N8518R

Service difficulty reports · 125

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 = 'N8518R' 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 SWAA2025081403903Cover · detachedOVERWING EXIT SIGN COVER FELL OFF. REINSTALLED OVERWING EXIT SIGN COVER REF AMM 33-51-01.Aug 13, 2025 · N8518R · Boeing 737824 · Emergency LightingSDR SWAA2025061682003Lens · detachedCENTER AISLE EXIT SIGN COVER FELL OFF. REINSTALLED LEN REF AMM 33-51-01.Jun 14, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025052273863Light · inoperativeEXTERIOR EMERGENCY LIGHT INOP AT AFT LT DOOR <[01]. RELAMPED EXTERIOR EMERGENCY SLIDE LIGHT BY AFT LT DOOR PER AMM 33-51-04.May 22, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025022498726Cover · looseEMERGENCY EXIT SIGN BY OVERWING EXIT FELL OFF. <[01] RESECURED OVERWING EXIT SIGN COVERS REF AMM 33-51-01.Feb 22, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012789561Flashlight · inoperativeAFT FLIGHT ATTENDANT POSITION FLASHLIGHT INOP<[01] REMOVED AND REPLACED AFT LEFT INBOARD FLIGHLIGHT REF AMM 25-64-00Jan 25, 2025 · N8518R · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025012187537Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1676 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.Jan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012187538Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M2335 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.Jan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012187539Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1694 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.Jan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012187540Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1670 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.Jan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012187541Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1672 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.Jan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012187536Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1671 WILL NOT CHARGE. REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805. OPS CHECK GOOD. WN4616. COMPLETE<BR>AUDIT C/WJan 19, 2025 · N8518R · Boeing 7378H4 · Emergency LightingSDR SWAA2025012287180Handle · looseL-2 DOOR LINER ASSIST HANDLE IS LOOSE.<[01] RESECURED L-2 DOOR LINER ASSIST HANDLE IS IAW AMM-52-13-31-400-802 3 A G 5;[02] VERIFIED ITEM 1 <BR> AUDIT C/WJan 18, 2025 · N8518R · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2025012179919Intercostal · corrodedDOT A24-11 AFT PIT INTERCOSTAL FOR FORWARD SHIELD IS CORRODED ON UPPER SURFACE BETWEEN STATIONS 767 THROUGH 787 RBL 24 WL 156.<[01] EVALUATED AREA; VERIFIED LIMITS ORIGINAL THICKNEES:0.050'; MATERIAL LOSS: 50%; WITH THE MAX. ALLOWABLE DAMAGE 10% (0.005); THEREDec 20, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012379194Floorbeam · corrodedAFT CABIN WET AREA STA 947 AT LBL 49 WL 208 'T' CAP LOWER SURFACE OF UPPER CHORD CORRODED.<[01] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00XP3L9 WHERE REPAIR WAS COMPLETED PER SRM 53-70-51-2R-5;[02] VERIFIED STEP 1<BR>AUDIT CWDec 19, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012179574Baffle · corrodedDOT A24-26 FORWARD CARGO PIT FOUND RH Z-ANGLE BAFFLE CORRODED BETWEEN STATIONS 500F AND 500G RBL 24; WL 156 DURING FOM INSPECTION.<[01] REMOVED DAMAGE FROM FORWARD CARGO PIT FOUND RH Z-ANGLE BAFFLE CORRODED BETWEEN STATIONS 500F AND 500G RBL 24. IAW SRM 51-10-Dec 19, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012079568Floor Panel · pulledDOT A24-6 CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] REPAIRED CABIN FLOORBOARD 241AF IAW SRM 53-00-50-2R-1. REFER TO FAULT TTG8Q00XPW59 WHERE EA 24-153-03518 WAS ADDED AS A SUBTASK.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/WDec 19, 2024 · N8518R · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025010279575Baffle · corrodedDOT A24-27 FORWARD CARGO PIT FOUND RH Z-ANGLE BAFFLE CORRODED BETWEEN STATIONS 500H AND 500I RBL 24; WL 156 DURING FOM INSPECTION.<[01] REMOVED DAMAGE FROM FORWARD CARGO PIT FOUND RH Z-ANGLE BAFFLE CORRODED BETWEEN STATIONS 500H AND 500I RBL 24. IAW SRM 51-10-Dec 19, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012179182Floor Panel · debondedPAX CABIN FLOOR PANEL 241RF HAS 2 AREAS OF HEAT DAMAGE WITH DISBOND 18' FWD OF AFT EDGE AT LBL 15 AND RBL 15<[01] REPLACED FLOOR PANEL 241RF BY FABRICATION IAW SRM 53-00-50-2R-0; DWG 146A5810-466. REFER TO FAULT TTG8Q00XPW59 WHERE EA 24-153-03518 WAS ADDED AS Dec 18, 2024 · N8518R · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025012079181Floor Panel · pulled154-66 FORWARD CABIN FLOOR BOARD 232AF DENTED AND HAS FIBERS PULLING OUT (MARKED)<[01] REPAIRED CABIN FLOORBOARD 232AF IAW SRM 53-00-50-2R-1. REFER TO FAULT TTG8Q00XPW59 WHERE EA 24-153-03518 WAS ADDED AS A SUBTASK.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/WDec 18, 2024 · N8518R · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025012378564Floorbeam · corrodedDOT#58 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AT STA 947 RBL 24 WL 208<[01] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00XP3L9 WHERE REPAIR WAS COMPLETED PER SRM 53-70-51-2R-5;[02] VERIFIED STEP 1<BR>AUDIT CWDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378749Floorbeam · corrodedDOT#62 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AT STA 947 LBL 24 WL 208<[01] REMOVED CORROSION FROM AFT CABIN WET AREA FLOOR BEAM AT STA 947 LBL 24; VERIFIED ALLOWABLE DAMAGE = 0.071 IN. REMAINING THICKNESS = 0.109 IN. LOSS 0.062' FOUND OUT OF LIMITS; PERDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378750Floorbeam · corrodedDOT#63 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AT STA 947 LBL 35 WL 208<[01] FAULT RESOLVED ON OTHER FAULT. SEE FAULT TTG8Q00XP3L9 WHERE REPAIR WAS COMPLETED PER SRM 53-70-51-2R-5;[02] VERIFIED STEP 1<BR>AUDIT CWDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378746Floorbeam · corrodedDOT#59 A-043 AFT CABIN WET AREA FLOOR SUPPORT ('T' BEAM) CORRODED AT STA 947+4' RBL 19 WL 208<[01] REMOVED CORROSION AFT CABIN WET AREA FLOOR SUPPORT ('T' BEAM) CORRODED AT STA 947+4' RBL 19 ; VERIFIED ALLOWABLE MDAMAGE : .080'; LOSS .042'; REMAINING .038';FOUDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378747Support Beam · corrodedDOT#60 A-043 AFT CABIN WET AREA LAV FITTING SUPPORT BEAM CORRODED AT STA 947+4' RBL 25 WL 208<[01] REMOVED CORROSION AT AFT CABIN WET AREA LAV FITTING SUPPORT BEAM CORRODED AT STA 947+4' RBL 25 WL 208 VERIFIED ALLOWABLE DAMAGE; FOUIND IT OUT OF LIMITS; ORIG T Dec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage, Equipment Attach FittingsSDR SWAA2025012378748Floorbeam · corrodedDOT#61 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AROUND DOMENUT HOLE AT STA 986 RBL 44 WL 208<[01] REMOVED DOMENUT ON STA 986 RBL 44 WL 208 I.A.W. SRM 51-40-02-0G-0<BR>REMOVED CORROSION ON AFT CABIN WET AREA FLOOR BEAM CORRODED AROUND DOMENUT HOLE AT STA 98Dec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378757Floorbeam · corrodedDOT#70 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AT DOME NUT HOLE STA 986 LBL 44 WL 208<[01] 04 - REPAIRED PER [SRM 53-70-51-2R-6-B00676 (REPAIR 6 - SECTION 47 - SMALL CORROSION DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT STA 986.5 - PERMANENT)];[02] VERDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378751Floorbeam · corrodedDOT#64 A-043 AFT CABIN WET AREA FLOOR SUPPORT (T BEAM) CORRODED AT NUTPLATE HOLE STA 947+4' LBL 19 WL 208<[01] REMOVED CORROSION ON AFT CABIN WET AREA FLOOR SUPPORT (T BEAM) AT NUTPLATE HOLE STA 947+4'; FOND TO BE OUT OF LIMITS ORIGINAAL T .080'; LOSS .038'; RDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378753Floorbeam · corrodedDOT#66 A-043 AFT CABIN WET AREA FLOOR BEAM CORRODED AT NUTPLATE HOLES 4EA STA 947+4' LBL 29 TO LBL 46 WL 208<[01] REMOVED CORROSION ON AFT CABIN WET AREA FLOOR BEAM CORRODED AT NUTPLATE HOLES 4EA STA 947+4' LBL 29 TO LBL 46 VERIFIED ALLOWABLE DAMAGE ON FLOOR BDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378755Floorbeam · corrodedDOT#68 A-043 AFT CABIN WET AREA FLOOR SUPPORT CORRODED BETWEEN AFT LAV MOUNT AND 947 'T' CAP AT STA 947 LBL 49 WL 208<[01] REMOVED DAMAGE AT AFT CABIN WET AREA FLOOR SUPPORT CORRODED BETWEEN AFT LAV MOUNT AND 947 'T' CAP AT STA 947 LBL 49; FOUND OUT OF LIMITS Dec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012378758Floor Support · corrodedDOT#71 A-043 AFT CABIN WET AREA FLOOR 'Z' SUPPORT CORRODED AT NUT PLATE HOLE STA 986+6' LBL 44 WL 208<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012378759Web · corrodedDOT#72 A-043 AFT CABIN WET AREA FLOOR WEB CORRODED AT STA 986+4' LBL 33 WL 208<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CWDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012278754Mount · corrodedDOT#67 A-043 AFT CABIN WET AREA FLOOR LAV MOUNT SUPPORT CORRODED AT STA 947+4' LBL 48 LBL WL 208<[01] DAMAGE PART FOUND OUT OF LIMITS DUE MATERIAL LOSS IS 100 % REPLACED PART ; NEW P/N (147A5660-21); LOCATED; DRILLED; INSTALLED AND APPLIED CIC. IAW SRM 51-40-0Dec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage, Equipment Attach FittingsSDR SWAA2025012278752Support Beam · corrodedDOT#65 A-043 AFT CABIN WET AREA FLOOR LAV MOUNT SUPPORT BEAM CORRODED AT NUTPLATE HOLE STA 947+4' LBL 24 WL 208<[01] REMOVED CORROSION ON AFT CABIN WET AREA FLOOR LAV MOUNT SUPPORT BEAM CORRODED AT NUTPLATE HOLE STA 947+4' LBL 24 ; EVALUATED ALLOWABLE DAMAGE FDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2025012278243Mechanism · loose154-46 FORWARD GALLEY DOOR INNER HANDLE AND MECHANISM LOOSE<[01] INSTALLED HANDLE MECHANISM IAW AMM 52-41-11-400-801 STEP: 3.F(5)(I;J & K);[02] VERIFIED STEP 1<BR>AUDIT CWDec 17, 2024 · N8518R · Boeing 7378H4 · Service DoorsSDR SWAA2025012178563Crease Beam · corrodedDOT#56 A-043 AFT CABIN WET AREA RH CREASE BEAM CORRODED AT STA 927+17' TO 967+17' RBL 54 WL 208<[01] REMOVED CORROSION ON AFT CABIN WET AREA RH CREASE BEAMAT STA 927+17' TO 967+17' RBL 54 WL 208 I.A.W. SRM 51-10-02-0G-<BR>EVALUATED AREA WITH ORIGINAL THICKNESSDec 17, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2025012278210Intercostal · corrodedDOT#44 A-043 AFT CARGO COMPARTMENT RH INTERCOSTAL UNDER 'Z' ANGLE CORRODED AROUND NUTPLATE HOLES STA 747 TO 767 LBL 24 WL 156<[01] REMOVED CORROSION AND EVALUATED DAMGE ORIG 'T'.032 REMAINING .025 LOSS .007 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 REMOVED ANDDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012278219Angle · corrodedDOT#54 A-043 AFT CARGO COMPARTMENT AFT BKHD LOWER STAINTION ANGLE CORRODED STA 947 RBL 20 WL 156<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[02] COMPLETE<BR>AUDIT C/WDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178198Web · corrodedDOT#23 A-043 FWD CARGO COMPARTMENT SILL WEB CORRODED STA 440 TO 480+10' RBL 26 WL 156<[01] LIMITS VERIFIED; ORIGINAL THICKNESS .045'; REMAINING THICKNESS .030'; MATERIAL LOSS OF .015'; LOSS OF UP TO .004' ALLOWED-OUT OF LIMITS IAW SRM 53-30-15-1A-1LOCATED & DRDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178200Angle · corrodedDOT#26 A-043 FWD CARGO COMPARTMENT LH 'Z' ANGLE CORRODED STA 500 TO 500I LBL 24 WL 156<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED VERIFIED LIMITS; ORIGINAL THICKNESS .040'; REMAINING THICKNESS .033'; MATERIAL LOSSDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178202Web · corrodedDOT#34 A-043 AFT CARGO COMPARTMENT SILL WEB CORRODED AT STA 787+7' TO 847 RBL 24 WL 156<[01] REMOVED SILL WEB IAW SRM 51-40-02 VERIFIED NEW PART WITH PN 146A8123U25ATSMRO A TAG WN49364 IAW DRAWING 146A8340; REV: A STARTED DRILLING HOLES IAW SRM 51-40-05 FINISHDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178214Strap · corrodedDOT#46 A-043 AFT CARGO COMPARTMENT THRESHOLD STRAP BOTTOM SIDE NUTPLATE STRAP CORRODED AT STA 787+3' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8128 REV: B.;[02] COMPLETE<BR>AUDIT C/WDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178215Strap · corrodedDOT#47 A-043 AFT CARGO COMPARTMENT THRESHOLD STRAP BOTTOM SIDE NUTPLATE STRAP CORRODED AT STA 794.3' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8128 REV: -;[02] REFER TO FAULT TTG8Q00XNBFR WHERE E.A. 25-153-0082 WAS ADDED AS A SUBTASK;[03] COMDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178194Floor Panel · corrodedDOT L7-014: FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] VERIFIED CORROSION AROUND SEVERAL FASTENER HOLES IAW SRM 53-00-53-1A-1. VERIFIED MATERIAL IAW SRM 53-60-53-01-1. 2024-T3 .071. A TAG A274684. CONTINUED FLOOR PANEL 120CF FABRICATION IDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025012178199Shield · corrodedDOT#23 A-043 FWD CARGO COMPARTMENT AFT SHEILD CORRODED STA 500+6' TO 500+18' RBL 24 WL 156 CORRECTION: DOT 24<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 AND VERIFIED WITH 10X MAGNIFIER GLASS; <BR>LIMITS VERIFIED; ORIGINAL THICKNESS .032'. REMAINING THICKNESSDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178205Angle · corrodedDOT#25 A-043 FWD CARGO COMPARTMENT RH 'Z' ANGLE CORRODED STA 500A TO 500I RBL 24 WL 156<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED VERIFIED LIMITS; ORIGINAL THICKNESS .040'; REMAING THICKNESS .028'; MATERIAL LOSS Dec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178208Angle · corrodedDOT#40 A-043 AFT CARGO COMPARTMENT LH 'Z' ANGLE CORRODED STA 727D+10 TO 827 LBL 24 WL 156<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[02] C/W<BR>AUDIT C/Dec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178209Tee Angle · corrodedDOT#42 A-043 AFT CARGO COMPARTMENT FLOORBOARD 'T' ANGLE DIVIDER CORRODED AROUND NUTPLATE HOLESCTOP AND BOTTOM STA 767+5' RBL/LBL 24 WL 156<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] VERIFIED TASK COMPDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025012178212Shield · corrodedDOT#43 A-043 AFT CARGO COMPARTMENT FWD SHIELD CORRODED AROUND NUTPLATE HOLES TOP AND BOTTOM STA 767 TO 787 RBL 24 WL 156<[01] REMOVED CORROSION AND EVALUATED DAMAGE IAW SRM .050 ORIG 'T' .035 REMAINING .015 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVEDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178213Strap · corrodedDOT#45 A-043 AFT CARGO COMPARTMENT TOP STRAP AT THRESHOLD CORRODED AT NUTPLATE HOLE STA 787+8' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8120 REV: -;[02] C/W<BR>AUDIT C/WDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025012178216Floorbeam · corrodedDOT#48 A-043 AFT CARGO COMPARTMENT FLOOR BEAM CORRODED AROUND NUTPLATE HOLES TOP AND BOTTOM AT STA 794.3' RBL 15 WL 156<[01] REMOVED CORROSION AND EVALUATED DAMGE ORIG. 'T' .063 REMAINING .044 LOSS .019 FOUND OUT LIMITS SRM 53-00-53-1A-2 ACCOMPLISHED REPAIR ARDec 16, 2024 · N8518R · Boeing 7378H4 · Fuselage Main, Floor Beam
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