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"

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 CALA9802037Fuse · blownINSPECTION FOUND LT AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE AND OPERATION CHECKED GOOD IAW MM 33-51-00.Nov 4, 1998 · N45793 · Boeing 727232 · Emergency LightingSDR CALA9802036Skin · delaminatedINSPECTION FOUND TOP SURFACE OF NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-81.Nov 4, 1998 · N45793 · Boeing 727232 · SpoilersSDR CALA9802034Stiffener · corrodedINSPECTION FOUND STIFFENER IN NOSE WHEEL WELL AT FS 300, RBL 12 TO LBL 12 CORRODED. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1.Nov 4, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9802033Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN LT O/B MIDFLAP I/B MOST RIB. THE CRACK WAS STOP DRILLED AND A REINFORCING ANGLE WAS INSTALLED IAW SRM 51-40-3 AND 51-10-2.Nov 4, 1998 · N59792 · Boeing 727232 · Trailing Edge FlapsSDR CALA9802032Shear Tie · corrodedINSPECTION FOUND FRAME TO SKIN SHEAR TIE CORRODED AT STA 720C, STRINGER 28R TO 28L. A REPAIR WAS INSTALLED IAW SRM 53-10-4 PAGE 52.Nov 4, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S982369Skin · crackedSKIN CRACKED APPROX 1.5 ON LWR SURFACE OF RT ELEV FWD AND I/B OF TAB CONTROL ROD. DYE CHECKED AND STOP DRILLED CRACKS, FABRICATED REPAIR PART PER SRM 55-20-3 FIG 5. OK TO INSTALL. INSTALLED DOUBLER, FASTENERS AND DOUBLE WEIGH 63G PER SRM 55-20-3 FIG 5.Nov 3, 1998 · N406DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S982363Angle · damagedNR 4 SLAT, ANGLE CRACKED IN CORNER. DYE CHECKED PER PS 900-6-3. NO CRACK FOUND. BURNISHED AREA, TREATED AND PAINTED PER PS 900-2 NR 5.Nov 3, 1998 · N406DA · Boeing 727232 · Leading Edge DevicesSDR CALA9802031Chord · crackedINSPECTION FOUND A .3125 INCH CRACK IN LOWER CHORD OF LT WING NR 2 SLAT AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-4 PAGE 11 AND 51-10-1 PAGE 6B.Nov 3, 1998 · N59792 · Boeing 727232 · Leading Edge DevicesSDR CALA9802030Plate · crackedINSPECTION FOUND A 1.25 INCH CRACK IN PLATE INSIDE LT I/B MIDFLAP AT I/B CARRIAGE SPINDLE CUTOUT ACCESS THROUGH PANEL 8443. THE PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 57-50-4 FIGURE 4.Nov 3, 1998 · N59792 · Boeing 727232 · Trailing Edge FlapsSDR CALA9802029Rib · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LT WING TIP RIB INSIDE OVAL ACCESS CUTOUT 8111. A REPAIR WAS ACCOMPLISHED IAW SRM 51-40-3, PAGE 3.Nov 3, 1998 · N59792 · Boeing 727232 · Wing, Rib/BulkheadSDR CALA9802028Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN O/B LOWER END OF SUPPORT BRACKET WHERE LT WING NR 1 L/E FLAP ACTUATOR MOUNTS INSIDE LEADING EDGE. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-20-2 FIGURE 7.Nov 3, 1998 · N59792 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9802027Frame · crackedINSPECTION FOUND THREE .75 INCH CRACKS IN VERTICAL FIN FRAME ON TOP OF S-DUCT AT FRAME 1303. A REPAIR WAS INSTALLED IAW SRM 51-40-2 PAGE 1 AND 51-30-2 PAGE 4.Nov 3, 1998 · N59792 · Boeing 727232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA9802026Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 320, LBL 20 TO 48. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT IAW SRM 53-10-8. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-8 AND 51-10-2 PAGE 12.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9802025Channel · corrodedINSPECTION FOUND RT AFT LAV FORWARD HAT CHANNEL FOR WALL CORRODED AT STA 1140, RBL 20 TO WALL. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-2 PAGE 4.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9802024Structure · corrodedINSPECTION FOUND RT AFT LAV SUBFLOOR CORRODED. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2 PAGE 4, 51-10-6 PAGE 2 AND 51-10-2 PAGE 1.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Main, StructureSDR CALA9802023Angle · corrodedINSPECTION FOUND RT AFT LAV DOOR ENDWALL ANGLE AND HAT BRACKET CORRODED AT STA 1130 TO 1183, RBL 20. A REPAIR WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9802022Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED IN RT AFT GALLEY AREA AT STA 1090 TO 1110, RBL 20. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5 AND 51-30-2.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9802021Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 1070, BL 0 TO RBL 52. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-10-8 PAGE 13.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9802020Web · corrodedINSPECTION FOUND CORROSION UNDER ANCHOR NUTS ON BOTTOM OF FLOOR WEB AT TWO DOUBLERS BETWEEN BS 1130 AND 1148, RBL 24 TO 42. THE WEB SECTION WAS REMOVED AND A NEW WEB SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-2 PAGE 4 AND 51-30-20 PAGE 1.Nov 3, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9802019Stiffener · corrodedINSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2.Nov 3, 1998 · N45793 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9802018Spar · crackedINSPECTION FOUND A .5 INCH CRACK IN LT ELEVATOR REAR SPAR. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1, PAGE 401 AND 402. RIG AND OPERATIONAL CHECK WAS ACCOMPLISHED IAW MM 27-30-81 PAGE 507.Nov 2, 1998 · N45793 · Boeing 727232 · Elevator, Spar/RibSDR CALA9802017Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOOR LEVEL RIB AT RT SIDE OF STA 344. A STRAP WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8 FIGURE 6.Nov 2, 1998 · N45793 · Boeing 727232 · Fuselage Main, FrameSDR CALA9802016Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN C-3 DOOR T-ANGLE AT LOWER AFT DOOR STOP AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-101.Nov 2, 1998 · N45793 · Boeing 727232 · Cargo/Baggage DoorsSDR CALA9802015Chord · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD AT WBL 135.2. THE CRACKED AREA WAS CUT OUT AND SPLICE ANGLE AND STRAPS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, ECRA 5740-01866.Nov 2, 1998 · N45793 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9802013Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR UPPER HINGE FITTING. THE UPPER HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.Nov 2, 1998 · N59792 · Boeing 727232 · Service DoorsSDR CALA9802012Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED IN RT AFT GALLEY AREA AT STA 1080-1110, RBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-5, PAGE 1 AND 51-30-02 PAGE 4.Nov 2, 1998 · N59792 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9802011Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD SUPPORT BRACKET AT LOWER END WHERE LT WING NR 1 L/E FLAP ACTUATOR IS MOUNTED. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-30-2, PAGE 3.Nov 2, 1998 · N45793 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9802010Skin · puncturedINSPECTION FOUND TWO .25 INCH DIAMETER HOLES IN RT ELEVATOR UPPER SKIN JUST AFT OF NR 3 ATTACH HINGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-20-3, PAGE 9.Nov 2, 1998 · N45793 · Boeing 727232 · Elevator, Plate/SkinSDR DL72S982244Fan · failedBURNING SMELL COMING FORM GASPERS. PAX NOTICED SMELL WHICH QUICKLY DISSAPATED. AFTER ARRIVING AT GATE GASPER FAN CB WAS FOUND OPEN. ALSO, PAX REPORT SMOKE WAS VISIBLE AROUND AIR EYELETS AT ROWS 16, 17, 18 SMOKE HAD A PLASTIC SMELL. SMOKE STOPPED AND DISIPANov 1, 1998 · N525DA · Boeing 727232 · Air Distribution FanSDR DL72S982252Coffeemaker · failedINDICATION OF SMOKE OBSERVED BY FLT ATTEND IN AFT GALLEY AND AFT CABIN. REPLACED COFFEEMAKER AND CANNON PLUG.Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/GalleysSDR DL72S982242Battery Pack · dischargedRT WING INTERIOR EMERGENCY EXIT LIGHTS TEST OK BUT DO NOT OPERATE IN THE ARMED POSITION. REPLACED BATTERY PACK.Oct 31, 1998 · N469DA · Boeing 727232 · Emergency LightingSDR DL72S982241Connector · shortedSMOKE IN AFT CABIN. FOUND THE CANNON PLUG FOR THE NR 3 COFFEEMAKER IN THE AFT GALLY SHORTED. PULLED AND COLLARD C/B, DISCONNECTED CANNON PLUG FROM COFFEEMAKER.Oct 31, 1998 · N536DA · Boeing 727232 · Buffet/GalleysSDR DL72S982231Module · leakingIN ROUTE, LOSS OF SYS -B- PRESS ENGAGED NR 2 -B- PUMP BOTH LOW PRESS LIGHTS ILLUMINATED. SYS -B- QTY READS ZERO, SYS -A- QTY READS 2 GAL. ACCOMPLISHED POM HYD SYS -B- LOSS PROCEDURE, NORM BRAKING USED FOR LANDING. UPON INSPECTION, FOUND -B- SYSTEM PRESSURE MOct 29, 1998 · N542DA · Boeing 727232 · Hydraulic Indicating SystemSDR DL72K982236Fitting · crackedO/B SUPPORT FOR ACTUATOR FITTING LOBE CRACKED AT NR 7 SLAT. REPAIRED PER MM 57-42-0.Oct 29, 1998 · N529DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S982225Bracket · crackedREF. SHIP 545 TPA LTR. CHECK C2 10/28/98, NO. 6 L/E FLAP ACTUATOR SUPPORT BOX FOUND CRACKED AT UPPER I/B ANGLE. REPAIRED PER MM 57-20-21 PG. 811Oct 28, 1998 · N545DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S982220Wire · shortedFOUND ON MAINT PREFLIGHT ROWS 12-19 EMERGENCY TRACK LIGHTINGINOP REPLACED BLOWN FUSE ON FWD POWER SUPPLY AFTER REPAIRINGBARE WIRES UNDER SEAT ROW 12 DEF LIGHT OPN NORMAL REPLACED FWD BATTERY PRECAUTIONARY.Oct 28, 1998 · N411DA · Boeing 727232 · Light System WiringSDR CALA9802001Skin · crackedINSPECTION FOUND A 5/16 CRACK IN L/H WING OUTBOARD FOREFLAP LEADING EDGE ABOVE #1 SEQUENCE CARRIAGE AREA. A REPAIR WAS INSTALLED IAW SRM 57-50-4, PAGES 16 AND 17, FIGURE 7.Oct 27, 1998 · N59792 · Boeing 727232 · Trailing Edge FlapsSDR CALA9802000Angle · crackedINSPECTION FOUND LOWER LEADING EDGE TO RIB SUPPORT ANGLE CRACKED AROUND EIGHT BOLT HEADS INSIDE L/H WING LEADING EDGE AT OUTBOARD SIDE OF RIB, FSS 121. THE RIB SUPPORT ANGLE WAS REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-1, AND 51-10-Oct 27, 1998 · N59792 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801999Skin · crackedINSPECTION FOUND A 3/16 CRACK IN R/H WING UPPER TRAILING EDGE OUTBOARD HINGE CUTOUT AT #11 SPOILER HINGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-1, AND 57-30-4, PAGE 29.Oct 27, 1998 · N59792 · Boeing 727232 · Wing, Plate/SkinSDR CALA9801998Skin · dentedINSPECTION FOUND L/H UPPER RUDDER SKIN DENTED FOUR INCHES FROM LEADING EDGE AND APPROXIMATELY TWENTY INCHES DOWN FROM RUDDER ACTUATOR PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 55-20-3, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, FIGURE 1 AND 51-10-2.Oct 27, 1998 · N59792 · Boeing 727232 · Rudder, Plate/SkinSDR CALA9801997Stringer · crackedINSPECTION FOUND A 7/16 CRACK AT R/H WING AFT VENT BOX STRINGER AFT MOUNT LEG, WS 656.50. THE CRACK WAS STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-2, EA 5762-01050, AND MM 28-20-00.Oct 27, 1998 · N59792 · Boeing 727232 · Wing, Longeron/StringerSDR CALA9801996Side Wall · crackedINSPECTION FOUND 1/4 CRACKS IN NLG WHEEL WELL TOP CENTER, TOP RIGHT, AND RIGHT SIDEWALL PANELS. THE CRACKED AREAS WERE REMOVED AND FILLER AND DOUBLER REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-2, PAGE 4.Oct 27, 1998 · N59792 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801994Skin · crackedINSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 440 ABOVE STRINGER 25R. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.Oct 27, 1998 · N59792 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801993Skin · debondedINSPECTION FOUND L/H INBOARD AILERON TAB DEBONDED AT UPPER SKIN AND TRAILING EDGE AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11.Oct 27, 1998 · N59792 · Boeing 727232 · Aileron TabsSDR CALA9801992Terminal · inopINSPECTION FOUND L-1 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED TERMINAL AT LIGHT SOCKET ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD AT MM 33-60-00, PAGE 201.Oct 27, 1998 · N45793 · Boeing 727232 · Emergency LightingSDR CALA9801991Wire · looseINSPECTION FOUND THE L-2 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN HARNESS. THE WIRE WAS REPQIRED AND OPERATIONAL CHECKS WERE GOOD IAAW MM 33-60-01, PAGE 201.Oct 27, 1998 · N45793 · Boeing 727232 · Light System WiringSDR DL72S982215Frame · crackedA .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME FWD END APPROX 6 BELOW UPPER STOP CASTING. REPAIRED PER SRM 53-10-9 FIG 11.Oct 26, 1998 · N496DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S982214Bracket · crackedFOUND ON C-1 LETTER CK, NR 1 SLAT I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.Oct 26, 1998 · N496DA · Boeing 727232 · Leading Edge DevicesSDR DL72S982440Skin · corrodedA SKIN BULGE AND TWO CRACKED FASTENER HOLES WERE DISCOVERED AT BS 681, 8 INCHES ABOVE STRINGER 14R. UPON FURTHER INSPECTION CORROSION WAS FOUND ON THE I/B SIDE OF THE WINDOW BELT SKIN PANEL. REPAIRED PER ERA 332473-14.Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S982439Frame · damagedLOWER LOBE FRAMES IN THE AFT B/B AT BS 1030 WERE FOUND DENTED BETWEEN S26R AND 27R. MISDRILLED HOLES WERE DONE DURING ACCOMPLISHMENT OF SRM REPAIR. REPAIRED PER ERA 332463-14AD.Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, Frame
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