Boeing 727-232

Service difficulty reports · 6,539

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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"

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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 SPLICJan 28, 1999 · N421DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 28, 1999 · N400DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 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.Jan 28, 1999 · N400DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990176Battery Pack · dischargedFOUND ON PREFLIGHT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.Jan 27, 1999 · N405DA · Boeing 727232 · Emergency LightingSDR 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.Jan 27, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 27, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 27, 1999 · N526DA · Boeing 727232 · Leading Edge DevicesSDR 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.Jan 27, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 27, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR 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 Jan 26, 1999 · N490DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 26, 1999 · N538DA · Boeing 727232 · Turbine Engine Oil SystemSDR 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.Jan 26, 1999 · N505DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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 Jan 25, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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 ENTIREJan 25, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 25, 1999 · N526DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 25, 1999 · N526DA · Boeing 727232 · Fuselage, Wing Attach FittingsSDR 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 11Jan 24, 1999 · N494DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 24, 1999 · N546DA · Boeing 727232 · Engine Fuel PumpSDR 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.Jan 23, 1999 · N514DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L990154Stiffener · crackedCHK D-1, O/B SPAR STIFFENER CRACKED, NR 6 L/E SLAT O/B TRACK BOX. REPLACED PER MM 57-20-21.Jan 22, 1999 · N514DA · Boeing 727232 · Leading Edge DevicesSDR DL72K990263Skin · corrodedAT HMV, FOUND SKIN BULGED, EXT SKIN STA 1030 TO 1050 STRINGER 28L-27L. REPLACED SKIN ON N/R 297.Jan 22, 1999 · N526DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 22, 1999 · N526DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 21, 1999 · N490DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 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 LJan 21, 1999 · N495DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 21, 1999 · N476DA · Boeing 727232 · Service DoorsSDR 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.Jan 21, 1999 · N476DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 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 EXTERJan 20, 1999 · N495DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 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.Jan 20, 1999 · N524DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 20, 1999 · N524DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 20, 1999 · N524DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 18, 1999 · N490DA · Boeing 727232 · Fuselage Main, Floor BeamSDR 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.Jan 18, 1999 · N490DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 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.Jan 16, 1999 · N411DA · Boeing 727232 · Trailing Edge FlapsSDR 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 Jan 16, 1999 · N10791 · Boeing 727232 · Turbine Engine Compressor SectionSDR 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.Jan 14, 1999 · N45793 · Boeing 727232 · Light System WiringSDR 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.Jan 13, 1999 · N541DA · Boeing 727232 · Emergency LightingSDR 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.Jan 11, 1999 · N519DA · Boeing 727232 · Leading Edge DevicesSDR 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.Jan 11, 1999 · N524DA · Boeing 727232 · Fuselage Main, BulkheadSDR 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.Jan 11, 1999 · N524DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 11, 1999 · N524DA · Boeing 727232 · Trailing Edge FlapsSDR 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.Jan 10, 1999 · N509DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K990057Battery Pack · dischargedFWD EVACUATION SLIDE LIGHTS INOP. REPLACED BATTERY PACK.Jan 10, 1999 · N481DA · Boeing 727232 · Emergency LightingSDR DL72K990050Battery Pack · dischargedRT OVERWING CENTER EMERGENCY LIGHT INOP. REPLACED BATTERY ON RACK M956, OPS CHKS GOOD.Jan 9, 1999 · N414DA · Boeing 727232 · Emergency LightingSDR CALA9900058Rib · crackedTWO RIBS ATTACHED TO NR 7 SPOILER ACTUATOR CASTING ARE CRACKED (1). REPLACED RIBS PER SRM 51-10-1 AND 51-30-2.Jan 9, 1999 · N33785 · Boeing 727232 · Wing, Rib/BulkheadSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Leading Edge DevicesSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Leading Edge Slat ActuatorSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Cargo/Baggage DoorsSDR 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.Jan 9, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous Structure
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