Boeing 747-249F
Service difficulty reports · 501
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 = '747249F' 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 = '747249F' 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 KCSA061211Stiffener · crackedNOSE WHEEL WELL, BS 370 LT SIDE BETWEEN WL 130 AND 140, LBL 10, 1 VERTICAL STIFFENER CRACKED.SDR KCSA061209Attach Angle · crackedAFT PIT BS 1780 RT PALLET SIDE RAIL ATTACH ANGLE CRACKED.SDR KCSA061208Floorbeam · corrodedUPPER DECK FLOORBEAM UPPER CHORD CORRODED AT BS 480, RBL3.SDR KCSA061207Seat Track · corrodedSEAT TRACK IS CORRODED AT STA 540 TO 560 RBL 27.99.SDR KCSA061206Skin Panel · corrodedLT HORIZ STAB UPPER SURFACE HAS CORROSION AT STAB STA 165.SDR KCSA061203Channel · crackedSTA 900 LEFT TENSION TIE FWD CHANNEL CRACKED AT STEEL U-CHANNEL ATTACH POINT.SDR KCSA061202Seat Track · damagedSTA 1940 TO 1960, LBL 11 SEAT TRACK SPLICE DAMAGED.SDR KCSA061201Stiffener · crackedLT NOSE WHEEL WELL SIDEWALL PANEL WEB STIFFENER CRACKED AT BS 265-280 WL 170.SDR KCSA061200Shear Tie · crackedFUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9L.SDR KCSA061199Shear Tie · crackedFUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 9R.SDR KCSA061198Shear Tie · crackedFUSELAGE FRAME SHEAR TIE CRACKED AT BS 440 BELOW STR 8R.SDR KCSA061197Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS 1000, RBL 51, WL 108, STR 43R.SDR KCSA061196Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS 1000, LBL 55, WL 109, STR 43L.SDR 0601636743Floorbeam · crackedDURING "H" CHECK FOUND CRACK IN UPPER DECK FLOORBEAM ATTACHMENT HOLE AT BS 380. REPAIRED PER EA 67-206280.SDR 0601616743Frame · crackedDURING H-CHECK FOUND CRACKS IN NR 1 PYLON REAR MOUNT BULKHEAD FRAMES. REPAIRED PER EA 67-206278.SDR 0601626743Channel · crackedDURING "H" CHECK AND ACCOMPLISHMENT OF EM 5310-01357-01A FOUND CRACK IN RT TENSION TIE FORWARD CHANNEL AT BS 820. REPAIRED PER EA 67-206276 SECTION I. SECTION II OF EA 67-206276 REQUIRES REPEAT INSPECTIONS TO BE PERFORMED AT INTERVALS NOT TO EXCEED 3000 CYCLESSDR 0601606743Frame · crackedDURING H-CHECK WHILE ACCOMPLISHING EM 5310-01351-01A FOUND CRACKS IN RT AND LT TENSION TIE AND FRAME AT BS 860. REPAIRED PER EA 67-206282 SECTION I AND II AND ESTABLISHED MONTIOR INSPECTION.SDR KCSA061124Light · failedRT EMERGENCY SLIDE LIGHT WILL NOT TEST.SDR P5CA0601454Line · crackedCREW REPORTED ON CLIMBOUT THROUGH FL 280, AIRCRAFT YAWED, NR 1 ENGINE SHUT DOWN. ATTEMPT TO RESTART UNSUCCESSFUL. DUMPED FUEL AND RETURNED TO PIK. FOUND SENSE LINE CRACKED AT REAR OF FUEL CONTROL. LINE REMOVED AND REPAIRED PER PRATT WHITNEY EM 72-09-7.SDR P5CA0601450Module · failedCREW REPORTED ON TAKEOFF ROLL, ANTI-SKID LIGHT CAME ON F/E PANEL, HAD R/F, R/R, L/F, AND L/R LIGHTS ON FOR R/H BODY GEAR. TAKEOFF ABORTED AT 60 KTS. REPLACED ANTI-SKID CONTROL MODULE PER MM 32-42-02, PERFORMED HIGH ENERGY STOP INSPECTION.SDR KCSA06014Seat Track · crackedCAPTAIN SEAT LEFT SEAT TRACK CRACKED 1.5 INCH AT STOP MOUNT. REPLACED LT AFT CAPT SEAT TRACK IAW AMM 25-11-01.SDR 06013Bulkhead · chafedREAR ENGINE MOUNT BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION, NAC STA 221.90. REMOVED REPAIR AREA FASTENERS AND DAMAGED MATERIAL IAW B747 SRM 54-14-03. FABRICATED 4 X 9 INCH DOUBLER IAW B747 SRM 54-14-13 FIG 16.SDR P5CA0601431Coupler · defectiveDURING APPROACH, CAPTAIN'S HSI AND F/O'S RMI FLAGS IN VIEW. REPLACED COMPASS COUPLER PER AMM 34-21-03. CHECKS OK.SDR P5CA0601430Coupler · failedCAPTAIN'S COMPASS SYSTEM HAS TO BE SLAVED EVERY 10 MINUTES. APPEARS THE COMPASS FLUX VALVE IS INOP. REMOVED AND REPLACED NR 1 COMPASS COUPLER AS PER MM 34-21-03. OPS CHECK OK.SDR KCSA061556Light · inoperativeLEFT UPPER DECK EMERGENCY LIGHT INOP.SDR P5CA0501409Starter · failedAFTER PUSH BACK, CREW REPORTED NR 3 ENGINE WOULD NOT START. PARAMETERS INDICATE NORMAL, NR N1 OR N2 INDICATION. REPLACED STARTER IAW MM 80-10-00. OPS NORMAL.SDR P5CA0501405Skin · corrodedLEFT WING LOWER SKIN CORROSION ON OUTBOARD JACK PAD AREA AT FSS 1295. REPAIR CARRIED OUT IAW BOEING FAA FORM 8100-9. SUPPLEMENTARY JOB CARDS AFM 0147 AND AFM 1068 FOR DETAILS.SDR P5CA0501403Beam · crackedFWD CARGO, FOUND CRACKS PROPAGATED FROM BLANKET HOLE AT STA 300 AND 320 AND LT NOSE WHEEL WELL VERTICAL BEAM WEB AT WL 160. REPAIR CARRIED OUT IAW LO-BY714-072 INTERIM WEB REPAIR. CONTINUE INSPECTION PER SB 747-53A2293.SDR P5CA0501374Yaw Damper · malfunctionedRUDDER WOULD NOT DEFLECT. REPLACED UPPER AND LOWER YAW DAMPER COMPUTERS PER AMM 22-16-02.SDR P5CA0501349Actuator · malfunctionedCREW RETURNED AIRCRAFT TO BLOCKS ADVISING ELEVATORS WERE STIFF DURING FLIGHT CONTROL CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER MM 27-31-17. OPS CHECK PER MM 27-31-14, NO DISCREPANCIES NOTED.SDR 0500556743Doubler · crackedDURING "L" CHECK, FOUND THREE CRACKED FASTENER HOLES ON DOUBLER AROUND APU PRESSURE PANEL CUTOUT AT BS 2360. REPAIRED PER EA 165204.SDR 0500566743Fitting · crackedDURING L-CHECK, FOUND CRACK AND CORROSION AT BS 1480 BULKHEAD CAP FITTING LOWER FLANGE SURFACE BETWEEN S36L AND S40L. REPAIRED PER EA 67-165203.SDR 0500576743Frame · crackedDURING L-CHECK, FOUND CRACK IN FRAME AT BS 380 S24R. REPAIRED PER EA 67-165195.SDR PCAO501328Pump · malfunctionedCREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL PUMP. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01.SDR P5CAO501327Fuel Control · malfunctionedCREW REPORTED NR 4 ENGINE WOULD NOT MAKE TAKEOFF POWER. ENGINE COULD ONLY MAKE 1.24 EPR. REPLACED FUEL CONTROL. PERFORMED TRIM RUN, ALL NORMAL PER 73-21-01 AND 73-11-01.SDR P5CA0501315Valve · leakingDURING WALKAROUND OBSERVED FUEL LEAKING FROM RIGHT FUEL JETTISON MANIFOLD. REMOVED AND REPLACED RIGHT FUEL JETTISON NOZZLE VALVE PER BOEING MM 28-31-03. OPS CHECK OK.SDR P5CA0501305Line · chafedNR 3 ENG OIL PRESS FLUCTUATES FROM 35 TO 45 PSI. ENG OIL PRESS LIGHT BLINKS ON & OFF. ALSO OIL QTY WENT FROM 3/4 TO 1/4 AND BACK TO 1/2. FOUND UPPER ENGINE OIL LINE AT OIL FILTER HOUSING CHAFED. REPLACED CHAFED LINE, COI ISSUED/ AMM 20-11-18.SDR 0500086743Window · failedDURING FLIGHT, HEATING ELEMENT ON WINDOW 1L OVERHEATED AND SMOKED. WINDOW HEAT WAS TURNED OFF AND SMOKE STOPPED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. WINDOW WAS MEL'D AND LATER REPLACED 19JAN05 IN SIN. OPERATIONAL CHECK GOOD.SDR P5CA0501304Actuator · failedWHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND DOWN LOCK ACTUATOR FAILED. REPLACED ACTUATOR PER MM 32-33-15.SDR P5CA0501303Actuator · failedWHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND EXTEND/RETRACT ACTUATOR FAILED. REPLACED EXTERNAL/RETRACT ACTUATOR PER MM 32-33-01.SDR P5CA0501302Actuator · leakingWHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYD SYSTEM. LANDING WAS NORMAL. FOUND LEFT BODY GEAR LEVELING CYLINDER FAILED. REPLACED PER MM-13-15.SDR P5CA0401274Engine · failedON TAKEOFF TOWER REPORTED SPARKS FROM NR 1 ENGINE DURING CLIMB.EGT HIGH (600 DEGREE) AS COMPARED TO OTHER ENGINES.N1 90% N2 94%, EXPERIENCED COMPRESSOR STALL AT FL 250 WHILE CDLIMBING TO FL 350. ENGINE REPLACED PER POLAR WORK CARD M71-00-02.SDR P55CA0401273Actuator · malfunctionedIN CLIMB AT 9200 FT, NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASHES OF LIGHT FROM LT SIDE. WIND MILL TIME 50 MINUTES, OIL PRESSURE 5 PSI, N1 22 PERCENT N2 18 PERCENT, FIRE SWITCHED PULLED & NR 1 EDP SUPPLY OFF. REVIEWED SDR P5CA0401277Engine · malfunctionedIN CLIMB AT 9200 FT NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASH OF LIGHT FROM LEFT SIDE OF A/C, WINDMILL TIME 50 MINUTES,MINIMUM OIL PRESSURE 5 PSI. REVIEWED EXCEDANCE,FOUND WITH IN LIMITS.VISUAL INSPECTION ACCOMPLISHEDSDR P5CA0401272Valve · failedNR 4 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. NR 4 ENGINE START VALVE MANUAL OPS OK DEFERRED PER DDPG 80-2.SDR P5CA0401271Start Valve · failedNR 3 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. REPLACED START VALVE NR 3 ENGINE, AMM 80-11-04, OPS CHECK OK.SDR P5CA0401270Fuel Sys · leakingA/C RETURN TO BLOCK DUE TO FUEL GOING OVERBOARD FROM RIGHT WING VENT BOX. DRAINED SURGE TANK, CHECKED FUELING SYSTEM PER AMM 28-21-00, CHECKS NORMAL WITH ALL PUMPS RUNNING & FUELING DUCTS PRESSURIZED.SDR P5CA0401267Connector · dirtyFUEL CONDITION ACTUATOR NR 1 ENGINE CIRCUIT BREAKER POPPED ON ENGINE START. REMOVED, CLEANED & REINSTALLED CONNECTOR AT J14-P, PERFORMED SYSTEM CHECK, GOOD PER AMM 76-11-00.SDR P5CA0401264Generator · malfunctionedNR 1 ENGINE GENERATOR FEEDER FAULT. REMOVED AND REPLACED NR 1 ENGINE GENERATOR PER AMM 24-21-01, SYSTEM OPS CHECK OK.SDR P5CA0401265Generator · failedNR 2 ENGINE GENRATOR WILL NOT COME ON LINE. REMOVED AND REPLACED NR 2 ENGINE GENERATOR, OPS CHECK OK PER AMM 24-21-01.
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