Boeing 747-212F
Service difficulty reports · 81
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 = '747212F' 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 = '747212F' 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 KCSA101172Stringer · crackedFWD PIT STA-660 STR-33R IS CRACKED .5 INCH.SDR KCSA101171Shear Web · corrodedFWD PIT STA-564 LBL-128 MAIN DECK FLOOR TO SKIN SHEAR WEB CORRODED.SDR KCSA101170Door · corrodedL-1 DOOR FWD LOWER CORNER INTERIOR HAS CORROSION.SDR KCSA101169Structure · corrodedL-1 DOOR FWD LOWER CORNER INTERIOR HAS CORROSION.SDR KCSA101168Stiffener · crackedSTIFFENER CRACKED .250 INCH AT STA 420 LBL 24 AFT SIDE OF FLOORBEAM.SDR KCSA101167Stiffener · crackedSTIFFENER CRACKED .5 INCH AT STA 420 LBL 16 AFT SIDE OF FLOORBEAM.SDR KCSA101165Seat Track · corrodedAFT PIT STA 1502 RBL 25 SEAT TRACK HAS CORROSION.SDR KCSA101159Fireshield · wornNR 1 PYLON O/B FIRESHIELD STRIP WORN AFT OF HALFMOON AT STA 242.SDR KCSA101158Fireshield · wornNR 1 PYLON I/B FIRESHIELD STRIP WORN AFT OF HALFMOON CUTOUT AT NAC STA 242.SDR KCSA101157Fireshield · tornNR 1 PYLON I/B FIRESHIELD STRIP TORN .5 INCH JUST FWD OF HALFMOON CUTOUT NAC STA 235.SDR UPS07450566Reveal · crackedINSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT REVEAL CRACKED AT LATCH CAM FTG, CRACK LENGTH 3/8" APPROX. M/D L1 DOOR FWD CUTOUT REVEAL PANEL REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR NWAA071696744Skin · crackedDURING "M" CHECK, FOUND CRACKS IN NR 4 PYLON SKIN AND STIFFENER AT NAC STA 218 AND ACCESS PANEL 483CL CUTOUT. REPAIRED PER EA 67-209238.SDR NWAA071706744Frame · crackedDURING "M" CHECK, FOUND CRACKS IN NR 3 PYLON FRAME AND STIFFENER AT NAC STA 210 AND CUT OUT SKIN AT ACCESS PANEL 473 CL. REPAIRED PER EA 67-209239.SDR NWAA071556744Frame · crackedDURING "M" CHECK, FOUND CRACK IN FRAME AT BS 2120 S25R AND S26R. REPAIRED PER EA 67-208996.SDR NWAA071666744Tension Tie · deformedDURING "M" CHECK, FOUND TENSION TIE FORWARD CHANNEL DEFORMED AT BS 900 RT. REPAIRED PER EA 67-208991.SDR NWAA071676744Tension Tie · crackedDURING "M" CHECK, FOUND CRACKS IN TENSION TIE CHANNEL FASTENER HOLES AT BS 880 LT AND RT. REPAIRED PER EA 67-208995.SDR NWAA071686744Floorbeam · corrodedDURING "M" CHECK, FOUND CORROSION ON UPPER DECK FLOORBEAM UPPER CHORD BS 440 LBL 76. REPAIRED PER EA 67-209236.SDR NWAA071646744Tension Tie · crackedDURING "M" CHECK FOUND CRACKS IN TENSION TIE FORWARD AND AFT CHANNEL FASTENER HOLES AT BS 800 LT AND RT. REPAIRED PER EA 67-208990.SDR NWAA071546744Frame · crackedDURING "M" CHECK, FOUND CRACKS IN FRAME FASTENER HOLES AT TENSION TIE AREA BS 820 LT AND RT. REPAIRED PER EA 67-208989.SDR NWAA071536744Frame · crackedDURING "M" CHECK FOUND CRACKS IN FASTENER HOLE FRAME WEB TENSION TIE AREA AT BS 840 LT AND RT. REPAIRED PER EA 67-208992.SDR NWAA071656744Tension Tie · crackedDURING "M" CHECK, FOUND CRACKS IN TENSION TIE CHANNEL FASTENER HOLES AT BS 860 LT. REPAIRED PER EA 67-208993.SDR NWAA071526744Floorbeam · damagedDURING "M" CHECK, FOUND SHORT EDGE MARGIN ON UPPER DECK FLOORBEAM REINFORCEMENT STRAPS AT BS 380 RT AND LT. ALSO, FOUND CRACK IN FLOORBEAM CHORD FASTENER HOLE AT BS 380 RBL 74. REPAIRED PER EA 67-208994.SDR 0501196744Hose · failedAFTER TAKEOFF, HAD A TOTAL LOSS OF NR 4 HYDRAULIC SYSTEM. COM WAS FOLLOWED, AN EMERGENCY WAS DECLARED WITH ATC AND RETURNED TO SIN, LANDING WAS UNEVENTFUL. FOUND LEFT HAND WING GEAR ACTUATOR UP FLEX LINE BROKEN AND REPLACED. REPLACED (EDP) ENGINE DRIVEN HYDSDR 0300536744Web · crackedDuring "H" check found cracks in frame webs of #3 pylon rear engine mount bulkhead. Repaired per EA 67-165041.SDR 0300446744Web · crackedDuring "H" check found crack in four frame webs on #1 pylon. Repaired per EA 67-165045.SDR 0300316744Web · crackedDuring "H" check found cracks in two fastener holes #37 & #39 at right and left wing upper mid spar web between MSS 387.99 & 417.20. Repaired per EA 67-165047.SDR 0300346744Web · crackedDuring "H" check found cracks in #4 pylon rear engine mount outboard forward and aft frame webs. Repaired per EA 67-165042.SDR 0300336744Bulkhead · crackedDuring "H" check found crack in #4 pylon aft torque bulkhead chord at the top fastener hole common to the lower spar fitting. Repaired per EA 67-165046.SDR 0300546744Skin · crackedDuring "H" check found cracks in forward upper corner of aft cargo door cutout. Repaired per EA 67-165048.SDR 0202986744Actuator · malfunctionedDURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED WITH THE LANDING GEAR HANDLE IN THE OFF POSITION. RECYCLED LANDING GEAR AND LIGHT WENT OUT BUT FLICKED ON/OFF FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCSDR 0004476744Hyd Line · leakingDURING LANDING, AIRCRAFT LOST HYDRAULIC FLUID IN THE NBR 1 SYSTEM. AIRCRAFT WAS TOWED FROM RUNWAY WITHOUT INCIDENT. REPLACED THE AIR DRIVEN PUMP HYDRAULIC PRESSURE LINE. OPERATIONAL CHECK GOOD.\N\NMFGR: BOEING\NMODEL: 747212F
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