Boeing 727-232

Service difficulty reports · 6,539

Newest first. General aviation reporting is voluntary.

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 CALA9901636Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, LBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-4 AND 51-30-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901635Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBOARD SUPPORT ANGLE AT STA 1070, LBL 28. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901634Angle · corrodedINSPECTION FOUND LOWER WEB ATTACH ANGLE CORRODED AT STA 750. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1, PAGE 7.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901633Support · crackedINSPECTION FOUND A .5 INCH CRACK IN O/B FLOOR SUPPORT AT RT FUSELAGE WALL FS 760. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901632Seat Track · corrodedINSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 950-990, LBL 24 AND FROM STA 1070-1110, LBL 24. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-0, AND 51-10-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9901631Web · corrodedINSPECTION FOUND AFT DOOR AFT TORQUE BOX WEB CORRODED WITH A 1 INCH CRACK AT RIVET, FS 1090-1130, S27R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A WEB AND NUT PLATES WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 53-10-4.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901630Cusp · corrodedINSPECTION FOUND CUSP WEB SECTION CORRODED ON BOTTOM SIDE AT FS 1090-1110, RBL 58. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW 51-10-1, 53-10-2, 51-10-6, 51-30-0, AND MM 51-20-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901629Web · corrodedINSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS AT WING CENTER SECTION, FS 760 LOWER TORQUE BOX KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901628Web · corrodedINSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION, FS 790 LOWER TORQUE BOX AT KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-40-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901627Web · corrodedINSPECTION FOUND WEB CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION FS 800 LOWER TORQUE BOX KEEL AREA, S29L-29R. THE WEB WAS CUT OUT AND A NEW WEB SECTION AND SPLICE WERE INSTALLED IAW SRM 51-40-2, FIGURE 1, 51-30-6, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901626Intercostal · corrodedINSPECTION FOUND AFT CARGO INTERCOSTAL CORRODED UNDER AND ON TOP OF NUTPLATES AT FS 950A-950B, S26R-27R. A REPAIR WAS INSTALLED IAW SRM 51-30-1.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901625Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN SUPPORT ANGLE FOR BODY TO FUSELAGE FAIRING AT RT WING AFT VERY I/B T/E PANEL. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-3.Dec 16, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9901624Floor Panel · corrodedINSPECTION FOUND AFT PIT FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Floor PanelSDR CALA9901623Intercostal · crackedINSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL AT STA 480-500, S28L. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901622Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 4R AT STA 580-600. THE CRACKED SECTION OF STRINGER WAS CUTOUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 53-10-3, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9901621Support · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FS 555 BETWEEN STRINGER 23L AND 27L. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901620Support · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLES AT FS 1070-1050, LBL 55 AND AT FS 1130, BL 0 CORRODED. THE FLOOR SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-30-2, 51-10-2, AND 51-20-02.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901619Stiffener · crackedINSPECTION FOUND A 1.4 INCH CRACK IN STIFFENER AT STA 1183, LBL 35. REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, MM 51-20-0, AND ECRA 5310-01600.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901618Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, RBL 12. SUPPORT ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30-3.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901617Frame · crackedINSPECTION FOUND FRAME BENT AND CRACKED AT UPPER FLANGE, STA 540, L25L. THE FRAME WAS REFORMED AND THE CRACKED AREA WAS TRIMMED OUT IAW SRM 51-40-4. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-4.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901616Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN STIFFENER AT STA 1183, LBL 60. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901615Angle · corrodedINSPECTION FOUND LOWER WEB SUPPORT ANGLE CORRODED AT FS 780. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901614Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LEFT MLG WING DOOR ANGLE AT T/E LOWER CORNER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Landing Gear DoorsSDR CALA9901613Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 1148-1166, L26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901612Rib · crackedINSPECTION FOUND A 1 CRACK IN UPPER RUDDER AFT UPPER LEFT T/E RIB. A DOUBLER WAS INSTALLED IAW SRM 51-40-2.Dec 16, 1999 · N33785 · Boeing 727232 · Rudder, Spar/RibSDR CALA9901611Angle · corrodedINSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION, STA 760 LOWER TORQUE BOX KEEL AREA. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.Dec 16, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9901610Bracket · crackedINSPECTION FOUND A 3 INCH CRACK IN SUPPORT BRACKET AT LEFT WING L/E PANEL NR 6215. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9901609Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR INNER SKIN AT CUTOUT FOR HANDLE ON LOWER FORWARD SIDE. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6D, 51-40-2, AND 51-30-1.Dec 16, 1999 · N33785 · Boeing 727232 · Passenger/Crew DoorsSDR CALA9901608Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN RT I/B FLAP TRACK FAIRING SKIN. A DOUBLER WAS INSTALLED IAW SRM 51-30-0, 51-10-2, 51-30-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Wing, Plate/SkinSDR CALA9901607Panel · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER LE PANEL 9202 CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 51-10-5, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR CALA9901606Skin · damagedINSPECTION FOUND LEADING EDGE ACCESS PANEL SKIN OF VERTICAL STABILIZER WITH FASTENERS PULLING THROUGH AT STA 134. A DOUBLER WAS INSTALLED IAW SRM 55-30-7, 51-10-6, 51-20-0, AND 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S992762Bulkhead · crackedTHE WEB OF THE FS 1183 BULKHEAD WAS FOUND WITH A .75 INCH LONG TYPICAL CRACK AT RBL 26 AND WL 169. THE CRACK IS TYPICAL OF BOEING S/B 727-53-0215. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER THE S/B AS DOCUMENTED IN ER/A 368897-14.Dec 15, 1999 · N540DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S992751Skin · crackedFOUND ON C1 LETTER CK, .375 INCH CRACK ON SKIN AT THE LOWER I/B FASTENER OF THE L4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.Dec 15, 1999 · N409DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K992754Battery Pack · dischargedEMERGENCY LIGHTS ON AFT CARGO DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK.Dec 15, 1999 · N495DA · Boeing 727232 · Emergency LightingSDR CALA9901642Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 360, BL 0 TO RBL 35. REPAIR ANGLES, FILLER, AND EXTRUSION WERE INSTALLED IAW SRM 53-10-8, FIGURE 8.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9901639Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN TRANSITION PANEL STRAP AT FS 720, RT FORWARD PIT. A NEW STRAP WAS INSTALLED IAW SRM 51-10-2.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901605Bracket · corrodedINSPECTION FOUND BRACKET CORRODED AT FS 700B, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901604Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN BRACKET AT FS 720C, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901603Angle · corrodedINSPECTION FOUND ATTACH ANGLE CUT AND CORRODED AT C-1 DOOR CUTOUT LOWER FORWARD SECTION, STA 540, STRINGER 26R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901602Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN VERTICAL SUPPORT LOWER END ATTACH BRACKET AT STA 1193, LBL 20. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901601Strap · crackedINSPECTION FOUND A 2.5 CRACK IN STRAP UNDER FLOORBEAM IN FORWARD CABIN AREA AT STA 328-344, LBL 50. THE STRAP WAS REPAIRED BY INSTALLING A DOUBLER IAW SRM 51-30-2 AND 51-40-3.Dec 15, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L992806Frame · dentedFRAMES DAMAGED AT STA 580, 600, 660 AND 700 AT STRINGER 22L. NEW SECTIONS BEING SPLICED IN ER/A 333911-14 REV A.Dec 14, 1999 · N512DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L992724Angle · corrodedON HUSH-KIT MOD, FOUND LT NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT AFT MOUNT SUPPORT CHORD ANGLE WITH ONE OF NEW MFG.Dec 13, 1999 · N511DA · Boeing 727232 · Engine Mount SectionSDR DL72L992744Track · corrodedINBOARD FLAP / NR 5 INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, AND WEAR AT FWD ATTACH LUGS AND MLG DOOR HINGE FITTING HOLES. AUTHORIZED BLEND REPAIRS AND OVERSIZED FASTENERS.Dec 12, 1999 · N501DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S992706Bracket · crackedA 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21.Dec 10, 1999 · N407DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L992725Angle · corrodedON HUSH-KIT MOD, FOUND RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH ONE OF NEW MFG.Dec 10, 1999 · N511DA · Boeing 727232 · Engine Mount SectionSDR CALA9901588Battery Pack · dischargedINSPECTION FOUND THE EMERGENCY LIGHT AT AFT AIRSTAIR INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED, OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.Dec 10, 1999 · N45793 · Boeing 727232 · Emergency LightingSDR CALA9901587Wire · brokenINSPECTION FOUND THE EMERGENCY PATH LIGHTS IN SECTION 3 AND 4 INOPERATIVE. BROKEN WIRES AT SECTION 3 AND 4 WERE REPAIRED IAW MM 33-10-00 AND OPERATIONAL CHECK WAS GOOD.Dec 10, 1999 · N45793 · Boeing 727232 · Light System WiringSDR CALA9901586Battery Pack · dischargedTHE RT OVERWING EMERGENCY EXIT LIGHTS IN THE MID AND AFT POSITIONS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6.Dec 10, 1999 · N45793 · Boeing 727232 · Emergency LightingSDR CALA9901585Battery · dischargedINSPECTION FOUND MID CABIN FIXED EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-00, PAGE 6.Dec 10, 1999 · N45793 · Boeing 727232 · Emergency Lighting
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