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 CALA9801815Chord · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2.Sep 18, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801814Stiffener · corrodedINSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4.Sep 18, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981957Stringer · crackedSTRINGER 8R WAS FOUND WITH A CRACK THROUGH THE INBD FLANGE AT A RIB ATTACH POINT WHICH PROGRESSED TO THE CENTER OF THE STRINGER WEB. THE CRACK WAS REPAIRED WITH TWO ALUMINUM ANGLES PER ER/A 365679-14, REV A.Sep 17, 1998 · N527DA · Boeing 727232 · Vertical StabilizerSDR CALA9801811Stiffener · corrodedINSPECTION FOUND VERTICAL STIFFENER CORRODED AT RT FUSELAGE STA 340. A NEW STIFFENER WAS INSTALLED IAW ECRA 5300-01196 AND SRM 51-30-2.Sep 17, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801810Stringer · corrodedINSPECTION FOUND STRINGER 25R CORRODED AT STA 1140 TO 1183. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3.Sep 17, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S981942Stiffener · damagedWING UPPER SURFACE J STIFFENER REPAIR (STR 17 RT AT WS 300). REPAIR PER ER/A 332215-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S981941Clip · crackedFS 400 FRAME CLIP BETWEEN STR 17 AND 18 WAS FOUND CRACKED. REPAIRED PER ER/A 332224-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981940Stringer Tab · crackedSTRINGER 18 TAB ON THE RT WING VENT BOX WAS FOUND CRACKED. REPAIR PER ER/A 332222-14.Sep 16, 1998 · N408DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S981939Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN, SIMILAR TO S/B 727-53-0172. STRINGER 18A LOWER FLANGE WAS FOUND WITH A CRACK. REPAIR PER ERA 332141-14.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981938Chord · gougedTHE C-2 DOOR STA 990 INBOARD CHORD WAS FOUND WITH A GOUGE AT STRINGER 26R. THE GOUGE WAS LOCATED ON THE OUTER CORNER OF THE INTERSECTION OF THE 2 LEGS OF THE L-SHAPED CHORD. REPAIRED PER ER/A 332209-14 REV A.Sep 16, 1998 · N408DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801798Angle · corrodedINSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3.Sep 16, 1998 · N14788 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801797Mechanism · out of adjustTHE LT FORWARD OVERWING EMERGENCY EXIT DOOR FAILED PULL CHECK. THE PULL FORCE ON THE DOOR WAS ADJUSTED TO SPECIFICATION IAW MM 52-21-0.Sep 16, 1998 · N14788 · Boeing 727232 · Emergency ExitsSDR CALA9801796Skin · corrodedINSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2.Sep 16, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801790Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 1090 TO 1130, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.Sep 16, 1998 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801789Skin · delaminatedINSPECTION FOUND LT INBOARD AILERON TAB TRAILING EDGE SEPARATED IN TWO AREAS. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11.Sep 16, 1998 · N15790 · Boeing 727232 · Aileron TabsSDR CALA9801788Bracket · corrodedINSPECTION FOUND NR 7 SPOILER ATTACH SUPPORT BRACKET CORRODED. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 16, 1998 · N15790 · Boeing 727232 · SpoilersSDR CALA9801787Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6.Sep 16, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801786Battery · dischargedINSPECTION FOUND MAIN CABIN EMERGENCY LIGHT AT ROW 8 HAD A WEAK BATTERY. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-50-00.Sep 16, 1998 · N15790 · Boeing 727232 · Emergency LightingSDR CALA9801785Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1065, STRINGER 28R. THE CORROSION WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-40-3 AND 51-10-6.Sep 16, 1998 · N15790 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9801784Skin · corrodedINSPECTION FOUND RT ELEVATOR LOWER SKIN CORRODED JUST AFT OF OUTBOARD LEADING EDGE TIP WEIGHT. THE CORRODED SKIN WAS REMOVED. NEW SKIN WAS INSTALLED IAW SRM 51-30-2 AND 51-40-5.Sep 16, 1998 · N15790 · Boeing 727232 · Elevator, Plate/SkinSDR CALA9801783Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN OUTBOARD ANGLE BRACKET UNDER J-BEAM AT RT WING NR 8 SPOILER. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.Sep 16, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9801782Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 7 SPOILER SUPPORT BRACKET SIDE BRACE ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.Sep 16, 1998 · N15790 · Boeing 727232 · SpoilersSDR DL72S982077Rib · crackedAT HMV, FOUND RIB NR 5 AND RIB NR 15 CRACKED. ROUTED FRAME 5. REPAIRED DOUBLER AND FILLER AS PER M/M 57-54-0 FIG 814. OK TO INST REPAIR NR 5 RIB. INSTALLED REPAIR ON NR 5 RIB PER M/M 57-54-0 FIG 814. BEGAN MAKING DOUBLER. FINISHED ROUTING RIB NR 15. REPSep 15, 1998 · N409DA · Boeing 727232 · Leading Edge DevicesSDR DL72S982076Frame · crackedAT HMV, FOUND FRAME CRACKED FS 930 BETWEEN STR 13R - 14R JUST ABOVE REPAIR. REMOVED DAMAGED PORTION OF FRAME. BEGAN DRILLING FRAME REPAIR, DRILLED FRAME REPAIR. TREATED AND PAINTED PER PS 900-3-6 NR 3. OK TO INSTALL, BEGAN INSTALL. COMPLETED INSTALL OF FRSep 15, 1998 · N409DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S981919Ball Nut · rustedAT HMV, LANDING GEAR CHECK OUT THE NOSE GEAR EMERGENCY EXTENSION FAILED TO OPERATE DUE TO THE BALL NUT AND SCREW ASSY BEING RUSTED AND FROZEN UP. REF IPC 32-31-00-06 ITEM 185 (P/N 10-60744-1). THE ASSY WAS REPLACED AND THE CHECK OUT COMPLETED SATISFACTORY.Sep 15, 1998 · N408DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S981918Rib · crackedUPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. REPAIRED PER ERA 332223-14.Sep 15, 1998 · N408DA · Boeing 727232 · Wing, Rib/BulkheadSDR DL72L981922Battery Pack · dischargedLAYOVER FOUND L-2 AND R-2 SLIDE EMERGENCY LIGHTS INOP. REPLACED M983 SLIDE LIGHT BATTERY PACK, OPN CKS OK.Sep 15, 1998 · N509DA · Boeing 727232 · Emergency LightingSDR CALA9801777Chord · corrodedINSPECTION FOUND SHEAR TIE T-CHORD CORRODED AT STA 351.5, BL 0, WL 148.5. THE T-CHORD WAS REMOVED AND A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-02.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801776Stringer · corrodedINSPECTION FOUND STRINGER 23R CORRODED AT LOWER NOSE WHEEL WELL RT LAP SEAM STA 294.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9801775Skin · impactedINSPECTION FOUND LIGHTNING STRIKE DAMAGE TO C-1 DOOR SKIN. DOUBLER WAS INSTALLED IAW SRM 52-00-3, FIGURE 4 AND ECRA 5232-01004.Sep 15, 1998 · N14788 · Boeing 727232 · Cargo/Baggage DoorsSDR CALA9801774Skin · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 448 TO 451, STRINGER 25R, AND AT STA 380, STRINGER 23R. DOUBLERS WERE INSTALLED IAW SRM 53-30-3.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801773Seat Track · corrodedINSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1136, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-2, 51-10-2, 51-30-2, AND MM 51-20-12.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801772Channel · crackedINSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3.Sep 15, 1998 · N14788 · Boeing 727232 · Nacelle/Pylon StructureSDR CALA9801771Strap · corrodedINSPECTION FOUND AFT CARGO PIT LT LOWER SIDE WALL PANEL STRAP CORRODED AT STA 1050. A NEW STRAP WAS INSTALLED IAW SRM 51-10-6.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801770Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 65 TO LBL 65. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-8, FIGURE 9, AND MM 51-20-12.Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S981912Web · crackedREF A/C 495 TPA LTR CHECK C-1, VERTICAL WEB CRACKED .5 INCH LT SIDE LWR LIGHTENING HOLE STA 1228. REPAIRED PER MM 53-11-0.Sep 14, 1998 · N495DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801761Floor · corrodedINSPECTION FOUND LT AFT SINK DRAIN FLOOR AREA CORRODED. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, PAGE 6 AND 51-10-2.Sep 14, 1998 · N15790 · Boeing 727232 · Fuselage Floor PanelSDR CALA9801756Panel · corrodedINSPECTION FOUND LT TRANSITION PANEL CORRODED IN FORWARD CARGO PIT AT FS 660 TO 720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801755Panel · corrodedINSPECTION FOUND FLOOR TRANSITION PANEL CORRODED AT BS 720A-720D, STRINGER 26R. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801754Panel · corrodedINSPECTION FOUND RT TRANSITION PANEL CORRODED AROUND NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 620-720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-12.Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801753Floor Pan · corrodedINSPECTION FOUND CABIN INTERIOR CENTER AISLE FLOOR PAN CORRODED AT BS 1173, RBL 22. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-30-2, 51-10-6, MM 51-20-11.Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801735Frame · crackedINSPECTION FOUND A 3.5 INCH CRACK AT FORWARD LOWER SIDE OF NR 3 CARGO DOOR FRAME BETWEEN STRINGER 25R AND 26R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-4.Sep 14, 1998 · N15790 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801734Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT INNER SKIN AT OUTBOARD STRIKER PLATE AREA. THE OUTBOARD STRIKER SKIN PLATE WAS REPLACED IAW SRM 51-10-1 AND 51-30-2.Sep 14, 1998 · N15790 · Boeing 727232 · Leading Edge DevicesSDR CALA9801733Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER OUTBOARD CORNER OF CAPTAIN'S WINDSHIELD CUTOUT AND A .125 INCH CRACK WAS FOUND IN SKIN AT LOWER FORWARD CORNER JUST FORWARD OF CAPTAIN'S SLIDING WINDOW. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE Sep 14, 1998 · N15790 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9801732Tab · debondedINSPECTION FOUND LT ELEVATOR TAB INBOARD MOST TRAILING EDGE AREA DEBONDED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.Sep 14, 1998 · N15790 · Boeing 727232 · Elevator, Tab StructureSDR DL72S981899P & D Valve · failedNR 3 ENG FAILED INITIALLY FELT SLIGHT SWERVE AND EPR DROPPED WHEN THE THROTTLE WAS ADVANCED. THE ENG CONTINUED TO SPOOL DOWN TO WINDMILLING. REPLACED P/D VALVE.Sep 13, 1998 · N400DA · Boeing 727232 · Fuel Controlling SystemSDR DL72S981896Rib · crackedFOUND ON L/O CK, NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED AT FWD END. REPAIRED PER MM 57-54-0.Sep 13, 1998 · N528DA · Boeing 727232 · Leading Edge DevicesSDR DL72L981898Web · crackedFOUND ON MV2 CK, .5 INCH CRACK IN THE STA 1309 WEB LEFT SIDE ABOVE THE S DUCT. REPAIRED PER SRM 53-10-4.Sep 13, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L981897Web · crackedFOUND ON MV2 CK, 1 INCH AND .5 INCH CRACKS FOUND IN STA 1309 WEB RT SIDE ABOVE S DUCT. REPAIRED PER SRM 53-10-4.Sep 13, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9801730Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT FS 303.9, LBL 0 TO 12. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
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