Boeing 737-375

Service difficulty reports · 174

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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 = '737375'
  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 AWXA200500447Skin · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON TOP LT WING IN SPAR SKIN AT BS 575, WBL 81.5. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING IN SPAR SKIN AT BS 575, WBL 81.5; FABRICATED A -5 FILLER AND 4 EACH REPAIR PLATES (DOUBLERS); IMar 11, 2005 · N336AW · Boeing 737375 · Wing, Plate/SkinSDR AWXA200500427Web · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF RT AFT OUTBOARD WEB BETWEEN BS 996 AND BS 1016, RBL 44 AND RBL 46. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF RT AFT OUTBOARD WEB FROM BS 996 TO BS 1016, RBLMar 11, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500426Skin · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BILGE SKIN BETWEEN BS 988 AND BS 1005, STR 26 LT AND STR 27 RT. MAINTENANCE CUT OUT CORRODED SKIN FROM BS 988 TO BS 1005, STR 26 LT TO STR 27 RT; FABRICATED A REPAIR DOMar 11, 2005 · N336AW · Boeing 737375 · Fuselage Main, Plate/SkinSDR AWXA200500420Floor Support · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT BETWEEN BS 1009 AND BS 1012, AT RBL 38. MAINTENANCE CUTOUT DAMAGE IN FLOOR SUPPORT AT RBL 38 FROM BS 1009 AND BS 1012; FABRICATED -1 AND -2 REPAIR PLATES; INSTALLED REPAIR PARMar 11, 2005 · N336AW · Boeing 737375 · Fuselage Internal Mounting StructureSDR AWXA200500414Channel · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB SUPPORT CHANNEL BETWEEN BS 995 AND BS 1001, RBL 41, WL 207. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE OF WEB SUPPORT CHANNEL FROM BS 995 TO BS 1001, AT RBL 41; FABRICATED A FILLER AND Mar 11, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500411Bracket · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL FWD ATTACH CLIP (BRACKET) AT BS 956, LBL 51. MAINTENANCE REMOVED CORRODED BRACKET AT BS 956, LBL 51; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 69-42747; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02.Mar 11, 2005 · N336AW · Boeing 737375 · Fuselage Main, Attach FittingsSDR AWXA200500407Web · corrodedDURING C-05 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT OUTBOARD WEB BETWEEN BS 995 AND BS 1015, LBL 38 AND LBL 42. MAINTENANCE REMOVED CORRODED LT AFT OUTBOARD WEB FROM BS 995 TO BS 1015, LBL 38 TO LBL 42; FABRICATED A NEW REPLACEMENT WEB PER DWG 65Mar 11, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500404Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986, BETWEEN LBL 3 AND LBL 40. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 986, FROM LBL 3 TO LBL 40; FABRICATED A NEWMar 11, 2005 · N336AW · Boeing 737375 · Fuselage Main, Floor BeamSDR AWXA200500403Stringer · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 986. MAINTENANCE CUTOUT DAMAGE IN STRINGER 27 LT AT BS 986; FABRICATED A CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201.Mar 11, 2005 · N336AW · Boeing 737375 · Fuselage Main, Longeron/StringerSDR AWXA200500385Web · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON RIGHT AFT OUTBOARD WEB BETWEEN BS 996 AND BS 1016, RBL 44 AND RBL 46. MAINTENANCE REMOVED DAMAGED RIGHT AFT OUTBOARD WEB FROM BS 996 TO BS 1016, RBL 44 TO RBL 46; FABRICATED A NEW REPLAMar 11, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500352Web · corrodedMCN - MAJOR REPAIR - DURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR SILL (WEB) BETWEEN BS 953 AND BS 985, RBL 48, WL 208. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL FROM BS 947 TO BS 986.5, RBL 48; FABRICATED A NEW REPLACEMENT Mar 11, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500450Skin · crackedMCN - MAJOR REPAIR - DURING C-05 CHECK A .625 INCH CRACK WAS FOUND IN SKIN AT R-1 DOOR FRAME CUTOUT IN LOWER AFT CORNER ABOVE STR 17 RT, BS 328. MAINTENANCE CUT OUT CRACK IN SKIN AT R-1 DOOR FRAME CUTOUT LOWER AFT CORNER STR 17 RT, BS 328. FABRICATED OUTER, Mar 10, 2005 · N336AW · Boeing 737375 · Fuselage Main, Plate/SkinSDR AWXA200500432Pin · corrodedMCN - FLIGHT CONTROL - DURING C-05 CHECK CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER INNER HINGE PIN. MAINTENANCE REMOVED AND REPLACED THE RT HORIZONTAL STABILIZER INNER HINGE PIN IAW T/C E6C55102.Mar 10, 2005 · N336AW · Boeing 737375 · Horizontal Stabilizer StructureSDR AWXA200500428Pin · corrodedMCN - FLIGHT CONTROL - DURING C-05 CHECK CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER INNER HINGE PIN. MAINTENANCE REMOVED AND REPLACED THE LT HORIZONTAL STABILIZER INNER HINGE PIN IAW T/C E6C55102.Mar 10, 2005 · N336AW · Boeing 737375 · Horizontal Stabilizer StructureSDR AWXA200500412Channel · crackedDURING C-05 CHECK A 11/16 INCH CRACK WAS FOUND ON INBOARD SIDE OF SUPPORT CHANNEL LOCATED ON AFT SIDE OF BS 520 FLOORBEAM AT RBL 24.75. MAINTENANCE REMOVED CRACKED SUPPORT CHANNEL AT BS 520. RBL 24.75; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 66-22187; INMar 10, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500377Skin · delaminatedMCN - MAJOR REPAIR - DURING C-05 CHECK, FOUND THE UPPER SURFACE OF THE NR 3 SLAT WEDGE DELAMINATED AT INBOARD END, SLAT STA 14. MAINTENANCE CUTOUT DAMAGE IN UPPER SURFACE OF NR 3 SLAT WEDGE FROM SS 12.25 TO SS 15.25; FABRICATED A CORE FILLER AND DOUBLER; BONDMar 10, 2005 · N336AW · Boeing 737375 · Leading Edge DevicesSDR AWXA200500384Web · crackedMCN - MAJOR REPAIR - DURING C-05 CHECK A 1.125 INCH CRACK WAS FOUND IN WEB AT LT MLG WHEEL WELL CEILING BS 664, LBL 32. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 664, LBL 32; FABRICATED 3 EACH FILLERS, A DOUBLER & STRAP; INSTALLED REPAIR PARTS IAW B737-30Mar 9, 2005 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200500072Proximity Switch · false indicationON DEPARTURE FROM LAS EN ROUTE TO DFW AFTER RAISING THE LANDING GEAR AN UNSAFE RT HAND MLG UNSAFE RED LIGHT APPEARED AND REMAINED ILLUMINATED. PILOT CYCLED THE LANDING GEAR ONCE AT DIRECTION OF LAS MX. LIGHT REMAINED ILLUMINATED AND AIRCRAFT DIVERTED TO PHX.Jan 21, 2005 · N336AW · Boeing 737375 · Landing Gear Position and WarningSDR AWXA200401233Bearing · disintegratedPHX - AIR TURN BACK - FLT 0158 - ON CLIMB OUT OF PHX EN ROUTE TO STL NOTICED A MODERATE AIRFRAME VIBRATION LEAVING FL 180, TURNED BACK TO PHX, VIBRATION CONTINUED THROUGH DESCENT AT FL 10 VIBRATION CEASED. MAINTENANCE REMOVED AND REPLACED R/H TURBINE FAN ASSEMNov 4, 2004 · N336AW · Boeing 737375 · Air Distribution SystemSDR AWXA200400386Battery · dischargedPHX - EMERGENCY EQUIPMENT - AFT CABIN EMERGENCY FLASHLIGHT DOES NOT TEST. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.Apr 20, 2004 · N336AW · Boeing 737375 · Emergency EquipmentSDR AWXA200400367Skin · crackedPHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.74 INCH CRACK WAS FOUND IN FUSELAGE SKIN APPROXIMATELY 3 INCHES BELOW AND FWD OF RIGHT FUSELAGE AFT WING TO BODY FAIRING AND EMERGENCY EXIT LIGHT BS 727D, STR 21 & STR 22 RIGHT. MAINTENANCE REMOVED CRACKED SKIN AT BApr 14, 2004 · N336AW · Boeing 737375 · Fuselage Main, Plate/SkinSDR AWXA200301553Web · crackedDURING C-04 CHECK A 2.125 INCH CRACK WAS FOUND AT FRAME FLANGE RELIEF CUTOUT ON FLIGHT COMPARTMENT FLOOR WEB 4 INCHES INBOARD OF FUSELAGE SKIN AT BS 194 LT, WL 207.5. MAINTENANCE REMOVED CRACKED WEB AT BS 194 LT, WL 207.5; FABRICATED A NEW REPLACEMENT WEB PERDec 2, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200301552Support · crackedDURING C-04 CHECK A 1.1875 INCH CRACK WAS FOUND COMING FROM HI-LOK FASTENER EXTENDING TOWARD BEND RADIUS ON HORIZONTAL SUPPORT IN FORWARD E&E COMPARTMENT, BS 179.5, LBL 25.5, WL 195.5. MAINTENANCE CUT OUT CRACKED AREA OF HORIZONTAL SUPPORT AT BS 179.5, LBL 25Dec 2, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200301551Web · crackedDURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND AT FRAME FLANGE RELIEF CUTOUT ON FLIGHT COMPARTMENT FLOOR WEB 4 INCH INBOARD OF FUSELAGE SKIN AT BS 194 RT, WL 207.5. MAINTENANCE REMOVED CRACKED WEB AT BS 194 RT, WL 207.5; FABRICATED A NEW REPLACEMENT WEB PER DWGDec 2, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200301550Beam · crackedDURING C-04 CHECK 2 EACH CRACKS WERE FOUND COMING FROM INSULATION PIN HOLE ON VERTICAL BEAM WEB IN FORWARD E & E COMPARTMENT BS 179.5, RBL 5.7, WL 173.25. MAINTENANCE CUT OUT CRACKED AREA OF VERTICAL BEAM WEB BS 179.5, RBL 5.7, WL 173.25; FABRICATED A REPAIR Dec 2, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200301548Beam · corrodedDURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM BS 787-847, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM BS 787-847, STR 25 RT; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED Nov 27, 2003 · N336AW · Boeing 737375 · Fuselage Main, StructureSDR AWXA200301555Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-04 CHECK A .625 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 13.5, WL 183; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLNov 25, 2003 · N336AW · Boeing 737375 · Fuselage Main, BulkheadSDR AWXA200301554Bulkhead · crackedDURING C-04 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE, AT RBL 5, WL 200.25 TO WL 201.25. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK END, STOP DRILLED CRACK, RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATEDNov 25, 2003 · N336AW · Boeing 737375 · Fuselage Main, BulkheadSDR AWXA200301549Intercostal · crackedDURING C-04 CHECK A 5 INCH CRACK WAS FOUND ON INTERCOSTAL AT BS 303, STR 3 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 303, STR 3 LT AND FOUND ATTACH STRAP CRACKED, REMOVED CRACKED ATTACH STRAP; ORDERED AND RECEIVED A NEW REPLACEMENT INTERCOSTAL, AND FANov 25, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200301526Web · corrodedLCQ - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FASTENER HEADS OF AFT CARGO DOOR THRESHOLD ALONG ENTIRE SURFACE, FORWARD CORNER 100 PERCENT EXFOLIATED MATERIAL LOSS INCLUDING UPPER STRAP, BS 807-847. MAINTENANCE REMOVED AFT CARGO DOONov 25, 2003 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200300545Cable · frayedPHX - EES - DURING INSPECTION THE R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE WAS FOUND FRAYED. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW T/C I1C25009.May 15, 2003 · N336AW · Boeing 737375 · Escape SlideSDR AWXA200300218Warning System · false activationON TAKEOFF ROLL SLC EN ROUTE FOR PHX REJECTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. DETERMINED STAB TRIM WAS ON AFT EDGE OF GREEN BAND, RESET STAB TRIM AND CONTINUED WITHOUT FURTHER EVENT.Feb 28, 2003 · N336AW · Boeing 737375 · Central WarningSDR AWXA200201054Switch · malfunctionedFLT 0836 - DURING POWER UP ON PHX RUNWAY EN ROUTE FOR LGB, THE FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED, REJECTED TAKEOFF AT 64KTS. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR WARNING SWITCH, OPERATIONAL TEST WAS GOOD IAW BMM 52-71-11-201.Oct 26, 2002 · N336AW · Boeing 737375 · Door Warning SystemSDR AWXA200201047Warning System · malfunctionedFLT 2220 - DURING TAKEOFF FROM SJD EN ROUTE FOR PHX TAKEOFF WARNING HORN SOUNDED, ABORTED TAKEOFF. RECONFIGURED AIRCRAFT, RETURNED TO RUNWAY, TOOK OFF WITHOUT FURTHER INCIDENT.Oct 23, 2002 · N336AW · Boeing 737375 · Central WarningSDR AWXA200200962Shear Tie · buckledDURING C-03 CHECK TWO SHEARS TIES WERE FOUND BUCKLED AT BS 1040, BETWEEN STR 12 - 14 LT. MAINTENANCE REMOVED THE DAMAGED SHEAR TIES AT BS 1040, BETWEEN STR 12 - 14 LT. FABRICATED 2 EACH REPLACEMENT SHEAR TIES, AND INSTALLED REPAIR PARTS.Sep 24, 2002 · N336AW · Boeing 737375 · Fuselage Main, StructureSDR AWXA200200950Channel · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON FLOORBEAM LINK ATTACH U CHANNEL AT BS 520, BL 0. MAINTENANCE REMOVED DAMAGED LINK ATTACH CHANNEL. FABRICATED A NEW REPLACEMENT LINK ATTACH CHANNEL, INSTALLED REPAIR PART IAW DWG 66-23250, BSep 13, 2002 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200200959Angle · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1" CRACK WAS FOUND ON THE L/H OUTBOARD MIDFLAP REAR SPAR TO RIB ATTACH ANGLE AT WBL 305.56. MAINTENANCE REMOVED L/H OUTBOARD MIDFLAP REAR SPAR TO RIB ATTACH ANGLE AT WBL 305.56. FABRICATED A NEW REPLACEMENT ANGLE, AND ISep 9, 2002 · N336AW · Boeing 737375 · Trailing Edge FlapsSDR AWXA200200965Angle · crackedDURING C-03 CHECK A 2.5 INCHES CRACK WAS FOUND ON LT & RT SUPPORT ANGLES OF THE VERTICAL STABILIZER TRAILING EDGE 20 INCH ABOVE TAIL CONE AT BS 1110. MAINTENANCE CUTOUT SUPPORT ANGLES, FABRICATED 2 EACH SPLICE ANGLES AND A BEAM EXTRUSION, AND INSTALLED REPAIR Sep 5, 2002 · N336AW · Boeing 737375 · Fuselage Main, Attach FittingsSDR AWXA200200967Shear Tie · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 3/8" CRACK WAS FOUND ON SHEAR TIE ANGLE AT BS 727E, ABOVE STR 14 R/H. MAINTENANCE REMOVED DAMAGED SHEAR TIE AT BS 727E, FABRICATED A NEW REPLACEMENT SHEAR TIE, AND INSTALLED REPAIR PART IAW AWA E.R. 03-5362-02270-ES2.Sep 4, 2002 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200200963Angle · wornDURING C-03 CHECK THE RT VERTICAL STABILIZER LOWER AFT PANEL SKATE ANGLE WAS FOUND WORN THROUGH, BS 1070 - 1100. MAINTENANCE REMOVED THE DAMAGED AREA OF SKATE ANGLE. FABRICATED A NEW SECTION OF REPLACEMENT SKATE ANGLE, 2 EACH STRAPS, AND A SHIM, AND INSTALLED Sep 4, 2002 · N336AW · Boeing 737375 · Fuselage Main, Attach FittingsSDR AWXA200200952Web · buckledYVR - MAJOR REPAIR - DURING C-03 CHECK A SHEAR WEB WAS FOUND BUCKLED AND TORN AT BS 520, LBL 25. MAINTENANCE REMOVED DAMAGED SHEAR WEB. FABRICATED A NEW REPLACEMENT SHEAR WEB AND INSTALLED REPAIR PART IAW DWG 69-35365, AND B737-300 SRM 51-40-02.Sep 4, 2002 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200200949Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STRINGER 5 R/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727E, STRINGER 5 R/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW DWG 69Sep 4, 2002 · N336AW · Boeing 737375 · Fuselage Main, Longeron/StringerSDR AWXA200200966Keelbeam · crackedDURING C-03 CHECK A 3 3/8 INCH CRACK WAS FOUND ON RT KEEL BEAM AT BS 540. MAINTENANCE CUTOUT DAMAGED SECTION OF KEEL BEAM AT BS 540, FABRICATED A REPAIR DOUBLER, SPLICE ANGLE, ATTACH ANGLE, RADIUS BLOCK, AND TIE CLIP, AND INSTALLED REPAIR PARTS IAW AWA E.R. 03Sep 3, 2002 · N336AW · Boeing 737375 · Fuselage Main, KeelSDR AWXA200200961Skin Panel · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/4" CRACK WAS FOUND ON THE # 1 ENGINE PYLON TOP FAIRING FORWARD OUTBOARD PANEL CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED., FABRICATED A DOUBLER, AND INSTALSep 2, 2002 · N336AW · Boeing 737375 · Nacelle/Pylon, Plate/SkinSDR AWXA200200953Web · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1.5 INCH CRACK WAS FOUND ON SHEAR WEB ALONG UPPER ANGLE AT BS 500 - BS 520, BL 0. MAINTENANCE REMOVED DAMAGED SHEAR WEB. FABRICATED A NEW REPLACEMENT SHEAR WEB, INSTALLED REPAIR PART IAW DWG 69-35365, AND B737-300 SRSep 2, 2002 · N336AW · Boeing 737375 · Fuselage Miscellaneous StructureSDR AWXA200200951Floorbeam · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1 INCH CRACK WAS FOUND ON FLOORBEAM UPPER TEE CAP AT FWD SIDE OF BS 520, RBL 25. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER TEE CAP. FABRICATED A NEW REPLACEMENT FLOORBEAM UPPER TEE CAP AND INSTALLED REPAIR PART IAW Sep 2, 2002 · N336AW · Boeing 737375 · Fuselage Main, Floor BeamSDR AWXA200200969Skin · corrodedYVR - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON SKIN OF THE # 1 ENGINE PYLON UPPER FAIRING JUST FORWARD OF THE UPPER ATTACH POINT, SKIN BULGED BETWEEN SKIN JOINTS AS VIEW FROM UPPER SURFACE. MAINTENANCE REMOVED FASTENERS AND LIFTED SKIN ; CLEANEDSep 1, 2002 · N336AW · Boeing 737375 · Nacelle/Pylon, Plate/SkinSDR AWXA200200960Shear Tie · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 3/8" CRACK WAS FOUND ON FRAME ATTACH ANGLE (SHEAR TIE) AT BS 727D, ABOVE STR 14 R/H. MAINTENANCE REMOVED DAMAGED SHEAR TIE AT BS 727D, FABRICATED A NEW SHEAR TIE, AND INSTALLED REPAIR PART IAW AWA E.R. 03-5362-02270-ES2Sep 1, 2002 · N336AW · Boeing 737375 · Fuselage Main, FrameSDR AWXA200200954Shear Tie · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON FRAME ATTACH ANGLE (SHEAR TIE) AT BS 727D, BELOW STR 15 R/H. MAINTENANCE REMOVED DAMAGED SHEAR TIE AT BS 727D, BELOW STR 15 R/H; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAWSep 1, 2002 · N336AW · Boeing 737375 · Fuselage Main, FrameSDR AWXA200200948Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-03 CHECK A 1/2" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STRINGER 4 L/H. MAINTENANCE REMOVED THE DAMAGED STINGER TIE CLIP AT BS 727B, STRINGER 4 L/H, FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-3Sep 1, 2002 · N336AW · Boeing 737375 · Fuselage Main, Longeron/Stringer
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