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 P5CA9700221Trunnion · corrodedREMOVED LEFT WING LANDING GEAR OUTER CYLINDER AFT TRUNNION SLEEVE TO CONFIRM SERVICE BULLETIN 32-2190 MODIFICATION STATUS. FOUND AFT TRUNNION WITH DEEP PITTING CORROSION. REWORKED PER DOWTY WORK ORDER NR 101000-1-1 AND OVERHAUL MANUAL 32-11-41.SDR P5CA9700019Air Speed Ind · reads highAFTER APPLICATION ON TAKEOFF, THRUST FIRST OFFICERS AIRSPEED INDICATOR INDICATED 20 KNOTS FASTER THAN CAPTAINS, INCREASED TO 85 KNOTS THEN STUCK AT THAT INDICATION. ABORTED TAKEOFF. REPLACED FIRST OFFICERS AIRSPEED INDICATOR PER BOEING MAINTENANCE MANUAL 34-SDR P5CA9700114Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1800 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700113Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1800 BETWEEN S51L AND S50L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700112Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1920 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700111Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1880 BETWEEN S51L AND S51R AT BL ZERO. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700110Shear Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1760 BETWEEN S49L AND S48L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700109Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1760 BETWEEN S49L AND S50L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700108Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1820 BETWEEN S50L AND S49L. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700107Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1820 BETWEEN S51R AND S50R. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700106Angle · corrodedLEVEL 2 CORROSION SHEAR ANGLE BS 1660 BETWEEN S47R AND S48R. REPAIRED PER BOEING SRM 53-10-04 FIGURE 3.SDR P5CA9700051Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S48L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700050Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S48L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700049Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S49L AND S50L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700048Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1660 BETWEEN S47R AND S48R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700047Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1820, BETWEEN S51R AND S50R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700046Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1820, BETWEEN S50L AND S49L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700045Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1920, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700044Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1880, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700043Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1800 BETWEEN S51L AND S50L. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700042Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1800, BL 0, BETWEEN S51L AND S51R. REMOVED CORROSION PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700040Shear Angle · corrodedLEVEL 1 CORROSION ON SHEAR ANGLE AT BS 1760 AT BL 0 BETWEEN S51R AND S51L. CORROSION REMOVED PER BAC SRM 53-10-04, FIGURE 3.SDR 97UAL900038Battery Pack · dischargedEMERGENCY SLIDE ILLUMINATION LIGHTS 1R, 2R, 2L, 4R, 4L, 5R, AND 5L ACTIVATE WHEN SWITCH IS ARMED. REPAIRED FRAYED WIRE THAT WAS SHORTING TO AIRCRAFT FRAME OVER DOOR 3 RIGHT.SDR 97UAL900065Power Feeder · failedEMERGENCY EXIT LIGHT, INOP ON RIGHT HAND AISLE FROM SEATS 21 TO 26. REPLACED POWER FEEDER FROM SIDEWALL TO ROW 27.SDR 96UAL901007Battery Pack · dischargedFOUND DOOR 1L, 5L AND 5R SLIDE EMERGENCY LIGHTS STAYED ON. UNABLE TO TURN OFF. REPLACED BATTERY PACK.SDR P5CA9601254Pitot Probe · malfunctionedRIGHT MAIN PITOT PROBE HEATER LIGHT ILLUMINATED IN CRUISE. DUE TO WEATHER EN ROUTE THE DECISION WAS MADE TO RETURN TO MELBORNE. REPLACED THE RIGHT MAIN PITOT PROBE, FUNCTIONAL AND LEAK CHECKED PER MAINTENANCE MANUAL 34-11-01.SDR 96UAL900974Selector Valve · crackedON LANDING HYDRAULIC SYSTEM NR 1 QUANTITY WENT TO ZERO. PRESSURE LIGHT CAME ON FOR AIR PUMP AND ENGINE PUMP. TAXIED OFF RUNWAY AND WAS TOWED TO THE GATE DUE TO LOSS OF BODY AND NOSE LANDING GEAR STEERING. *S/D* LOSS OF HYDRAULIC FLUID WAS DUE TO CRACKED BSDR 96UAL900968Power Supply · inoperativeEXIT EMERGENCY LIGHT ABOVE UPPER DECK CREW EXIT DOOR IS INOP. REPLACED BATTERY POWER SUPPLY OVER UPPER DECK EMERGENCY EXIT.SDR P5CA9601253Drain Cap · bad sealLOSS OF OIL QUANTITY NR 4 ENGINE ON TAXI OUT. FOUND DRAIN CAP SEAL LEAKING ON KIT INSTALLED FOR ENGINE DRIVEN HYDRAULIC PUMP DEACTIVATION PER MEL 29-01 PER MAINTENANCE MANUAL 29-11-05. REPLACED CAP LEAK CHECK OK.SDR P5CA9601251Airspeed Ind · inoperativeFIRST OFFICER'S AIRSPEED INDICATOR READ ZERO WHILE CAPTAIN'S ASI INDICATED 100 KNOTS. PERFORMED HIGH ENERGY STOP INSPECTION PER BAC MM 05-51-10 AND REPLACED FIRST OFFICER'S AIR SPEED INDICATOR PER BAC MM 34-13-05.SDR 96UAL900956Bulkhead Fitting · loose fastenersDURING ROUTINE ENGINE CHANGE ON NR 4 ENGINE FOUND 4 LOOSE FASTENERS ON THE PYLON FWD ENGINE MOUNT FITTING INBOARD SIDE COMMON TO THE BULKHEAD. INSTALLED NEW FASTENERS. ADJACENT FASTENERS WERE INSPECTED WITH NO DEFECTS NOTED. BOEING S/B 747-54A2069 WAS PREVISDR P5CA9601252Radar Scope · inoperativeCAPTAIN'S WEATHER RADAR INDICATOR WENT BLANK WITH SMELL OF SMOKE IN COCKPIT - PULLED CIRCUIT BREAKER. REPLACED RADAR INDICATOR PER BAC MM 34-43-05 AND TESTED PER MM 34-43-00.SDR 96UAL900944Drive Unit · failedLEFT NR 2 LEADING EDGE FLAP WOULD NOT RETRACT. RETURNED TO FIELD. *S/D* NR 2 LEFT HAND LEADING EDGE FLAP DRIVE UNIT WAS REPLACED. REMOVED UNIT WAS DISASSEMBLED IN THE SHOP WITH NO DEFECTS NOTED.SDR P5CA9600981Access Panel · crackedACCESS PANEL 191ML FORWARD HINGE AREA UNDER HINGE CRACKED FIBERGLASS. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9600979Control Rod · brokenMAIN DECK CARGO DOOR WOULD NOT CLOSE NORMALLY AFTER CARGO LOADING. FOUND FORWARD PULL IN HOOK CONTROL ROD BROKEN. REPLACED ROD PER M/M 52-32-00.SDR P5CA9600980Tires · flatON WALKAROUND CHECK, FOUND NR 2 AND NR 4 TIRES FLAT. REPLACED NR 1, 2, 3 AND 4 TIRES PER MAINTENANCE MANUAL 32-45-01. COMPLETED BRAKE ANTI-SKID OPERATIONAL CHECK PER M/M 32-42-00, ALL CHECKS SATISFACTORY.SDR P5CA9600975Skin · missingRIGHT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE OF MID-FLAP LEADING EDGE HAS APPROXIMATELY 2.5 INCH BY 3 FOOT SECTION OF SKIN MISSING WITH EXPOSED HONEY COMB DAMAGED AND PROTRUDING, AREA SURROUNDING THE MISSING MATERIAL SOFT. REPAIRED PER BOEING SRM 51-40-07.SDR P5CA9600971Panel · creasedRIGHT UNDERWING FIBERGLASS PANEL AFT OF OUTBOARD LANDING LIGHT HAS A CREASE APPROXIMATELY 4 INCHES LONG BY .25 INCH DEEP WING STATION 294.600. REPAIRED PER BOEING SRM 51-40-07.SDR P5CA9600976Panel · crackedA 4 INCH CRACK ON LEFT WING LOWER, PANEL FORWARD OF WING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9600967Panel · crackedA 4 INCH CRACK IN LEFT WING LOWER PANEL FORWARD OF WING LANDING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9600954Bracket · corrodedLEVEL 2 CORROSION KEEL BEAM ACCESS PANELS 191HH AND 191KK 6 INNER ATTACHMENTS BRACKETS. FABRICATED AND REPLACED BRACKETS PER BOEING SRM 51-10-01.SDR P5CA9600952Sleeve · dentedDEEP LONG DENT NR 1 ENGINE FAN REVERSER SLEEVE AT 7 O'CLOCK POSITION. REPAIRED PER POLAR AIR CARGO MA 7830-01:01 AND BOEING SRM 51-40-06 PARA 3 AND 51-24-11.SDR P5CA9600931Bracket · brokenTHREE BROKEN HANGER BRACKETS FOR NR 4 FLAP TRACK CANOE FAIRING. REPLACED BRACKETS PER BAC MM 27-51-26.SDR P5CA9600930Rib · crackedCRACKED AFT UPPER RIB AND BRACKET ON NR 4 ENGINE OUTBOARD COWL. FABRICATED AND INSTALLED NEW RIB AND BRACKET PER BAC SRM 51-10-01.SDR P5CA9600927Bracket · crackedBROKEN FORWARD CANOE HANGER BRACKET ON NR 4 FLAP TRACK. REPLACED BRACKET PER BAC MM 27-51-26.SDR P5CA9600925Skin · delaminatedDELAMINATED OUTBOARD TRAILING EDGE CORNER OF LEFT INBOARD ELEVATOR. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11.SDR P5CA9600950Keel Beam · corrodedLEVEL 1 CORROSION KEEL BEAM PANELS 191GG, 191HH, 191JJ AND 191KK. CLEANED CORROSION ON PANELS 191HH AND 191KK SRM 51-10-01 AND REPLACED 191GG AND 191JJ FOR CONVENIENCE PER SRM 51-10-01 AND 51-10-02.SDR P5CA9600953Fitting · crackedCRACKED LOWER L-1 DOOR LOWER TORQUE TUBE PIVOT HINGE BEARING FITTING. REPLACED FITTING PER BOEING SRM 51-30-03.SDR P5CA9600933Flange · crackedCRACKED UPPER FORWARD FLANGE ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW FLANGE PER BAC SRM 51-10-01.SDR P5CA9600932Cutout · crackedCRACKED PRECOOLER DOOR CUTOUT ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW PART PER BAC SRM 51-10-02.
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