N8675A

Service difficulty reports · 130

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 = 'N8675A' 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 SWAA2026093046583Battery · inoperativeLEFT AFT INBD FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE, OK TO CONTINUE PER MEL 25-12-01. R & R THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.Sep 26, 2026 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026081002003Engine · failedNR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED THE NR 1 ENG IAW MT 771-00-01. REF TTG8Q008F2S8.Aug 4, 2026 · N8675A · Boeing 7378H4 · Engine (Turbine/Turboprop)SDR SWAA2025121551604Bracket · brokenFWD MEGAPHONE BRACKET BROKEN. R & R BRACKET IAW AMM 25--64-00 SIP.Dec 11, 2025 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025110731884Tray · delaminatedPASSENGER CABIN SEAT BACK MOUNTED TRAY TABLE DELAMINATED AT 15E. REMOVED AND REPLACED FOOD TRAY TABLE AT 15E IAW CMM 25-22-46Nov 5, 2025 · N8675A · Boeing 7378H4 · Passenger Compartment EquipmentSDR SWAA2025091113312Battery · intermittentCREW REPORTS FWD MEGAPHONE WORK INTERMITTENTLY. R & R FWD MEGAPHONE BATTERIES IN REF TO AMM 25-64-00. NEXT INSPECTION DUE SEP 2026Sep 9, 2025 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025052772867Tab · crackedLEFT WING FIXED TRAILING EDGE DEFLECTION ROLLERS ASSEMBLYS PANEL ATTACHMENT TAB HAS A VISIBLE CRACKED 1.7 INCHES IN THE RADIUS FROM THE AFT EDGE.PICTURE ATTACHED. REPAIRED ATTACHMENT TAB ON LH DEFLECTION CONTROL RIB REF SRM 57-51-02-2R-3 REPAIR 3. REINSTALLEDMay 20, 2025 · N8675A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2025042125874Girt Bar · failedFWD ENTRY DOOR GIRT BAR NOT DISARMED WHEN DOOR WAS OPENED. SLIDE CAME PARTIALLY OUT OF DOOR. SLIDE DID NOT DEPLOY. REINSTALLED FORWARD ENTRY ESCAPE SLIDE PER MT 725-60-01Apr 17, 2025 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025012086390Battery Pack · inoperativeRT HAND EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSY AND BATTERY IAW AMM 33-51-06 SYSY OPERATION NORMAL;[02] INSPECTED REMOVED AND REPLACED CHARGER ASSY AND BATTERY IAW AMM 33-51-06 SYSY OPERATION NORMALJan 15, 2025 · N8675A · Boeing 7378H4 · Emergency LightingSDR SWAA2025012084581Angle · crackedIN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04] RII: VERIFIED C.A STEP 3 (P. GIETZEN AMT) OF FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5.;[05] Jan 9, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012083721Angle · crackedBAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INSTJan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012083722Angle · crackedBAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; FWD SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INSTJan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012083723Angle · crackedBAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500G RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INSTJan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012081294Angle · crackedIN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04] RII: VERIFIED C.A STEP 3 OF FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5.;[05] OK TO INSTALL REPDec 28, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012081291Panel · damagedPANEL 551GB PANEL HAS 2 ELONGATED FASTERNER HOLES. MARKED.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSPECTED REPAIR PER SRM 51-70-06-2R-9.Dec 28, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2025012081293Strap · frayedLEFT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (TECHNICIAN); 28-DEC-2024 20:55 UTC<BR>REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400Dec 28, 2024 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025012081292Strap · frayedRIGHT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (TECHNICIAN); 28-DEC-2024 20:50 UTC<BR>REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-40Dec 28, 2024 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025012081165Floor Support · crackedPASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-RBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02.Dec 27, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012081166Floor Support · crackedPASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-LBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02.;[02] CORRECTED FAILURE TYPE LINE FROM NO TO YES PER TELECOM FOR PHONEVILAY VANRACHACK E62007.;[03] CERTIFIEDDec 27, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012080925Panel · damagedRIGHT WING LOWER WING L/E PANEL #621FB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIVDec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2025012080922Panel · damagedRIGHT WING LOWER WING L/E PANEL #621PB HAS 1EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIVDec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2025012080926Panel · damagedRIGHT WING LOWER WING L/E PANEL #621VB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIVE EXDec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2025012080581Angle · crackedFOUND 'L' ANGLE CRACKED AT STA 663 R/H SIDE A/C BAY FROM FASTENER HOLE. 5TH FASTENER FROM O/B BULKHEAD DIVIDER.<[01] INSPRJCT: WORK ACCOMPLISHED IN STEPS 1; 2 AND 3 ARE MISSING THE WORK REFERENCE AS REQUIRED PER MPM 51.3.1. WORK ACCOMPLISHED IN STEPS 1; 2 ANDec 24, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012080577Angle · crackedL/H WING FIXED T/E ANGLE THAT IS ATTACHED TO THE I/B SIDE OF THE DEFLECTION CONTROL RIB IS CRACKED (MARKED) AFT UPPER T/E<[01] REMOVED OLD ANGLE AND DRILLED NEW ANGLE PER SRM 51-10-02. OK TO INSTALL.;[02] REMOVED OLD ANGLE AND DRILLED NEW ANGLE PER SRM 51-10-0Dec 24, 2024 · N8675A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2025012080580Support Bracket · crackedFIXED TRAILING PANEL ABOVE DEFLECTION CONTROL RIB HAS SUPPORT BRACKET (FWD SIDE) CRACK LOCATED AT WBL 190.<[01] REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.;[02] VERIFIEDDec 24, 2024 · N8675A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2025012080578Rib · damagedR WING TRAILING EDGE STRUCTURE DEFLECTION CONTROL RIB UPPER TAB HAS ELONGATED FASTENER HOLES.(2EA) [MARKED]<[01] CUT OUT DAMAGE IN UPPER TAB IAW SRM 57-51-02-2R-4.;[02] INSPECTED AND VERIFIED CA#1 DANIEL HONKOMP (TECHNICIAN); 27-DEC-2024 23:47 UTC<BR>CUT OUT DDec 24, 2024 · N8675A · Boeing 7378H4 · Wing, Rib/BulkheadSDR SWAA2025012080345Web · frayedFWD CARGO; LEFT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; LEFT OF DOOR- HALF MOON CARGO NET PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 25-52-12-401-NG (CARGO COMPARTMENT NET - REMOVAL/INSTALLATION - PERMANENT)]Dec 22, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012080346Web · frayedFWD CARGO; RIGHT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; RIGHT OF DOOR- HALF MOON CARGO PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 25-52-12-401-NG (CARGO COMPARTMENT NET - REMOVAL/INSTALLATION - PERMANENT)]Dec 22, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102452279Girt Bar · out of alignmentFLIGHT ATTENDANT REPORTS THAT FWD SERVICE DOOR GIRT BAR IS HARD TO STOW ON HOOKS<[01] RR?D FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01Oct 23, 2024 · N8675A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024070106876Lens · unsecureCENTER AISLE EXIT SIGN NOT SECURE<[01] SECURED EXIT SIGN LENS COVER PER M/M 33-51-01Jun 27, 2024 · N8675A · Boeing 7378H4 · Emergency LightingSDR SWAA2024020546548Pump · low pressureA HYD SYSTEM FAILURE CREW NOTED LOSS OF A SYSTEM ENGINE PUMP PRESSURE AND LOSS OF 50% OF FLUID. 'FOLLOWING CHECKLIST' RAN ELECTRIC PUMP TILL ZERO PRESSURE AND ZERO QUANTITY INDICATION AT WHICH TIME SHUT OFF ELECTRIC PUMP. NOTED 18% REMAINING AFTER SHUTDOWN ANDJan 30, 2024 · N8675A · Boeing 7378H4 · Hydraulic Pump (Electric/Engine), MainSDR SWAA2023121832365Filler · missingEXTERNAL ELECTRICAL PLUG CUTOUT; EXTERNAL DOUBLER TAB IS MISSING AT THE LOWER LATCH STRIKER PLATE.<[01] REMOVED FASTENERS AT MISSING FILLER FROM PREVIOUS REPAIR. NO ADDITIONAL DAMAGE NOTED. FABRICATED NEW FILLER PER SRM 53-10-15-2R-4. OK TO INSTALL;[02] INSPECDec 15, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023121531422Battery Pack · inoperativeRIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED RIGHT AFT GALLEY EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00;[02] REMOVED AND REPLACED RIGHT AFT GALLEY EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CHDec 13, 2023 · N8675A · Boeing 7378H4 · Emergency LightingSDR SWAA2023121830127Handle · gougedFWD SERVICE DOOR LINER UPPER ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE MOUNTING CUP IN REFERENCE AMM 52-41-31.;[02] REPLACED FWD SERVICE DOOR ASSIST HANDLE MOUNTING CUP IN REFERENCE AMM 52-41-31. C/W INSPECTIONDec 10, 2023 · N8675A · Boeing 7378H4 · Service DoorsSDR SWAA2023121530128Handle · gougedFWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE MOUNTING CUPS IN REFERENCE AMM 25-21-31-420-802 STEP 3.A; B; (6).;[02] REPLACED FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE MOUNTING CUPS IN REFERENCE AMDec 10, 2023 · N8675A · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2023121529579Battery Pack · inoperativeCABIN BULL NOSE EMERGENCY LIGHT; LEFT SIDE INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT SEATS 7; 13; AND 20ABC; OPS CHECKS GOOD; CABIN BULL NOSE EMERGENCY LIGHTS ARE OPERATIONAL. REF. AMM 33-51-06.;[02] REMOVED AND REPLACED BATTERY PACKS AT SEATS 7; 13; ANDDec 8, 2023 · N8675A · Boeing 7378H4 · Emergency LightingSDR SWAA2023121529132Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE IS CRACKED.<[01] REMOVED AND REPLACED AFT CARGO SCUFF PLATE PER AMM 53-11-02Dec 8, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121825199Floorbeam · corrodedFLOOR BEAM CORRODED AT STA 947 LBL 24 NEAR EDGE OF LAV MOUNT<[01] REMOVED CORROSION IAW SRM 51-10-02. THE REWORKED AREA IS OUT OF LIMIT PER SRM 53-70-51-1A-1 FIG 104 DETAIL N.;[02] REJECT: THERE ARE NUMEROUS MEASUREMENT BLOCKS THAT HAVE N/A LISTED AS THE REASONov 27, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2023121525200Radome · crackedNOSE RADOME RUBBER BOOT HAS MULTIPLE CRACKS<[01] REMOVED AND REPLACED RADOME PER MM 53-52-00. SEE CARD [TTG8Q00PX78K FOR TOOLING AND SIGH OFFS.Nov 27, 2023 · N8675A · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2023121524848Light · inoperativeOPS CHECK EMERGENCY LIGHTS<[01] CABIN EMERGENCY LIUGHTS OPS CHECKS GOOD PER MM 33-51-00Nov 26, 2023 · N8675A · Boeing 7378H4 · Emergency LightingSDR SWAA2023121829963Stringer · incorrectBS 727 INNER CHORD AT STRINGER 18A LEFT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE .029 (GAP MEASUREMENT IS GREATER THAN 0.006 INCH)<[01] SHIMED GAP PER 5311-E-14577-NG;[02] C/W INSPECTION;[03] C/W INSPECTIONNov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Longeron/StringerSDR SWAA2023121829964Stringer · incorrectBS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE .021 (GAP MEASUREMENT IS GREATER THAN 0.006 INCH)<[01] SHIMED GAP PER 5311-E-14625-NG;[02] C/W INSPECTION;[03] C/W INSPECTIONNov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Longeron/StringerSDR SWAA2023121824197Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 2 ' APROX AT STA 747 + 2 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824192Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE AROUND ATTACH HOLE AT STA 767 { MARK }<[01] CORROSION REMOVED PER SRM 51-10-02. DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE WAS REMOVED FOR REPLACEMENT FROM STA 727H=+11? - STA 767 PER SRM 51-40-02.;Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824203Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 10 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM<BR>53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGNov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824207Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 6 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE (SIDEPLATE) Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824208Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 14 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.035' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] FABRICATED REPAIR PARTS PER SRM 53-00-Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824209Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 18 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.038' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE FROM STA 72Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824187Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 6 ' APROX AT STA 747 + 6 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824188Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 +14 ' APROX AT STA 747 +14 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023121824198Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 10 ' APROX AT STA 747 + 10 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE ISNov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
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