Boeing 747 212B
Service difficulty reports · 2,202
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 = '747212B' 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 = '747212B' 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 EIA2006242Skin · corrodedRIGHT WING LEADING EDGE FRONT SPAR AND LOWER SKIN INTERFACES FOUND CORROSION AT FSSI 1430. CORROSION AREA REPAIRED IAW EA57-0511.SDR EIA2006204Fan · odorWHEN RECIRC FAN TURNED ON DURING TAXI IMMEDIATELY SMELLED BURNING ODOR, FAN TURNED OFF AND PUT ON DMI. REMOVED AND REPLACED RECIRC FAN, LEAK AND OPS CHECK OK. DMI CLEARED.SDR KCSA061290Bulkhead · corrodedCORROSION ON BS 2360 BULKHEAD FORWARD LOWER CHORD BETWEEN STR 25R AND STR 44L.SDR KCSA061289Fitting · corrodedSTA 2360 BULKHEAD CHORD STRINGER 46L FWD SIDE END FITTING CORRODED.SDR KCSA061288Fitting · corrodedSTA 2360 BULKHEAD STRINGER END FITTING 50R FWD SIDE CORRODED.SDR KCSA061287Fitting · corrodedSTA 2360 BULKHEAD CHORD 49L FWD SIDE CORRODED.SDR KCSA061286Fitting · corrodedSTA 2360 BULKHEAD STRINGER END FITTING 48L FWD SIDE CORRODED.SDR KCSA061285Fitting · corrodedSTA 2360 BULKHEAD FWD SIDE STRINGER 51L END FITTING CORRODED.SDR KCSA061284Fitting · corrodedSTA 2360 BULKHEAD CHORD STRINGER 48R END FITTING CORRODED FWD SIDE.SDR KCSA061283Fitting · corrodedSTA 2360 STRINGER END FITTING 48L FWD SIDE IS CORRODED.SDR KCAS061282Fitting · corrodedSTA 2360 STRINGER END FITTING FWD SIDE 42R CORRODED FWD SIDE.SDR KCSA061281Fitting · corrodedSTA 2360 STRINGER END FITTING FWD SIDE STRINGER 38R CORRODED.SDR KCSA061280Fitting · corrodedSTA 2360 STRINGER END FITTING FWD SIDE STRINGER 50L CORRODED.SDR KCSA061279Fitting · corrodedSTA 2360 STRINGER END FITTING 48L AFT SIDE CORRODED.SDR KCSA061278Fitting · corrodedSTA 2360 STRINGER END FITTING 49L AFT SIDE CORRODED.SDR KCSA061277Fitting · corrodedSTA 2360 STRINGER END FITTING 50L CORRODED AFT SIDE.SDR KCSA061276Fitting · corrodedSTA 2360 STRINGER END FITTING 51L AFT SIDE CORRODED.SDR KCSA061275Fitting · corrodedSTA 2360 STRINGER END FITTING 48R CORRODED.SDR KCSA061274Fitting · corrodedSTA 2360 STRINGER END FITTING 49R AFT SIDE CORRODED.SDR KCSA061273Fitting · corrodedSTA 2360 STRINGER END FITTING 50R AFT SIDE CORRODED.SDR KCSA061272Fitting · corrodedSTA 2360 STRINGER END FITTING 51R CORRODED.SDR KCSA061271Fitting · corrodedBOLT BORE 77R CORRODED.SDR KCSA061270Fitting · corrodedBOLT BORE 85R CORRODED.SDR KCSA061269Frame · crackedCRACK INDICATION AT FASTENER HOLE AT BS 2598 BULKHEAD LT SIDE AFT INNER CHORD WL 314.SDR EIA2006203Duct · crackedRT WING PNEUMATIC DUCT CRACKED, DUCT TO GRP 2 RIGHT LED. REPLACED DUCT, LEAK AND OPS CHECK OK.SDR KCSA061265Bulkhead · scratchedBS 2360 BULKHEAD WEB SCRATCHED ABOVE STR 19L, LBL 88.SDR KCSA061264Seat Track · crackedFIRST OFFICER`S RT FWD SEAT TRACK CRACKED.SDR KCSA061263Seat Track · crackedCAPT`S FWD I/B SEAT TRACK CRACKED.SDR KCSA061262Seat Track · crackedFIRST OFFICER`S FWD I/B SEAT TRACK CRACKED.SDR KCSA061261Seat Track · crackedCAPT`S O/B AFT SEAT TRACK CRACKED.SDR KCSA061259Skin · corrodedAPPROX STA 580, C1 DOOR EXTERIOR HAS BULGING SKIN JUST ABOVE LAP 34RSDR KCSA061258Fireshield · gougedGOUGE ON NR 3 PYLON STA 2363.85 ON FIRE SHIELD APPROX 2 INCH SQUARE.SDR UPS06447712Beam · crackedAC FERRIED FOR REPAIR, CRACK IN LT WING LEADING EDGE UPPER CHORD AT STA 952. CRACK HAS BEEN STOP DRILLED IAW MFG ENG INSTRUCTIONS. DEACTIVATED GROUP A LEADING EDGE FLAPS, NR D331311. R/R LE BULLNOSE SKIN IAW SRM 57-20-03, FIG 7; RMVD DMGD PART OF UPR. CHORDSDR KCSA061256Stringer · crackedFUSELAGE STRINGER IS CRACKED AT STA 240, STR 45R.SDR EIA2006159Door · malfunctionedNOSE GEAR DOORS COME OPEN WHEN LANDING GEAR LEVER IS SELECTED TO OFF. CYCLED NOSE GEAR DOOR PER MM 32-22-00, OPS CHECK OK AND UNABLE TO DUPLICATE ON GROUND.SDR UPS06447466O-Ring · wornINSPECTION TYPE:N/A ATB - IMMEDIATELY AFTER T/O SMOKE WAS SENSED IN C/P. SMOKE WAS COMING FROM THE AREA OF WINDOW L1. WINDOW HEAT WAS TURNED OFF. RAN CHECKLIST. FUEL WAS JETTISONED TO LANDING WT AND FLIGHT RETURNED TO ANC. FOUND TERMINAL-A LOOSE. REMOVEDSDR EIA2006107Smoke Detector · inoperativeAFT CARGO SMOKE DETECTOR INOP. MOVED CARGO TO ACCESS DETECTOR.SDR EIA2006095Smoke Detector · no testFOUND LOWER AFT CARGO NR 3 SMOKE DETECTOR NO TEST. RELAMPED BEACON BULB, OPS CHK OK.SDR KCSA061193Bulkhead · chafedNR 4 PYLON NAC STA 221.90 BULKHEAD WEB HAS A WORN CHAFED AREA AROUND HYDRAULIC LINES.SDR KCSA061192Bulkhead · gougedNR 1 PYLON BULKHEAD WEB HAS A TOOL MARK NEXT TO HYDRAULIC LINES AT NAC STA 221.90.SDR EIA2006091Fairing · damagedDURING PREFLIGHT INSPECTION, FOUND HOLE IN INBOARD FLAP FAIRING. DAMAGE APPROX 3 IN OF DAMAGE PENETRATING HONEYCOMB, PARTS AVAILABLE TO REPAIR. NR 6 FLAP CANOE FAIRING REMOVED FOR REPAIR PER CDL 27-51-2 AND MM 27-51-00.SDR EIA2006087Pump · failedON TAXI CHS AFTER TURNING OFF RUNWAY NR 1 ENGINE OIL PRESSURE WENT TO ZERO WITH ASSOCIATED LOW OIL PRESS WARNING LIGHT. ENG WAS SHUT DOWN. FOUND BAD MAIN OIL PUMP. REMOVED AND REPLACED OP CHECK GOOD PER MM 72-61-17.SDR EIA2006081Engine · power lossDURING DESCENT THROUGH FL340 NR 3 ENGINE ROLLED BACK TO IDLE AND WOULD NOT RESPOND TO THROTTLE LEVER INPUTS. PERFORMED UNRECOVERABLE STALL PROCEDURES, TOOK TWO ATTEMPTS AND ENGINE RETURNED TO NORMAL OPERATION FOR REMAINDER OF FLIGHT.SDR EIA2006080Engine · malfunctionedNR 3 ENG NO THROTTLE RESPONSE AT FL 370.SDR UPS06446991Structure · crackedFOUND CRACK IN FWD LWR CARGO DOOR STRUCTURE. A/C WILL FERRY TO PAE. STOP DRILLED END OF CRACK TO .250 DIA HOLE. ROUTED OUT CRACK. RE- WORK OUTER SKIN TO INITAL CONTOUR IAW SRM 52-30-06. HFEC THE STOP DRILL HOLE. FABRICATED WEB REPAIR DOUBLER. ALODINE/PRIMED SDR EIA200677Clutch · malfunctionedALL FOUR ENGINE THROTTLE LEVERS WILL NOT GO INTO REVERSE. CLUTCH PACK REMOVED AT 0300Z/17. CONFIRMED CLUTCH PACK FAULTY. T/R LEVERS SEIZED WITH CLUTCH PACK ISOLATED. CLUTCH PACK ON HAND. EST COMPLETION AT 0400 - 0600Z/18.SDR UPS06446943Angle · corrodedINSPECTION TYPE:C M/D BS800-810 LBL117 FLOOR SUPPORT "L" ANGLE LWR FACE FOUND CORROSION. CORROSION BLEND OUT 0.028" BY 1/2" BY 2" EXCEED SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.SDR EIA2006075Sensor · damagedAT FL 380, PWR WAS REDUCED FOR SPEED CONTROL AND WAS NOT RESPONSIVE UNTIL REACHING FL 250. REPLACED NR 3 TT2 SENSOR AS PER MM 72-21-04, OPS CHK GOOD PER MM 71-00-00 TEST 3.SDR EIA2006066Engine · stalledWHILE DESCENDING FORM FL370 TO FL350, NR 3 ENGINE WENT INTO UNRECOVERABLE STALL. NO FLAMEOUT, VIBRATION OR EXCEEDENCES NOTED. NO SUCCESS WITH TWO ATTEMPTS TO RELIGHT. RAN IN-FLIGHT SHUTDOWN PROCEDURES, WAS ABLE TO RESTART AT FL 180. CHECKED PS3, PT3 PER MMSDR UPS06446954Stringer · corrodedINSPECTION TYPE:C BULK CARGO STR CORROSION FROM BS 1945-1960 S50R. CORROSION BLEND OUT 0.055" BY 1" BY 6" EXCEED SRM LIMIT. BULK CARGO COMPT BS 1930-1960 STR 50R AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 8.
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