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 UIEA2025032700394Skin · debondedLHW O/B FORE FLAP LOWER T/E O/B AREA FOUND DEBOND(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800395Skin · damagedRHW I/B MID FLAP O/B T/E SCREW HOLE FOUND ELONGATED(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. K. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800396Skin · delaminatedLH ELEVATOR UPPER I/B AREA FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800397Skin · chafedRHW I/B AILERON LOWER O/B AREA FOUND CHAFING(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-06 PAR 5. G. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800398Skin · puncturedLHW O/B FORE FLAP LOWER T/E MID AREA FOUND PUNCH(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800399Skin · delaminatedLHW O/B MID FLAP MOST O/B L/E FAIRING FOUND DELAMINATION(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800400Access Door · worn#2 PYLON I/B ACCESS DOOR #462ER FOUND 2EA SCREW HOLES WORN(<P>PANEL FABRICATED AS PER RI-54-50-17522 REV A . NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800401Skin · bulgedLHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800402Skin · bulgedLHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800403Skin · bulgedRHW I/B FORE FLAP LOWER SURFACE I/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800404Skin · bulgedRHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025032800405Skin · chafedRHW I/B AFT FLAP UPPER SURFACE MOST I/B PANEL FOUND CHAFING(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-53-17513 REV. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800406Skin · chafedRHW I/B AFT FLAP UPPER SURFACE MOST O/B PANEL FOUND CHAFING(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-53-17526 REV. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800407Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE I/B PANEL FOUND PUNCH(<P>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.201. NO FURTHER DEFECTS NOTED</P> / <P> </P>)SDR UIEA2025032800408Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE O/B PANEL FOUND SCRATCH(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800409Skin · scratchedLHW O/B AFT FLAP UPPER SURFACE MID PANEL FOUND SCRATCH(<P>PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800410Frame · crackedLH BS 2231 FRAME STR 16 ONE EACH FASTENER HOLE FOUND 2EA CRACK.(<P>STR 16 AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800411Frame · crackedLH BS 2231 FRAME STR 17 ONE EACH FASTENER HOLE FOUND CRACK(<P>STR 16L AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. (WORK DETAIL REFER WO.4545643 (5.738)). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800412Spar · crackedRHW I/B MID FLAP REAR SPAR WEB O/B EDGE FWD CRACK(<P>REAR SPAR WEB CRACK AREA REPAIRED AS PER RI-57-53-17514 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800413Floorbeam · puncturedAFT CARGO COMPT RH STA 1880 RBL 36 FLOOR BEAM SUPPORT WEB FOUND PUNCH(<P>WEB REPAIRED AS PER RI-53-65-17515 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800414Web · cracked1EA CRACK WAS FOUND ON WEB AROUND 2EA FASTENERS ON LHW MID SPAR WEB UPPER FROM WS 382 TO WS 441(<P>M/D SPAR WEB REPAIRED AS PER RI-57-20-17528 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032800415Web · cracked5EA CRACK WERE FOUND ON WEB AROUND 2EA FASTENERS ON RHW MID SPAR WEB UPPER FROM WS 382 TO WS 411(<P>MID SPAR WEB REPAIRED AS PER RI-57-20-17527 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025040100420Keelbeam · corrodedKEEL BEAM PNL 191KK AFT SUPPORT BEAM FOUND CORROSION(<P>KEEL BEAM PNL 191KK APT CORROSION SUPPORT BEAM REPLACED AS PER SRM 51-10-02. NEW SUPPORT BEAM HOLES TRANSFER AS PER SRM 51-40-05. NEW SUPPORT BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.<SDR UIEA2025041300456Indication Sys · false indicationNO FUEL QTY INDICATION ON MAIN TANK #2.(<P>CONFIRMED NO FUEL LEAKS, DRIP STICK READING ACCOMPLISHED, AND DDG 28-41-01 APPLIED. TRANSFER TO DMI 229181 PER MEL 28-41-01 CAT C DUE DATE 24APR25.</P>)SDR UIEA2025040900447Skin · crackedFUSELAGE - SEC46 SKIN EXTERIOR SURFACE STA1733-1735 S-41R AREA FOUND SKIN CRACKED WITH CORROSION.(<P>JOB ACCOMPLISHED AS PER EN #1023-25 REV.0. FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FORSDR UIEA2025040900451Floor Support · crackedMAIN DECK - MAIN DECK FLOOR PANEL SUPPORT MOST O/B AT ABOUT STA 1100-1140 FOUND 2 EA FASTENER HOLE CRACK.(<P>JOB ACCOMPLISHED AS PER EN #3003-25 REV.0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300134Seat Track · corrodedCORROSION AT SEAT TRACK/FLOOR BEAM AT LBL 11.33 AND STA 1635 AFT CARGO COMPARTMENT.<BR>(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;"><SPAN>REPAIRED SEAT TRACK/FLOOR BEAM FROM STA 1590 TO STA. 1650 PER B747 SRM 53-00-52-2R-12 REPAIR 12 AFT CARGO COMSDR UIEA2025021300135Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 AMD STA 1710 AFT CARGO COMPARTMENT.(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;">REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610 TO 1766.5 TO FACTORY SPLICE AND SECOND SECTION FROM 17SDR UIEA2025021300136Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR AT RBL 11.33 AND STA. 1675 AFT CARGO COMPARTMENT.(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;">REPLACED TWO EACH SECTIONS OF SEAT TRACKS FROM PREVIOUSLY REPAIR STA 1610 TO 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM SSDR UIEA2025021300137Seat Track · corrodedCORROSION ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770 TO 785 AT MAIN CARGO DECK.(<P>CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770-785 AT MAIN DECK CARGO DECK. NO CORROSION NOTED. PER BSOPM 20-30-80 PAR. 1.A. REV 153. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300138Seat Track · corrodedCORROSION ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 760-770 MAIN DECK CARGO.(<P>CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 760-770 AT MAIN CARGO DECK, NO CORROSION NOTED PAR. 1.A REV 153 SOPM 30-20-80. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300139Bushing · corrodedCORROSION FOUND AT INNER FACE ON LH BODY LANDING GEAR LOWER BUSHING (INNER BEARING CAP).<BR>(<P>REMOVED AND REPLACED BUSHING PER B747 SRM 53-40-90-2R-1 REPAIR 1 AND B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025021300140Bearing Cap · corrodedCORROSION FOUND ON FLANGE OF LH BODY LANDING GEAR BEARING CAP.(<P>REMOVED AND REPLACED LH BODY GEAR BEARING CAP PER B747 SRM 53-40-90-2R-1 REPAIR 1 FIG. 201. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025021300141Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 AT STA 1900.(<P>REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA 1610 TO STA 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM STA 1766-.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRMSDR UIEA2025021300142Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 STA. 1820.(<P>REPLACED 2 EACH SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610-1766.5 TO FACTORY SPLICE AND 2ND SECTON FROM STA. 1766.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRM 53-SDR UIEA2025021300143Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740.(<P>CLEANED AREA ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740 AT MAIN CARGO DECK. NO CORROSION NOTED PER SOPM 20-30-03 PAR. 1.A. REV 153 & SRM 53-60-52-001-1 FIG. 001 REV 102. NO FURTHER DEFECTSDR UIEA2025021300144Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1620,<BR>(<P>REPAIRED SEAT TRACK FROM STA 1590-1650 LBL PER B747-400 SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025021300145Bearing Cap · corrodedCORROSION FOUND ON FLANGE ON RH SIDE BODY LANDING GEAR BEARING FITTING CAP.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;">REMOVED AND REPLACED RH SIDE BODY LANDING GEAR BEARING FITTING CAP PER B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. SRM 53-40-90-2R-1SDR UIEA2025021800151Tire · failed#8 TIRE FAILURE ON TAKEOFF WITH NO FLIGHT DECK INDICATIONS. NORMAL FLAPS 30 LANDING WAS ACCOMPLISHED. REPLACED MLG TIRE #7 & #8 PER AMM 32-45-01 & IPC 32-45-01-02A. VERIFIED PN PER IPC 32-45-03-02. VERIFIED TIRE PRESSURE 210 PSI. RO INSTALLED. C/W INSPECTION SDR UIEA2025021600147Spoiler · damagedDURING LOADING, FOUND #5 SPOILER DAMAGED/PARTIALLY MISSING.(<P>R/R LEFT WING SPOILER #5 IAW B747 AMM 27-62-01/401. OPS CHECKED GOOD. NO DEFECTS NOTED. IPC REF: 27-11-01-01.</P>)SDR UIEA2025021000125Frame · damagedFOUND EXISTING REPAIR AT FRAME WEB UPR CHORD STA 560 RBL 13.5.(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 102. 2. ACCOMPLISHED EI T2025A53M-234 REV 0. 3. ACCOMPLISHED EI T2025A53M-234 REV 1. 4. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025021000124Bulkhead · misrepairedDEVIATION - PERFORMED STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER.(<P>1. PERFORM EI T2025A53M-192 REV 1 AND EI T2025A53M-140 REV 3. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025021000123Longeron Splice · damagedDURING PERFORMING EO 4453B761 PART 1-2 (SB747-53A2899), FOUND L/H S-11L LOWER LONGERON SPLICE FITTING AREA ONE HOLE OVERSIZE.(<P>1. ACCOMPLISHED EI T2025A53M-174 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025021000122Skin · debondedDISBOND-SKIN, R/H WING INBD AILERON, OUTBD AFT EDGE AREA.(<P>1. PERFORM REPAIR OF R/H WING INBD AILERON, PLEASE REF THE JOB CARD ATTACHING SHEETS FOR THE DETAILED REWORKING INFORMATION. 2. CONDITION CHECK IS SATISFACTORY. B747-400F SRM 57-60-01-0I-1 REV. 102, SDR UIEA2025021000130Feeder Cable · damagedFOUND #1 ENG POWER FEEDER CABLE (W274) DAMAGE NEAR REFUELING STATION.(<P>1. IAW WDM 24-21-11 REV 68 AND SWPM 20-30-13 & 20-10-12 REV 87 REPAIRED #1 ENG POWER FEEDER (W274) NEAR REFUELING STATION. 2. IAW AMM 24-11-00-70J-001 REV. 112 PERFORMED GENERATOR DRIVE SSDR UIEA2025021000129Hose · missingFOUND #3 ENG FIRE EXTINGUISHER HOSE MISSING.(<P>1. IAW AMM 70-50-00-912-034-J00 REV=112, INSTALLED THE NEW FIRE EXTINGUISHER HOSE ASSY WITH NEW PARTS ON #3 ENG. 2. REFER TO NRC:10591633 (508) PERFORM ENGINE FIRE EXTINGUISHING SYSTEM TEST. 3. CLOSED THIS JOB. NSDR UIEA2025021000128Fitting · damagedFND ENTRY DOOR FITTING DAMAGE AT L1 DOOR AFT LOWER SIDE.(<P>1. IAW AMM 20-51-01-912-008 REV=112 REPLACE L1 DOOR LATCH FITTING. 2. IAW AMM 52-11-01-735-080 REV=112 ADJUST L1 DOOR LATCH FITTING. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025021000127Web · misrepairedREPAIR - ONE EXISTING UNDOCUMENTED REPAIR ON LH CENTER WEB (P/N= 65B15071-122) OF KEEL BEAM AT STA 1460.(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV=102. 2. ACCOMPLISHED EI T2025A53M-199 REV=1. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025020200111Rib · crackedEMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB WEB P/N: 65B03520-60 FOUND CRACKED.(<P>EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB WEB P/N: 65B03520-60 REPAIRED IAW SRM 55-10-09-2R-13 REPAIR 13 DETAIL III. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025020200110Rib · crackedEMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB LOWER CHORD P/N: 65B03520-54 FOUND CRACKED.(<P>EMP HORIZONTAL STABILIZER TIP MOST O/B CLOSURE RIB LOWER CHORD P/N: 65B03520-54 REPAIRED IAW SRM 55-10-09-2R-13 REPAIR 13 DETAIL V. NO FURTHER DEFECTS NOTED</P>)
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