Boeing 747-121
Service difficulty reports · 3,030
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 = '747121' 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 = '747121' 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 P5CA9601220Skirt Clamp · brokenSKIRT NR 4 CLAMP UNDER RETURN LINE BROKEN. CLAMP REPLACED PER MM 20-11-24.SDR P5CA9601219Skirt · corrodedSKIRT NR 4 SUPPORT RODS EYEBOLTS CORROSION. CORROSION REMOVED AND TREATED PER MM 51-21-03.SDR P5CA9601218Skirt · chafedSKIRT NR 1 FWD BRIDGE ABOVE PRESS MODULE CHAFED. SMOOTHED CHAFED AND AREA TREATED PER SRM 51-40-03.SDR P5CA9601038Door · corrodedNR 2L ENTRY DOOR 2 CORROSION SCREWS ON OUTER DOOR HANDLE. CORROSION REMOVED AND TREATED PER MM 51-21-03.SDR P5CA9601037Door · corrodedNR 2R ENTRY DOOR SURFACE CORROSION ON DOOR STOPS. CORROSION REMOVED AND TREATED PER MM 51-21-03.SDR P5CA9600667Mount Bolts · corrodedLEVEL 1 CORROSION ON MOUNT BOLTS NR 2 ENTRY DOOR. REMOVED AND TREATED CORROSION PER BOEING SRM 51-21-03.SDR P5CA9600665Stringer · corrodedFOUND LEVEL ONE CORROSION ON STRINGER 47 NEAR STATION 1920 RT SIDE. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01.SDR P5CA9600664Support · corrodedFOUND LEVEL 2 CORROSION ON FAIRING SUPPORT AT LOWER FUS STA 880 BETWEEN BL 0 TO LBL 15. REPAIRED IAW SRM 53-50-04. CPCP BASE LINE INSPECTION.SDR P5CA9600663Bracket · corrodedFOUND LEVEL ONE CORROSION ON BRACKET AND AROUND GROUNDING BOLT AT FAIRING SUPPORT, FUSELAGE RT SIDE STA 1660, BETWEEN STR 44 TO 45. REMOVED CORROSION IAW SRM 51-10-01, INSTALLED HI-LOCK IAW SRM 51-30-02.SDR P5CA9600662Skin · corrodedFOUND LEVEL ONE CORROSION AND PROTRUDING HI-LOCK ON FUSELAGE SKIN RT SIDE AT STR 40 AREA STA 1700. REMOVED CORROSION FROM SKIN IAW SRM 51-10-01. INSTALLED NEW HI-LOCK AND RIVET IAW SRM 51-30-02.SDR P5CA9600661Bracket · corrodedFOUND LEVEL ONE CORROSION ON SUPPORT BRACKET AT CENTER LOWER FUSELAGE BETWEEN STA 920 TO 960. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01. REPAIRED IAW SRM 51-40-03.SDR P5CA9600660Support · corrodedFOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FS RT SIDE STA 1540 BETWEEN STR AREA 33 TO 36. REMOVED CORROSION IAW SRM 51-10-01. FOUND WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600659Support · corrodedFOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STATION 1540 BETWEEN STR AREA 28 TO 37. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.SDR P5CA9600658Support · corrodedFOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STAION 1580 BETWEEN STR AREA 29 TO 40. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.SDR P5CA9600657Support · corrodedFOUND LEVEL ONE CORROSION ON CENTER FAIRING SUPPORT AT LOWER FUSELAGE BETWEEN STATIONS 1480 TO 1660. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02.SDR P5CA9600656Support · corrodedFOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT LOWER FS 1580 BETWEEN AREA RBL 100 TO LBL 100. REMOVED CORROSION IAW SRM 51-10-01. FOUND WITHIN THE LIMITS OF SRM 53-10-01.SDR P5CA9600643Bracket · chafedFOUND LEFTHAND FORWARD MOUNTING BRACKET CHAFED AND ONE ANCHOR NUT MISSING NEAR NR 4 PYLON. FABRICATED NEW BRACKET AND INSTALLED BRACKET AND ANCHOR NUT IAW SRM 51-30-02.SDR P5CA9600642Bracket · crackedLEFT WING NR 2 DIAGONAL FITTING BRACKET AT RIGHT SIDE IS CRACKED. FABRICATED NEW BRACKET AND INSTALLED AS PER SRM 51-20-01 AND 51-30-02.SDR P5CA9600641Skin · corrodedFOUND LEVEL ONE CORROSION ON UPPER SKIN NEAR FRONT SPAR AT ROOT AREA, WING TO FUSELAGE STA WS 294.62. CORROSION REMOVED AND TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01.SDR P5CA9600640Skin · corrodedFOUND LEVEL ONE CORROSION ON UPPER WING SKIN STA 580 IN MID SPAR AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01. TREATED AREA IAW SRM 51-10-02.SDR P5CA9600639Skin · corrodedFOUND SWELLING ON UPPER WING WS 1230 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 57-30-01.SDR P5CA9600638Skin · corrodedFOUND SWELLING ON UPPER WING AT WS 1020 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09.SDR P5CA9600637Skin · corrodedFOUND SWELLING ON UPPER WING SKIN WS 800 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09.SDR P5CA9600636Skin · corrodedFOUND SWELLING ON UPPER WING SKIN WS 750 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.SDR P5CA9600635Skin · corrodedFOUND SWELLING ON UPPER WING SKIN WS 1340 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION PER 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.SDR P5CA9600634Skin · corrodedFOUND SWELLING AND PROTRUDING RIVET ON UPPER WING SKIN, STA 1340 TO 1380 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.SDR P5CA9600633Skin · corrodedFOUND SWELLING ON UPPER WING SKIN STA WS 1270 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09.SDR P5CA9600632Panel · corrodedFOUND CORROSION ON UPPER SKIN LEFT WING AT STRINGER 3, ROOT AREA CONNECTION WING TO FUSELAGE, WS 353.02. LEVEL ONE CORROSION REMOVED AND AREA TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-10-01.SDR P5CA9600631Angle · crackedFOUND CRACK ON SUPPORT ANGLE AT WS 670 AT ATTACHMENT OF FRONT SPAR. NEW ANGLE INSTALLED PER SB 57-2159.SDR P5CA9600630Access Panel · crackedFOUND CRACKED ACCESS PANEL AND ATTACH ANGLE IN WING L/E TO INBOARD RIB IN NR 4 PYLON CAVITY. REPAIRED IAW SRM 51-40-03 AND SRM 51-40-02.SDR P5CA9600629Fitting · corrodedFOUND HYDRAULIC FITTINGS CORRODED IN WING NEAR ATTACHMENT TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-01.SDR P5CA9600628Rod · corrodedFOUND CORRODED ROD BEHIND HYDRAULIC TANK IN WING NEAR ATTACH TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03.SDR P5CA9600627Hyd Fitting · corrodedFOUND CORRODED HYDRAULIC FITTINGS IN WING BY NR 4 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03.SDR P5CA9600626Bracket · brokenFOUND BROKEN BRACKET AT BAY CUTOUT ABOVE PYLON NR 2. NEW BRACKET AND FASTENERS INSTALLED AS PER SRM 51-30-02.SDR P5CA9600610Spar · crackedFOUND CRACK ON UPPER CHORD AT STATION 669 NEAR THE FRONT SPAR. REMOVED AND REPLACED CHORD IAW SB 57-2273.SDR P5CA9600609Support · corrodedFOUND CORROSION ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 840 BETWEEN AREA LBL 15 TO RBL 30 AND SHEARED RIVET AT AREA. REMOVED LEVEL ONE CORROSION FROM FAIRING SUPPORT IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600608Stringer · corrodedFOUND CORROSION ON STRINGER 51 BETWEEN STA 1940 TO 1960 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600607Tie Clips · corrodedFOUND CORROSION ON TIE CLIPS STATION 1940 RT SIDE AT STRINGERS 28, 29, 30, 31, 32. REMOVED LEVEL ONE CORROSION AND TREATED IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600606Stringer · corrodedFOUND CORROSION ON STRINGER 42 BETWEEN STA 1980 TO 2000 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA AS PER SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600605Skin · corrodedFOUND SURFACE CORROSION ON LOWER FUSELAGE SKIN AT STA 2180 BETWEEN STR 46 RT TO 46 LT. REMOVED LEVEL ONE CORROSION FROM SKIN, TREATED AREA IAW SRM 51-10-01. CORROSION FOUND WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600604Skin · dentedFOUND DENTS, SCRATCHES AND CORROSION ON HEAD OF RIVETS AT FUS SKIN BETWEEN STA 720 TO 820, BETWEEN STRINGERS 26 TO 28 LT. STRAIGHTENED AND SMOOTHED PANEL, REMOVED LEVEL ONE CORROSION IAW SRM 51-10-01. CORROSION WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600603Bracket · chafedFOUND TRIANGLE BRACKET UNDER NR 2 PYLON AFT FAIRING CHAFED. INSTALLED NEW BRACKET WITH RIVET AS PER SRM 51-30-02.SDR P5CA9600602Panel · dentedFOUND DISTORTION ON PANEL AT FUS SKIN RT BETWEEN STA 540 AND 560 AND BETWEEN STRINGERS 35 TO 36. STRAIGHTENED AND SMOOTHED PANEL IAW SRM 51-40-01.SDR TWRA96264Wire · brokenDURING DAILY CHECK, FOUND EVAC LIGHT UPPER DECK NEAR FLOOR FORWARD OF CREW SLIDE IS INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M)SDR TWRA96202Bulb · failedDURING DAILY CHECK, FOUND EVAC OVERWING LEFT SIDE AND RIGHT SIDE. FIRST LIGHT FROM BOTTOM INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M)SDR TWRA96205Bulb · failedDURING DAILY CHECK, FOUND SEAT 45C EVAC LIGHT INOP. REPLACED BULB, OPS CHECK NORMAL PER MM 33-51-00. (M)SDR TWRA96204Connector · looseDURING DAILY CHECK, FOUND L1 MED UPPER BUSTLE EVAC LIGHT INOP. FOUND CANNON PLUG OFF OF BUSTLE. RECONNECTED, OPS CHECK NORMAL PER MM 33-51-00. (M)SDR TWRA96207Terminal · failedDURING DAILY CHECK, FOUND LEFT SIDE STATION 1600 EXTERIOR EMERGENCY LIGHTS INOP. REPLACED TERMINAL. OPS CHECK OK PER MM 33-51-00. (M)SDR TWRA96206Bulb · failedDURING DAILY CHECK, FOUND UPPER DECK CREW DOOR EXIT LIGHT OUT OF SERVICE. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M)SDR TWRA96191Wire · brokenDURING DAILY CHECK, FOUND 30ABC, 40ABC, 58ABC SEAT EVAC LIGHT INOP. REPAIRED BROKEN WIRE UNDER SEAT, OPS CHECK OK PR MM 33-51-00. (M)
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