N8677A

Service difficulty reports · 118

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 = 'N8677A' 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 SWAA2024012936529Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF UPPER AND LOWER SURFACE CORROSION FROM STA747+2 - STA747+18<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 747+2 TO STA 747+18. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936593Plate · corrodedFWD. CARGO BILGE; R/H SIDEPLATE CORRODED HOLES FROM BS 490R-BS 500A.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED WORK IN C/A #1;[03] REMOVED AND REPLACED SIDEPLATE SHIELD ASSY PER SRM 5Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936614Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS500B-BS500+10.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF SIDE PLATE TO BE REPLACED NON NR# TTG8Q00QLSX7 FROM STA. 500A TDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936598Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500E-500F.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-020-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CARDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936602Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500F-BS 500G.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .009' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936605Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500G-BS 500H.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936607Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500H-BS 500I.<[01] THIS SECTION TO BE REPLACED ON TASK CARD TTG8Q00QLSX7;[02] BLENDED AREAS; REMOVED .007' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON TASK CDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012636594Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500B+16.<[01] BLENDED AREAS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS; REMOVED 0.008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] FABRICATED REPLACEMENT SECTIDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012636601Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500E-BS 500F.<[01] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.<BR>THIS SECTION TO BE REPLACED ON TTG8Q00QLSX2;[02] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012636603Plate · corrodedFWD. CARGO; L/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500F-BS 500G.<[01] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.<BR>THIS SECTION TO BE REPLACED ON TTG8Q00QLSX2;[02] REMOVE DAMAGE(0.008' MATERIAL) FOUND TO BE OUT OF LIMDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012636486Strap · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; MULTIPLE AREAS OF CORROSION ON FLOOR SUPPORT STRAP AT STA767+5<[01] FLOOR SUPPORT STRAP TO BE REPLACED NEW REF SRM 53-00-53;[02] VERIFIED CORRECTIVE ACTION #1Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536512Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA 727C+16<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727C+16?. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; FOUDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536467Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727D+3- STA727D+6<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727D+3 TO STA 727D+6. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536468Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727J+6 - STA727J+14<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J +6 - STA 727J+14. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS ISDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536516Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 727I+10- STA727I+18<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I +10- STA 727+18. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536470Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 747+6- STA747+14<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747 +6 - STA 747+14. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.00Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536471Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA 767+10- STA767+15<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 767 +10- STA767+15. ORIGINALS MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.0Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536517Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA807<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 807. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO BE OUDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536518Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727E+13<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727E+13. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536475Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727E+16<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727E+16. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536477Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727F+9<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727F +9. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536520Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION AT STA727G+6<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727+6. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536478Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727+15<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727+15. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TODec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536523Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727A+12<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727+12. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND TDec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536525Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727E+12.5<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727E+12.5. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005?; MAX ALLOWED IS 0.004?; FODec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536479Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND TO BE ODec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536526Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727G<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727G. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TO BE Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536480Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F+9<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F+9. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; FOUND TODec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536527Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS SURFACE CORROSION AT STA727F+19<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727F+19. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.004?; FOUND Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536481Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA727H+6 - STA727H+16<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727H+6 TO STA 727H+16. ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012536482Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; RIGHT SIDE PLATE HAS AREAS OF SURFACE CORROSION FROM STA727I+7 - STA727I+16<[01] REMOVED CORROSION FROM AFT CARGO R/H SIDE PLATE FROM STA 727I+7 TO STA 727I+16 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012436595Plate · corrodedFWD. CARGO; R/H SIDEPLATE HAS CORROSION AT HOLES FROM BS 500C-BS 500D.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED R/H TRANSITION ANGLE FROM 727 A TO 727 I PER SRM 51-10-02;Dec 30, 2023 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024012936189Seal · cracked343AT SLIDER SEAL RETAINER CRACKED.<[01] REPLACED BLADE SEAL ASSY PER SRM 51-40-02.;[02] C/W INSPECTIONDec 29, 2023 · N8677A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024012936186Seal · crackedSLIDING SEAL RETAINER CRACKED ON PANEL 333AT<[01] REPLACED BLADE SEAL ASSY PER SRM 51-40-02.;[02] C/W INSPECTIONDec 29, 2023 · N8677A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2023071076473Light · inoperativeL2 EMERGENCY LIGHT INOP.<[01] RELAMPED L2 SLIDE EMERGENCY LIGHT IAW AMM. 33-51-04. OPS CHECK GOOD.Jul 8, 2023 · N8677A · Boeing 7378H4 · Emergency LightingSDR SWAA2023041726470Panel · crackedAFT CARGO LH CENTER PANEL 141DW IS CRACKED ALONG BOTTOM EDGE<Apr 12, 2023 · N8677A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023041426469Panel · crackedAFT CARGO LH CENTER PANEL 1412EW IS CRACKED AND DELAMINATED ALONG BOTTOM EDGE.<Apr 12, 2023 · N8677A · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2023012493167Bracket · brokenAFT CARGO DOOR ASSIST HANDLE BRACKET BROKEN<[01] REMOVED AND REPLACED ASSIST HANDLE CABLE BRACKET AT FLOOR STRUCTURE ;REF B737 AMM 52-31-00 .Jan 20, 2023 · N8677A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022121280484Slide · low pressureSF DOOR SLIDE LOW PRESSURE / [01] R&R FS SLIDE ASSY PER AMM 25-66-01;[02] R&R FS SLIDE ASSY PER AMM 25-66-01Dec 10, 2022 · N8677A · Boeing 7378H4 · Escape SlideSDR SWAA2022100552082Lens · missingEXIT SIGN LENS COVER MISSING ON CAPTAINS SIDE OVER WING HATCH / [01] INSTALLED LENS PER M/M 33-51-01Oct 3, 2022 · N8677A · Boeing 7378H4 · Emergency LightingSDR SWAA2022082645280None · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1672; M1670; M1675 EMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1672 M1670 M1675 / [01] REPLACED M1672; M1670; AND M1675 ELBP?S REF 33-51-06;[02] AMM 33-51-06Aug 24, 2022 · N8677A · Boeing 7378H4 · Emergency LightingSDR SWAA2022052409880Pin · shearedFWD ENTRY DOOR WILL NOT OPEN / [01] FOUND BROKEN SCREW ON THE UPPER GUIDE ARM PIN. R/R PIN AND SCREW PER AMM 52-11-21. AND OPS CHECK OF FWD ENTRY DOOR IS O.KMay 20, 2022 · N8677A · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2022021672223Battery Pack · inoperativeALL FWD CABIN EMERGENCY LIGHTS POWERED BY BATTERY PACK M2816 ARE INOP / [01] REPLACED CHARGER ASSY PACK PER AMM 33-51-06-960-806;[02] FOR FWD CEILING BATTERY M2816;[03] REPLACED BATTERY PACK IN FWD CEILING M2816 PER AMM 33-51-06-960-805;[04] OPS TEST PASSEDFeb 13, 2022 · N8677A · Boeing 7378H4 · Emergency LightingSDR SWAA2022021672221Battery Pack · inoperativeALL AFT CABIN EMERGENCY LIGHTS POWERED BY BATTERY PACK M1672 ARE INOP / [01] REPLACED BATTERY PACK IN AFT RIGHT CEILING M1672 PER AMM 33-51-06-960-805;[02] OPS TEST PASSED;[03] VERIFIED ITEMS 1 AND 2. AUDIT COMPLETEFeb 13, 2022 · N8677A · Boeing 7378H4 · Emergency LightingSDR SWAA2022021670370None · crackedDOT A-24-10. PANEL 551FB AFT SUPPORT CLIP CRACKED OFF ABOUT 2 FEET O/B OF I/B END. / [01] REMOVED AND REPLACED PNL 551 FB AFT SUPPORT CLIP CRACKED WITH A NEW SUPPORT CLIP P/N 287A9152-23; A TAG# WN7755. IAW SRM 51-40-02-OG-0; IPC # 57-50-00-38.;[02] VERIFIED IFeb 8, 2022 · N8677A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022021464378Angle · corrodedAFT CARGO FWD SHIELD ATTACH ANGLE (146A8125-53) CORRODED AROUND NUTPLATE HOLES RBL 24 WL 156 ; / [01] REMOVED CORROSION ON ATTACH ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : .050 ORIGINAL 'T'.030 REMAINING .020 LOSS FOUND OUT OF LIMIJan 26, 2022 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022021464377Support · crackedCABIN FLOOR PANEL SUPPORT ANGLE AT STATION 540 RBL 1' CRACKED AT FASTENER HOLE. ; / [01] REMOVED CABIN FLOOR BOARD 231UF FOR ACCESS IAW SRM 51-40-02-G0-G; [02] REMOVED CRACKED FLOOR SUPPORT ANGLE IAW SRM 41-40-02-0G-0; [03] VERIFIED NEW FLOOR SUPPORT ANGLE PN:Jan 25, 2022 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022021463529Angle · crackedRIGHT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] RH PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER TANK AT STA 663 WAS REPLACED OJan 23, 2022 · N8677A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022021664518Shield · crackedA-061 DOT 054. #1 ENGINE INBD FAN COWL ATTACH ANGLE FOR DOOR 414AR CRACKED / [01] REMOVED CRACKED FAN COWL ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW PART; SHIELD ATTACH ANGLE P/N 314-2259-4 IAW CMM 71-13-30<BR>ATAG A111638;[03] VERIFIED STEPS 1 AND Jan 18, 2022 · N8677A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2022021462279Angle · corrodedDOT#14-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 500E+7 TO 500I RBL 24 WL 156 ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : .040 ORIGINAL .010 REMAINING .030 LOSS FOUND OUT OF LIMITS IAW SRM 53-00 53-1A-2 TOOLJan 18, 2022 · N8677A · Boeing 7378H4 · Fuselage Miscellaneous Structure
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