Boeing 747-121
Service difficulty reports · 3,030
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 = '747121' 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 = '747121' 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 P5CA9500536Rib · crackedCRACKED UPPER LEFT CHORD ON FORGE RIB AT WS 930 LEFT WING LEADING EDGE CAVITY. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.SDR P5CA9500535Rib · crackedCRACKED FORGE RIB LEFT WING LEADING EDGE CAVITY WS 960 AFT RIGHT SIDE UPPER CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.SDR P5CA9500534Rib · crackedCRACK ON LEFT WING LEADING CAVITY WS 850 FORGED RIB AT THE AFT UPPER LEFT SIDE CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500533Intercostal · crackedCRACKS ON INTERCOSTAL AT S30R BETWEEN BS 500 AND 520. MANUFACTURED NEW INTERCOSTAL PER BOEING SRM 53-10-21, INSTALLED PER 51-30-02.SDR P5CA9500532Frame · corrodedCORROSION AT BS 1060 FRAME UNDER RIGHT FAIRING. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01.SDR P5CA9500531Pressure Deck · corrodedCORROSION ON PRESSURE DECK WEBS RBL 11 BETWEEN BS 1280 AND 1400 RBL 33 BS 1300 TO 1400. MANUFACTURED AND INSTALLED REINFORCEMENT PER BOEING SRM 53-10-07 FIG 2 DETAIL 2.SDR P5CA9500530Bracket · corrosionCORROSION ON U-CHANNEL FAIRING ON HINGE BRACKET, INBOARD HINGE OF NR 14 LEADING EDGE FLAP. MANUFACTURED BRACKET PER BOEING SRM 51-20-01, INSTALLED PER 51-30-02.SDR P5CA9500687Skin · corrosionSWELLING IN FUSELAGE SKIN BETWEEN BS 1780 AND 1800 AT S49R. AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHING LIMITS, INSTALLED FASTENERS PER 51-30-01.SDR P5CA9500686Skin · corrodedSWELLING ON EXTERNAL SKIN AT BS 1940 S47R. REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED FASTENERS PER 51-30-02.SDR P5CA9500685Angle · corrodedCORROSION ON SUPPORT ANGLE FOR FLOOR, BETWEEN BS 1240 AND 1260 LBL 100. REPLACED ANGLE PER BOEING SRM.SDR P5CA9500684Angle · corrodedCORROSION ON SUPPORT ANGLE FOR FLOOR MAIN DECK WL 178 LEFT SIDE BETWEEN BS 1320 AND 1350. REPLACED SUPPORT ANGLE, INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500683Bulkhead · corrodedCORROSION UNDER BOLTS BS 1000 LEFT SIDE. SURFACE CORROSION REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS.SDR P5CA9500682Angle · crackedRIGHT WING LEADING EDGE CAVITY WS 630 RIB TO LEADING EDGE CONNECTION ANGLE IS CRACKED. REPLACED ANGLE MANUFACTURED PER BOEING SRM 51-20-02, INSTALLED 51-30-02.SDR P5CA9500681Skin · corrodedSWELLING AND PROTRUDING RIVETS IN FUSELAGE SKIN, AT BS 1940 BETWEEN S47L AND S51L. REWORKED AREA AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02.SDR P5CA9500680Skin · corrosionSWELLING IN FUSELAGE SKIN RIGHT SIDE BETWEEN BS 1860 AND 1800 S47R. SWELLING AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02.SDR P5CA9500679Bracket · brokenBROKEN BRACKET RIGHT WING LEADING EDGE CAVITY WS 1168. MANUFACTURED PART PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02.SDR P5CA9500678Skin · corrodedSURFACE CORROSION ON HI-LOCK HEADS, ON EXTERNAL SKIN MAIN SIDE CARGO DOOR CUTOUT. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500677Fitting · crackedCRACK ON FITTING AT BS 1820 S40R. REPLACED FITTING, INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500676Skin · crackedCRACK ON AFT BULK CARGO DOOR CUTOUT, AT INTERNAL LOWER FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-10.SDR P5CA9500675Skin · separatedLEFT WING OUTBOARD FLAP UPPER SURFACE 2 POINTS OF SEPARATION. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9500674Chord · corrodedCORROSION ON LOWER FLANGE OF THE LOWER CHORD LANDING GEAR BEAM, AT BS 1350 LEFT AND RIGHT. REWORKED PER BOEING SB 53-2310 WITHIN LIMITS.SDR P5CA9500673Spoiler · crackedCRACK AT SKIN NEAR PCU FITTING ON NR 7 SPOILER RIGHT WING. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9500672Exhaust Bellow · crackedAPU EXHAUST BELLOW BENT AND CRACKED. REPLACED BELLOW.SDR P5CA9500671Chord · crackedCRACK ON CHORD RIGHT SIDE NOSE WHEEL CORNER. REPAIRED PER BOEING DRAWING 141U1098 (SB 53-2272).SDR P5CA9500670Cowling · crackedCRACK ON FORWARD EDGE NR 3 ENGINE RIGHT COWLING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500669Skin · corrodedCORROSION FUSELAGE SKIN EXTERNAL AND INTERIOR, BS 1000 BETWEEN S38L AND S40L. REPAIRED PER EO B747-53-84022-A40-010.SDR P5CA9500668Cowl Frame · crackedCRACKED FRAME 3RD HOOK NR 4 ENGINE RIGHT MAIN COWL UPPER. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500667Turbine Case · crackedENGINE NR 2 S-FLANGE AT 2 O'CLOCK IS CRACKED IN TWO PLACES ONE ON THE OD AND ONE FROM RAIL TO CASE OF TURBINE. REPAIRED PER 72-53-01SDR P5CA9500666Clips · corrodedCORRODED FASTENERS AND CLIPS AT MAIN DECK WINDOWS BETWEEN BS 2060 AND 2080. REPLACED CLIPS AND FASTENERS PER BOEING MAINT MANUAL 56-21-01.SDR P5CA9500665Cowling · corrodedSURFACE CORROSION ON RIVET HEADS AND SHEARED RIVETS ON THE EXTERIOR SURFACE OF NR 2 LEFT COWLING. REPLACED RIVETS PER BOEING SRM 51-30-02.SDR P5CA9500664Cowling · corrodedSURFACE CORROSION ON INTERIOR SURFACE SKIN OF NR 2 ENGINE RIGHT COWLING. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500663Cowling · corrodedSURFACE CORROSION AND LOOSE RIVETS ON NR 3 ENGINE COWLING, RIGHT EXTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS. REPLACED LOOSE RIVETS.SDR P5CA9500662Cowling · corrodedSURFACE CORROSION ON NR 3 ENGINE RIGHT COWLING INTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500661Cowling · damagedDAMAGE ON NR 3 ENGINE LEFT FAN COWL EXTERIOR SKIN. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500660Bracket · brokenBROKEN HOLDING BRACKET FOR SUPPORT ROD NR 3 ENGINE LEFT COWLING. MANUFACTURED BRACKET PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02.SDR P5CA9500659Cowling · corrodedSURFACE CORROSION ON NR 3 ENGINE LEFT COWLING INTERIOR. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500658Door · crackedCRACK LEFT WING LANDING GEAR UPPER HALF DOOR FWD SIDE EDGE. REPAIRED PER BOEING SRM 51-40-03.SDR P5CA9500657Skin · crackedCRACK AROUND FASTENER AT BS 520 S43R. REPAIRED PER BOEING SRM 53-30-03 FIG 47 SHEET 3.SDR P5CA9500656Fitting · crackedCRACKS ON S3L, BS 1240 FWD SIDE. REPLACED FITTING PER BOEING SRM 51-30-02.SDR P5CA9500655Fiiting · corrodedCRACKS AND CORROSION ON FITTINGS TO S1L AND S1R, BS 1240. REPLACED FITTINGS INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500654Angle · crackedCRACK ON VERTICAL STABILIZER AT STA 232.5 LEFT ANGLE ON NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-40-04.SDR P5CA9500653Cowl · crackedCRACK WITH STOP HOLE ON EXTERIOR SURFACE O, NR 2 LEFT COWLING, UNDER CSD OIL FILL PANEL. REPAIRED PER BOEING SRM 51-40-02.SDR P5CA9500652Skin · corrodedSURFACE CORROSION ON LOWER RIGHT WING SKIN BETWEEN WBS 254 AND 614. REMOVED CORROSION PER BOEING SRM 57-10-01.SDR P5CA9500651Bracket · crackedCRACKED APU AFT MOUNT SUPPORT ROD MOUNTING BRACKET IS CRACKED BOTH SIDES. REPAIRED PER BOEING SRM 51-20-02.SDR P5CA9500650Skin · crackedCRACKS IN FUSELAGE SKIN BETWEEN BS 740 AND 760 S26R. REPAIRED PER BOEING SRM 53-30-03 FIG 1.SDR P5CA9500649Seal Groove · crackedMAIN SIDE CARGO DOOR FWD INTERIOR SIDE PRESSURE SEAL GROOVE IS DAMAGED AND CRACKED IN 2 PLACES. REPAIRED PER BOEING SRM 51-40-01.SDR P5CA9500648Bracket · crackedCRACKED BRACKET NR 1 PYLON NS 253 INTERNAL ON LEFT WALL. MANUFACTURED NEW BRACKETS PER BOEING SRM 54-10-02.SDR P5CA9500647Web · crackedCRACK ON PRESSURE DECK WEB BS 1241 RBL 106. TRIMMED AREA TO REMOVE CRACK PER BOEING SRM 53-10-07 FIG 16 DETAIL 2.SDR P5CA9500646Fitting · plugged holeBS 1740 S4L ON THE LOWER FORWARD FITTING THAT CONNECTS THE INTERCOSTAL TO THE FRAME ON LEFT SIDE OF THE T-CHORD HAS 2 PLUG HOLES 1.8750 INCHES IN DISTANCE AND SECOND .3750 INCH IN DISTANCE FROM EXISTING HILOCK. INSTALLED STRAP PER IAI E.O. MF-MAN-B47-53-84008SDR P5CA9500645T-Chord · double drilledBETWEEN BS 1950 AND BS 2000 ON S4L ON T-CHORD, FOUND DOUBLE HOLES AND OVAL HOLES. REPAIRED PER IAI E.O. MF-MAN-B47-53-83972.
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