Boeing 747-48EF
Service difficulty reports · 267
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 = '74748EF' 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 = '74748EF' 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 UIEA2010081700143Skin · delaminatedDURING WALK AROUND INSP AT MX, REPORTED RT NR 14 L/E KRUEGER FLAP EXTERNAL SKIN (EDGEBAND) - DELAMINATION MEASURING 0.4 INCH WIDTH AND 10 PERCENT OF EDGEBAND LENGTH (REF FIG 1). DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR IAW SRM 51-70-02-1A FIG 101 SSDR UIEA2010070900097Skin · dentedDURING SPECIAL CHECK INSP BEING PERFORMED; DAMAGE WAS FOUND TO THE RT WING - INBD & OTBD T/E MID & AFT FLAPS WITH DENT/DELAMINATION AREAS AS DESCRIBED BELOW: RT WING INBD T/E MID FLAP INBD L/E FAIRING DENT (REF N/CR 50072 AND FIG 1). RT WING OTBD T/E AFT FLAP SDR UIEA201000187Floorboard · damagedMX FOUND DAMAGE/DELAMINATION TO THE MAIN DECK - FLOORBOARDS BS 385 LBL 3.75 & BS 410 LBL 4.0 (REFERENCE FIG 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 25 FC AND PERMANESDR UIEA201000139Lens · crackedDMI 16202 LT TAIL NAV LIGHT CRACKED. INSP LT TAIL NAV LIGHT IAW EO4433 A023 FOUND SATIS, NO FURTHER DAMAGE. DMI REMAINS OPEN. AFTER RECEIVING PART, LENS REPLACED & FIC SATUS IAW MM 33-43-01 REV 67 DMI 16202. (CLOSED)SDR UIEA201000166Door · damagedDURING INSPECTION, BODY LANDING GEAR DOORS 8014 TALLY 116 FOUND DAMAGE AND CRACKS ON RT AND LT BODY GEAR WHEEL WELL INBD DOOR. REPAIR IN CONJUNCTION WITH ATTACHED ENGINEERING ADVISE/EMAIL. "STOP DRILLED CRACKS IAW SRM 52-80-02. FIG 101"SDR UIEA201000115Wedge · damagedLT WING INBD AFT FLAP LWR SURFACE T/E WEDGE FOUND HOLE AS MARKED. LTW AND INBD ALT FLAP LOWER SURFACE T/E WEIGHT REPAIRED IAW SRM 51-70-02. FIG 5 AND REF TO PROCESS CARD. CONTROL SEQ NO CHW 505020-1.SDR UIEA201000111Seat Track · damagedM/D BS 1780 - 1820 RBL 75 SEAT TRACK LIP FOUND CHIPPED AND WORN AT SEVERAL LOCATIONS. PERMANENT REPAIR WAS ACCOMPLISHED IAW 747-400 F SRM 53-00-52 FIGURE 201, REPAIR 8.SDR UIEA201000114Skin · damagedFX STA 1920 - S40R BODY SKIN FOUND SCRATCH MARK. FX STA 1920 S, 40R SCRATCH OVERLAPPING SKIN TRIMMED OFF. REPAIRED IAW SRM 53-00-01-2R-10, FIG 201, REPAIR 10 WITHOUT ZERO TIME.SDR UIEA201000113Attach Angle · crackedRT WING - T/E CAVITY FIXED PANEL (OTBD OF NR 12 SPOILER) OTBD ATTACH ANGLE CRACK AT AFT SECTION. RT WING T/E CAVITY UPER FIXED PANEL OTBD OF NR 12 SPOILER OTBD UPPER ATTACH CRACKED ANGLE REPAIRED IAW SRM 51-70-12, FIG 201 REPAIR 1.SDR UIEA201000112Web · crackedM/D STA 1220 TO 1220 BL R117 TO R117 WEB CRACKED. BS 1220 RBL 117 BELOW FLOOR. INTERCOSTAL CRACKED WEB REPARIED IAW SRM 51-70-13. FIG 201, REPAIR 1.SDR UIEA201000110Doubler · crackedLT DOOR UPPER HINGE DOUBLER FOUND CRACK. LT NR 1 DOOR UPPER HINGE AREA CRACKED SKIN AND DOUBLER REPAIRED IAW MSG 2HKA-TLS-09-0009-01C.SDR UIEA201000169Support Angle · crackedDURING OFF LOADING DAMAGE TO THE MDSCD BS 1920 SUPPORT ANGLE FOUND TO BE CRACKED (REF. FIGURE 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY 10FC AND PERMANENT REPAIR ATSDR UIEA201000170Floor Support · corrodedCORROSION AT UPPER DECK GALLEY FLOOR FWD. OTBD SUPPORT FITTING WITH CORROSOIN DAMAGE. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND PERMANENT REPAIR AT THE NEXT CSDR UIEA201000167Fairing · damagedDURING WALKAROUND INSPECTION DAMAGE WAS FOUND TO THE LT WING TO BODY FAIRING 191AHL MEASURING APPROX 12.0 IN X 12.0 IN. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 44SDR UIEA201000168Panel · damagedDURING DAILY CHECK INSPECTION, A 6.0" X 6.0" PORTION OF PANEL 65B15964-267 WAS FOUND MISSING. THE -267 PANEL IS PART OF THE LT WING GEAR WBL 235 LG BEAM TO REAR SPAR LWR IST - IN ADDITION, THE PANEL SUPPORT STRUCTION SHIFTED (BENT) OB 1.0 INN. NDT HFEC INSP ACSDR UIE2008F00013Skin · crackedFOUND FIBERGLASS SKIN PANEL 293CL CRACKED. REPAIRED IAW SRM 53-00-70 AND SRM 51-70-07. (K)SDR UIE2008F00012Skin · crackedFOUND FIBERGLASS SKIN PANEL 294CR CRACKED. REPAIRED IAW SRM. (K)
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