Boeing 737-401

Service difficulty reports · 2,961

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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 = '737401'
  ORDER BY difficulty_date DESC"

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SDR USAA951191Strap · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 40 INCH CORROSION ON STRAP, STATION 800 TO 840. INSTALLED NEW PART, REPAIRED PER SRM 51-10-02, DRAWING 65-47957. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951190Floor Beam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 TO 2 INCH DIAMETER SPOTS OF CORROSION ON THE FLOOR BEAM AT SCREW HOLES, BS 986 LBL 45 TO RBL 45. CUT OFF 'T' CAP AND INSTALLED NEW 'T' CAP AND REPAIR ANGLE. REPAIRED PER EA 40072A. CORROSION TASK NR C53-107-Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951189Angle · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 59 INCHES CORRODED AREA, BS 947-1006, S-17 L (AFT ENTRY DOOR Z-ANGLE). REMOVED CORRODED CHORD Z-ANGLE. DRILLED UP AND INSTALLED NEW ANGLE FROM STOCK. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951188Beam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORRODED AREA, ON BEAM AT STATION 947 LBL 5 - RBL 15. INSTALLED CAP AND REPAIRED ANGLE. REPAIRED PER EA 40080. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951187Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORRODED AREA, ON INTERCOSTAL AT 25, BETWEEN BS 947 AND BS 967, WL 208. REMOVED CORRODED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL FROM STOCK P/N 65C333701. REPAIRED PER SRM 51-10-0Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951186Support · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION ON SUPPORT AT STATION 947 TO 967 RBL 51. REPLACED SUPPORT CHANNEL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951185Support · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH AREA CORRODED, ON SUPPORT AT 967 AT LBL 51. REMOVED AND REPLACED SUPPORT CHANNEL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951184Support · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 10 INCH AREA CORRODED ON SUPPORT AT STATION 947 TO 967 AT LBL 25. REMOVED AND REPLACED CHANNEL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951183Angle · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON Z ANGLE BS 947-BS 1006, RBL 53. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951182Angle · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 46 INCH CORRODED AREA BS 280-326, STRINGER 17 RT (RT SERVICE DOORWAY CHORD ANGLE). REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE WITH SAME P/N FROM STOCK. REPAIRED PER SRM 51-10-02. CORROSION TASK NNov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951181Sill · corrosionIND - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 4 INCH BY 4 INCH CORRODED AREAS BETWEEN BS 794 AND BS 847 (AFT CARGO DOORWAY SILL). INSTALLED NEW WEB. REPAIRED PER SRM 51-10-02, DRAWING 65-47957. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951180Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA RBL 14 CARGO FLOOR SUPPORT STRINGER (BEAM) AT BS 747. CUT OUT CORRODED SECTION OF BEAM BS 733-778. FABRICATED AND INSTALLED NEW SECTION OF BEAM (TRACK) AND SPLICES. REPAIRED PER Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951179Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 312 TO BS 328, LBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951178Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA BS 294 TO BS 312, RBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951177Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AREA, BS 328 TO BS 312, RBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951176Seat Track · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 16 INCH CORRODED AREA ON SEAT TRACK AT BS 344 TO BS 360 LBL 25 INCHES. REMOVED AND REINSTALLED REPAIR PART COMPLETED REPAIR. REPAIRED PER SRM 53-00-52, FIG 202. CORROSION TASK NR C53-107-02, CORROSIONov 3, 1995 · N417US · Boeing 737401 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951175Intercostal · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, INTERCOSTAL UPPER FLANGE STATION 328 TO 344 LBL 12, WL 208. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951174Floor Beam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 68 INCH CORRODED AREA ON FLOOR BEAM BS 344 LBL 51 TO RBL 17. INSTALLED T-CAP AND REPAIRED ANGLE. REPAIRED PER SRM TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951173Floor Beam · corrosionINT - DURING A-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, STATION 328 FLOOR BEAM UPPER FLANGE AT NUT PLATE HOLES. SECTION CUT OUT AND REPLACED PER SRM 53-10-51 FIG 205. REPAIRED PER SRM 53-10-51, FIG 205. CORROSION TASK NR C53-107-02, Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951172Angle · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 36 INCH AREA CORRODED, FORWARD ENTRY DOOR Z-ANGLE. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Passenger/Crew DoorsSDR USAA951171Floor Beam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED AREA ON FLOOR BEAM AT BS 328. REMOVED CORRODED AREA, INSTALLED REPAIR PARTS COMPLETED REPAIR. REPAIRED PER SRM 53-10-51, FIG 205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (MNov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951170Intercostal · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, APPROXIMATELY 1 INCH BY 12 INCH AREA CORRODED STATION 952 BETWEEN LBL 25 AND LBL 51. REPAIRED AND REPLACED INTERCOSTAL. REPAIRED PER SRM DOCUMENT 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951169Skin · dentedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO SKIN DENTS, AT STATION 265 TO 277 ABOVE STRINGER 11 R AND 13 R. CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. REPAIRED PER SRM 53-00-01. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA951168Floor Beam · crackedINT - DURING Q-5 CHECK NDT INSPECTION, FOUND 1.25 INCH CRACK FLOOR BEAM, .75 INCH CRACK SEAT TRACK SUPPORT CHANNEL DETECTED BY VISUAL INSPECTION, STATION 520 FLOOR BEAM LBL 25, WL 207.75. DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 4Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951167Floor Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 25, WL 207.75. DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 40020, REF SB 737-53-1120. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951166Floor Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 45, WL 207.75. STOP DRILLED AND INSTALLED DOUBLER REPAIR/MODIFICATION. REPAIRED PER EA 40020. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951165Floor Beam · crackedINT - DURING Q-5 CHECK NDT INSPECTION, FOUND ONE .25 INCH CRACK, STATION 520, FLOOR BEAM UPPER RADIUS LBL 45, WL 207.75. DOUBLER INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 40020 REF SB 737-53-1120. (M)Nov 3, 1995 · N417US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951045Air Data Comp · failedPIT - FLT NR 0497 - AFTER TAKEOFF FROM PIT, FLIGHT OFFICERS AIRSPEED, ALTIMETER, AND RATE OF CLIMB INDICATORS FAILED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ADC. OPERATIONS CHECKED OK. (M)Sep 26, 1995 · N407US · Boeing 737401 · Air Data ComputerSDR USAA951022Skin · dentedCLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A DENT 2.5 INCHES BY 5 INCHES BY .060 DEEP AT STATION 921 BETWEEN STRINGER 17R AND 18R. INSTALLED DOUBLER. (M)Aug 31, 1995 · N418US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA951019Skin · dentedCLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A SKIN DENT 3.5 INCHES BY 3.5 INCHES BY .180 INCH DEEP IN THE LAV SERVICE DOOR STATION 288 AT STRINGER 20R AND 21R. INSTALLED SKIN. (M)Aug 31, 1995 · N418US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA950951Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCHES STATION 344 LBL 24 INCHES - RBL 24 INCHES. REPLACED SECTION OF T-CAP. REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 30, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950949Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 14 INCH CORRODED BS 328 RBL 28-42 ON FLOOR BEAM. SPLICED IN NEW SECTION OF T-CAP. REPAIRED 737-300/400 TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 30, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950948Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 13 INCH CORROSION BS 312 RBL 7 INCHES THROUGH RBL 20 INCHES ON FLOOR BEAM T-CAP. REPAIRED PER SRM 737-400 53-10-51 FIG 206 PAGE 224. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Aug 30, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951014Floor Beam · corrosionCLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED A 2 INCH CORRODED AREA LOCATED AT THE FLOOR BEAM STATION 312 RBL 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP. (M)Aug 14, 1995 · N418US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950956Intercostal · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 16 BS 967 TO BS 987 ON INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 11, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950962Intercostal · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION, RBL 16 BS 967 TO 987 INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950961Intercostal · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER SPOT OF CORROSION RBL 17 BS 947-BS 967. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950960Angle · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOT OF CORROSION Z-ANGLE AT LEFT AFT ENTRY DOOR SILL. REPAIRED PER SRM 53-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950959Angle · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOTS OF CORROSION Z-ANGLE AT RIGHT AFT SERVICE DOOR SILL. REPAIRED PER SRM 51-10-2. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950958Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 947 LBL 4 TO RBL 4. CUT OFF UPPER FLANGE INSTALLED NEW T-CAP. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950957Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 986.5 RBL 18 TO LBL 50. CUT OFF UPPER FLANGE AND INSTALLED NEW T-CAP. CORROSION TASK NR C53-107-02, CORROSION LEVEL. (M)Aug 10, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951018Floor Beam · corrosionCLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORROSION AT FLOOR BOARD ATTACH HOLES AND AT TOP HORIZONTAL EDGE 10 INCHES LOCATED ON FLOOR BEAM AT STATION 986.5 ATTACH HOLES ALONG SPAN OF BEAM AND LEADING EDGE BL 33R TO BL 44R. CORROSION TASK NR C53-107-Aug 8, 1995 · N418US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951015Door Frame · corrosionCLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A 1 INCH BY 4 INCH CORRODED AREA AFT CARGO BIN DOOR FRAME AT LOWER FORWARD CORNER. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. DOUBLER INSTALLED ON FRAME. (M)Aug 8, 1995 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950953Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE CORRODED SPOTS (.5 INCH BY 2 INCHES EACH) BS 967, RBL 19, RBL 31, RBL 43 ON FLOOR BEAM. CUT OUT CORRODED SECTIONS ON AFT SIDE OF UPPER T-CAP, AND INSTALLED REPAIR ANGLES AND FILLERS. REPAIRED PER SRM 53-3Aug 8, 1995 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951017Floor Beam · corrosionCLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES 30 INCHES AT STATION 328 FROM LBL TO RBL 55, ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP (UPPER) PER TYPICAL REPAIR 53-10-0Aug 7, 1995 · N418US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA951016Floor Beam · corrosionCLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES (40 INCHES) AT STATION 344 RBL 8 TO LBL 45.5, ON FLOOR BEAM. CORROSION TASK NR C53-127-02, CORROSION LEVEL 2. REMOVED AND REPLACED T-CAP. (M)Aug 7, 1995 · N418US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950950Intercostal · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 26 INCH BY .5 INCH CORROSION AT BS 328-344 RBL 12 INCHES ON INTERCOSTAL. REPAIRED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-02 PG 16. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Aug 7, 1995 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA951023Track Assy · crackedCLT - DURING A Q6-CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.8 INCH CRACK LOCATED AT STATION 520, CENTERED AT LBL 45.5. INSTALLED TUB FITTING AND TRACK ASSY KIT 65C3468827. (M)Aug 4, 1995 · N418US · Boeing 737401 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951021Track · crackedCLT - DURING A Q-6 CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.9 INCH CRACKED TRACK LOCATED AT STATION 520 EXTENDING 1.1 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75. INSTALLED DOUBLERS AND TUB FITTINGS. (M)Aug 4, 1995 · N418US · Boeing 737401 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951020Seat Track · crackedCLT - DURING A Q6-CHECK, INSPECTION FOUND BY EDDY CURRENT A 2.2 INCH CRACKED TRACK LOCATED AT STATION 520 A CENTERED RBL 45.5. INSTALLED DOUBLERS, TRIMMED FITTINGS, TRACKS AS REQUIRED. (M)Aug 4, 1995 · N418US · Boeing 737401 · Fuselage, Seat/Cargo Attach Fittings
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