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 KCSA071200Light · inoperativeEMERGENCY LIGHT ABOVE UPPER DECK EXIT DOOR INOP.SDR KCSA07041Filter · contaminatedAT 8000', IDLE THRUST EGT NR 4 AT 874 DEGREES CELSIUS AND N2 AT 43 PERCENT. ALL OTHER INSTRUMENTS NORMAL. ACCOMPLISHED ENGINE STALL IN FLT (ABNORMAL EGT) CHECKLISTS. ATTEMPTED RESTART WITH RAPID RESTART PROCEDURE QRH-69. RESULTED IN DUPLICATE INDICATIONS. SDR KCSA07011Engine · flamed outFLT LEVEL 34.0 NR 4 ENG FLAMED OUT, DESCENDED TO F.L 280. RESTARTED ENG - ALL PARAMETERS NORMAL. ENG RESTARTED ON FIRST ATTEMPT. CLIMBED TO FL 340 ENG OPERATES NORMAL. PERFORMED ENG FLAME OUT INSPECTION IAW MM 71-00-42 P-118. PERFORMED ENG WINDMILL INSPECTIONSDR KCSA071004Skin · damagedAFT CARGO DOOR FWD LOWER CORNER HAS APPROX .750 INCH X 1.5 INCH AREA OF EDGE SKIN DAMAGED.SDR KCSA071003Floorbeam · damagedAFT PIT FLOORBEAM DAMAGED AT BS 1800, LBL 50.SDR KCSA071001Bulkhead · chafedNR 2 PYLON HYD PRESSURE SUPPLY LINE JAM NUT CHAFING INTO AFT SIDE OF NAC STA 221 BULKHEAD WEB.SDR KCSA061554Sign · inoperativeUPPER DECK DOOR EMERGENCY EXIT SIGN INOP.SDR KCSA061490Light · inoperativeUPPER DECK EMERGENCY LIGHT INOP AT UPPER DECK SERVICE DOOR.SDR KCSA061328Sign · no testFOUND UPPER DECK EXIT SIGN AND SLIDE LIGHT X325 WILL NOT TEST.SDR KCSA06082Line · leakingNR 1 HYD LOW LIGHT FOR SYS NR 1 ILLUMINATED. NR 1 HYD SYS QTY WAS 2 GALS WHEN ADP TURNED OFF AND ADP DEPRESSURIZED. ON POST FLT, FOUND NR 1 ADP BLOWOUT DOOR OPEN AND SKYDROL LEAK FROM ACCESSORY PANEL. REPLACED NR 1 HYD SYSTEM RETURN LINE IAW AMM 29-11-00.SDR KCSA061255Frame · crackedNR 2 PYLON NAC STA 221.9 FRAME CRACKED AT FWD I/B UPPER CORNER.SDR KCSA061254Bulkhead · chafedNR 2 PYLON STA NAC 221.9 BULKHEAD WEB CHAFED AROUND HYDRAULIC UNION.SDR KCSA06060Bulb · inoperativeDURING CLIMB LWR AFT CARGO FIRE WARNING LIGHTS AND BELL CAME ON INTERMITTENTLY. PERFORMED QRH PROCEDURE, EMERGENCY RETURN. INSPECTED AFT LOWER CARGO COMP. AND CARGO. FOUND NO EVIDENCE OF FIRE OR SMOKE. FOUND SMOKE DET NR 3 INTERMITTENT ON TEST. REPLACED BUSDR 061159Stiffener · crackedBS 2658 BULKHEAD STIFFENER CRACKED AT LBL 30, WL 277.SDR 061157Rib · chafedRIGHT WING L/E RIB AT FSSI 1022 IS CHAFED.SDR 061156Rib · chafedRIGHT WING L/E RIB AT FSSI 887 IS CHAFED.SDR 061158Bolt · looseEXTERNAL FUSELAGE RT SIDE OVERWING FITTING HAS A BOLT LOOSE AT STA 1346, WL 156.SDR 061154Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND LT OUTFLOW VALVE CUTOUT AREA AT STA 2210, STR 43L.SDR 061153Seat Track · corrodedMAIN DECK SEAT TRACK HAS CORROSION AT STA 910, RBL 11.33.SDR 061152Stiffener · corrodedCORROSION ON TOP OF BS 1480 BULKHEAD HORIZONTAL STIFFENER WEB AT LBL 48, WL 118.SDR KCSA061149Frame · crackedBULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, LBL 18.SDR KCSA061148Frame · crackedBULK PIT FUSELAGE FRAME WEB CRACKED AT BS 2080, RBL 18.SDR KCSA061147Bulkhead · gougedMAIN CABIN STA 2360 PRESSURE BULKHEAD WEB FORWARD SIDE IS GOUGED AROUND FASTENER ADJACENT TO STR 24R.SDR KCSA061143Skin · damagedEXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 2484, BETWEEN STR 22L & 23L.SDR KCSA061146Frame · crackedNR 4 PYLON INTERNAL RT SIDE LOWER FRAME IS CRACKED AT NAC STA 236.SDR KCSA061145Fitting · corrodedFUSELAGE STRINGER END FITTING IS CORRODED AT AFT SIDE OF STA 2360 BULKHEAD, STR 48L.SDR KCSA061144Bulkhead · corrodedMAIN CABIN STA 2360 BULKHEAD LOWER FORWARD CHORD IS CORRODED IN HOLES AT STRINGER END FITTING STR 48L.SDR 061141Skin · corrodedEXTERNAL FUSELAGE SKIN HAS CORROSION AT STA 600, ABOVE STR 6R.SDR 061140Frame · crackedBULK PIT BS 2140 FUSELAGE FRAME WEB CRACKED AT RBL 18.SDR 061139Doubler · damagedNR 3 PYLON I/B EXTERNAL SKIN DOUBLER AT NAC STA 221 ABOVE REAR ENGINE MOUNT HAS DAMAGE.SDR 061137Stringer · crackedLEFT HORIZONTAL STAB UPPER STR 4 CRACKED AT STAB STA 260.SDR 061136Bulkhead · dentedBS 2360 BULKHEAD HAS DENTS AT LBL 7.5, WL 347.SDR 061135Bulkhead · dentedBS 2360 BULKHEAD HAS DENTS AT RBL 54, WL 313.SDR 061134Stiffener · crackedNR 4 PYLON MID SPAR WEB LOWER SIDE STIFFENER CRACKED AT O/B END IN RADIUS AT NAC STA 231.SDR 061133Stringer · bentFUSELAGE STRINGER IS BENT AT STA 1930, STR 1R.SDR 061132Fitting · corrodedFUSELAGE STRINGER END FITTING IS CORRODED AT STA 1480, STR 47R.SDR 061131Strap · corrodedAFT BILGE LOWER FUSELAGE FRAME UPPER CHORD STRAP IS CORRODED AT STA 1810, RBL 61 AROUND C-2 DOOR OPENING AREA.SDR KCSA061130Bulkhead · dentedFOUND BS 2360 BULKHEAD HAS A DENT AT RBL 50, WL 242.5.SDR KCSA061129Skin · dentedFOUND FUSELAGE SECTION 48 SKIN HAS A DENT AT BS 2600 JUST AFT AND BELOW TAIL JACKING POINT MOUNT AREA.SDR KCSA061128Skin · damagedNR 4 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED AT NAC STA 190.SDR 061127Skin · damagedNR 1 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED NAC STA 180 TO 230.SDR 061126Bulkhead · crackedNR 3 PYLON REPAIR STOP DRILLED 2" VERTICAL CRACK ON THE AFT ENGINE MOUNT BULKHEAD UPPER I/B AFT FLANGE RADIUS.SDR 061125Skin · damagedNR 4 PYLON I/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED FROM NAC STA 215 TO 236.SDR 061123Skin · corrodedFOUND EXTERNAL FUSELAGE SKIN IS CORRODED AT STA 1715, STR 21L AROUND L4 DOOR CUTOUT AREA.SDR 061122Stiffener · crackedNR 4 PYLON INTERNAL FORWARD BULKHEAD HORIZONTAL STIFFENER IS CRACKED AT NAC STA 180.SDR 061121Fitting · corrodedFUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 17L.SDR 061120Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 48L.SDR KCSA061119Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 38R.SDR KCSA061118Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 26R.SDR KCSA061116Fitting · corrodedFOUND FUSELAGE STRINGER END FITTING HAS BOLT HOLES CORRODED AT STA 2360, STR 42R.
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