMPS REPLACED AND OPERATION TEST ' NORMAL ' IAW AMM 33-51-00, REV 110, 15 MAR 2024</P>)SDR UIEA2024070600585Elec Connector · dirtyBLEED 3 EICAS MESSAGE(<P>FOUND #2 WIRE ON HPSOV WAS READING 12 MEGA OHMS. REMOVED CANNON PLUG AND CLEANED, RESEATED CANNON PLUG AND FOUND RESISTANCE CHECK TO BE .2 MEGA OHMS WHICH IS NORMAL PER FIM 36-11 TASK 803. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061400520Stringer · cracked#3 PYLON - I/B LOWER STRINGER CRACK FOUND AT MOST AFT END AREA (APPROX NAC STA 374) AS MARKED(<P>3 PYLON - I/B LOWER STRINGER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 REV 101 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024061400521Structure · corrodedCENTER SECTION AFT FACE FOUND CORROSION ( NEAR LH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED. REMAIN 0.783" ORG 0.806" WIDTH 1.4, LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWASDR UIEA2024061400522Structure · corrodedCENTER SECTION AFT FACE CORROSION ( NEAR RH O/J PUMP BONDING AREA )(<P>CENTER SECTION AFT FACE CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 AND MEASURED : REMAIN 0.755" ORG 0806, WIDTH 1.4" LENGTH 2" WITHIN SRM 57-10-10-1A-2 ALLOWABLE DASDR UIEA2024061700526Structure · crackedBS 2598 LH LOWER INNER CHORD 1EA CRACK FOUND ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) AT 2 O'CLOCK POSITION WITH THROUGH THICKNESS CRACK(<P>BS 2598 LH LOWER INNER CHORD 1EA CRACK ON FASTENER HOLE 2ND LAYER ( COUNT FROM AFT ) REPAIRED IAW RI-53-00-16937 RESDR UIEA2024061800535Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800536Fairing · delaminatedLHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061800538Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024061800548Frame · unknownMAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 INSPECTION THE SCREW CANNOT BE INSTALLED AFTER MOVED DUE TO BRACKET BLOCKED(<P>MAIN DECK BS 2231 FRAME BETWEEN STRINGERS 15 TO 31 SCREW CANNOT BE INSTALLED. CASE REPAIRED IAW RI-53-60-16951 REV A AND SB 747-53SDR UIEA2024061800549Support Rod · damagedLH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) FOUND HOLE ELONGATED(<P>LH LDG SUPPORT BEAM O/B UPR SUPPORT ROD ( WS 522 AREA ) ROD FITTING FABRICATED IAW RI-57-22-16946 REV A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 101 DATE 20SDR UIEA2024061900556Skin · chafedLHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SEVERAL CHAFING MARKS(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16950 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024062000558Panel · corrodedM/D BELOW FSK STOWAGE PNL FOUND CORROSION(<P>M/D - BELOW FSK STOWAGE PNL REPAIR IAW FVCI EO - 24090-1, 2A, 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024062000557Tire · delaminated#8 TIRE DELAMINATION(<P>R/R MLG TIRE #8 PER AMM 32-45-01/401. SPACER INSTALLED.. REF AIPC 32-45-03-02. DUE TO #8 MLG TIRE TREAD LOSS, PERFORMED TIRE TREAD LOSS INSPECTION IAW AMM 5-51-34-202-001. FOUND MULTIPLE DAMAGES ON PANELS 193BLM, 193CL, 193DL & 193FL. RSDR UIEA2024061400519Fmc · failedLEFT FMC FAILURE(<P>R/R LEFT FMC IAW AMM 34-61-01 AND IPC 34-61-01-01B. OPS CHECK GOOD. TEST PASSED.</P>)SDR UIEA2024060800506Window · crackedWINDOW LEFT SIDE CREW REST CRACKED IN CRUISE. LOUD BANG AND WINDOW CRACKED. PRESSURE NORMAL(<P>RPLD CABIN WINDOW PER AMM 56-21-01. OPS CHK GOOD.</P>)SDR UIEA2024053000471Pitot Tube · faultedHEAT P/S F/O EICAS & STS MSG(<P>AIRCRAFT RETURNED TO ICN. REPLACED F/O UPPER RH PITOT PROBE PER AMM 34-11-01. OPS CHK GOOD</P>)SDR UIEA2024052800455Channel · crackedFOUND M/D R/H TENSION TIE AFT CHANNEL CRACK AT STA 800.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40389 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800456Channel · crackedFOUND M/D L/H TENSION TIE AFT CHANNEL CRACK AT STA 760.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40388 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800457Rib · crackedCRACK- LWR CHORD, UPPER CHORD AND WEB, R/H H.S.T TIP CLOSURE RIB, STAB BL 421.5.(<P>1. ACCOMPLISHED WORKSHEET #40372, SRM 55-10-09-2R-132 REV 100 AND EI T2024A55M-1231, REV 1 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800458Cargo Track · corrodedIND M/D CGO FLOOR STRUCTURE SEAT TRACK CORROSION AT STA 1980 RBL 11.33.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 100 2. REPAIRED DAMAGED AREA IAW W/S #40379 AND SRM 53-00-52-2R-12 REV 100 3. INSTALLED FASTENERS IAW SRM 51-40-02-4G-0 REV 100 AND DWG #SDR UIEA2024052800459Control Panel · abnormalFOUND ELT REMOTE PANEL FUNCTION ABNORMAL WHEN PFM OPERATIONAL TEST.(<P>IAW AMM 23-24-01/401 REV 110, REPLACED ELT CONTROL PANEL AND PERFORMED ELT CONTROL PANEL INSTALLATION TEST. THE RESULT WAS SATISFACTORY.</P>)SDR UIEA2024052800460Actuator · faultedFND L/H BLG ALTERNATE EXTENSION ELECTRICAL MOTOR CAN'T STOP WHEN PFM OPERATION TEST.(<P>1. IAW AMM 32-35-01-004-001, REV 110 AND AMM 32-35-01-404-007, REV 110 RDL L/H BLG ALTERNATE EXTENSION ELECTRICAL MOTOR. 2. IAW AMM 32-35-00-715-059 REV 110 PFM L/H BLG ALTSDR UIEA2024052200401Skin · delaminatedLHW I/B MID FLAP L/E FAIRING TO I/B EDGE 157" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200402Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING I/B EDGE110" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200403Skin · delaminatedLHW I/B FORE FLAP L/E FAIRING I/B EDGE 230" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200404Skin · delaminatedRHW I/B AFT FLAP LOWER T/E I/B EDGE 172" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200405Skin · delaminatedRHW O/B MID FLAP L/E FAIRING I/B EDGE14" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200406Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING 158" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200407Skin · delaminatedLHW I/B AFT FLAP UPPER T/E FROM I/B EDGE 122" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300408Skin · dentedRHW O/B AFT FLAP LOWER T/E 24" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300409Skin · dentedLHW O/B AFT FLAP LOWER T/E 36" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300410Structure · corrodedFX - LH AIRCON BAY STA 1220 - 1240 CENTER TANK LWR SURFACE O/B CHORD CRACK(<P>LH AIR COND BAY STA 1220-1240 CENTER TANK LWR SURFACE O/B CHORD REPAIR AS PER RI NO : RI-57-00-16879 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024052300411Fuel Tank · corrodedFX - LH AIRCON BAY STA 1240 CENTER TANK LOWER SURFACE CORR AT O/B AREA(<P>LH AIRCON BAY STA 1240 CENTER TANK LOWER SURFACE AT O/B AREA REPAIRED IAW RI NO : RI-57-10-16896 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300413Structure · corrodedCENTER SECTION AFT FACE FOUND CORROSION ( RH O/J PUMP BONDING AREA )(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300414Stiffener · crackedNO.3 PYLON - I/B STIFFENER FOUND CRACK AT NAC STA 300(<P>NO.3 PYLON - I/B STIFFENER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300431Access Panel · chafedLHW O/B T/E AFT FLAP O/B UPPER ACCESS PANEL 588IT EXTERIOR SURFACE SERVERAL AREA FOUND CHAFING(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16892 REV.A. NO FURTHER DEFECTS NOTED.</P>)
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