Boeing 727-232
Service difficulty reports · 6,539
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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 = '727232' 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 = '727232' 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 DL72S990185Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 681 INDICATED POSSIBLE CRACKS IN THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 18 CRACK LOCATIONS IN LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE PANEL. THE LAP SPLICSDR DL72S990183Web · crackedA 1.5 INCH CRACK AT TORQUE BOX VERTICAL WEB STA 1213 LT SIDE AT HORIZONTAL ROW OF RIVETS. REPAIRED PER M/M 53-11-0 FIG 819.SDR DL72S990182Web · crackedA .5 INCH CRACK AT UPPER TORQUE BOX VERTICAL WEB STA 1233 RT SIDE AT UPPER ROW OF HORIZONTAL RIVETS. REPAIRED PER M/M 53-11-0 FIG 819.SDR DL72S990176Battery Pack · dischargedFOUND ON PREFLIGHT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.SDR DL72K990336Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.SDR DL72K990330Skin · crackedTHE COVE SKIN WAS FOUND CRACKED 37 FROM IB END OF FLAP. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 809.SDR DL72K990329Angle · crackedTHE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION 20 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY INSTALLING A DOUBLER AND NEW SECTION OF ANGLE.SDR DL72K990328Angle · crackedTHE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 34 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0.SDR DL72K990327Angle · damagedTHE AFT LOWER CHORD ANGLE WAS FOUND DAMAGED 33 FROM OB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY INSTALLING A DOUBLER.SDR DL72S990169Skin · corrodedTHE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 485 AND STRINGER 28R. THE CORROSION WAS REMOVED WITH A 7 X 3.5 CUTOUT. THERE WERE THREE OTHER REPAIR DOUBLERS NEAR THIS AREA FOR REPAIRS OF SIMILAR CUTOUTS. THE REPAIRS WERE REMOVED RESULTING IN 4 SDR DL72S990167O Ring · leakingENGINE NR 2 LOW OIL PRESS LIGHT ON, QYT GAUGE TO ZERO AND OIL PRESS EVENTUALLY TO ZERO. SHUT DOWN NR 2 ENG PER POM. REPAIRED OIL LEAK AT BANJO FITTING.SDR DL72L990184Skin · gougedA GOUGE WAS FOUND IN THE SKIN PANEL AT FS 500 BELOW THE STRINGER 26L LAP SPLICE. THE DAMAGE WAS TRIMMED OUT OF THE SKIN WITHOUT DAMAGING THE EXISTING LAP. THE CUTOUT WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366548-14.SDR DL72S990180Skin · crackedLFEC INSPECTION OF THE STRINGER 4R LAP SPLICE ALONG THE PANEL LENGTH FROM FS 681 TO 740 INDICATED POTENTIAL CRACKS IN THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 31 CRACKED FASTENER HOLES ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. THE SDR DL72S990179Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE ON THE PANEL BETWEEN FS 481 AND 680 INDICATED POSSIBLE CRACKS. INTERNAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS IN THE LOWER SKIN PANEL CONFIRMED A TOTAL OF 46 CRACKS ALONG THE PANEL LENGTH. THE ENTIRESDR DL72K990573Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 21 INCHES FROM O/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY INSTALLING A REPLACEMENT SECTION OF ANGLE AND A SPLICE DOUBLER.SDR DL72K990265Pin · corrodedAT HMV, FOUND BOTTLE PIN CORRODED. PITTED ON AFT FACE, RUSTY ON CAFER, AND BORE IS CORRODED. MACHINED BORE TO 40501 PER SRM 53-40-1. REMOVED ALL PER SAME AND INSTALLED.SDR DL72S990178Skin · crackedDURING ACCOMPLISHMENT OF LFEC INSPECTIONS OF THE LOWER ROW OF FASTENERS IN THE STRINGER 4R LAP SPLICE OF THE FS 360 TO 481 PANEL, CRACK INDICATIONS WERE NOTED. INTERNAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS OF THE LOWER SKIN PANEL CONFIRMED 11SDR DL72S990168Fuel Pump · failedAT FL 330, AFTER DEPARTURE SAT, NR 3 ENG FLAMEOUT. ALL IND NORMAL. FOUND FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL RAN ENG PER PFHB TEST.SDR DL72L990161Chord · crackedTHE I/B UPPER CHORD OF THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A 1 INCH TYPICAL CRACK AT FS 1273. THE DAMAGED SECTION OF CHORD WAS REMOVED AND A NEW SECTION SPLICED PER BAC S/B 727-53-0129. THE REPAIR WAS DOCUMENTED PER ER/A 366542-14AD.SDR DL72L990154Stiffener · crackedCHK D-1, O/B SPAR STIFFENER CRACKED, NR 6 L/E SLAT O/B TRACK BOX. REPLACED PER MM 57-20-21.SDR DL72K990263Skin · corrodedAT HMV, FOUND SKIN BULGED, EXT SKIN STA 1030 TO 1050 STRINGER 28L-27L. REPLACED SKIN ON N/R 297.SDR DL72K990237Skin · corrodedAT HMV, FOUND SKIN CORRODED THROUGH AND ENTRAPPING WATER BETWEEN STA 1050 TO 1030 STRINGER 29L TO 28L. REMOVED FXD FLOOR RT STA 1030 TO 1060, REMOVED SKIN, REPAIRED PER MM 53-30-0 FIG 809 AND ERA 332746-14. FLOOR PANELS INSTALLED ON NR1162.SDR DL72S990159Angle · corrodedFOUND DURING MV-1 CHECK, CORROSION ON SUPPORT ANGLE AT STA 740 STR 27 RT. REPLACED ANGLE PER M/M 53-11-0 FIG 826.SDR DL72S990150Skin · crackedDURING SPECIAL HFEC INSPECTION, THE STRINGER 4R SKIN LAP SPLICE WAS FOUND WITH 4 CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE INNER SKIN PANEL. THE ENTIRE LAP SPLICE WAS CUT (UPPER AND LOWER SKIN) AND REMOVED FOR FURTHER EVALUATION. THE CUT SKIN LSDR DL72S990137Frame · crackedFOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT FRAME OF R-1 DOOR AT FWD SIDE OF LWR STOP CASTING. REPAIRED PER MM 52-12-0.SDR DL72S990136Frame · crackedFOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9.SDR DL72S990151Skin · crackedDURING ACCOMPLISHMENT OF SPECIAL HFEC AND LFEC INSPECTIONS, 82 CRACK INDICATIONS WERE FOUND IN THE LOWER ROW OF THE LOWER SKIN OF STRINGER 4R LAP SPLICE BETWEEN FS 480 TO 681. THE SKIN LAP AREA WAS CUT AWAY AND REMOVED. THE SPLICE WAS RESTORED WITH AND EXTERSDR DL72K991370Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED AT 35 FROM THE I/B END. THE COVE SKIN WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 809.SDR DL72K990977Skin · damagedDURING SHOP INSPECTION, THE AFT COVE SKIN WAS FOUND WITH TOOL DAMAGE 60 FROM O/B END. THE SKIN WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 PAGE 819.SDR DL72K990975Skin · wornDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND WORN 35 FROM O/B END OF FLAP. A REPAIR DOUBLER WAS INSTALLED PER MM 57-52-0, FIG 809.SDR DL72S990149Floorbeam · corrodedFOUND DURING MV-1 CORROSION VISIT NRC 46, CORROSION AT FLOORBEAM STA 344 RBL 5 TO LBL 60 UPPER AND LOWER SIDES. REPAIRED PER SRM 53-10-8 FIG 11.SDR DL72S990148Frame · crackedFOUND DURING MV-1 CORROSION VISIT NRC 16, .25 INCH CRACK VISIBLE AT AFT ENTRY DOOR FRAME UPPER LT LOCATION. REPAIRED PER SRM 53-10-9 FIG 11.SDR DL72S990462Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.SDR CALA9900024Stator · migratedENGINE NUMBER THREE FAILED ON CLIMB-OUT. CONSTANT VIBRATION, OVER TEMP, ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT RETURNED TO LAS. ENGINE AND DAMAGED COWLING REPLACED AND AIRCRAFT RETURNED TO SERVICE. PRELIMINARY ENGINE INSPECTION REVEALED A FAILURE IN THE HIGH SDR CALA9900021Wire · shortedEMERGENCY EXIT LIGHT RIGHT HAND CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FOUND WIRE SHORTED IN AFT LEFT TAIL COMPARTMENT. SECURED WIRES AND PROTECTED PER STANDARD PRACTICES. LIGHTS OPS CHECK NORMAL.SDR DL72S990080Battery Charger · failedON LAYOVER CHECK, FOUND EMERGENCY EXIT LIGHTS INOP OVER THE RIGHT WING OVER WING EXITS. REPLACED BATTERY CHARGER OPERATION NORMAL DPN 334701744 S/N OFF 10007, ON DL52.SDR DL72S990065Skin · cracked4.5 INCH CRACK IN NR 8 SLAT COVE SKIN ANGLE AT O/B UPSTOP PAD. REPAIR PER MM 57-54-0 PG 816.SDR DL72S990060Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE LBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACK IS LOCATED APPROX AT WL 238 AND IS APPROX 2 IN LENGTH. REPAIRED PER ERA 332664-14.SDR DL72K991006Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 31 INCHES FROM I/B END. A REPAIR DOUBLER WAS INSTALLED PER MM 57-52-0, FIG 809.SDR DL72K991005Skin · damagedDURING SHOP INSPECTION THE COVE SKIN WAS FOUND TO HAVE A TEMPORARY REPAIR INSTALLED 34 FROM I/B END OF FLAP. THE SKIN WAS REPAIRED BY INSTALLING A PERMANENT REPAIR DOUBLER PER MM 57-52-0, FIG 809.SDR DL72L990344Web · crackedROUTED OUT .125 INCH CRACK IN 48 SECTION TORQUE BOX WEB RT SIDE AT LIGHTNING HOLE FWD OF STA 1243 PER M/M 53-11-0 PG 828.SDR DL72K990057Battery Pack · dischargedFWD EVACUATION SLIDE LIGHTS INOP. REPLACED BATTERY PACK.SDR DL72K990050Battery Pack · dischargedRT OVERWING CENTER EMERGENCY LIGHT INOP. REPLACED BATTERY ON RACK M956, OPS CHKS GOOD.SDR CALA9900058Rib · crackedTWO RIBS ATTACHED TO NR 7 SPOILER ACTUATOR CASTING ARE CRACKED (1). REPLACED RIBS PER SRM 51-10-1 AND 51-30-2.SDR CALA9900057Bracket · crackedBRACKET HAS .3125 INCH CRACK AT INBOARD SIDE AT LEFT WING NR 1 SLAT WHERE INBOARD TRACK MOUNTS TO LOWER SKIN. REMOVED AND REPLACED CRACKED BRACKET PER SRM 51-30-2.SDR CALA9900056Bracket · crackedLEFT WING NR 1 L/E KRUEGER FLAP ACTUATOR I/B MOUNT BRACKET IS CRACKED .375 INCH. REMOVED BRACKET, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1.SDR CALA9900055Tip · crackedLEFT WING LOWER WING TIP SURFACE HAS .5 INCH LONG HOLE WORK THROUGH AND .5625 INCH CRACK. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-30-2.SDR CALA9900054Angle · crackedRIGHT WING I/B OF I/B AILERON ANGLE IS CRACKED (.5) LOCATED ABOVE JACK SCREW AREA. REMOVED FASTENERS, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-30-2 AND 57-20-4.SDR CALA9900053Channel · crackedINBOARD SIDE OF C2 DOOR UPPER AFT CORNER METAL CHANNEL IS CRACKED (1) AT SEAL DEPRESSOR AREA. REMOVED CRACKED SECTION, FABRICATED, TREATED, PRIMED INSTALLED PER SRM 51-30-2, 51-10-6, AND 51-20-1.SDR CALA9900052Tip · crackedRIGHT WING TIP AT LOWER SURFACE AFT OF MOUNT SCREWS HAS A 1 INCH LONG CRACK. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 AND 51-30-2.
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