Boeing 747-45EF
Service difficulty reports · 348
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 = '74745EF' 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 = '74745EF' 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 UIEA2026101600989Controller · faultedBLD 1 OVHT/PRV CAUTION(<P >REPLACED PRV CONTROLLER AND ENG 1 BLEED SYSTEM. OPS CHECK NORMAL IAW AMM 36-11-20</P>)SDR UIEA2026101200981Packing · missing1:30HR INTO FLIGHT AT 36000 ENG 4 OIL QTY INDICATED 10 MAGENTA, DECREASED APPROX EVERY 10-20 MINS. 0 QTS INDICATED AT TOP OF DESCENT, DURING DESCENT IT INDICATED 1QT, LDG 0 QTS, & ENG SHUTDOWN 2 QTS. AFTER ENG 4 EDP REMOVAL, FOUND EDP DRIVE SHAFT MISSING PACSDR UIEA2026093000932Skin · gougedDURING INSPECTION OF THE LOWER LOBE FWD CARGO DOOR STRINGER 34R SKIN LAP SPLICE, A GOUGE WAS FOUND C/T UPPER SKIN. WORK ACCOMPLISHED IAW EN#3792-26, REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026100600954Mount · crackedFOUND CRACK INDICATION DURING OPEN HOLE INSPECTION IN OTBD BARREL NUT BORE OF #2 PYLON AFT ENGINE MOUNT BULKHEAD FITTING ASSY.(<P>NACELLE STRUT NO.2 AFT ENGINE MOUNT BULKHEAD OUTBOARD BARREL NUT BORE REWORKED IAW EN # 3743-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026100600955Skin · crackedDURING LFEC INSPECTION AT LH WING FRONT SPAR UPPER SKIN BETWEEN WS621-WS637, FOUND 02 EA FASTENERS WITH CRACKED INDICATIONS.(<P>REFER TO EN 3800-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026100600956Skin · crackedDURING LFEC INSPECTION AT RH WING FRONT SPAR LOWER SKIN BETWEEN WS540-WS560 FOUND 01 EA FASTENER WITH CRACK.(<P>REFER TO EN#3799-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100600957Fitting · corrodedDURING OPEN HOLE INSPECTION AT RIGHT UPPER SPLICE FITTING AT STA2598 BULKHEAD, FOUND 01 EA ELONGATED HOLE AND 02 EA HOLES WITH CRACK INDICATION AT 9 O'CLOCK POSITION VIEW LOOKING INBD.(<P>REF TO EN 3842-26 REV.0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</PSDR UIEA2026100600958Fitting · corrodedDURING OPEN HOLE INSPECTION AT LEFT UPPER SPLICE FITTING AT STA 2598 BULKHEAD, FOUND 01 EA HOLE WITH CORROSION AT 9 O'CLOCK POSITION AND 01 EA WITH CRACK INDICATION AT 12 O'CLOCK POSITION.(<P><!--STARTFRAGMENT-->WORK ACCOMPLISHED PER EN 3842-26 REV.0. NO FURTHSDR UIEA2026100600959Skin · not reportedHFEC INTERNAL SKIN INSPECTION AT STA1820 S34L UNABLE TO BE COMPLETED AS INSPECTION AREA IS BLOCKED BY INTERNAL STRUCTURE.(<P>REFER EN #3772-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100100934Seat Track · chafedMAIN DECK COMPT SEAT TRACK BETWEEN STA 1480 - 1500 LBL 11.33 FOUND WORN DUE TO CHAFING. SPLICE REPAIR PERFORMED IAW EN3764-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100100936Floor Support · not reportedFOUND EXISTING REPAIR ON CARGO FLOOR SUPPORT AT STA 760 RBL48. PERFORMED REPAIR PER SRM 53-20-07 REPAIR 11. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100200938Door Frame · not reportedDURING LFEC INSPECTION AT MAIN DECK SIDE CARGO DOOR CUTOUT, FOUND 01 EA FASTENER AT STA1780 S22L. UNABLE TO INSPECT DUE TO LFEC PROBE NOT BEING ABLE TO SIT PROPERLY, BLOCKED BY DOUBLER.(<P>WORK ACCOMPLISHED REFER EN#3725-26 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026100400942Floorbeam · corrodedFOUND CORROSION ON MAIN DECK FLOOR BEAM AT STA 460 LBL 53.(<P>REPAIR CARRIED OUT ON CORROSION FLOOR BEAM PER EN 3785-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100500946Support Frame · modificationSECTION 48 BODY STA 2598 BULKHEAD H/STAB HINGE SUPPORT FRAME MOD, FOUND RH 08 EA FASTENERS AFFECT THE TRIPLER LOCATION.(<P>REFER TO EN #3801-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100500947Fuel Tank · dentedFWD CGO COMPT CENTER TANK AT STA 991 RBL 4 WL 128 FOUND DENTED(<P>REFER TO EN#3682-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100500948Support Rib · crackedLH BODY GEAR W/W DOOR ACTUATOR UPPER RIB SUPPORT FITTING FOUND CRACKED AT MID O/B AREA.(<P>REFER TO EN #3760-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100500949Access Panel · bulgedCARGO DOOR AT 1898 ACCESS PANEL #836JL FOUND BULGING DUE TO CORROSION.(<P>REFER TO EN#3757-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026100500951Fuel Tank · dentedFWD CARGO CENTER TANK AT BS 991, LBL 15, WL 128, FOUND DENTED.(<P>REFER TO EN#3682 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026100500953Bearing · migratedRT WING T/E FLAP TRACK #6 FITTING SUSPECT MIGRATION. RT WING T/E FLAP TRACK #6 FWD FITTING BEARING REMOVED AND INSTALLED OVERSIZED BEARING AS PER EN 3687-26 REV. 0.NO FURTHER DEFECTS NOTED.SDR UIEA2026092300909Spar Web · corrodedFOUND CORROSION ON RH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT UNDER BONDING STRIP.(<P>REPAIR ACCOMPLISHED IAW EN# 3635-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026092300910Spar Web · corrodedFOUND CORROSION ON LH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT UNDER BONDING STRIP.(<P>REPAIR ACCOMPLISHED IAW EN 3635-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026092700917Battery Pack · no testDURING THE EMERGENCY LIGHTS BATTERY PACKS TESTS, FOUND M5168 AND M5169 POWER SUPPLY BATTERY PACKS FAILED TO TEST.(<P>02 EA EMERGENCY BATTERY PACK ASSY M5168 AND M5169 WERE REPLACED, AND OPS TEST WAS COMPLETED PER AMM 33-51-04-902-001-001 REV 117. OPS TEST WAS SDR UIEA2026092900921Frame · corrodedFRAME AT STATION 400 RBL 60 FOUND WITH SURFACE CORROSION.(<P>WORK ACCOMPLISHED ON SURFACE CORROSION AREA AT MAIN E/E EQUIPMENT CTR CMPT FRAME STA 400 RBL 60 PER EN NO.3779-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026092900924Floorbeam · corrodedDURING HFEC INSPECTION AT FLOOR BEAM UPPER CHORD LOWER SURFACE STA 660 LHS, FOUND CORROSION & CRACK APPROX 0.15" AS MARKED(<P>WORK ACCOMPLISED IAW EN 3767-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026093000928Beam · corrodedRH WING FIXED T/E BEAM UPPER CHORD ( P/N: 65B11614-28) FOUND WITH EXFOLIATION CORROSION ON THE INBD TOP EDGE SECTION. LENGTH OF DAMAGE IS APPROX 4".(<P>SPLICE REPAIR ACCOMPLISHED IAW EN #3696-26 REV 0. PERMANENT REPAIR CLASSIFIED AS CATEGORY A. NO FURTHER DEFESDR UIEA2026093000931Floor Support · crackedBS 1220, LBL 117, WL 199.30 FLOOR PANEL SUPPORT FOUND CRACKED(<P>CRACKED FLOOR PANEL SUPPORT REPAIRED AS PER EN #3690-26 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026091900885Engine · failedENGINE 4 FAIL AFTER TAKEOFF. REPLACED NR 4 ENG DURING ENG RUN-UP. NO FAULT MSG; LEAK CHK NML AND OPS CHK NML AS PER AMM 71-00-00, 71-00-02 AND AIPC 71-00-51-06A ITEM 10. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026061200464Floorbeam · corrodedM/D BS 1180 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>INTERCOSTAL WEB REPAIRED AS PER RI-53-40-18379 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061200465Web · corrodedM/D BS 1180 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061200466Floorbeam · corrodedM/D BS 1220 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18378 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300467Floorbeam · corrodedM/D BS 1220 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18381 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300468Floorbeam · corrodedM/D STA 1200 RBL 105" BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18382 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300469Floor Support · corrodedM/D STA 1200 LBL 105 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-53-40-18377 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300470Seat Track · corrodedM/D BS 1020 TO 1070 LBL 11 SEAT TRACK RHS FLANGE BOTTOM SIDE FOUND CORROSION(<P>SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300471Panel · corrodedRHW L/E UPPER FIXED PANEL O/B EDGE NEAR #3 PYLON O/B FOUND CORROSION(<P>CHORD REPLACED AND INSTALLED AS PER RI-57-41-18383 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300472Structure · corrodedLHW STA 1241 CETNER LH O/J PUMP CUTOUT FOUND CORROSION(<P>WEB CORROSION AREA REPAIRED AS PER RI-57-10-18352 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300473Structure · corrodedRHW STA 1241 RH CENTER O/J PUMP CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18355 REV A. NO DEFECTS NOTED</P>)SDR UIEA2026061300474Spar · crackedLHW - UPPER WING T/E MOST I/B FIXED PNL SUPPORT P/N 65B11532-41 CRACK(<P>SUPPORT P/N 65B11532-41 REPLACED AS PER RI-57-20-18384 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300475Fitting · crackedRH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA FOUND 1EA CRACK(<P>LONGERON EXTENSION FITTING REPLACED AS PER ATLAS AIR EO 4453A818 REV 20 PART 4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061300476Doubler · corrodedNR 3 FUEL AFT BOOST PUMP FOUND CUTOUT DOUBLER CORROSION. DOUBLER FABRICATED AS PER BOEING DWG 65B19560 AND PL, NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061400477Doubler · crackedRHS STA 2524.4 UPPER LOBE DOUBLER ALONG THE RADIUS FOUND 1EA CRACK APPROX 8" IN LENGTH(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 10 PART 2 AND RI-53-80-18477 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061400479Doubler · chafedRH STA 980 UNDERWING LONGERON AREA FOUND REPAIR DOUBLER ADJ SKIN CHAFING(<P>SKIN REPAIRED AS PER RI-53-20-18357 REV B. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2026061400480Fitting · corrodedRT WING T/E L/G SUPPORT BEAM APPROX 200 UPPR CHORD FWD SUPPORT ROD O/B FITTING FOUND CORROSION WEAR #5 FLAP TRACK. FITTING ASSY FABRICATED AS PER BOEING DWG 69B11720 AND PL REV LTR A AND NEW FITTING ASSY HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FITTING ASDR UIEA2026061400481Frame · chafedNR 4L CORE COWL NR 2 FRAME PATCH FOUND CHAFING ( COUNT FROM FWD )(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECT NOTED</P>)SDR UIEA2026061400482Longeron Splice · crackedRH BS 1480 LONGERON EXTENSION FITTING INTERIOR SPLICE FITTING 1EA HOLE FOUND CRACK(<P>CRACK FASTENER HOLE REPAIRED AS PER RI-53-60-18406 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061500487Angle · crackedRHW L/E ILES APPROX 268.81 UPPER SUPPORT RIB AFT AREA. ANGLE REPLACED AND INSTALLED IAW RI-57-41-18376 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026061500488Angle · crackedLHW L/E ILES APPROX 268.81 UPPER SUPPORT RIB AFT CORNER SPLICE FITTING FOUND CRACK. ANGLE REPLACED AND INSTALLED AS PER RI-57-41-18375 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026061500489Panel · nickedM/D LHS BS 1620 TO 1720 DADO PNL AFT EDGE FOUND NICKED. DADO PANEL NICK AREA REPAIRED AS PER RI-25-21-18349 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026061500490Step · crackedM/D BS 500 LHS LADDER #7 STEP ( COUNT FROM BOTTOM ) I/B WEB FWD AREA FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-25-13-18347 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026061500491Step · crackedM/D BS 500 LHS LADDER #8 STEP ( COUNT FROM BOTTOM ) I/B WEB FWD AND AFT FOUND CRACK(<P>I/B WEB FWD AND AFT CRACK AREA REPAIRED AS PER RI-25-13-18348 REV A. NO FURTHER DEFECTS</P>)
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