Boeing 737-301

Service difficulty reports · 4,797

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 = '737301'
  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 AWXA200500314Strap · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL UPPER STRAP BETWEEN BS 794 AND BS 847 AT STR 25 RT. MAINTENANCE REMOVED CORRODED SECTION AFT CARGO DOOR SILL UPPER STRAP FROM BS 794 TO BS 847 AT STR 25 RT; FABRICATFeb 12, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050281Door Frame · crackedPIT - FOUND DOOR WITH THREE .5 INCH CRACKS, AFT CARGO DOOR FORWARD FRAME. REMOVED AND REPLACED DOOR PER JOB CARD J3-57-52301. (M)Feb 11, 2005 · N585US · Boeing 737301 · Cargo/Baggage DoorsSDR SB05026Light · inoperativePILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.Feb 11, 2005 · N340US · Boeing 737301 · Emergency LightingSDR AWXA200500303Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 3 EACH .25 INCH CRACKS WERE FOUND IN FUSELAGE FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT. MAINTENANCE CUT OUT CRACKS IN FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT; FABRICATED FILLERS AND A REPAIR ANGLE; INSTALLFeb 10, 2005 · N326AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200500293Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .1875 INCH CRACKS WERE FOUND IN R-2 DOOR LOWER FORWARD FRAME SECTION BS 957, STR 16 RT. MAINTENANCE CUT OUT DAMAGE IN R-2 DOOR LOWER FORWARD FRAME SECTION; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PAFeb 10, 2005 · N326AW · Boeing 737301 · Fuselage Main, FrameSDR SWAA050395Slide · reads lowDURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.Feb 10, 2005 · N660SW · Boeing 737301 · Escape SlideSDR AWXA200500235Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM STIFFENER ANGLE ON AFT SIDE FLOORBEAM AT BS 328, BETWEEN RBL 43 AND RBL 60. MAINTENANCE REMOVED CORRODED FLOORBEAM STIFFENER ANGLE AT BS 328, FROM RBL 43 TO RBL 60; FABRICATEFeb 8, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500310Reveal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER FORWARD REVEAL AT 957, STR 17 RT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR LOWER FORWARD REVEAL IAW B737-300 SRM 51-40-02.Feb 7, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500232Crease Beam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN WEB UNDER CREASE BEAM INNER CHORD AT BS 986.5, LBL 43. MAINTENANCE REMOVED DAMAGED WEB FROM BS 986.5 TO BS 1016, LBL 37 TO LBL 45; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLEFeb 7, 2005 · N326AW · Boeing 737301 · Fuselage Main, StructureSDR SWAA050340Skin · crackedDURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 10, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.Feb 7, 2005 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500167Wheel · overheatedPHX - ABORTED TAKEOFF - FLT 227 - ON TAKEOFF AT APPROX 135 KTS. A BIRD STRIKE WAS REPORTED HITTING THE FORWARD LEFT AND RIGHT WINDSHIELDS. TAKEOFF WAS ABORTED. MX PERFORMED A BIRD STRIKE INSPECTION IAW TASKCARD I8M05030. NO DAMAGE NOTED. MX PERFORMED AN IFeb 6, 2005 · N325AW · Boeing 737301 · Wheel/Ski/FloatSDR AWXA200500292Skin · wornMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND FUSELAGE SKIN WORN IN SEVERAL AREAS AT LT AND RT DORSAL FIN SEALS BETWEEN BS 860 AND BS 907.5. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT LT AND RT DORSAL FIN SEALS FROM BS 860 TO BS 907.5; PERFORMED HFEC INSPEFeb 3, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA050221Plate · crackedPIT - FOUND HINGE DOUBLER PLATE CRACKED .3750, MED TOP FORWARD HINGE CUTOUT INSIDE BOTTOM FORWARD CORNER. INSTALLED WEB PER SRM 51-40-02 AND DWG 65-17684. (M)Feb 1, 2005 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500326Support · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW T/C I3R57057.Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500325Gimbal Joint · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE WBL 185.0. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW T/C I3R57057.Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500324Support · corrodedMCN - FLIGHT CONTROL - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT WBL 71.24. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT IAW BOEING SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500226Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMAGED AREA OF UPPER NR 2 SLAT SKIN FROM SS 249.77 TO SS 254.27; FABRICATED A CORE FILLER AND EXTERNALJan 31, 2005 · N326AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200500191Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL INDEX PLATE AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL ASSEMBLY IAW SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500190Gimbal Joint · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL OUTER SUPPORT AT WBL 184. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT IAW SOPM 20-50-01.Jan 31, 2005 · N326AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500329Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947; FABRICATED 2 EACJan 28, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500296Strap · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN LOWER FORWARD INBOARD EDGE OF FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED DAMAGED FRAME STRAP AT BS 349, STR 16 LT; INSTALLED A NEW REPLACEMENT FRAME STRAP IAW ER 03-5300-05053-SJan 28, 2005 · N326AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200500248Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT. MAINTENANCE CUT OUT CRACK IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT; FABRICATED REPAIR DOUBLER; INSTAJan 28, 2005 · N326AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500294Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .0625 INCH CRACKS WERE FOUND IN L-1 DOOR FORWARD FRAME INTERCOSTAL WEB BS 294.5, STR 7 LT. MAINTENANCE REMOVED DAMAGED L-1 DOOR FORWARD FRAME INTERCOSTAL WEB FROM BS 294.5 TO BS 303.9; FABRICATED A NEW REPLACEMENTJan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500287Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0265 INCH CRACK WAS FOUND IN RADIUS OF ANGLE CLIP AT AFT SIDE OF STRINGER SPLICE CHANNEL BS 348.2, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE CLIP FROM BS 348.2 TO BS 351.2, STR 16 LT; FABRICATED NEW REPLACEMENT CLIJan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500286Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN INBOARD FORWARD LOWER EDGE OF STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 16 LT; Jan 27, 2005 · N326AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200500282Web · chafedMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND L-1 DOOR UPPER HINGE CUTOUT UPPER WEB CHAFED ON LOWER SIDE BETWEEN BS 294.5 AND BS 303.9, STR 13 LT. MAINTENANCE REMOVED CHAFED WEB AT L-1 DOOR UPPER HINGE CUTOUT FROM BS 294.5 TO BS 303.9, STR 13 LT; FABRICATED A NJan 27, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500261Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK, A 3" CRACK WAS FOUND IN AFT SIDE L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT. MAINTENANCE REMOVED CRACKED L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT; FABRICATED A NEW REPLACEMENT ATTJan 27, 2005 · N326AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200500081Light · inoperativePHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 12 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD.Jan 27, 2005 · N325AW · Boeing 737301 · Emergency LightingSDR AWXA200500080Light · inoperativePHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH SIGN INOPERATIVE AT SEAT ROW 11 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH SIGN AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.Jan 27, 2005 · N325AW · Boeing 737301 · Emergency LightingSDR SB05017Wire · faultyPVD - MAINTENANCE REPORTED THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHT CIRCUIT BREAKER ON THE P-18 PANEL. OPERATIONAL CHECK GOOD.Jan 27, 2005 · N563AU · Boeing 737301 · Light System WiringSDR USAA050219Skin · crackedPIT - FOUND SKIN CRACKED THREE PLACES, .125 INCH .8750 INCH AND .125 INCH, E/E COOLING DUCT SKIN, LOWER FUSELAGE BS 380 S27R AND S27L. SKIN DOUBLER INSTALLED PER EO 5300V258. (M)Jan 26, 2005 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500302Light · inoperativeMCN - EEL - DURING C-18 CHECK FOUND THE L-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHECK WAS GOOD.Jan 26, 2005 · N326AW · Boeing 737301 · Emergency LightingSDR USAA050152Skin · crackedCLT - RON - SKIN, 1.750 INCH CRACK, STRINGER 23R STATION 727E; INSTALLED DOUBLER. (K)Jan 26, 2005 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB05015Csd · failedORF - FLT178 - DURING CRUISE, EN ROUTE FROM CLT TO BOS, THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE APU WAS ALREADY ON MEL, SO THE CREW DISCONNECTED THE NR 1 ENGINE CSD AND DIVERTED TO ORF WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. Jan 26, 2005 · N558AU · Boeing 737301 · Alternator-Generator DriveSDR SB05016Light · failedCLT - FLT1435 - DURING DESCENT INTO CLT FROM ORD, CREW REPORTED SMOKE ENTERING COCKPIT FROM BEHIND FIRST OFFICER "PULL UP" ANNUNCIATOR LIGHT ON FIRST OFFICER'S INSTRUMENT PANEL. ALSO, ALL LIGHTS ASSOCIATED WITH THE LIGHT TEST SWITCH ILLUMINATED. MOVING TEST Jan 26, 2005 · N353US · Boeing 737301 · Flight Compartment LightingSDR AWXA200500328Plate · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND IN CLOSE PANEL BETWEEN FORWARD END OF R-2 DOOR CUTOUT AND BS 947. MAINTENANCE REMOVED CRACKED CLOSE PANEL FROM BS 947 TO BS 957, STR 14 RT TO STR 16 RT; FABRICATED A NEW REPLACEMENT CLOSE PANEJan 25, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500327Reveal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-1 DOOR UPPER AFT REVEAL. MAINTENANCE REMOVED CRACKED R-1 DOOR UPPER AFT REVEAL FROM BS 320 TO BS 328 AT STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-53594; INSTALLED REPAIR PARTJan 25, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA050218Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, AFT SERVICE DOOR TOP HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-60-01. (M)Jan 25, 2005 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500301Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN EMANATING FASTENER HOLE AT LOWER HINGE CUTOUT BS 328, STR 15-16 RT. MAINTENANCE REMOVED EXISTING DOUBLER AND CUT OUT CRACK IN R-1 DOOR EXTERNAL SKIN; FABRICATED A FIJan 25, 2005 · N326AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200500300Flashlight · inoperativeMCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Jan 25, 2005 · N326AW · Boeing 737301 · Emergency EquipmentSDR AWXA200500299Flashlight · inoperativeMCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Jan 25, 2005 · N326AW · Boeing 737301 · Emergency EquipmentSDR AWXA200500285Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD UPPER CORNER CUTOUT OF R-1 DOOR. MAINTENANCE TRIMMED OUT CRACK IN FUSELAGE SKIN FORWARD UPPER CORNER CUTOUT OF R-1 DOOR; FABRICATED FILJan 25, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA050206Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA.Jan 25, 2005 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200500331Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 986, LBL 44, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 986, FROM BL 0 TO LBL 50; FABRICATED A NEW REPLACEMENT SECTION OF T-CAP, AND 2 EACH SUPPORT ANGLES & SJan 24, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500290Sill · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL INNER CHORD BETWEEN BS 950 AND BS 994, LBL 50. MAINTENANCE REMOVED CORRODED L-2 DOOR SILL INNER CHORD FROM BS 917 TO BS 1016, LBL 50; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500262Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK, A 0.8125 INCH CRACK WAS FOUND IN UPPER AFT CORNER OF INTERCOSTAL AT BS 293, LBL 33, WL 208. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL AT BS 293, LBL 33; FABRICATED A REPAIR ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW B737Jan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500249Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27. MAINTENANCE CUT OUT DAMAGE IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAWJan 24, 2005 · N326AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500333Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 1016, RBL 5, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 1016, RBL 5; FABRICATED A 3 EACH REPAIR PLATES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 5Jan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500295Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND LOWER SURFACE OF TRANVERSE FLOORBEAM T-CAP AT BS 986, BETWEEN RBL 40 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM T-CAP AT BS 986 FROM RBL 0 TO RBL 50; FABRICATED A NEW REPLACEMENT SECTIJan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200500229Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 445, BL 0. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER AND CUT OUT DAMAGED AREA OF SKIN AT BS 445, BL 0; PERFORMED A HFEC INSPECTION OF CUTJan 23, 2005 · N326AW · Boeing 737301 · Fuselage Main, Plate/Skin
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