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 UIEA2024012500024Skin · damagedLHW I/B FORE FLAP LWR SURFACE FOUND DAMAGED AS MARK (156" FROM O/B TO I/B).(<P>LHW I/B FORE FLAP LWR SURFACE 156" FROM O/B TO I/B DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024012500025Skin · delaminatedL/H I/B FLAP MID FLAP MOST O/B LWR SURFACE FOUND DELAMINATION AS MARK (15" TO O/B EDGE).(<P>L/H I/B FLAP MID FLAP MOST O/B LOWER SURFACE (15" TO O/B EDGE) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTSDR UIEA2024012500026Skin · delaminatedLHW T/E I/B AFT FLAP L/E 66" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>LHW T/E I/B AFT FLAP L/E 66" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500028Skin · dentedLHW I/B AFT FLAP LWR T/E SURFACE AT MID AREA FOUND 1EA DENT AS MARK (155" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP LWR T/E SURFACE 155" FROM I/B DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500029Skin · puncturedL/H I/B FLAP AFT FLAP T/E UPPER SURFACE FOUND 1EA PUNCH DAMAGED AS MARK.(<P>LH I/B FLAP AFT FLAP T/E UPPER SURFACE PUNCH DAMAGED AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500030Skin · dentedLHW I/B AFT FLAP O/B LWR SURFACE FOUND 1EA DENT AS MARK (146" FROM I/B TO O/B).(<P>LHW I/B AFT FLAP O/B LWR SURFACE (146" FROM I/B TO O/B) DENT AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500031Skin · delaminatedLHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" FOUND DELAMINATION AS MARK. (COUNT FROM I/B TO O/B)(<P>LHW T/E I/B AFT FLAP LOWER SURFACE T/E 130" (COUNT FROM I/B TO O/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIGURE 5. NOSDR UIEA2024012500032Skin · delaminatedLHW T/E I/B FLAP FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) FOUND DELAMINATION AS MARKED.(<P>LHW T/E I/B AFT FLAP LOWER SURFACE L/E 47" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTSSDR UIEA2024012500033Panel · delaminatedL/H O/B FLAP MID FLAP O/B CARRIAGE ASSY COVER PANEL FOUND DELAMINATION AS MARK.(<P>L/H O/B FLAP MID O/B CARRIAGE ASSY COVER PANEL DELAMINATION AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500034Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 100" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500035Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 122" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500036Skin · delaminatedRHW T/E I/B MID FLAP LOWER SURFACE L/E 124" FOUND DELAMINATION AS MARKED (COUNT FROM TO I/B).(<P>RHW T/E I/B MID FLAP LOWER SURFACE L/E 124" (COUNT FROM TO I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500037Frame · crackedFX STA 1480 RH BULKHEAD FRAME WEB FOUND CRACK(<P>FRAME WEB REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500038Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 48" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024012500039Skin · delaminatedRHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) FOUND DELAMINATION AS MARK.(<P>RHW T/E I/B MID FLAP L/E 2" (COUNT FROM I/B) DELAMINATION AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500040Panel · delaminatedR/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER APNEL FOUND DELAMINATION AS MARK.(<P>R/H I/B T/E FLAP MID FLAP O/B CARRIAGE ASSY UPPER COVER PANEL DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500041Skin · delaminatedRHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" FOUND DELAMINATION AS MARKED (COUNT FROM I/B).(<P>RHW T/E I/B AFT FLAP LOWER SURFACE T/E 155" (COUNT FROM I/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012500042Fairing · delaminatedRHW O/B FWD FLAP FWD FAIRING 48" FOUND DELAMINATION AS MARKED (COUNT FROM O/B).(<P>RHW O/B FWD FLAP FWD FAIRING 48" (COUNT FROM O/B) DELAMINATION AREA. PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800046Seat Track · damagedM/D STA 1890 RBL 11 SEAT TRACK CTR GUIDE STOP HOLE FOUND ELONGATED(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800047Tension Tie · crackedLH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800048Tension Tie · crackedLH BS 880 UPPER DECK TENSION TIE 1EA CRACK FOUND AT AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800049Tension Tie · crackedRH BS 840 UPPER DECK TENSION TIE 1EA CRACK FOUND AT 1 O/C POSITION OF THE AFT CHANNEL(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800050Channel · crackedLH BS 900 UPPER DECK TENSION TIE AFT CHANNEL 1EA HOLE FOUND CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012800051Skin · corrodedFUSELAGE SKIN AT LOWER LOBE CIRCUMFERENTIAL SPLICE LOCATION STA 1715 S45R FOUND CORROSION APPROX 1" X 1"(<P>SKIN REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024012900052Skin · corrodedLHW I/B AFT FLAP FOUNDÂ BULGE UP(<P>PERFORMED REPAIR AT BULGE UP AREA IAW RI-57-53-16705. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024013000053Skin · dentedLHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16699 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024013000054Skin · dentedRHW O/B T/E AFT FLAP O/B PANEL UPPER SURFACE FOUND SEVERAL AREA DENT MARK AS MARKED.(<P>METAL HOT BOND REPAIR CARRIED OUT AS PER RI-57-51-16700 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024013100055Frame · crackedLH BS 2598 B/HEAD INNER CHORD 1EA HOLE FOUND CRACK AT 3ND LAYER (COUNTING FROM AFT) AT 5 O'CLOCK POSITION APPROX 0.050" IN DEPTH(<P>INNER CHORD CRACK AREA REPAIRED AS PER RI-53-73-16683 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024013100057Longeron · crackedFUS - 2EA CRACKS WERE FOUND ON RH BS 1480-1540 STR 32-33 LONGERON EXTENSION FITTING(<P>LONGERON EXTENSION FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453A818 R19 PART 4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024013100058Panel · crackedM/D STA 1720 L/H DADO PNL FOUND CRACK(<P>DADO PNL CRACK AREA REPAIRED AS PER RI-25-21-16675 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100059Ladder · crackedM/D CREW LADDER I/B SIDE #7 & 10 STEP FOUND CRACK(<P>#7 AND #10 STEP CRACK AREA REPAIRED AS PER RI-25-50-16667 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100060Skin · corrodedFX R/H AIRCON BAY STA 1000-1003 CENTER SECTION LOWER SURFACE CORR. AT RBL 15" - RBL 29"(<P>SKIN CORROSION AREA REPAIRED AS PER RI-57-10-16703 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100061Bracket · damagedAPU COMPT L/H FRAME STA 2674 WIRE BRACKET AND ATT FRAME RIVET HOLES FOUND ELONGATED(<P>WIRE BRACKET REPLACED AS PER SRM 51-10-02, NEW BRACKET HOLES TRANSFERRED AS PER SRM 51-40-05, NEW BRACKET INSTALLED AS PER SRM 51-40-02 AND FRAME REPAIRED AS PER SRM 53-80-0SDR UIEA2024020100062Skin · crackedFX - FUSELAGE SKIN STA 1680 STR 41R FOUND CORR CRACK(<P>SKIN REPAIRED AS PER RI-53-61-16685 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100063Support · crackedLHW L/E CAVITY HOLES 1300 FIXED PNL SUPPORT CRACK (AFT OF #4 V/C FLAP)(<P>SUPPORT BEAM REPAIRED AS PER RI-57-41-16684 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024020100064Closeout Panel · crackedM/D STA 1241 LBL 77-99 CLOSURE PNL FOUND CRACK.(<P>CLOSURE PNL REPLACED AS PER SRM 51-10-02, NEW PNL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PNL INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100065None · noneACCOMPLISHMENT OF EO 4453A301 REV.11, WE FOUND ONE EACH FREEZE PLUG INSTALLED ON UPPER DECK R/H STA 880 FRAME AREA.(<P>FRAME REPAIRED AS PER RI NO. RI-53-20-16702 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100066Skin · chafedFX SKIN STA 724 STR 0-1R FOUND CHAFING.(<P>CHAFING AREA REPAIRED AS PER RI NO. RI-53-20-16706 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100067Support Bracket · cracked#3 FUEL TANK JETTISON TRANSFER VALVE SUPPORT BRACKET FOUND CRACK.(<P>BRACKET REPAIRED AS PER RI NO. RI-28-21-16701 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020200068Skin · corrodedFX - AIRCON BAY L/H STA 1240 CENTER WING LWR SURFACE CORR AT LBL 91" - LBL 102" AND LBL 105" - LBL 113".(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO. RI-57-10-16704 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024012600044Rotor · unknownENG 3 CONTROL STS MSG. SUSPECT EEC FAILURE(<P>R/R #3 EEC & ROTOR OF CONTROL ALTERNATOR. OPS CHECK GOOD IAW AMM 73-21-08 & AMM 73-21-15. DMI 201757 CLOSED.</P>)SDR UIEA2024012100020Floor Panel · damagedM/D STA 1850-1920 LBL 78-99 BALL MAT FLOOR PNL FOUND DAMAGE(<P>THE DAMAGED CASTER PANEL TOP SKIN REPAIR HAS BEEN CARRIED OUT PER EO.4425A500 REV.1</P>)SDR UIEA2024011400013Cdu · unknown30 MINS INTO FLIGHT, FO CDU LOST POWER. THIS HAPPENED JUST AS THEY WERE COASTING OUT. REPEAT WRITE-UP(<P>FOUND 115 VAC AT PLUG (DM7440A) PIN 40 TO P41. VOLTAGE NORMAL DURING WIRE SHAKE. GND ALSO NORMAL DURING WIRE SHAKE. OPS CHECK NORMAL FOR RH CDU. FOR T/S PUSDR UIEA2023120800977Actuator · unknownPILOT REPORTS RH BODY GEAR DOOR DROOPS IN FLIGHT. GEAR DOORS OPEN WHEN LANDING GEAR HANDLE IS IN THE OFF POSITION.(<P>REMOVED AND REPLACED R BLG UPLOCK ACTUATOR IAW B747 AMM 32-33-94. OPS CHK AND LEAK CHK GOOD.SDR UIEA2023101200901Unknown · unknownLEFT WING GEAR TILT ACTUATOR BROKE. CAUSED DAMAGE TO STRUCTURE AND WING GEAR.(<P>MX IN WORK WHILE IN AOGD FOR LH WING GEAR TILT ACTUATOR INOP. AOGD ETR: 26OCT23</P>)SDR UIEA2023100700892Brake · unknownSUSPECTED LIGHTNING STRIKE DEPARTING UIO, RETURNED TO UIO, HEAVY WEIGHT LANDING, BRAKE TEMPERATURE CAUSED TIRE FUSE PLUGS TO MELT ON MAIN LANDING GEAR TIRES #1, 2, 3, 4, 5, 6, 7, 8 AND 10.(<P>UPON LANDING, COMPLETED LIGHTING STRIKE INSP IAW AMM 05-51-13, OVERWSDR UIEA2023093000861Unknown · unknownLIGHTNING STRIKE DURING CLIMB, AIR TURN BACK. OVERWEIGHT LANDING AND HIGH ENERGY STOP RESULTED IN 9 MELTED MAIN LANDING GEAR TIRE FUSE PLUGS AND DEFLATION OF TIRES.(<P>AXLES NEED REPLACEMENT. MX CURRENTLY IN WORK PER AMM 05-51-10.</P>)SDR 9WGA2023091525801Cylinder · shearedDISCREPANCY: DIVERTED DUE TO GEAR NOT RETRACTING. EICAS "GEAR TILT" STATUS MESSAGE "GEAR MONITOR". CORRECTIVE ACTION: FOUND LH IB BODY GEAR LEVELING CYLINDER SHEARED. REMOVED AND REPLACED LEVELING CYLINDER IAW AMM 32-13-15.SDR UIEA2023070500690Packing · unknownHYD QTY LOW 4Â EICAS MESSAGE(<P>ITEM 1: FOUND ACCUMULATOR ISOLATION VALVE UPPER BLANK AND LOOSE, TIGHTENED 1 TURN IAW AMM 20-51-01 (FOR SOURCE SELECTOR 1 VALVE). ITEM 4: LEAK CHECK C/W AND FAILED. ITEM 7: FOUND O-RING ON TOP PLUG OF ACCUMULATOR VALVE DAMAGEDSDR UIEA2023062800661Fan · unknownE& E COOLING STATUS MESSAGE(<P>REPLACED FWD EQUIPMET COOLING FAN IAW 21-58-01, OPS CHK IAW AMM 21-58-00. NO DEFECTS NOTED AT THIS TIME. AIPC 21-58-01-01 REV 83 11APR23</P> / <P> </P> / <P> </P>)
Back to Boeing 747-47UF