Boeing 747-123
Service difficulty reports · 2,292
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 = '747123' 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 = '747123' 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 UPS97421997Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME CUT-OUT CORNERS AT BS 2040, LBL AND RBL 17.5. REPAIRED CU-TOUT CORNER BS 2040 LBL 17.5 ACC. SRM 53-10-04, FIG.43. REPAIRED CUT-OUT CORNER BS 2040 RBL 17.5 ACC. KLM DFX 97-025, ISSUE NR 2. REPAIR APPROVED PER USDR P5CA9700224Skin · gougedGOUGES IN NR 4 PYLON LEFT SIDE NAC STA 145. REPAIRED PER BOEING SRM 53-30-01 AND 51-10-02.SDR UPS97422009Stringer · corrosionINSPECTION TYPE: C. FOUND CRACK DUE TO CORROSION IN STRINGER-END AT BS. 2176, S46R. REPAIRED STRINGER ACCORDING SRM. 53-10-03 FIG.1.SDR UPS97422026Floorbeam · corrodedINSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE: FLOORBEAM UPPER CHORD BS 1580 IS CORRODED ON LOWER SIDE OF FLANGE AT LBL 70. CORROSION FOUND TO BE BEYOND LIMITS OF SRM 53-10-01. FLOORBEAM UPPER CHORD BS 1580 LBL 0 TO OUTBOARD REPLACED ACC TO SRM 51-30-02.SDR UPS97421998Longeron · crackedINSPECTION TYPE: C. DUE TO CRACK AT BSTA 1480 AT OVERWING LONGERON LT SIDE. REPLACE LT OVERWING LONGERON UPPER CHORD FROM STA 1350 TO BSTA.1480 PER SB 747-53-2291. REPLACED O/W LONGERON AT STA.1350 THROUGH 1480 LT ACCORDING SB 747-53-2291 AND DWG. 624U0008SDR UPS97422003Trunnion Fitting · corrodedINSPECTION TYPE: C. FOUND DURING INSPECTION OF NLG FITTINGS, CORROSION ON THE INBOARD SIDE FACE OF RT AND LT TRUNNION CAP AND SOME CORROSION ON THE INSIDE OF BOTH FITTINGS. REPAIRED LT AND RT NLG TRUNNION FITTINGS ACC. SRM.53-10-08. MACHINED LT TRUNNION FISDR UPS97422002Shear Tie · crackedINSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUTOUTS AT BS.1780 BETWEEN S46/47 AND S43/44 LT. REMOVED DAMAGED SECTIONS OF SHEAR TIES AND REPAIRED SHEAR TIES ACC. SRM.53-10-04, FIG. 3.SDR UPS97422001Shear Tie · crackedINSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUTOUTS AND SKIN ATTACHMENT AT BS.1840, BETWEEN S43/44, S45/46 AND S46/47LT. REMOVED DAMAGED SHEAR TIES AND REPAIRED SHEAR TIES ACC SRM.53-10-04, FIG.42.SDR UPS97421999Floorbeam · corrosionINSPECTION TYPE: C. FLOOR BEAM UPPER CHORD BS.2060 IS CORRODED BEYOND LIMITS AT LBL 51. CORROSION AT BS 2060 LBL 151. REMOVED ACC TO SRM 51-10-01, FOUND TO BE BEYOND LIMITS OF SRM 53-10-01, REPLACED UPPER CHORD ACC. SRM 53-10-0 7 FIG. 12.SDR UPS97421996Intercostal · crackedINSPECTION TYPE: C. FOUND CRACK IN ATTACHMENT ANGLE OF INTERCOSTAL TO FRAME AT BS 1840, RBL 34. REPLACED ATTACHMENT ANGLE ACC. SRM.51-30-02.SDR UPS97421994Shear Tie · crackedINSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUT-OUTS AT BS 1820, BETWEEN S43/44, S45/46, S46/47 LT. REMOVED DAMAGED SHEAR TIES AND REPAIRED SHEAR TIES ACC. SRM 53-10-04 FIG 3A.SDR UPS97421991Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME WEB CUTOUT CORNER AT BS 2160, S49/48LT. REPAIRED FRAME WEB CUTOUT CORNER ACCORDING SRM 53-10-04 FIG. 43.SDR UPS97421992Shear Tie · crackedINSPECTION TYPE: C. FOUND CRACK ON SHEAR TIE AT SKIN ATTACHMENT AT BS.1740 BETWEEN S-44/45 LT. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACCORDING SRM 53-10-04 FIG. 3.SDR UPS97422000Shear Tie · corrosionINSPECTION TYPE: C. FOUND CORROSION ON SHEAR TIE FLANGE TO SKIN AT BS 2340, S44/46R. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC. SRM 53-10-04, FIG 3.SDR UPS97421980Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN FRAME INNER FLANGE AT END OF LEG OF SIDE GUIDE ATT. BRACKET, AT BS.1520, BETWEEN S-40/39LT. STOP DRILLED CRACK AND REPAIRED FRAME INNER CHORD ACC. SRM 53-10-04, FIG. 66.SDR UPS97422008Frame Web · crackedINSPECTION TYPE: C. FOUND CRACK IN LOWER FRAMEWEB CUTOUT CORNER AT BS. 2060, LBL.17.5. REPAIRED CUTOUT CORNER ACC. SRM.53-10-04 FIG.43.SDR UPS97422004Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME CUTOUT CORNER AT BS 220 LBL 17.5. REPAIRED CUTOUT CORNER ACC. SRM.53-10-04 FIG. 43.SDR P5CA9700218Fairing · crackedNR 3 PYLON CLOSE OUT FAIRING CRACKED EXISTING WELDS. CLOSE OUT FAIRING WELDED ON TRAVELER NR 67277 PER BAC 5975.SDR P5CA9700217Skin · damageFUSELAGE SKIN AT BS 1780 TO 1800 BETWEEN STR'S 15R AND 16R SKIN BULGED. REPAIRED PER SRM 53-30-03 FIG 1A AND 53-30-01 FIG 1A, 51-10-01, 51-10-02 AND 51-30-00.SDR P5CA9700216Panel · damageRIGHT WING UPPER FIBERGLASS PANEL PUNCTURE ABOUT 4 FT FROM FUSELAGE. REPAIRED DAMAGED LEADING EDGE PANEL IAW SRM 51-40-09.SDR P5CA9700215Skin · damageUPPER RUDDER LT SMALL PUNCTURE ON SURFACE STA 157.7. REPAIRED IAW SRM 51-40-09 BY APPLYING FIBERGLASS OVERLAYS AND PAINTED IAW SRM 51-24-11.SDR P5CA9700211Skin · delaminationLEFT WING I/B FLAP LWR SURFACE HAS SEVERAL DELAMINATIONS. CLEANED, SANDED AND REMOVED DELAMINATED SKIN IN 3 AREAS. APPLIED CORE FILLERS WHERE NEEDED AND REPAIRED USING FIBERGLASS OVERLAYS IAW SRM 51-70-04 AND 51-24-11.SDR P5CA9700206Fairing · crackedRT BODY FAIRING 194DR DELAMINATED AND CRACKED AT EDGE. ALSO, 2 INCHES INBD OF EDGE. SANDED DAMAGED AREA SMOOTH, CLEANED, APPLIED FIBERGLASS OVERLAYS AND STOP DRILLED CRACK IAW SRM 51-40-09.SDR P5CA9700201Sailboat · delaminationNR 2 PYLON I/B SAILBOAT INNER SURFACE DELAMINATED ALONG EDGE. REMOVED DELAMINATED AREA, CLEANED, PRIMED, FABRICATED DOUBLER AND HOT BONDED IAW SRM 51-40-06.SDR P5CA9700196Panel · damagePANEL NR 572EB LEFT WING CORNER BROKEN OFF. POTTED, APPLIED FILLERS AND DOUBLERS AND REPAIRED PER SRM 51-40-09 AND PAINTED PER SRM 51-24-11.SDR P5CA9700195Panel · damagePANEL NR 531 AB NR 1 PYLON O/B TRIANGLE PANEL HAS ENLARGED SCREW HOLES. ALSO, FORWARD EDGE ERODED. REPAIRED BY APPLYING FIBERGLASS OVERLAYS AND PAINTED PER SRM 51-40-15 AND 51-24-11.SDR P5CA9700190Bracket · corrodedLEVEL 2 CORROSION RIGHT WING I/B FOREFLAP I/B BOOMERANG FITTING MOUNT BRACKET. REMOVED AND REPLACED RIGHT WING FOREFLAP MOUNT BRACKET IAW SRM 51-30-02.SDR P5CA9700176Skin · damageNR 2 PYLON UPPER SKIN FLANGE IS CHAFED. REMOVED AND REPLACED WITH NEW STRAP IAW SRM 51-30-02.SDR P5CA9700167Skin · delaminatedTWO SOFT SPOTS ON LEADING EDGE OF THE LEFT WING INBOARD FLAP OUTBOARD END OF THE FORE FLAP. REPAIRED PER BOEING SRM 51-40-12.SDR P5CA9700164Skin · delaminatedREPAIR COMING LOOSE ON WING UNDERSIDE TRAILING EDGE JUST INBOARD OF INBOARD AILERON. REPAIRED PER BOEING SRM 51-40-09, PAINTED PER 51-24-11.SDR P5CA9700161Panel · delaminatedDELAMINATED PANEL LEFT WING UPPER AFT INBOARD WING. REPAIRED PER BOEING SRM 51-40-09 AND PAINTED PER 51-24-11.SDR P5CA9700099Skin · dented2 DENTS ON NR 5 LEFT DOOR LOWER EXTERNAL SKIN. REPAIRED PER BOEING SRM'S 52-10-02 AND 51-24-11.SDR P5CA9700214Web · damageGOUGES/CRACK ON WEB AT STA 82-8 LT VERTICAL STAB. BLENDED GOUGES SRM 51-10-01. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-02.SDR P5CA9700213Brackets · crackedNR 4 FLAP AFT I/B BOGIE ASSY CRACKED. REMOVED AND REPLACED BROKEN BOGIE ASSY BRACKETS AS PER OHM 27-51-81.SDR P5CA9700212Bracket · crackedAPU SURGE BLEED VALVE BRACKET CRACKED. WELDED BRACKET IAW BAC 5975, DYE CHECKED PER SOPM 20-20-02, NO CRACKS NOTED. INSTALLED BRACKET PER MM 49-53-01.SDR P5CA9700210Panel · corrodedLIGHT CORROSION ON PANEL NR 191BB. SANDED OFF CORROSION, APPLIED FIBERGLASS OVERLAYS AS REQUIRED AND PAINTED PER SRM 51-40-09 AND 51-24-11.SDR P5CA9700209Panel · dentedDENT IN PANEL NR 191XL. SANDED AND REMOVED DAMAGED AREA, APPLIED FIBERGLASS FILLER OVERLAYS IAW SRM 51-40-09 AND SEALED APPLIED CONDUCTIVE COATING AND PAINTED PER SRM 51-40-11 AND 51-24-11.SDR P5CA9700208Panel · corrodedCORROSION ON PANEL NR 191HH. REMOVED MINOR SURFACE CORROSION AND TREATED WITH NEG MAT LOSS PER SRM 51-10-01 AND 51-10-02.SDR P5CA9700207Panel · delaminatedPANEL NR 193GL DELAMINATED. REPAIR PANEL AND PAINTED PER SRM 51-40-09 AND 51-24-11.SDR P5CA9700205Panel · corrodedKEEL BEAM PANEL FOR ROTATING BEACON HAS CORROSION AT BASE OF ROTATING BEACON. REMOVED MINOR SURFACE CORROSION AND TREATED WITH NEG MAT LOSS PER SRM 51-10-01 AND 51-10-02.SDR P5CA9700204Stiffeners · corrodedNUMEROUS AREAS OF CORROSION ON ALL STIFFENERS ON PANEL NR 191MM. REMOVED CORROSION AND TREATED AREAS WITH NEG MAT LOSS IAW SRM 51-10-01 AND 51-10-02.SDR P5CA9700203Fairing · damageNR 2 FIXED FWD FLAP TRACK FAIRING HAS HEAVY WIND EROSION AND HOLES. SANDED DAMAGED AREA, SMOOTH POTTED HOLES, APPLIED FIBERGLASS OVERLAYS AND PAINTED PER SRM 51-40-15 AND 51-24-11.SDR P5CA9700202Fairing · damageNR 3 FIXED FWD FLAP TRACK FAIRING HAS DEEP PUNCTURE. REPAIRED PER SRM 51-40-15 AND PAINTED PER SRM 51-24-11.SDR P5CA9700200Fairing · damage1 PYLON AFT FIXED FAIRING MOUNTING FLANGE WORN AND CRACKED. REPLACED PYLON FAIRING IAW SRM 51-10-03 AND FABRICATED MOUNTING BRACKET.SDR P5CA9700199Fairing · delaminatedPANEL NR 194FR WING TO BODY FAIRING DELAMINATED. REPAIRED PER BOEING SRM 51-40-09 AND 51-24-11.SDR P5CA9700198Panel · wornEDGE OF PANEL 294BR WORN THROUGH. REPAIRED PER BOEING SRM 51-40-09 AND 51-24-11.SDR P5CA9700197Fairing · puncturedHOLE IN PANEL NR 292BR RIGHT FORWARD WING TO BODY FAIRING. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9700194Fairing · delaminatedRT FWD WING TO BODY FAIRING PANEL 292AR DELAMINATED AT PREVIOUS REPAIR. REMOVED OLD REPAIR, SANDED AND CLEANED, APPLIED FIBERGLASS FILLERS AND OVERLAYS, PAINTED PER SRM 51-40-09 AND 51-24-01.SDR P5CA9700193Angle · crackedNR 2 ENG I/B CORE COWL AFT HINGE ARM ATTACH ANGLE IS CRACKED AND FASTENERS LOOSE. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02.SDR P5CA9700191Fairing · puncturedHOLE IN PANEL NR 292CR RIGHT FORWARD WING TO BODY FAIRING. REPAIRED PER BOEING SRM 51-40-09 AND PAINTED PER BOEING SRM 51-40-11.
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