Boeing 747-47UF
Service difficulty reports · 3,115
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 UIEA2026042200235Floor Panel · puncturedBULK CARGO CTR FLOOR PANEL AT STA 2040 TO 2060 RH SIDE AREA WITH A PUNCTURE.(<P>FLOOR PNL PUNCTURE AREA REPAIRED AS PER RI-25-54-18173 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200236Skin · cracked2L CORE COWL EXTERIOR SURFACE T/E AT 12 O'CLOCK POSITION FOUND CRACKED(<P>SKIN CRACK AREA REPAIRED AS PER ATLAS AIR EA-1971A268 REV 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042400245Floorbeam · corrodedU/D LBL 10 TO 30 BS 500 FLOOR SUPPORT SPLICE PLATE FOUND CORROSION(<P>SPLICE PLATE FABRICATED AS PER BOEING DWG 141U5422 AND PL, AND NEW SPLICE PLATE HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SPLICE PLATE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS SDR UIEA2026042400246Web · crackedU/D LBL 10 TO LBL 35 BS 500 - BS 540 FLOOR SUPPORT SHEAR WEB CORROSION(<P>SHEAR WEB FABRICATED AS PER BOEING DWG 141U5421 AND PL, AND NEW SHEAR WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTEDSDR UIEA2026042600248Floor Support · crackedM/D BS 1860 - 1880 RHS O/B RBL 116" FLOOR SUPPORT L ANGLE FOUND CRACK.(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-25-21-18246 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026042700250Seat Track · crackedM/D - BS 1050-1070 RBL 77 SEAT TRACK RHS FLANGE FOUND CRACK(<P>SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-40-52-2R-3 REPAIR 3 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700252Skin · misrepairedFUSELAGE SKIN AT STA 2564-2575 STR 38R - STR 42R FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER RI-53-80-18257 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700253Stringer · noneFWD CARGO STA 790 - 810 STR 43L FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR REINSTALLED AS PER BOEING NON-CONFORMANCE NUMBER 430034F. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800254Duct · crackedNHR 3 ENG RH CORE COWL PRECOOLER OUTLET DUCT INNER GILL FOUND CRACKED.(<P>NEW PRECOOLER DUCT REPAIRED AND INSTALLED AS PER ATLAS AIR EA-1971A274 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800256Skin · corroded1EA CORROSION FOUND ON FUSELAGE LOWER SKIN INNER SURFACE AT STA 2185 STR 47R(<P>SKIN CORROSION AREA REPAIRED AS PER RI-53-60-18178 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800257Longeron · cracked1EA CRACK WAS FOUND ON RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA APPROX 1/4" IN LENGTH(<P>CRACK LONGERON EXTENSION FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800258Web · crackedFX RH BS 1480 WEB CRACK 5/8" ADJACENT LONGERON EXTENSION FITTING LOWER AREA(<P>WEB CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8 AND RI-53-20-1823 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800259Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 790 SUPPORT RIB FOUND CRACK(<P>L/E RIB CRACK AREA REPAIRED AS PER RI-57-41-18188 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800260Skin · cracked2EA CRACK WERE FOUND ON SKIN 2EA FASTENER RUNNING AFT ON RH FUSELAGE SKIN LAP BETWEEN BS 1438 AND BS 1460 STR 23R(<P>SKIN LAP CRACK AREA REPAIRED AS PER RI-53-40-18228 REV. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800261Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 766.45 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18205 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800262Door · abnormalAFT CARGO DOOR LOWER AFT CORNER FOUND EXISTING REPAIR(<P>DOOR SKIN REPAIRED AS PER RI-52-35-18240 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042900263Seat Track · crackedM/D STA 1375 RBL 11" LONGITUDINAL SEAT TRACK FOUND CRACKED(<P>SEAT TRACK CRACK AREA REPAIRED AS PER RI-53-40-18239 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900265Beam · damagedLHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD AREA FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER RI-57-41-18199 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900266Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900267Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900268Skin · unsecureLHW L/E SKIN NEAR #1 PYLON I/B AREA FOUND RIVETS LOOSE.(<P>L/E SKIN REPLACED AS PER SRM 51-10-02, AND NEW L/E SKIN HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW L/E SKIN INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026043000269Skin · crackedRHW L/E SKIN NEAR #4 PYLON O/B AREA FOUND CRACK(<P>L/E SKIN CRACK AREA REPAIRED AS PER RI-57-41-18141 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026043000270Beam · damagedRHW L/E D-BEAM NOSE SKIN AT #4 PYLON I/B FASTENER HOLES FOUND ELONGATED(<P>L/E SKIN REPAIRED AS PER RI-57-41-18210 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100278Panel · crackedM/D STA 2320 TO 2350 LH S/W LOWER DADO PANEL FOUND CRACK(<P>DADO PANEL CRACK AREA REPAIRED AS PER RI-53-60-18177 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100279Beam · crackedRHW L/E #17 VC FLAP CAVITY I/B D-BEAM O/B WEB FOUND CRACK ( #3 PYLON O/B )(<P>WEB REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100280Beam · crackedRHW L/E #17 V/C FLAP CAVITY I/B D-BEAM O/B UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100281Skin · damagedSKIN REPAIR FOR RHW LE D-BEAM FOR O/B UPPER CHORD REPAIR (3 PYLON OB)(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100282Panel · crackedCOCKPIT LHS FLOOR FLIGHT KIT STOWAGE BASE PNL FOUND CRACK(<P>BASE PNL CRACK AREA REPAIR AS PER RI-25-10-18213 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100283Skin · damagedL/E SKIN REPAIRED AT #4 PYLON I/B D-BEAM FOR UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100284Strap · corrodedRHW L/E D-BEAM LOWER STRAP AT ILES 665 FOUND HEAVY CORROSION(<P>CORROSION STRAP FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW STRAP REPLACED AS PER SRM 51-10-02, AND NEW STRAP HOLES TRANSFERRED AS PER SRM 51-40-05, AND STRAP INSTALLED AS PER SRM 51-40-SDR UIEA2026050100285Beam · crackedRHW L/E D-BEAM ILES 693 LOWER CHORD FOUND CRACK(<P>LWR CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100287Flap Track · corrodedLHW #4 FLAP TRACK FOUND SURFACE CORROSION AT BEARING PLATE CONTACT AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18196 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100288Flap Track · corrodedRHW #5 FLAP TRACK UPPER SURFACE CORROSION AT BEARING PLATE CONTACK AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18221 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400289Liner · tornBULK CARGO STA 2160 LINER FOUND TORN AT SEVERAL LOCATION(<P>CARRY OUT REPAIR AS PER RI-25-54-18224 REV C. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400290Panel · damagedM/D STA 1720 TO 1780 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18164 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400291Panel · damagedM/D STA 1620 TO 1720 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18163 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400292Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMSDR UIEA2026050400293Beam · crackedRHW L/E D-BEAM ILES 691 WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-57-41-18266 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050500296Stop Fitting · missingRHW L/E TO FRONT SPAR CAVITY ILES 756-766.45 UP STOP FITTING MISSING(<P>STOP FITTING FABRICATED AS PER RI-57-21-18259 REV A, AND NEW FITTING HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW FITTING INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050600304Panel · damagedM/D LHS BS 1920 - 2020 DADO PANEL FOUND DAMAGED(<P>DADO PANEL FWD CUTOUT GOUGE AND AFT CUTOUT DEFORM AREA REPAIRED AS PER RI-25-21-18165 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050800306Skin · not enteredAFT CARGO DOOR LOWER FWD CORNER FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER SRM 52-30-01-2R-2 REPAIR 2 FIG 201 DETAIL III. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051000308Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMSDR UIEA2026051700323Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700324Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700325Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700326Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700327Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700328Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700329Skin · delaminatedLHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700330Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)
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