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.

SDR CALA9801622Angle · crackedINSPECTION FOUND CORROSION AND A .75 INCH CRACK IN L-ANGLE IN FORWARD PIT AFT OF DOOR AT STA 620, STRINGER 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-12.Sep 3, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981850Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT FS 700 BETWEEN STR 28R AND 28L. THE CORROSION WAS CUT OUT WITH A 9 X 6.5 CUTOUT. THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR FOR ANOTHER SKIN CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS WERE REPAIRSep 2, 1998 · N507DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801618Angle · corrodedINSPECTION FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CORRODED AT BS 304-280, WL 208.1, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.Sep 2, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981813Panel · delaminatedFOUND AREA OF DELAMINATION ON NR 2 SPOILER UPPER SURFACE. REPAIRED PER SRM 57-50-6.Sep 1, 1998 · N535DA · Boeing 727232 · SpoilersSDR DL72S981812Web · crackedFOUND ON D2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED .1562 INCH AT LIGHTENING HOLE STA 1243 RT. ROUTED OUT DAMAGED AREA PER MM 53-11-0.Sep 1, 1998 · N535DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981811Web · crackedFOUND ON D2 LETTER CK, 2 EA .5 INCH CRACKS STA 1303 VERT WEB ABOVE S-DUCT RT SIDE. REPAIRED PER SRM 53-10-4.Sep 1, 1998 · N535DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981810Angle · crackedFOUND ON B2 LETTER CK, HORIZONTAL TORQUE BOX ANGLE CRACKED RT STA 1273. REPLACED ANGLE PER SRM 53-10-10.Sep 1, 1998 · N535DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801615Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT ELEVATOR ATTACH ANGLE. AN ANGLE WAS INSTALLED IAW SRM 51-30-2.Sep 1, 1998 · N14788 · Boeing 727232 · Elevator StructureSDR CALA9801614Frame · corrodedINSPECTION FOUND RT FUSELAGE FRAME CORRODED AT STA 340. THE CORRODED AREA WAS REMOVED. REPAIR PARTS WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-02, AND MM 51-20-11.Sep 1, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801613Skin · crackedINSPECTION FOUND A 1 INCH CRACK AT FASTENER ON OUTBOARD SKIN APPROXIMATELY 28 INCHES FROM AFT END OF RT OUTBOARD MID FLAP OUTBOARD JACKSCREW FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-40-2.Sep 1, 1998 · N14788 · Boeing 727232 · Trailing Edge FlapsSDR CALA9801612Seat Track · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF LT OUTBOARD SEAT TRACK AT STA 344. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-10-5, FIGURE 7.Sep 1, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801611Longeron · crackedINSPECTION FOUND A 1 INCH CRACK LONGERON 13R AT ATTACH ANGLE, STA 965. THE CRACKED AREA WAS CUT OUT IAW SRM 53-02, FIGURE 18. A REPAIR LONGERON AND TWO SPLICES WERE INSTALLED IAW SRM 51-30.Sep 1, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9801609Stringer · corrodedINSPECTION FOUND STRINGER 21R CORRODED BETWEEN STA 360 AND 380. THE CORRODED AREA WAS CUT OUT AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 53-10-4.Sep 1, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9801608Cowl · crackedINSPECTION FOUND A 1 BY .25 INCH PIECE OF SKIN CRACKED OUT BY NOSE COWL OF NR 3 ENGINE UPPER FORWARD END OF FIXED COWL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-4, 51-30-2, AND MM 51-20-11.Sep 1, 1998 · N14788 · Boeing 727232 · Engine Cowling SystemSDR CALA9801607Floorbeam · corrodedINSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 328, LBL 29.5. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-2, AND MM 51-20-11.Sep 1, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801606Fairing · crackedINSPECTION FOUND A 1 INCH CRACK AT NUT PLATE HOLE OF LT BODY FAIRING PANEL NR 3337. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-40-3, FIGURE 1, 51-10-2, 51-30-2, AND MM 51-20-12.Sep 1, 1998 · N14788 · Boeing 727232 · Aerodynamic FairingsSDR CALA9801605Web · crackedINSPECTION FOUND LT WING O/B MID FLAP INBOARD WEB CRACKED AT INBOARD JACKSCREW FAIRING MOUNT BRACKET. THE CRACK WAS .75 LONG. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, 57-50-1, 51-10-2, 51-30-2, AND MM 51-20-11.Sep 1, 1998 · N14788 · Boeing 727232 · Trailing Edge FlapsSDR DL72S981805Fan · failedSMOKE AND FUMES IN COCKPIT AND CABIN, RAN CK LIST AND COULD NOT FIND SOURCE. ALSO, ELECTRICAL BURNT PLASTIC SMELL. INSPECTED COALESCER BAGS, CKS GOOD. INSPECTED E & E AREA, CKS GOOD. INSPECTED GALLEY AREA, CKS GOOD. FOUND SMELL COMING FROM GASPER FAN, RANAug 31, 1998 · N416DA · Boeing 727232 · Air Distribution FanSDR CALA9801596Seat Track · corrodedINSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 1030, RBL 24. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND MM 51-20-12.Aug 31, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801595Skin · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 389 BETWEEN STRINGERS 23R AND 24R. THE DAMAGED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-1 AND 51-20-4.Aug 30, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801594Skin · damagedINSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 373 BETWEEN STRINGER 22R AND 23R. THE DAMAGED AREA WAS CUT OUT IAW SRM 53-30-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2.Aug 30, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981790Switch · inoperativeRT PACK SWITCH FAULTY. INFLT BUMPED SWITCH TO INTERMEDIATE POS, CAUSING PACK TO NOT OPERATE AT FL 330. PAC APPEARED TO BE ON, BUT ACTUALLY WAS OFF. RESULT WAS DEPRESSURIZATION TO ABOVE 10,000 FT, CABIN ALT O2 DROPPED. CABIN ALT REGAINED IN STBY MODE AND SWAug 29, 1998 · N520DA · Boeing 727232 · Cabin Cooling SystemSDR CALA9801593Support · crackedINSPECTION FOUND A 1.5 INCH CRACK IN SIDEWALL SUPPORT ON RT SIDE AFT OF C-1 DOOR. THE CRACKED SECTION OF SUPPORT WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-0.Aug 29, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801592Frame · crackedINSPECTION FOUND A 1 AND 1.5 INCH CRACK IN DOOR FRAME AT FS 375 JUST FORWARD OF R-1 DOOR CUTOUT STRINGER 17R ABOVE FLOOR LINE. A DOUBLER, TRIPLER, AND FILLERS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-30, 51-10-2, AND MM 51-20.Aug 29, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801591Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER SLIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2.Aug 29, 1998 · N14788 · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L981873Web · crackedA .375 INCH CRACK IN TORQUE BOX VERTICAL WEB STA 1223 LT SIDE, ABOVE STAIRS CLOSE OUT PANEL. REPAIRED PER MM 53-11-0.Aug 28, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801590Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN LT INTERIOR FUSELAGE FRAME AT FS 910 AT STRINGER 15L. THE CRACKED AREA WAS TRIMMED OUT, A REPAIR WAS INSTALLED IAW SRM 51-30-2.Aug 28, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801582Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 29.5. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. DOUBLERS AND A TEE WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-40-3, 51-30-2, AND MM 51-20-1.Aug 28, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801581Track Guide · gougedINSPECTION FOUND THE OUTBOARD TRACK GUIDE FOR NR 3 SLAT INBOARD TRACK GOUGED. THE TRACK GUIDE WAS REMOVED AND A NEW GUIDE WAS INSTALLED IAW SRM 51-30-2.Aug 28, 1998 · N14788 · Boeing 727232 · Leading Edge DevicesSDR CALA9801580Angle · crackedINSPECTION FOUND .5 TO 1 INCH CRACKS IN INTERCOSTAL UPPER ANGLE AT FS 970 TO 990, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.Aug 28, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801579Stringer · corrodedINSPECTION FOUND STRINGER 23R CORRODED AT STA 477. THE CORRODED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11.Aug 28, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S981772Switch · failedAMBER LEADING EDGE FLAP LIGHT WOULD NOT EXTINGUISH WHEN FLAPS WERE MOVED FROM 5 TO 2 DEGREES. REPLACED RETRACT SWITCH ON NR 1 SLAT ACTUATOR.Aug 27, 1998 · N401DA · Boeing 727232 · Leading Edge Slat Position Indicating SystemSDR CALA9801565Frame · corrodedINSPECTION FOUND FUSELAGE FRAME CORRODED ON FORWARD SIDE AT STA 372 BETWEEN STRINGER 17R AND 20R. THE CORRODED SECTION WAS REMOVED AND A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.Aug 27, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR DL72S982067Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER WAS FOUND CRACKED IN 2 PLACES, 32 AND 37 FROM IB END. THE ANGLE WAS REPAIRED PER 727MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Aug 26, 1998 · N408DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981781Bulkhead Web · crackedTWO CRACKS OF .75 INCH LENGTH OR LESS WERE FOUND IN THE FS 1183 BULKHEAD WEB AT RBL 18 BETWEEN WL 166 AND 169 AND ONE .375 INCH CRACK WAS FOUND IN THE WEB AT LBL 25, WL 169. THE CRACKS WERE REPAIRED WITH A DOUBLER PER ER/A 365537-14 AND SET UP FOR REPETITIVE Aug 26, 1998 · N403DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S981779Skin · dentedTHE FUSELAGE SKIN AT FS 1067 WAS FOUND DENTED JUST O/B OF STRINGER 29R. THE DAMAGE WAS ADJACENT TO AND EXISTING DOUBLER REPAIR FOR ANOTHER SKIN CUTOUT. THE DENT WAS CUT OUT OF THE SKIN, THE EXISTING DOUBLER REMOVED, AND A NEW EXTERNAL ALUMINUM DOUBLER WAS INAug 26, 1998 · N538DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981770Battery Pack · dischargedFIRST CLASS CEILING EMERGENCY LIGHT OUT. REPLACED BATTERY PACK.Aug 26, 1998 · N475DA · Boeing 727232 · Emergency LightingSDR DL72S981769Battery Pack · dischargedFOUND LEFT OVERWING EMERGENCY EXIT LIGHT FWD POS INOP. REPLACED BATTERY PACK.Aug 26, 1998 · N475DA · Boeing 727232 · Emergency LightingSDR DL72L981895Angle · corrosionFOUND DURING MV2 CORROSION VISIT NRC 154, WHILE WORKING NRC 91 FOUND RT SKIN SUPPORT ANGLE CORRODED UNDER STR 27R STA 740. REPLACED SKIN SUPPORT ANGLE PER M/M 53-11-0 PG 859.Aug 26, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981890Stiffener · crackedA .625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFFENER PER M/M 57-20-21 PG 813.Aug 26, 1998 · N507DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L981872Frame · cracked2 INCH CRACK ON R-1 DOOR AFT FRAME AT LOWER CORNER. REPAIRED PER MM 52-12-0 FIG 804.Aug 26, 1998 · N507DA · Boeing 727232 · Passenger/Crew DoorsSDR CALA9801564Frame · crackedINSPECTION FOUND A 1 CRACK AT FASTENER HOLE OF WEB AT NR 2 CARGO DOORWAY FORWARD FRAME BS 950E. A REPAIR WAS INSTALLED IAW SRM 51-30-2.Aug 26, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801563Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING TIP RIB AT PANEL NR 8110. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 26, 1998 · N14788 · Boeing 727232 · Wing, Rib/BulkheadSDR CALA9801562Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 24-65. A CHORD, ANGLES, STRAPS, AND STIFFENERS WERE INSTALLED IAW SRM 53-10-8, FIGURE 1.Aug 26, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801561Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166 ABOVE STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11.Aug 26, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801560Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED WITH TWO .5 INCH CRACKS AT BS 1010 BETWEEN STRINGERS 27R AND 28R. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, FIGURE 1.Aug 26, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981765Bracket · crackedNR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED O/B LOWER END. FOUND ON D1 LETTER CK. REPAIRED PER MM 57-20-21.Aug 25, 1998 · N538DA · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9801529Frame · corrodedINSPECTION FOUND LT FUSELAGE FRAME CORRODED AT STA 340. A REPAIR WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.Aug 25, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801528Frame · gougedINSPECTION FOUND LT FUSELAGE FRAME GOUGED AT STA 560, WL 294. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1, 51-30-2, 51-10-2, AND MM 51-20-0.Aug 25, 1998 · N14788 · Boeing 727232 · Fuselage Main, FrameSDR CALA9801527Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 460 TO 480, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5, FIGURE 1, 51-10-2, AND MM 51-20-12.Aug 25, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
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