Boeing 747-46NF
Service difficulty reports · 1,079
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 = '74746NF' 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 = '74746NF' 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 UIEA2025070700848Seat Track · chafedM/D STA 646 TO STA 656 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:5" X W:0.3" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2025070700849Seat Track · chafedM/D STA 1890 TO 1893 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHAFING SMOOTHED OUT AREA MEASURED AS PER SRM 53-00-52-1A-1. WITHIN ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DESDR UIEA2025070700850Seat Track · chafedM/D STA 1968 TO STA 1970 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:4" X W:03" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NSDR UIEA2025070700851Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1370, STA 1390, STA 1410. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DSDR UIEA2025070700852Seat Track · corrodedM/D STA 780, 783 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L=5" X W=0.7", D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DSDR UIEA2025070700854Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1430, STA 1450 & STA 1470. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.009", WITHIN SRM 53-00-52-1A-1 ALLOWSDR UIEA2025070800855Seat Track · corrodedM/D STA 606-STA 624 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMTIS. NO FURTSDR UIEA2025070800856Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1611, STA 1631, STA 1772. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:3" X W:0.7" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWASDR UIEA2025070800857Seat Track · corrodedM/D STA 566-STA 592 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=15" X W=0.7" X D=0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURSDR UIEA2025070800858Seat Track · corrodedM/D STA 545-STA 559 LBL 11 SEAT TRACK CROWN CORRODED. CORRSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHSDR UIEA2025070800859Seat Track · corrodedM/D STA 872-STA 875 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTSDR UIEA2025070800860Seat Track · corrodedM/D STA 750-STA 783 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED" L=4" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTSDR UIEA2025070800861Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREA FOUND SCRATCHED AT LBL 11 STA 1430, STA 1450, STA 1470. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA MEASURED L:4' X W:0.7" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLSDR UIEA2025070800862Seat Track · corrodedM/D STA 730-STA 752 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTSDR UIEA2025070800863Seat Track · corrodedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11.33 STA 1853 AND STA 1913. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:6" X W:0.7" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DSDR UIEA2025070800864Seat Track · corrodedM/D STA 687-STA 694 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHSDR UIEA2025070800865Guide · corrodedM/D STA 1920 - 1980 SCD AFT SIDE GUIDE FOUND CORROSION. CORROSION AREA REMOVED AS PER CMM 25-55-06 AND REPROTECTED AS PER SRM 51-20-01 AND CORROSION REMOVED AREA MEASURE L:13" X W:2" X D:0.028", ORG THICKNESS 0.152" WITHIN CMM 25-55-06 LIMITS. NO FURTHER DEFSDR UIEA2025070800868Seat Track · chafedM/D STA 1457 TO STA 1461 RBL 11 SEAT TRACK CROWN CHAFING. CHAFING AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:7" X W:0.3" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NOSDR UIEA2025070800869Seat Track · corrodedM/D STA 617 - STA 635 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:13" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FUSDR UIEA2025070800870Seat Track · corrodedM/D STA 570 - STA 593 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:6" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURSDR UIEA2025070800871Seat Track · corrodedM/D STA 546 TO STA 559 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:8 X W:0.7" X D:0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FUSDR UIEA2025070800872Seat Track · corrodedM/D STA 2200 - STA 2210 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:4" X W:0.7" X D:0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FSDR UIEA2025070800873Tee Angle · crackedNR 3 PYLON O/B INNER MOST LWR TEE CRACKED AT NAC STA 344 APPROX. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900874Tee Angle · crackedNO. 2 PYLON - O/B MOST LOWER TEE CRACK FOUND AT NAC STA 332. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900875Beam · crackedNWW SIDE PANEL HAS 1EA CRACK FOUND AT BEAM LHS WL130 BETWEEN STA 320 AND STA 340. BEAM REPLACED AS PER BOEING DWG: 65B07942&PL AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900878Beam · crackedNWW SIDE PANEL HAS 1 EA CRACK FWD AT BEAM RHS WL180 BETWEEN STA 265 AND 280.(<P>CRACKED BEAM REPLACED AS PER BOEING DWG NO.65B07942 & PL & EO 4453A043 REV 11 PART 2 ITEM 3 AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-SDR UIEA2025070900879Seat Track · crackedM/D STA 981 TO 983 LBL 75" SUBSTITUTE TRACK FOUND CRACKED. SUBSTITUTE TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900880Seat Track · corrodedM/D STA 650 - STA 654 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:9' X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURSDR UIEA2025070900881Frame · crackedNR 4 ENG NACELLE LT CORE COWL FRAME NR 2 FOUND CHAFED. FRAME CHAFE AREA REPAIRED IAW SRM 54-45-02-2R-1 REPAIR FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900883Frame · cracked#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900884Floor Support · crackedMDC - STA 1160 - 1180 LH O/B FLOOR SUPPORT CRACK. FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-53-40-17764 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900885Skin · crackedLEFT WING #10 VC FLAP BULLNOSE O/B EDGE FOUND DEFORMED AND CRACKED. O/B EDGE DAMAGE AREA REPAIRED AS PER RI-57-40-17758 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071000886Duct · chafedNR 4 ENG RH C-DUCT FWD BLOWOUT DOOR L/E FOUND CHAFING. CHAFING AREA REPAIRED AS PER ST ENGINEERING CMM 78-32-09 REPAIR 5. NO FURTHER DEFECTS NOTED.SDR UIEA2025071000887Skin · crackedAPU RIGHT DOOR SKIN AT NR 1 LATCH OPENING AND FWD LOWER FOUND CRACKED AND CHAFING. NR 1 LATCH CUTOUT CRACK & FWD LWR SKIN CHAFING AREA REPAIRED AS PER RI-52-48-17747 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071000888Bulkhead · cracked1 EA CRACK FOUND ON BS2598 BULKHEAD LH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION VIEW LOOKING FWD, CRACK DEPTH APPROX 0.080" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-80-17737 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071000893Bulkhead · cracked1 EA CRACK FOUND ON BS 2598 BULKHEAD RH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION (VIEW LOOKING FWD) CRACK DEPTH APPROX 0.015" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-53-80-17738 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071000895Duct · crackedNO. 2 ENG - RH C-DUCT OUTER GROOVE UPPER AREA CRACK FOUND. FRAME CRACK AREA REPAIRED AS PER ATLAS AIR EA NO.EA-1978A227 REV.0. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100901Web · crackedM/D STA 1180 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 FIG 8. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100902Web · crackedM/D STA 1180 RH O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 REPAIR 8. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100903Web · crackedM/D STA 1220 L/H O/B BELOW FLOOR INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-5 REPAIR 5. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100904Web · crackedM/D STA 1200 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-9 REPAIR 9. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100905Failsafe · crackedUPPER DECK LH BS820 TENSION TIE FAIL SAFE CHORD 1EA CRACK FOUND. FAIL SAFE CHORD CRACK AREA REPAIRED AS PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100926Plate · damagedSTEEL PLATE FOUND 4EA FASTENER HOLES SEM AT UPR DECK R/H STA 760 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100927Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA800 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100928Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA840 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100929Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100930Plate · damagedSTEEL PLATE FOUND 2 EA FASTENER HOLE SEM AT UPR DECK LH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100931Plate · damagedSTEEL PLATE FOUND 1 EA FASTENER HOLE SEM AT UPR DECK LH STA880 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071100932Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK LH STA840 TENSION TIE AREA.(<P>STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071100933Frame · crackedUPPER DECK TENSION TIE AT RH BS860 1 EA CRACK FOUND. FRAME REPLACED CARRIED OUT AS PER SRM 51-10-02 AND NEW FRAME HOLES AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
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