Boeing 737-232

Service difficulty reports · 1,700

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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 = '737232'
  ORDER BY difficulty_date DESC"

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SDR ABXR2019071900294Skin · corrodedCORRODEDJul 19, 2019 · N316CM · Boeing 737232 · Wing, Plate/SkinSDR NACA2019021200027Tee Fitting · crackedNOSE LANDING GEAR - CRACKS FOUND ON SUPPORT STRUCTURE FOR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED TEE ANGLE PN: 65-45819-45 AND GUSSET 65-45819-45, REF BOEING DRAWING 65-45819 AND B737-200 SRM 51-10-1, 51-30-2, 3 AND 5. NDT OPEN HOLES REF NDT MANUAL PARFeb 4, 2019 · N321DL · Boeing 737232 · Nose/Tail Landing GearSDR NACA2018082800067Skin · crackedFUSELAGE SKIN WAS CRACKED, BS 468, STRINGER 16R. A REPAIR WAS INSTALLED IAW SRM 53-30-03, FIG 48, DETAIL XI, PROCEDURE VII.Aug 27, 2018 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2018080600066Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER 16R JUST AFT OF BS 480. A DOUBLER AND TRIPLER WAS INSTALLED IAW SRM, 53-30-03, REPAIR 48, DETAIL VII.Aug 6, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2018071800002Skin · cracked3 INCH LONG CRACK FOUND IN FUSELAGE SKIN DIRECTLY BELOW S23R AT BS 344. CAT B REPAIR INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL XVIII.Jul 16, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2018031400001Skin · crackedSKIN CRACK FOUND ON RIGHT SIDE FUSELAGE S16R AND BS445 (VERIFIED WITH HFEC). DAMAGE REMOVED, DOUBLER INSTALLED REF SRM 53-30-3, FIG 48, REV SEP 2016. DETAIL XI AND III, PROCEDURE VII.Mar 12, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2017080900045Pump · weakNR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. RAN ENGINES, NO FAULTS. CLEANED SUMP TUBE AND DRAINED WATER. CHECKED RESERVOIR PRESSURE FILTER BOWL AND REMOVED WATER. CHECKED CASE DRAIN FILTERS FOR BOTH ENGINES. NO METAL FOUND IAW AMM 29-11-00, Aug 9, 2017 · N320DL · Boeing 737232 · Hydraulic Pump (Electric/Engine), MainSDR NACA2017072000044Engine · failedNR 2 ENGINE FAILED AT 2000 FEET ON TAKEOFF. MI AT 1705 FEET DURING CLIMB, LOUD NOISE FROM NR 2 ENGINE, NO EPR, SMOKE IN COCKPIT, AND ENGINE VIBRATION. NR 2 ENGINE HAD A FAILURE OF MULTIPLE STAGES OF THE TURBINE SECTION. THE ENGINE AND THRUST REVERSER WERE REMJul 18, 2017 · N321DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR NACA2017022700018Floorbeam · corrodedCORROSION ON TOP SURFACE OF FLOORBEAM AT BS 827 LBL 49 - 56. CORROSION BLENDED OUT OF LIMITS IAW SRM 53-10-1, FIG 1, REV 113. REPAIRED THE FLOORBEAM IAW DWG R23093.1-053-023-001, REV NC.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA2017022700016Frame · crackedCRACKED FRAME AT BS 787, RBL42, STRINGER 13R. REPAIRED IAW SR 4-3658265861, & 8100-9.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2017022700012Fitting · corrodedRIGHT OUTBOARD FLAP, NR 7 CARRIAGE SUPPORT FITTING CORRODED ON THRUST BEARING SURFACE (IN MID FLAP). REPLACED WITH REPAIRED ASSY.Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge FlapsSDR NACA2017022700011Spindle · corrodedLEFT OUTBOARD FLAP, NR 1 CARRIAGE SPINDLE CORRODED. THE CARRIAGE WAS REPLACED IAW MM 27-51-81, REV 123.Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge FlapsSDR NACA2017022700009Flap Track · damagedRIGHT INBOARD FLAP OUTBOARD TRACK REPAIR BUSHING CAD PLATING DETERIORATED. FLAP TRACK REPLACED IAW AMM 27-51-161, REV 12.Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge FlapsSDR NACA2017022700007Bulkhead Web · crackedCRACKED RIVETS ON BS 1016 BULKHEAD WEB BETWEEN STRINGERS 5 - 7L. REPAIRED IAW SRM 113 53-10-4, FIGURE 15.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, BulkheadSDR NACA2017022700005Intercostal · crackedCRACK IN RADIUS OF INTERCOSTAL AT BS 294.5, STRINGER 14R. REPLACED THE INTERCOSTAL IAW SERVICE BULLETIN 737-53A1241 REV 1.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2017022700019Support Fitting · crackedCRACK FOUND IN RIGHT AFT SUPPORT FITTING FOR MAIN LANDING GEAR AT RSS 224. REPLACED THE SUPPORT FITTING IAW SERVICE BULLETIN 737-57-1216, REV 2, & SR 4-3648350626, AND 8100-9.Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Landing Gear Attach FittingsSDR NACA2017022700017Angle · crackedANGLE CRACKED AT BS 663, LBL 24.82. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW DWG PL65-45410 REV DD, BSB 737-57A1296, SRM D6-15565 REV 113, AND 51-30-02.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2017022700015Stringer Clip · crackedCRACKED STRINGER CLIP BS 663, STRINGER 10R, REPLACED THE STRINGER CLIP IAW SRM 51-30-2, REV 113.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA2017022700014Stringer Clip · crackedCRACKED STRINGER CLIP BS 663, STRINGER 10L, WL 256. REPLACED THE STRINGER CLIP IAW SRM 51-30-2 REV 113, & DWG 65-46541 REV H.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA2017022700013Attach Fitting · corrodedRIGHT OUTBOARD FLAP, NR 8 TRACK FORWARD ATTACH FITTING (ON WING) HAS EVIDENCE OF CORROSION BETWEEN TRACK ATTACH BUSHINGS. REPLACED THE FWD ATTACH FITTING IAW BAC5047, AMM 20-50-11 REV 123, & DWG 65-45455 REV E.Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Control Surface Attach FittingsSDR NACA2017022700010Flap Track · corrodedLEFT OUTBOARD FLAP NR 1 TRACK CORRODED. REPLACED THE FLAP TRACK IAW AMM 27-51-151, REV 123.Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge FlapsSDR NACA2017022700008Bulkhead Web · crackedONE CRACK ON BS 1016 BULKHEAD WEB AT STRINGER 15R. REPAIREDTHE BULKHEAD WEB IAW SR 4-3633491853, & 8100-9.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, BulkheadSDR NACA2017022700006Intercostal · crackedCRACK IN RADIUS OF INTERCOSTAL BS 277 STRINGER 10R FORWARD OF R1 DOOR. REPLACED INTERCOSTAL ANGLE IAW SERVICE BULLETIN-737-53A1241 REV 1.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2017022700003Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 967, STRINGER 22L. REPLACED IAW SRM 51-30-2 REV 113 AND DWG 65-46563 REV -.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA2017022700002Tee Fitting · crackedCRACKED TEE ON FORWARD CARGO DOOR INTERNAL STRUCTURE AT BS 470. THE TEE WAS REPLACED IAW DWG 65-46921 REV M, AND SRM D6-15565 REV 113 51-30-02.Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA2017010300001Skin · crackedA SKIN CRACK WAS FOUND AT BS727B, S19R WHILE PERFORMING THE AD 2005-13-30 ZONE 1 INSPECTION. THERE WAS AN EXISTING REPAIR IN THE AREA THAT HAD TO BE INCORPORATED; THE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL IX.Jan 1, 2017 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016111400077Skin · crackedFUSELAGE SKIN CRACKED AT BS 760, STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL X.Nov 13, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016110900076Structure · crackedCOMPRESSION CHORD AT BS 663.75 IN CABIN CRACKED BL0. COMPRESSION CHORD @ BS 663.75 IN CABIN @ BL 0 REPAIRED IAW AERONAUTICAL ENGINEERS INC # EO 2933Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2016110900075Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 663, BL0. REPAIRED THE FLOOR SUPPORT IAW EO 2933 REV A.Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA2016110100073Skin · corrodedCORROSION ON RIGHT HAND WING LOWER SURFACE AT WS 475 AFT SPAR. CORROSION ON RT WING LOWER SURFACE AT WS 500-510 REMOVED/BLENDED AND AREA REPAIRED IAW SERVICE REQUEST NUMBER 4-3237034623. RII COMPLETED.Oct 2, 2016 · N320DL · Boeing 737232 · Wing, Plate/SkinSDR NACA2016110100072Skin · corrodedCORROSION ON RIGHT HAND WING LOWER SURFACE AT WS 521 - WS552 AFT SPAR. CORROSION ON RT WING LOWER SURFACE AT WS 521-552 AT AFT SPAR REMOVED/BLENDED AND REPAIRED IAW SERVICE REQUEST NR 4-3237034632 REF NRC 15104120 FOR DOCUMENTATION. RII COMPLETED.Oct 2, 2016 · N320DL · Boeing 737232 · Wing, Plate/SkinSDR NACA2016100200071Drag Angle · crackedCRACKED ANGLED STRAP BS 520 - BS 560 S23L UNDER WING TO BODY FAIRING. REPLACED CRACKED DRAG ANGLE AT STA 520 - 560 STR 23L UNDER WING TO BODY FAIRING IAW 2298 REV K & DWG R23092.1-053-021-001 REV NC.Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2016081100070Frame · crackedCRACK FOUND ON INSULATION BLANKET STUD HOLE AT BS 360, STRINGERS 19 - 20R. REPAIRED THE FRAME IAW ST 4-3262647741..Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100069Door Sill · crackedR1 DOOR SILL CRACKED AT BS 291 - 297 RBL 60 STRINGER 17R. REPLACED THE DOOR SILL IAW DWG 141A8310-0007 REV.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2016081100068Frame · crackedCOMPRESSION FRAME AT BS 663.75 IN CABIN CRACKED AT LBL 25 AND RBL 35. REPAIRED COMPRESSION CHORD AT BS 663.75 IN CABIN AT LBL 25 AND RBL 35 IAW SB B737-53-1184 MARCH 21, 1996.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100067Stringer · corrodedCORROSION FOUND ON STRINGER 26L, BS 1006. CORROSION FOUND TO BE BEYOND LIMITS IAW SRM 53-10-1 REV 110. REPAIRED THE STRINGER IAW SRM 53-10-3 FIG 1, REV 110.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA2016081100066Frame · corrodedCORROSION FOUND ON FRAME BS 927 BETWEEN STRINGER 26 & 27R. CORROSION IS BEYOND LIMITS IAW SRM 53-10-01, REV 110. REPAIRED IAW SRM 53-10-4 FIG 10, REV 110.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100065Frame · corrodedCORROSION FOUND ON FRAME BS 947 BETWEEN S27L & 27R. CORROSION FOUND BEYOND LIMITS IAW SRM 53-10-01, REV 110. REPAIRED IAW SRM 53-10-4 FIG 10, REV 110.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100064Beltframe · corrodedCORROSION ON BELTFRAME BS 360 S27 - 28R AFT OF E&E BAY DOOR CUT OUT. REPAIRED IAW SRM 53-10-4, REV 110.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100063Beltframe · crackedCRACK IN BELTFRAME LOWER FLANGE BS 917 S21R. REPAIRED IAW SRM 53-10-4 FIGURE 10, REPAIR 1, REV 110.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA2016081100062Bulkhead Web · crackedFORWARD BS 178 PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT WL 190 AND RBL 17. REPAIRED THE BULKHEAD WEB IAW SRM 53-10-11 FIG 11 REV 110. .Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, BulkheadSDR NACA2016081100061Floorbeam · crackedFLOORBEAM WEB CRACKED AT BS 663 LBL 24.82. REPAIRED THE FLOORBEAM. REPAIRED IAW SERVICE REQUEST 3-363025-4704.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA2016081100060Floorbeam · crackedFLOORBEAM WEB CRACKED AT BS 663 RBL 24.82 LOWER CHORD. REPAIRED THE FLOORBEAM IAW SERVICE REQUEST 3-363254704.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA2016081100059Doubler · corrodedCORRODED INTERNAL DOUBLER BETWEEN STA 967 TO 996 STR 25L. REPLACED WITH MADE REPAIR PART AND MAT IDENTIFIED IAW 65-45776 REV ER. DOUBLER INSTALLED WITH NEW SKIN REF NRC 1493466 AND NRC 1493379. RII COMPLETED.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016081100058Shear Web · corrodedCORROSION ON LEFT SHEAR WEB BS 711 TO 727 STRINGER 18A LT. REPAIRED THE SHEAR WEB.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2016081100057Skin · crackedCRACKED FASTENER HOLES AT STA 303 JUST BELOW STR 13L AND AT STR 10L, UPPER AND LOWER DOOR HINGE CUT OUTS REPAIRED IAW SR 3-3626171693. RII COMPLETED.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016081100056Skin · crackedSKIN FOUND CRACKED DURING NDT, BS 291 JUST ABOVE STRINGER 10R. REPAIRED IAW BOEING SR 3-3628117058.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016081100055Skin · corrodedCORROSION ON TOP OF RT HORIZONTAL STAB BEAM AT ELEVATOR STA 149.12. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM REV 110 55-10-01 FIGURE 1. REPAIRED IAW SRM REV 110 55-10-7 FIGURE 1.Aug 11, 2016 · N320DL · Boeing 737232 · Horizontal Stabilizer, Plate/SkinSDR NACA2016081100053Skin · crackedSKIN CRACKED BS 259.5 STRINGER 22L. REPAIRED IAW SRM 53-30-3 FIG. 49 DETAIL V REV 101.Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA2016081100052Flap Track · corrodedCORROSION ON NR 2 FLAP TRACK AT AFT SPAR ATTACH POINT. THE FLAP TRACK WAS REPLACED IAW AMM 27-51-151 REV. 122.Aug 11, 2016 · N320DL · Boeing 737232 · Trailing Edge Flaps
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