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 TSAA20160112001Pitot Tube · obstructedDURING CLIMB OUT AT 4000’ FEET, DIFF PRESS LIGHT ILLUMINATED. NO OTHER ABNORMAL INDICATIONS NOTED. CREW COMPLETED QRH CHECKLIST & RETURNED FOR A NORMAL LANDING. CLEANED BUG DEBRIS FROM PITOT TUBES & TESTED OK IAW AMM 27-31-131.Jan 12, 2016 · N320DL · Boeing 737232 · Pitot/Static SystemSDR NACA201511160001Frame · damagedFRAME DAMAGED AT BS 500 BETWEEN STRINGERS 13-14R. INSTALLED REPAIR TO FRAME IAW SRM 51-40-3, FIG 1.Nov 13, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010059Failsafe · misinstalledDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. AT REQUEST, NON-CONFORMING FRAMES IN THE AREA WERE INSPECTED AND ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-016-001May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010058Floor Support · crackedUPPER FUSELAGE MAIN CABIN BL0 BS719 LONGITUDINAL FLOOR BEAM WEB CRACKED 3 PLACES. REPLACED UPPER FUSELAGE MAIN CABIN BL0 BS719 LONGITUDINAL FLOOR BEAM WEB WITH MADE REPAIR PART IAW SB 737-57-1210, REV 4. REPLACED LOWER CHORD UPPER FUSELAGE MAIN CABIN BL0 BS6May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010057Failsafe · crackedDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE AREA WERE ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-016-001, REV NC AND EO1847, REF KMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010056Failsafe · crackedDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE AREA WERE ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-016-001, REV NC AND EO1847, REF May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010055Failsafe · crackedDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE AREA WERE ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-016-001, REV NC AND EO1847. REFMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010054Failsafe · crackedDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE AREA WERE ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-016-001 REV NC AND EO1847, REF KFMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010053Failsafe · crackedDURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE AREA WERE ADDRESSED. THIS FRAME WAS REPAIRED IAW DWG R23094.1-053-017-001, REV NC AND EO1847, KF MCMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010052Web · crackedUPPER FUSELAGE AT BS 1016, LBL40 FLOOR WEB CRACKED. CRACK IN THE AFT CABIN STRESS WEB. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-46812 AND SRM R108.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010051Beltframe · crackedAFT CARGO PIT, BS 847 BELTFRAME CRACKED INBD OF STR 25L. CRACK FRAME AT BS 847 AT S25L +5, REPAIRED IAW SRM R108 53-10-4, FIG 7.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010050Frame · crackedFRAME AT BS 277, S16L CRACKED IN UPPER FUSELAGE. REPAIRED FRAME AT BS 277, STR 16L IN UPPER FUSELAGE IAW SRM 53-10-04 FIG 7, REPAIR 2, R108. REF KFC MCO 3218, WO 1367632.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010049Frame · damagedDAMAGE ON FRAME, BS 380, S15-16R. DURING INSPECTION, DAMAGE WAS NOTED ON THE INNER CHORD OF THE FRAME AT THIS LOCATION. REPAIRED IAW DWG R23094.1-053-012-001, REV NC.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010048Intercostal · corrodedAFT CARGO BAY BS 789, RBL 23 INTERCOSTAL CORRODED. BLENDED, MEASURED AND FOUND TO BE BEYOND THE LIMITS OF SRM R108, 53-10-1. FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 65-47959, SHEET 2, REV J.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010047Shear Web · corrodedUPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 639 TO BS 663, LBL 65, STR 17R. DURING INSPECTION, CORROSION THAT WAS VISIBLY BEYOND LIMITS WAS NOTED ON THE CREASE BEAM WEB AT S17L THAT RUNS BETWEEN BS639 AND BS663. FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010046Web · corrodedUPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 616 TO BS 639, RBL 65, STR 17R. DURING INSPECTION, OUT OF LIMITS, CORROSION WAS NOTED ON THE CREASEBEAM WEB BETWEEN BS 616 AND BS 639, RT. FABRICATED AND INSTALLED REPLACEMENT WEB.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010045Web · corrodedUPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 616 TO BS 639, LBL 65, STR 17L. FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-10-02, FIG 1, ITEM 3, REV 108, REF KFC MCO 3218, WO 1367615.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010044Fitting · corrodedCORROSION ON VERTICAL STABILIZER ON RT AFT FITTING FWD SIDE. DURING THIS INSPECTION, CORROSION WAS NOTED IN THIS FITTING AND FOUND TO BE BEYOND LIMITS. FITTING WAS REPLACED WITH NEW IAW BAC DWG 65-53744, REV C AND SRM R108, REF KFC MCO 3218, WO 1367614.May 1, 2015 · N322DL · Boeing 737232 · Vertical Stabilizer, Attach FittingsSDR NACA201505010043Support Fitting · crackedOTBD MLG SUPPORT BEAM FITTING CRACKED. THE FITTING WAS REPLACED WITH THE NEWER STYLE AS SHOWN SB 57-1216R2, REF KFC MCO 3218, WO 1367210.May 1, 2015 · N322DL · Boeing 737232 · Wing, Landing Gear Attach FittingsSDR NACA201505010042Attach Fitting · corrodedCORROSION ON VERTICAL STABILIZER ATTACH FITTING LT AFT FWD FACE. DURING INSPECTION CORROSION WAS NOTED ON THE VERTICAL STABILIZER ATTACH FITTING, LT SIDE, AFT. FITTING WAS REPLACED WITH NEW. STABILIZER REMOVAL WAS NOT NECESSARY.May 1, 2015 · N322DL · Boeing 737232 · Vertical Stabilizer, Attach FittingsSDR NACA201505010041Skin · crackedCRACKED EXTERIOR FUSELAGE BETWEEN BS 747 & BS 767 AT STR 18L. REPAIRED CRACK WITH EXTERNAL DOUBLER AT BS 747-BS 767 IAW SB 737-53-1065, REV 2, APRIL 19, 2001, REPAIR FIGURE 54.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA201505010040Stringer · corrodedAFT CARGO BAY BS 904, STRINGER 26R CORRODED OUT OF LIMITS. . FABRICATED AND INSTALLED REPLACEMENT STRINGER SECTION AND ASSOCIATED SPLICES.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA2015105010039Door Frame · corrodedAFT CARGO BAY BS 797, RBL 26, LWR CARGO ENTRY WAY SKIN CORRODED. OUT OF LIMITS CORROSION NOTED ON THE STRUCTURAL SILL WEB AND THE C2 THRESHOLD. REPLACED WITH NEW WEB, DWG 65-47957 AND SRM R108.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010038Support · crackedAFT CARGO BAY BS 775, RBL 2 ANTENNA SUPPORT STRUCTURE HAS 2 CRACKS. THE INTERIOR STRUCTURE WAS REPLACED AND AN EXTERNAL DOUBLER WAS INSTALLED. DOUBLER IS IN PROXIMITY TO A DER INSTALLED EXTERNAL DOUBLER USED ON TI: VRX4. DUE TO THE NATURE OF THIS REPAIR, 1 May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010037Skin · crackedFWD CARGO BAY DOOR INNER SKIN LIGHTING HOLE CRACKED AT BS 480, RBL 44. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED AT BS 480, RBL 44 WITH FABRICATED PART IAW 52-30-1, FIG 1, REV 108, SRM 51-40-02, FIG 1, REV 108, SRM, REF KFC MCO3218, W/O 1365812.May 1, 2015 · N322DL · Boeing 737232 · Cargo/Baggage DoorsSDR NACA201505010036Floorbeam · crackedUPPER FUSELAGE FLOORBEAM SUPPORT ANGLE AT BS 328, RBL 34 HAS CRACK. REPLACED CRACKED ANGLE WITH FABRICATED NEW PART IAW 51-20-01, FIG 7, REV 108, SRM, REF KFC MCO3218, W/O 1365671.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA201505010035Intercostal · crackedUPPER FUSELAGE DOOR FRAME SUPPORT INTERCOSTAL AT BS 294 BETWEEN STR 12R AND STR 13R CRACKED. DURING INSPECTION OF THE SURROUND STRUCTURE OF THE R1 ORIFICE, A CRACK WAS NOTED ON AN ANGLE THAT ATTACHES AN INTERCOSTAL BETWEEN S12 AND S13, RIGHT TO THE AIRCRAFT SMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010034Skin · damagedFWD AIR STAIR DOOR INNER SKIN DAMAGE IN UPPER FWD CORNER. DURING INSPECTION, SIGNIFICANT DAMAGE WAS NOTED ON THE INNER SKIN OF THE FORWARD AIRSTAIR DOOR. FABRICATED AND INSTALLED REPLACEMENT SKIN IAW DWG 65-27942 AN, REF KFC MCO 3218, WO 1365636.May 1, 2015 · N322DL · Boeing 737232 · Entrance StairsSDR NACA201505010033Angle · crackedAFT CARGO BAY BS 727, RBL 18, WL 200 CRACKED CLIP. DURING INSPECTION, A CRACKED CLIP WHICH SERVES TO SECURE THE UPPER END OF THE RBL 18 VERTICAL BEAM OF THE BS 727 BULKHEAD WAS NOTED. FABRICATED AND INSTALLED A REPLACEMENT CLIP IAW DWG 65-46547, REV DK AND SRMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010032Floor Support · corrodedFLOORBEAM CHORD AT RBL24 FROM BS 540 TO BS 727B HAS CORROSION AROUND CLIPNUT HOLES. OUT OF LIMITS CORROSION NOTED IN SEVERAL PLACES DURING INSPECTION NECESSITATING REPLACEMENT OF THE ENTIRE UPPER CAP. REF DWG 65-45410, REV P AND SRM R108 AND SB 57-1139 R4, FIMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010031Floor Support · corrodedUPPER FLOOR BS 673 TO BS 639, LBL 65 HAS CORROSION ON TOP & BOTTOM OF SILL. DURING INSPECTION, CORROSION WHICH WAS VISUALLY BEYOND LIMITS WAS NOTED ON THE CREASE BEAM INNER CHORD IN THIS AREA. CHORD REPLACED IAW BAC DWG 65-47943 AND SRM R108, REF KFC MCO 3218May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010030Floor Support · corrodedUPPER FUSELAGE FLOOR BS727B TO 540 LBL25 CORROSION ON FLOORBOARD FLANGE STRUCTURE. AWAITING PAPERWORK FROM C-CHECK.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010029Floor Support · crackedUPPER FUSELAGE FLOOR BS 616 & BS 639 AT RBL 65 SIDE RAIL CRACKED. DURING INSPECTION, CRACKS WERE NOTED AT THE CREASE BEAM INNER CHORD. THIS CHORD ALSO SUPPORTS THE FLOORBOARD EDGES. THE 62" SECTION OF CHORD WAS REPLACED IAW DWG 65-48973 AND SRM R108.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA2015105010028Floor Support · corrodedUPPER FUSELAGE FLOOR HAS CORROSION ON FLOORBEAM FLANGE STRUCTURE AT BS 727B TO BS 540, RBL45. OUT OF LIMITS CORROSION WAS NOTED ON THE UPPER CAP OF THE LONGITUDINAL FLOORBEAM LOCATED AT RBL45. IT WAS NOTED THAT THERE WAS PREVIOUS BLEND ACTIVITY ON THIS CAP. May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010027Floorbeam · corrodedUPPER FUSELAGE BS 807, LBL 65 TO RNL 65 HAS CORROSION ON LWR FLANGE OF FLOORBEAM & LWR STRAP. DURING INSPECTION, CORROSION WAS NOTED ON THE LOWER FLANGE OF THE BS 807 FLOORBEAM AND ON THE AEI STRAP ON THE UNDERSIDE OF THE BEAM. THE STRAP WAS BLENDED, MEASUREMay 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA201505010026Floorbeam · corrodedUPPER FUSELAGE BS 867, LBL 25 TO LBL 45 CORRODED ON LWR FLANGE OF FLOORBEAM. CORROSION BEYOND LIMITS WAS NOTED ON THE LOWER FLANGE OF THE MAIN DECK FLOORBEAM AT BS 867 FROM LBL 25-LBL 45. REPAIRED IAW SRM R108, 53-10-9, FIG 7. REF KFC MCO3218, W/O 1364373.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA2015051100001Floorbeam · corrodedUPPER FUSELAGE BS 867, LBL 25 TO LBL 45 CORRODED ON LWR FLANGE OF FLOORBEAM. CORROSION BEYOND LIMITS WAS NOTED ON THE LOWER FLANGE OF THE MAIN DECK FLOORBEAM AT BS 867 FROM LBL 25-LBL 45. REPAIRED IAW SRM R108, 53-10-9, FIG 7, REF KFC MCO3218, W/O 1364373.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA201505010025Web · corrodedUPPER FUSELAGE BS 887 TO BS 907, RBL 65 CORRODED ON FLOOR STRESS WEB. CORROSION WAS NOTED ON THE CREASE BEAM WEB AT FLOOR LEVEL DURING INSPECTION. CORROSION WAS VISIBLY BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT WEB, REF KFC MCO 3218, WO 1364309.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010024Floorbeam · corrodedUPPER FUSELAGE FLOOR BS 480, RBL 65-45 HAS CORROSION ON FLOORBEAM. UPPER FUSELAGE BS 480 RBL 65-45 HAD CORROSION ON FLOORBEAM BEYOND LIMITS. REPAIRED FLOORBEAM IAW SRM 53-10-01, FIG 7, REV 108.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA201505010023Floorbeam · corrodedUPPER FUSELAGE FLOOR BS 887, RBL 25 TO LBL 12.5 HAS CORROSION ON LOWER FLANGE OF FLOORBEAM. REPAIRED FLOOR BEAM IAW SRM R108, 53010-9, FIG 7. REF KFC MCO 3218, WO 1364162.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA201505010022Frame · damagedUPPER FUSELAGE FRAME BS 360 S16L DAMAGE ON FRAME.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010021Failsafe · crackedFORWARD CARGO PIT AT BS 520, LBL 30, FAILSAFE CRACKED.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, StructureSDR NACA201505010020Frame · damagedUPPER FUSELAGE, BS 787 BETWEEN S17R-16R DAMAGED FRAME. REPAIRED IAW KF DWG R23094.1-053-007-001, REV NC.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, FrameSDR NACA201505010019Web · crackedCRACKED LIGHTNING HOLE AT BS 450, RBL 44. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED AT BS450, RBL 44 WITH FABRICATED PART IAW 52-30-1, FIG 1, REV 108, SRM 51-40-02, FIG 1, REV 108, SRM, REF KFC MCO3218, W/O 1364044.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010018Skin · crackedFWD CARGO BAY DOOR INNER SKIN LIGHTING HOLE CRACKED AT BS 450 AND RBL 34. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED IAW 52-30-1, FIG 1, REV 108, AND SRM 51-40-02, FIG 1, REV 108.May 1, 2015 · N322DL · Boeing 737232 · Cargo/Baggage DoorsSDR NACA201505010017Support Angle · crackedFWD CARGO BAY STRINGER SUPPORT ANGLE CRACKED AT BS 440 AT STR 24R. REPLACED WITH MADE PART IAW DWG 65-20722, REV K. FASTENERS INSTALLED IAW -200, SRM 51-30-2.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010016Web · corrodedAFT CARGO BAY WEB FROM BS 927 TO BS 947, RBL65 CORROSION FOUND. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-45855, REV CV.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010015Web · corrodedAFT CARGO BAY BS 907 STRINGER 17R WEB CORROSION FOUND AT RBL65. FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-10-2, FIG 13, PG 97, REV 108, DWG 65-47976, REV T.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA201505010014Skin · corrodedLOWER LOBE SKIN CORROSION UNDER MARKER BEACON ANTENNA BS 620. REPLACED IAW BAC DWG 65-45866, REV G.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA201505010013Shear Tie · corrodedCORROSION FOUND AT BS 986.5 ON SHEAR TIE BETWEEN STR 19R AND STR 20R. REPLACED SHEAR TIE IAW DWG 65-46564, REV D. INSTALLED IAW 51-30-02, REV 108 SRM.May 1, 2015 · N322DL · Boeing 737232 · Fuselage Internal Mounting Structure
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