Boeing 747-269B
Service difficulty reports · 160
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 = '747269B' 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 = '747269B' 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 CKSA97210Skin · wrinkledDURING HARD LANDING INSPECT, FOUND LT FUSELAGE PANEL 2F FROM STA 1740 TO APPROX STA 1840 STR 40 TO STR 46 HAS WRINKLED SKIN. SKIN WAS REMOVED AND REPLACED PER BOEING MSG CKF-010-97-0036RE. REPLACEMENT SKIN WAS MADE FROM 2 PIECES .063 INCH THICKNESS 2024-T3 ALSDR CKSA97209Skin · wrinkledDURING HARD LANDING INSPECT, FOUND CHECK LIMITS ON LEFT FUSELAGE SKIN WRINKLES STA 1840 TO STA 1961 STRINGER 40 TO STRINGER 46 PANEL MARKED 2F. SKIN WAS REMOVED AND REPLACED PER BOEING MSG CKF-ORD-97-0036RE. REPLACEMENT SKIN WAS MADE FROM 2 PIECES .063 INCH SDR CKSA97208Web · crackedDURING C-2 CHECK INSPECTION, FOUND NAC WEB AT NAC WL 181.6, NAC STA 246 AT DUCT ATTACH HOLE HAS SEVERAL CRACKS ON EDGE OF HOLE. REPAIRED WEB AS PER AIA ENGINEERING DRAWING AIA/E/2555. C-CHECK WORK CARD NUMBER 7TK7198. NON-ROUTINE TASK CARD NR 102153.SDR CKSA97207Skin · wrinkledDURING HARD LANDING INSPECTION, FOUND RIGHT FUSELAGE SKIN PANEL FROM STA 1480 TO STA 1740 STRINGER 34 TO STRINGER 40 HAS WRINKLED SKIN. INSTALLED NEW SKIN FROM STA 1480 THRU STA 1741 STRINGER 43R THRU STRINGER 40R IAW B747 DRAWING 65B04132-2 REV H WITH THE EXSDR CKSA97206Skin · wrinkledDURING HARD LANDING INSPECT, FOUND RT FUS SKIN PNL FROM STA 1600 TO STA 1740 STR 40 THRU STR 46 HAS WRINKLED SKIN. INSTALLED NEW SKIN FROM STA 1630 THRU STA 1741 STR 40R THRU STR 46R IAW B747 DWG 65B04133-2 REV. G WITH EXCEPTION OF ALL REMOVED EXISTING HI-LOKSDR CKSA97205Skin · wrinkledDURING HARD LANDING INSPECT, FOUND LEFT FUSELAGE SKIN PANEL FROM FS1600 TO FS1740 HAS WRINKLED SKIN STR 40L TO STR 46L. INSTALLED NEW SKIN FROM STA 1630 THRU STA 1741 STR 40L THRU STR 46L IAW B747 DWG 65B04133-1 REV. G WITH EXCEPTION OF ALL REMOVED EXISTING FSDR CKSA97204Skin · wrinkledDURING HARD LANDING INSPECT, FOUND LT FUSELAGE SKIN WRINKLED AT STA 1480 TO STA 1740 STR 34 TO STR 40, SKIN PANEL MARKED 1F. INSTALLED NEW SKIN FROM STA 1480 - STA 1741 STRINGER 34L THRU STRINGER 40L IAW B747 DEG 65B04132-1 REV H WITH THE EXCEPTION OF ALL REMSDR CKSA97203Skin · corrodedDURING C-2 CHECK INSPECTION, FOUND LEVEL 2 CORROSION BS 2436 BULGE IN SKIN. REMOVED CORRODED AREA OR SKIN AND REPAIRED IAW SRM 53-30-03 FIGURE 17 (7075-T6). C-CHECK WORK CARD NUMBER 7ES5249. NON-ROUTINE TASK CARD NUMBER 101882.SDR CKSA97202Trunnion Cap · corrodedDURING HARD LANDING INSPECT, FOUND RT BODY GEAR TRUNNION LOWER CAP CORRODED (SEVERE PITTING). REMOVED AND REPLACED CAP, TORQ SERV. TRUNNION CAP IN POSITION. CHECKED ALIGN, MEASURED BORE AND FACES. FOUND ALIGN, BORE AND FACE DIMENSIONS IN TOLERANCES WITH INBSDR CKSA97023Turbine · damagedNR 1 ENGINE STARTED LOOSING POWER RIGHT AFTER TAKEOFF. EPR AND N1 DROPPING EGT AT 800 DEGREES. TRIED RAPID RESTART, ENGINE WOULD NOT RUN. SHUTDOWN PER EMERGENCY CHECKLIST. WINDMILL TIME 1 HOUR 16 MINUTES OIL PRESSURE 10 PSI. NOTE: DUMPED FUEL DOWN TO 630
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