Boeing 747-132
Service difficulty reports · 1,451
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 = '747132' 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 = '747132' 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 P5CA9800097Reveal · crackedL4 DOOR FWD CUTOUT UPPER CORNER REVEAL CRACKED 2 PLACES. REPAIRED PER HAECO REPAIR SCHEME R-53-61-33667.SDR P5CA9800096Bulkhead · crackedNR 2 PYLON BULKHEAD RT TOP CORNER FILLET PLATE FASTENER HOLES 2 EA CRACKED. DOUBLER REPAIRED PER REPAIR SCHEME 54-51-33638 AND SB.SDR P5CA9800095Frame · crackedFRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 1760 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33626 AND BOEING TELEX.SDR P5CA9800094Frame · crackedFRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 2040 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33627 AND BOEING TELEX.SDR P5CA9800093Shear Tie · crackedFRAME SHEAR TIE CRACKED AT BS 880 LEFT STRINGERS 10 TO 11. REPAIRED PER REPAIR SCHEME 53-22-33669 AND BOEING TELEX.SDR P5CA9800092Frame · crackedFRAME CRACKED AT STRINGER CUTOUT DOUBLER. REPAIRED PER REPAIR SCHEME RS 53-22-33668 REF BOEING TELEX NR PAO HKG 98-0036RE.SDR P5CA9800091Tie Clip · crackedSTRINGER TIE CLIP AT BS 2180 STRINGER 12 FOUND CRACKED. REPLACED CLIP PER SRM 51-10-01.SDR P5CA9800090Frame · crackedFRAME AT BS 2060 STRINGER 15 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33628.SDR P5CA9800089Frame · crackedFRAME AT BS 2080 STR 25 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33629.SDR P5CA9800035Floorbeam · crackedAFT PIT STA 1800 FLOORBEAM FLANGE CRACKED AT RT END APPROX RBL 50. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-10-01. FABRICATED NEW FLOORBEAM IAW SRM 51-30-02.SDR P5CA9800034Fan Blade · crackNR 3 ENGINE, NR 5 FAN BLADE HAS A CRACK AT L/E. REMOVED CRACK BY BLENDING IAW MM 72-31-02.SDR P5CA9800033Rivet · failedKEEL BEAM AREA, BS 1300 RIVET HEAD POPPED OFF. REMOVED AND REPLACED FASTENER IAW SRM 51-30-02.SDR P5CA9800010Inertial Nav Sys · failedNR 1 INS FAILED. THIS A/C EQUIPED WITH ONLY 2 INS SYSTEMS. A/C RETURNED TO AMS. REPLACED NR 1 INU IAW MM 34-41-07. NIL MALFUNCTION CODES FINE ALIGNMENT C/W.SDR P5CA9800088Stringer · crackedSTRINGER 23 AT BS 740 CRACKED. REPLACED STRINGER PER SRM 51-10-01.SDR EIAA970202Line · leakingANC - LOG PAGE: F47048 - 2.5 HOURS INTO FLIGHT, NR 1 ENGINE OIL QTY WAS DOWN TO 1/2 ON THE GAUGE. REMOVED EXHAUST PLUG AND FOUND TRACE OF OIL AROUND PRESSURE LINE TO NR 6 BEARING COMPARTMENT. REMOVED HEAT SHIELD FROM PRESSURE AND SCAVENGE LINE, TIGHTENED LISDR P5CA9701815Seal · misinstalledENGINE SHUT DOWN AT 21,000 FEET DUE TO LOSS OF NR 1 ENGINE OIL QUANTITY AND LOSS OF OIL PRESSURE WITH INCREASE IN OIL TEMPERATURE OF APPROXIMATELY 25 DEGREES. FOUND NR 1 ENGINE DRIVEN PUMP DEACTIVATED WITH KIT. DRIVE SEAL LINE IN CASE NOT PROPERLY REMOVED ANSDR P5CA9701814Hyd Line · holeLOST NR 1 HYDRAULIC SYSTEM QUANTITY ON APPROACH. FOUND HOLE ON NR 1 AIR DRIVEN HYDRAULIC PUMP PRESSURE LINE REPLACED LINE AND LEAK CHECKED PRE BOEING M/M 29-11-00. DEACTIVATED NR 1 ENGINE DRIVEN PUMP PER MEL 29-1 DUE TO PUMP OPERATED WITH SUPPLY TO OFF POSITSDR P5CA9701810Plate · cracked2 INCH CRACK ON NR 4PYLON, OUTBD SIDE ABOVE AND FWD OF HALF MOON PLATE. REPAIRED PER MA 5430-06:01.SDR P5CA9701809Cowl · damagedDAMAGE TO NR 4 ENGINE NOSE COWL AT 9 O'CLOCK POSITION. REPAIRED PER SRM 51-70-00.SDR P5CA9701822Canoe · holeHOLE IN NR 2 CANOE FWD RT SIDE. SANDED DOWN AREA, FILLED HOLE WITH AERODYNAMIC FILLER, SANDED DOWN AND APPLIED FIBERGLASS OVERLAY AS PER SRM 51-40-07.SDR P5CA9701821Mounting Ring · corrodedCORRODED AND BUCKLED MOUNTING RING, LOW RANGE ALT. BLENDED OUT CORROSION AND REWORKED MOUNTING RING.SDR EIAA970199Fuel Filter · contaminatedHKG - LOG PAGE: F47136 - UNSCHEDULED THRUST LOSS OF THROTTLE MOVEMENT DURING DESCENT. PERFORMED ENGINE SHUT DOWN. INSPECTED ENGINE, FOUND FUEL FILTER CONTAMINATED, REPLACED FUEL FILTER PER MM 73-11-02. LEAK CHECKED GOOD, PERFORMED ENGINE RUN. (X)SDR EIAA970196Actuator · failedCAPTAIN'S SEAT SLIDES AFT WHEN RUDDER PEDAL FORCE EXERTED. REMOVED AND REPLACED CAPTAIN'S HORIZONTAL SEAT MOTOR IAW OHM 25-10-00 PAGE 509. (X)SDR P5CA9701593Shaft · shearedSHEARED NOSE LANDING GEAR DOOR GROUND OPERATING HANDLE SHAFT. REPLACED SHAFT PER BOEING MAINTENANCE MANUAL 32-34-07 OPERATIONAL CHECK NORMAL.SDR P5CA9701592Engine · flamed outAFTER TAKEOFF APPROXIMATELY 400 FT AGL, NR 2 ENGINE FLAMED OUT. ENACTED INFLIGHT RESTART PROCEDURES. ENGINE RESTARTED NORMALLY AND RETURNED TO BFM AND LANDED UNEVENTFULLY. CHECKED PT3 AND PS3 WATER TRAPS AND FOUND CLEAN PER M/M 75-31-01 AND CHECKED FUEL CONSDR P5CA9701590Fuse Pin · corrodedLEVEL 2 CORROSION ON NR 4 PYLON OUTBOARD FUSE PIN INSERT. REPLACED FUSE PIN PER BAC MM 54-10-03.SDR P5CA9701589Panel · delaminatedDELAMINATION ON LEFT WING NR 2 SPOILER. REPLACED SPOILER PANEL PER BAC MM 27-61-02.SDR P5CA9701588Panel · delaminatedDELAMINATION ON RIGHT WING LEADING EDGE PANEL BETWEEN ENGINES 3 AND 4. REMOVED DAMAGE AND REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.SDR P5CA9701587Frame · crackedCRACK ON LEFT SIDE OF NR 3 PYLON INTERIOR FRAME. REPLACED FRAME PER BAC SRM 51-10-01.SDR P5CA9701586Frame · crackedCRACK ON RIGHT SIDE OF NR 3 PYLON INTERIOR FRAME. REPLACED FRAME PER BAC SRM 51-10-01.SDR P5CA9701585Fitting · crackedCRACKS AND LEVEL 2 CORROSION ON OUTBOARD END FITTING OF LEFT WING LANDING GEAR SUPPORT BEAM PER ULTRASONIC INSPECTION. REPLACED END FITTING PER BAC MM 57-15-01.SDR P5CA9701584Clip · crackedCRACKED ATTACH CLIP FORWARD OF DIAGONAL LINK ON NR 2 PYLON. REPLACED DAMAGED ATTACH CLIP PER BAC SRM 51-10-01.SDR P5CA9701583Flange · crackedCRACK ON NR 1 ENGINE TURBINE EXHAUST CASE S-FLANGE AT 1:30 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701582Flange · crackedCRACK ON NR 1 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 6:00 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701581Flange · crackedCRACK ON NR 2 ENGINE TURBINE EXHAUST CASE S-FLANGE AT 2 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701580Flange · crackedCRACK ON NR 2 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 2 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701579Flange · crackedCRACK ON NR 2 ENGINE TURBINE EXHAUST CASE R-FLANGE AT 6:30 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701578Flange · crackedCRACK ON NR 4 ENGINE TURBINE EXHAUST CASE FLANGE (RAIL) AT 7 O'CLOCK. WELD REPAIR AND STRESS RELIEF PER PWA MM 72-53-01.SDR P5CA9701577Panel · delaminatedDELAMINATION ON PANEL NR 474AR ON NR 3 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.SDR P5CA9701576Panel · delaminatedDELAMINATION ON PANEL NR 484AR ON NR 4 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.SDR P5CA9701575Panel · puncturedPUNCTURE ON PANEL NR 474AL ON NR 3 PYLON. POTTED CORE AND APPLIED A DOUBLER PER BAC SRM 51-40-06.SDR P5CA9701574Panel · puncturedPUNCTURE ON PANEL NR 484 ON NR 4 PYLON. REPAIRED PUNCTURE PER BAC SRM 51-40-06.SDR P5CA9701573Panel · puncturedTWO PUNCTURES ON NR 3 PYLON PANEL NR 474AR. POTTED CORE AND APPLIED DOUBLER PER BAC SRM 51-40-06.SDR P5CA9701572Access Panel · crackedCRACKS AROUND TWO FASTENER HOLES ON AILERON POWER PACKAGE ACCESS PANEL ON LEFT WING. REPAIRED PANEL PER BAC SRM 51-10-02.SDR P5CA9701571Skin · delaminatedDELAMINATION ON THE LEFT HORIZONTAL STABILIZER TRAILING EDGE ADJACENT TO THE NAVIGATION LIGHT. REMOVED DELAMINATION, POTTED CORE AND INSTALLED AND BONDED FIBERGLASS OVERLAYS PER BAC SRM 51-40-14.SDR P5CA9701570Panel · crackedCRACK ON PANEL NR 462EL ON NR 2 PYLON. FABRICATED AND INSTALL REPLACEMENT PANEL PER BAC SRM 51-30-02.SDR P5CA9701569Exhaust Cone · crackedCRACKED NR 2 ENGINE EXHAUST PLUG END CAP. WELD REPAIRED PER BAC MM 78-11-04 AND INSPECTED PER BAC SOPM 20-20-02.SDR P5CA9701568Fairing · gougedGOUGED NR 8 FLAP TRACK FAIRING (CANOE) ON RIGHT WING. REPAIRED USING FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.SDR P5CA9701567Skin · crackedCRACKED RIGHT OUTBOARD FOREFLAP LEADING EDGE. REPAIRED USING FIBERGLASS FILLERS AND OVERLAYS PER BAC SRM 51-40-09.SDR P5CA9701566Skin · corrosionLEVEL 1 CORROSION ON RIGHT WING UPPER SKIN AT FRONT SPAR APPROXIMATELY 9 FEET INBOARD OF WING TIP. BLENDED OUT CORROSION PER BAC SRM 57-30-01, MATERIAL REMOVED WITHIN SRM LIMITS.
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