N8697C

Service difficulty reports · 80

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N8697C' AND registry_match = 'registration'
  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 SWAA2026101500242Doubler · crackedEGPR SURROUND DOUBLER CRACKED AT LOWER FLANGE. ACCOMPLISHED REPAIR ON EGPR SURROUND DOUBLER LOWER FLANGE IAW SRM 53-10-15-2R-4.Oct 2, 2026 · N8697C · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2026091838814Slide · exposedFWD ENTRY ESCAPE SLIDE HANGING OUT. TUCKED IN ESCAPE SLIDE EXCESS MATERIAL IAW AMM 25-66-00. DID NOT REMOVE OR OPEN SLIDE.Sep 14, 2026 · N8697C · Boeing 7378H4 · Escape SlideSDR SWAA2026090378156Engine · no discrepancyNR 2 ENGINE AUTO SHUTDOWN WITH FLASHING WHTE BOX, NR 2 ENGINE FOUND AC TO BE POSTIONED WITH TAIL DIRECTLY INTO THE WIND DURING ENG START. NO DEFECTS NOTED IAW 71-00-00.Aug 30, 2026 · N8697C · Boeing 7378H4 · Engine (Turbine/Turboprop)SDR SWAA2026061710896Lens · missingAFT COVE CEILING PANEL EMERGENCY LIGHT LENS MISSING. INSTALLED LENS IAW B737-NG AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED. INSTALLED LENS IAW AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED.Jun 10, 2026 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2026061611064Bracket · missingL1 DOOR FWD GIRT BAR FITTING MISSING. INSTALLED L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801. VERIFIED INSTALLED SERVICEABLE L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801.Jun 10, 2026 · N8697C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026012864552Battery · no testFORWARD GALLEY FLASHLIGHT WILL NOT TEST. R & R THE FWD GALLEY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.Jan 26, 2026 · N8697C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026010657926Cover · brokenLIGHT COVER BROKEN AT ROW 10 CABIN AISLE EMERGENCY LIGHT HOUSING MOUNTED IN THE OVERHEAD BIN BULLNOSE. OK TO CONTINUE IAW MEL 33-15-02 SP1. REMOVED AND REPLACED ROW 10 DEF EMERGENCY LIGHT LENS COVER REFERENCING AMM 33-51-03. OPS CHECK GOOD.Jan 3, 2026 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2025091914809Lens · brokenAFT SERVICE DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS PER AMM 33-51-01.Sep 16, 2025 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2025091911824Battery Pack · inoperativeLT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM 33-51-06-960-805-NG.Sep 5, 2025 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2025091907310Bezel · brokenESCAPE HATCH; LEFT SIDE PANEL 833 CLOSING STRAP BEZEL ATTACHED TO DOOR LINER IS BROKEN. SECURED CLOSING STRAP BEZEL TO THE LEFT OVERWING EXIT DOOR 833 PANEL PER SOPM 20-50-12.Aug 22, 2025 · N8697C · Boeing 7378H4 · Emergency ExitsSDR SWAA2025091907318Strap · unsecureESCAPE HATCH; LEFT SIDE PANEL 833 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE. SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.Aug 22, 2025 · N8697C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025091907317Strap · out of adjustESCAPE HATCH; RIGHT SIDE PANEL 843 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE.<[01] SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.;[02] VERIFIED SECURED ESCAPE STRAP RED VELCRO COVER TAug 22, 2025 · N8697C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025092207019Attach Angle · crackedCRACK FOUND AT BS 663, RBL 34, ON VAPOR BARRIER ATTACH ANGLE. REMOVED VERTICAL ATTACHED FASTENERS ON RT 663 CHORD IAW SRM 51-40-02. REMOVED FUEL TANK FASTENERS AT BS 663 ON VAPOR BARRIER ATTACH ANGLE RBL 6 TO RBL 43 IAW SRM 51-40-02. REMOVED AND REPLACED Aug 21, 2025 · N8697C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025092206615Angle · crackedNUMBER 1 ENGINE INBD FAN COWL ANGLE AT AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED AT UPPER CORNER. REMOVED AND REPLACED THE NR 1 ENGINE INBD FAN COWL WEB AT OIL SERVICE DOOR IAW AMM 51-40-02.Aug 21, 2025 · N8697C · Boeing 7378H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2025092206607Skin · delaminatedLEFT WING OTBD AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON INBD CORNER. REMOVED LT WING OTBD AFT FLAP IAW AMM 27-51-22. INSTALLED LT WING OTBD AFT FLAP IAW AMM 27-51-22.Aug 20, 2025 · N8697C · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2025092206605Plate · crackedHFEC SHOWS EVIDENCE OF CRACK IN WIGGLE PLATE ON FWD INBD CORNER OF PANEL 551EB ATTACH POINT.<[01] HFEC WIGGLE PLATE PER NDT MANUAL 51-00-00 PROCEDURE 23;[02] REMOVED DAMAGED WIGGLE PLATE PER SRM 51-40-02.;[03] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02Aug 20, 2025 · N8697C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2024122380474Lens · missingBOTH AFT GALLEY EXIT SIGN LENSES MISSING<[01] REINSTALLED GALLEY EXIT SIGN LENSES IAW AMM 33-51-01Dec 22, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024082228088Slide · dislodgedL1 DOOR SLIDE IS COMING OUT OF ITS CASE<[01] REPOSITION L1 DOOR ESCAPE SLIDE IAW MT 725-61-06Aug 19, 2024 · N8697C · Boeing 7378H4 · Escape SlideSDR SWAA2024072616381Battery Pack · inoperativeAFT LEFT EMERGENCY LIGHTS BATTERY PACK INOP. R&R BATTERY PACK PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.Jul 24, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024072614281Battery Pack · inoperativeFWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C L/H IS INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT POWER PACK AT STA 500C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024072614282Battery Pack · inoperativeFWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C R/H IS INOP. REMOVED AND. REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500 R/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024072614283Battery Pack · inoperativeAFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-0Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024072614284Battery Pack · inoperativeAFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C RT IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C R/H PER AMM 3-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency LightingSDR SWAA2024072613573Floor Support · crackedPASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; RBL 2.<[01] REMOVED AND REPLACED PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1Jul 17, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072613574Floor Support · crackedPASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; LBL 2.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1Jul 17, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072909913Floor Support · corrodedFLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON FWD/RH EDGE<[01] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 25. ORIGINAL THICKNESS OF 0.084; MATERIAL REMOVED .024; REMAINING THICKNESS IS Jul 7, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072608010Angle · corrodedFWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 58 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES AND RADIUS AREA. (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PEJul 2, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072608012Angle · corrodedFWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 61 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES. (M) (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-Jul 2, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907627Floor Support · corrodedFLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STAS 927-947; LBL 51 HAS CORROSION AT STA 946.<[01] REMOVED FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02;[02] REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHIJul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907628Attach Angle · corrodedUPPER WEB ATTACH ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 HAS CORROSION AT STA 946.<[01] REMOVED CORROSION UPPER WEB ATTACH ANGLE LOCATED BETWEEN STA?S 927-947; RBL 25 . ORIGINAL THICKNESS OF 0.070; MATERIAL REMOVED .019; REMAINING THICKNESS IS 0.051. ANGLE Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2024072907623Intercostal · corrodedFLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 51 HAS CORROSION ON TOP/FWD SURFACE.<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN SJul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907789Plate · corrodedCORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727I-727J (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I-727J ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907777Plate · corrodedCORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727J-747 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J-747 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OFJul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907779Plate · corrodedCORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 747-767 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747-767 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LJul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907622Floor Support · corrodedFLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 25 HAS CORROSION ON FWD/LH EDGE<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907793Skin · delaminatedLH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B Jul 1, 2024 · N8697C · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2024072907516Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500E-500F.(MARKED)<[01] BLENDED AREAS; REMOVED .010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[02] BLENDED AREAS; REMOVED .010 ' MATERIAJun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907520Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500A-500B.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05 ;OK TO Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907511Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500C-500D.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-0Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072607513Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500F-500G.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNJun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072607514Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500H-500I.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNJun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072607525Plate · corrodedCORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500D-500E.(MARKED)<[01] BLENDED AREAS REMOVED .009' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED OUT OF LIMITS;[03] FABRICATED REPAIR PARTS PER SRM 53-00-53-2R-5 AND EA MJun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072907360Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL50 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 50 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.075IN MATERIAL; REMAINIJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072907356Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL25 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 25 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINIJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072907361Intercostal · corrodedPASSENGER CABIN BS952 LBL25 SCREW HOLE HAS POSSIBLE CORROSION.<[01] REMOVED LIGHT SURFACE CORROSION ON PASSENGER CABIN BS952 LBL25 SCREW HOLE. ORIGINAL THICKNESS OF 0.083; MATERIAL REMOVED .003; REMAINING THICKNESS IS 0.080. INTERCOSTAL FOUND TO BE WITHIN LIMIJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024072607354Angle · corrodedPASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. NDT PART 6;51-00-00 PROCEJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072617793Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE.<[01] REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[03] C/W INSPECTIOJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072607355Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 LBL51 UNDER LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.100IN MATERIAL; REMAINING THICKNESJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072607357Floorbeam · corrodedPASSENGER CABIN FLOOR BEAM BS947 RBL28 HAS SURFACE CORROSION ON TOP SIDE .<[01] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING 0.128IN; FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1..;[02] ENTIRE LENGTH OF FLOOR BEAM UPJun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024072906727Bracket · corrodedRH WING LEADING EDGE FUEL GAUGE BRACKET HAS CORROSION MARKED<[01] REMOVED AND REPLACED WING REFUEL PANEL PER SOPM 20-50-01 AND MM 28-41-61.REFUELING PANELS OPS CHECKED GOOD PER MM 28-41-61;MM 28-21-81 AND MM 28-21-00;[02] C/W INSPECTIONJun 28, 2024 · N8697C · Boeing 7378H4 · Wing Miscellaneous Structure
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