Boeing 747-122
Service difficulty reports · 2,143
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 = '747122' 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 = '747122' 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 P5CA9600380False Spar · corrodedRT FALSE SPAR FORWARD SIDE FROM WING GEAR TRUNNION ATTACH I/B TO END HAS BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02.SDR P5CA9600376Mount Bracket · crackedNR 3 ENGINE CLAMP MOUNTING BRACKET IS CRACKED FOUR INCHES FORWARD OF R-RAIL AT 6 O'CLOCK POSITION. FABRICATED NEW BRACKET AND INSTALLED IAW MM 70-50-00.SDR P5CA9600374Le Fairing · delaminatedALL EIGHT FLAP TRACK FIXED L/E FAIRINGS HAVE HEAVY EROSION AT FORWARD END WITH SEVERAL AREAS DELAMINATED AND CRACKED. REPAIRED DELAMINATION WITH FIBERGLASS OVERLAYS AND REPAIRED EROSION IAW SRM 51-40-09 AND 51-40-11.SDR P5CA9600373Air Duct · crackedNR 2 ENGINE INBOARD CORE COWL LOWER FORWARD AIR DUCT IS CRACKED. WELDED AND REINSTALLED IAW SRM 51-30-02.SDR P5CA9600372Support Plate · crackedNR 2 ENGINE OUTBOARD CORE COWL, LOWER FORWARD CORNER SUPPORT PLATE IS CRACKED IN THE LIGHTENING HOLE. WELDED BRACKET AND REINSTALLED IAW SRM 51-30-02.SDR P5CA9600371S-Rail · crackedNR 2 ENGINE S-RAIL HAS A RADIAL CRACK AT THE 2 O'CLOCK POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01.SDR P5CA9600370S-Rail · crackedNR 4 ENGINE S-RAIL HAS A RADIAL CRACKED AT 1:30 POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01.SDR P5CA9600379Bracket · crackedNR 2 ENGINE AIR DUCT MOUNT ANGLE BRACKET IS CRACKED AT THE 6 O'CLOCK POSITION FORWARD OF MAIN GEARBOX. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-01.SDR P5CA9600377Tr Sleeve · corrodedNR 4 ENGINE HAS SURFACE CORROSION ON THRUST REVERSER SLEEVE AT RT UPPER JACKSCREW BARREL NUT HOLES. REMOVED LEVEL ONE CORROSION AND TREATED IAW SRM 51-10-01.SDR P5CA9600375Door · corrodedRIGHTHAND OUTBOARD BODY GEAR DOOR HAS LARGE AREA OF BARE METAL WITH SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-24-11, 51-10-01.SDR P5CA9600381Press Deck · corrodedNOSE WHEEL WELL UPPER PRESSURE DECK HAS NUMEROUS SPOTS OF BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02.SDR P5CA9600363Tire · blownNR 2 AND 3 MAIN TIRES FOUND BLOWN ON ARRIVAL. NR 1 MAIN TIRE HAD FLAT SPOT AND THERMAL RELIEF AT BLOCKS. NR 4 MAIN TIRE HAD FLAT SPOT BUT RETAINED AIR. REMOVED AND REPLACED NR 1, 2, 3, 4 WHEEL ASSEMBLIES IAW MM 32-45-01. REMOVED AND REPLACED NR 4 BRAKE ASSSDR P5CA9600359Fairing · punctureNR 4 FLAP TRACK CANOE FAIRING HAS PUNCTURE IN LOWER AFT END. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED REPAIR IAW SRM 51-40-15.SDR P5CA9600358Skin · puncturedLEFT WING OUTBOARD AFT FLAP UPPER SURFACE HAS SMALL PUNCTURE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED REPAIR IAW SRM 51-40-11 AND 51-40-15.SDR P5CA9600357Skin · delaminatedLEFT WING OUTBOARD FOREFLAP HAS PREVIOUS GOUGE AND DELAMINATION AT OUTBOARD LEADING EDGE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-15.SDR P5CA9600356Cove Panel · crackedLEFT WING OUTBOARD MIDFLAP TRAILING EDGE COVE PANEL CRACKED AT MIDPOINT. REMOVED DAMAGED PANEL AND CORE, FABRICATED CORE, FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-09 AND 51-40-12.SDR P5CA9600346Door · crackedRIGHT WING LANDING GEAR STRUT LOWER DOOR LEADING EDGE AREA CRACKED ALONG FAIRING ASSEMBLY. REPAIRED PER BOEING SRM 51-40-05.SDR P5CA9600345Pulley · brokenMAIN DECK TO UPPER DECK LADDER PULLEY BROKEN. REPLACED PULLEY I/A/W MAINTENANCE MANUAL 25-50-01.SDR P5CA9600344Angle · wornLEFT BODY GEAR STRUT DOOR OUTER AFT ANGLE WORN WITH A HOLE. REPLACED ANGLE PER BOEING SRM 51-30-02.SDR P5CA9600343Cowl · crackedNR 3 LEFT FAN COWL LOWER EDGE IS CRACKED BETWEEN THE AFT AND MIDDLE U-BOLTS. REPAIRED CRACK PER BOEING SRM 51-40-06.SDR P5CA9600342Panel · crackedNR 4 ENGINE PYLON LOWER EDGE PANEL CRACKED. REMOVED FABRICATED AND INSTALLED PANEL PER BOEING SRM 51-10-01.SDR P5CA9600341Channel · bentNR 1 ENGINE OUTBOARD CORE COWL LOWER EDGE CHANNEL VERY BENT, WITH PULLED RIVETS AND LOST DOUBLERS. REMOVED FABRICATED AND INSTALLED CHANNEL PER BOEING SRM 51-40-03.SDR P5CA9600340Fairing · delaminatedDELAMINATED BODY FAIRING PANEL LOCATED BETWEEN LEADING EDGE OF MAIN LANDING GEAR CENTER DOORS. REPLACED PANEL PER BOEING SRM 51-30-02 AND 51-24-11.SDR P5CA9600338Angle · crackedNR 1 OUTBOARD CORE COWL HAS CRACKED REPAIR ANGLE INSIDE TO EDGE AT BEND. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING SRM 51-30-02 AND 51-10-01.SDR P5CA9600337Skin · crackedNR 1 ENGINE INBOARD FAN COWL, TOP FORWARD HINGE HAS CRACK IN SKIN TOP SURFACE. WORKED AND BLENDED OUT CRACK IAW BOEING SRM 51-10-06, TREATED AND PRIMED IAW SRM 51-40-02.SDR P5CA9600336Bracket · crackedHORIZONTAL ANGLE CRACKED ON VERTICAL BEAM RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL BS 320. REMOVED, FABRICATED AND INSTALLED ANGLE PER BOEING SRM 51-10-01, 51-10-02 AND 51-40-03.SDR P5CA9600335Skin · crackedLEFT BODY GEAR INBOARD DOOR LOWER INNER SKIN LEADING EDGE MID SECTION CRACKED AND DEFORMED. REPAIRED PER BOEING SRM 52-80-02.SDR P5CA9600334Skin · crackedNR 4 PYLON INBOARD SIDE LOWER SKIN FLANGE CRACKED. REMOVED, FABRICATED AND INSTALLED SKIN FLANGE IAW BOEING SRM 51-30-02 AND 54-12-01.SDR P5CA9600333Angle · crackedNR 4 ENGINE PYLON UPPER END OF SUPPORT ANGLE CRACKED IN RADIUS INBOARD AND OUTBOARD STATION 221.9 ABOVE AFT ENGINE MOUNT INSIDE PANEL. INSTALLED DOUBLERS IAW BOEING SRM 54-10-03 FIG 19.SDR P5CA9600332Cowl · tornNR 4 ENGINE CORE COWL FRONT LATCH AREA TORN AND DEFORMED. REMOVED, FABRICATED AND INSTALLED U-CHANNEL PER BOEING SRM 51-30-02 AND 51-10-01.SDR P5CA9600331Door Sill · crackedBULK CARGO DOOR SILL CRACKED 2 PLACES. WELD REPAIRED PER BAC59755905 USING TITANIUM TIG ROD, INSTALLED PER BOEING SRM 51-10-01.SDR P5CA9600330Angle Bracket · crackedNR 4 ENGINE PYLON, ANGLE BRACKET BENT AND CRACKED INBD AFT. REMOVED, FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51-32-01 AND 51-10-02.SDR P5CA9600329Bracket · crackedCRACKED SUPPORT BRACKET NR 4 PYLON, GENERATOR LEAD SUPPORT. REMOVED, FABRICATED AND REPLACED BRACKET PER BOEING SRM 51-30-02 AND 51-10-01.SDR P5CA9600328Seal Retainer · bentFWD LOWER CARGO COMPARTMENT CUTOUT SEAL RETAINER AFT EDG BENT AND DEFORMED. FABRICATED NEW SEAL RETAINER PER BOEING SRM 51-32-01, INSTALLED PER BOEING SRM 51-10-01.SDR P5CA9600349Panel · puncturedLEFT WING INBOARD MIDFLAP INBOARD UPPER STRESS PANEL PUNCTURED. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-06.SDR P5CA9600348Skin · wornRIGHT HAND INBOARD MIDFLAP TRAILING EDGE HAS EXPOSED HONEYCOMB. POTTED SMALL PUNCTURE, APPLIED FILLER AND OVERLAY IAW SRM 51-40-09.SDR P5CA9600327O-Rings · cutNR 1 HYDRAULIC SYSTEM FLUID LOSS AFTER TAKEOFF. LEAK STOPPED WHEN PUMPS SHUT OFF, SYSTEM QUANTITY STABLE AT 2.5 GALLONS. EXTENDED GEAR AND FLAPS BY ALTERNATE SYSTEM. UPON APPROACH TO MIAMI HAD BODY GEAR AND NOSE GEAR STEERING AVAILABLE FOR TAXI IN. FLUID LSDR P5CA9600354Fitting · crackedFOUND NR 4 PYLON FORWARD FAIRING OUTBOARD LATCH 'U' FITTING CRACKED. REMOVED AND REPLACED FORWARD FAIRING RETAINER FITTING IAW SRM 54-10-03 AND MM 54-32-01.SDR P5CA9600360Support · crackedNR 1 FLAP TRACK SEQUENCE TOGGLE ROLLER SUPPORT LINK CRACKED. REMOVED AND REPLACED SUPPORT LINK IAW MM 27-51-00.SDR P5CA9600355Panel · delaminatedRIGHT HAND INBOARD MIDFLAP TOP SURFACE CENTER PANEL HAS LARGE AREAS OF DELAMINATION. REMOVED PANEL AND INSTALLED NEW PANEL IAW SRM 51-10-01.SDR P5CA9600352Bogie Pin · pittedFOUND NR 7 FLAP TRACK BOGIE PINS PITTED. REMOVED AND REPLACED PINS IAW MM 27-51-04.SDR P5CA9600353Brace · crackedFOUND NR 4 MOVEABLE CANOE FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED BRACE IAW MM 27-51-00 AND MM 27-51-45.SDR P5CA9600351Channel · crackedNR 3 INBOARD CORE COWL LOWER EDGE CHANNEL CRACKED AND BENT. REMOVED CHANNEL, FABRICATED CHANNEL AND SPLICE AND INSTALLED IAW SRM 51-40-03.SDR P5CA9600350Cover · crackedNOSE GEAR STEERING CABLE HOUSING COVER CRACKED. SANDED OUT CRACK, COLD BOND PLY LAYUP BONDED AND SEALED IAW SRM 51-40-09.SDR P5CA9600302Overheat Sensor · bare wireDURING TAXI OUT, LEFT WING OVERHEAT LIGHT ILLUMINATED. RETURNED TO BLOCKS. FOUND NR 4 LED GROUP WITH AN AIR LEAK, REPLACED SEAL IAW MM 36-11-01. FOUND SENSOR NR 2 INBOARD OF NR 2 PYLON WITH A BARE WIRE. REPAIRED SAME IAW MM 26-18-02. L/E OVERHEAT SYSTEM CSDR P5CA9600301Attach Fitting · brokenON ARRIVAL, FOUND LEFT HAND BODY GEAR DOOR FOLLOW-UP ROD ATTACH FITTING BROKEN. REMOVED AND REPLACED FITTING IAW MM 32-14-01. INSPECTION REVEALED NO SIGN OF CORROSION. SUSPECT FATIGUE CRACK/WEAR OF BUSHINGS FOR ROD END BOLT.SDR P5CA9600361Stop Fitting · crackedAFT CARGO DOOR FRAME STRUCK BY PALLET AND DAMAGED DURING LOADING. FOUND WEB DAMAGE AT BS 1820 AT LOWER STOP FITTING, FITTING CRACKED. REPAIRED WEB AND FITTING IAW SRM 53-10-04.SDR P5CA9600248Press Module · crackedON ARRIVAL, FOUND HYDRAULIC LEAK FROM NR 3 HYDRAULIC SYSTEM IN SAILBOAT AREA. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODULE HOUSING CRACKED. REMOVED AND REPLACED SAME, OPS AND LEAK CHECK NORMAL IAW MM 29-11-23.SDR P5CA9600247Air Driven Pump · press fluxON TAXI OUT, NR 1 ADP INOP, PRESSURE FLUCTUATION 0 TO 2500 PSI, RETURNED TO BLOCKS. CLEANED FILTERS, RESET OVERSPEED SWITCH AND LUBED REGULATOR SHUTOFF VALVE AND OPERATIONAL CHECK GOOD IAW MM 29-11-05.SDR 96UAL900455Lamp · inoperativeNR 1 RIGHT OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP ASSY AND REPAIRED BROKEN GROUND WIRE.
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