N8685B

Service difficulty reports · 84

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 = 'N8685B' 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 SWAA2026071532882Megaphone · looseCREW REPORTS AFT MEGAPHONE NEEDS SECURED. RESECURED AFT MEGAPHONE IAW AMM 25-64-00.Jul 12, 2026 · N8685B · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026020563410Battery Pack · inoperativeFWD RIGHT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY BACK AND PERFORMED A GOOD OPS CHECK IAW AMM 33-51-06-960-805.Jan 21, 2026 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2025110330315Sign · unsecureAFT GALLEY CEILING EXIT SIGN NEEDS TO BE SECURED. SECURED SCREWS IAW AMM 33-51-01-201-NG.Oct 31, 2025 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2025061776810Bulb · inoperativeIN THE CABIN ABOVE THE FWD ENTRY DOOR, THE EXIT LIGHT HAS ONE INOP BULB. REMOVED AND REPLACED LAMP OPS CHECK OK PER AMM 33-25-00.Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2025061176811Battery Pack · inoperativeIN THE PASSENGER CABIN; THE EMERGENCY EXIT LIGHT FWD OF THE LEFT HAND FWD MID EXIT DOOR IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 PER AMM 33-51-06. ALL ASSOCIATED EMERGENCY LIGHTS OPS CHECK GOOD PER AMM 33-51-06.Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2025061176809Battery Pack · inoperativeIN THE PASSENGER CABIN; THE EMERGENCY EXIT LIGHT FWD OF THE RIGHT HAND FWD MID EXIT DOOR IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 PER AMM 33-51-06. ALL ASSOCIATED EMERGENCY LIGHTS OPS CHECK GOOD PER AMM 33-51-06.Jun 1, 2025 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2025061676296Seal · crackedLEFT HORIZONTAL UPPER FORWARD SLIDER SEAL IS CRACKED; TORN ON FORWARD TRACK. REMOVED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31. REPLACED LH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.May 29, 2025 · N8685B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025061772760Angle · crackedANGLE CRACKED I/B OF LH DEFECTION RIB (MPN 115A2156-7). REMOVED ANGLE PER SRM 51-40-02. LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02.May 20, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025061772761Angle · crackedANGLE ASSY CRACKED I/B OF LH DEFECTION RIB (MPN 115A2156-17). REMOVED ANGLE PER SRM 51-40-02. LOCATED AND DRILLED NEW FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02. INSPECTED PER SRM 51-40-02-0G-0-B00069 (GENEMay 20, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025061171464Seal · crackedRH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] INFO: PARTS ORDERED 5/15/25. AMM REFERENCE IS 53-31-31.;[02] INSTALLED ATTACH FITTING ON SEAL PER SRM 51-40-02.;[03] VERIFIED INSTALLED ATTACH FITTING ON SEAL PER SRM 51-40-02.;[04] INSTALLED RH HORMay 15, 2025 · N8685B · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025061170066Seat Track · corrodedCAPT'S FWD O/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. REMOVED CAPT. FWD. OTBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02. REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NGMay 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025061170065Seat Track · corrodedCAPT'S FWD I/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. REMOVED CAPT. FWD INBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02.May 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025061170064Seat Track · corrodedF.O.'S FWD O/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. MRKD<[01] REMOVED FO'S FWD. OTBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG (FLIGHT COMPARTMENT SEAT TRACKS - INSTALLATION AND ALMay 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025061170063Seat Track · corrodedF.O.'S FWD I/B SEAT TRACK HAS POSSIBLE CORROSION AT FWD MOUNT BOLT AREA. MRKD<[01] REMOVED FO'S FWD. INBD. SEAT TRACK IN REFERENCE TO SRM 51-40-02;[02] 01 - REMOVED AND REPLACED PER [AMM 25-11-11-400-801-NG (FLIGHT COMPARTMENT SEAT TRACKS - INSTALLATION AND ALMay 13, 2025 · N8685B · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025061170778Attach Angle · crackedCRACKS FOUND AT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE RBL 9 & 32.<[01] MATCH DRILLED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000. NEED OK TO INSTALL ANGLE.;[02] REMOVED 663 VAPOR BARRIER ANGLE PER SRM 51-40-02.;[03] C/W RII INSPECMay 13, 2025 · N8685B · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025061769935Bracket · crackedBRACKET CRACKED I/B OF RH DEFECTION RIB. REMOVED CRACKED SUPPORT ANGLE BRACKET PER SRM 51-40-02. THE CRACKED SUPPORT ANGLE BRACKET HAS BEEN VERIFIED AS BEING REMOVED AS STATED IN ITEM #1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SUPPORT ANGLE BRACKET PER SMay 12, 2025 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2025061669934Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP HAS DELAM ON UPPER INBOARD AFT SURFACE.<[01] REMOVED R/H WING O/B AFT FLAP PER AMM 27-51-22.;[02] OK TO INSTALL RIGHT WING OTBD FLAP.;[03] INSTALLED SERVICEABLE R/H O/B AFT FLAP PER AMM 27-51-22.;[04] VERIFIED RII WORK ACCOMPLISHEDMay 12, 2025 · N8685B · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2025061168741Attach Angle · crackedCRACK FOUND AT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 9<[01] FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5. NEED OK TO INSTALL PARTS.;[02] REMOVED R/H A/C DISTRIBUTION DUCTING F.O.M.;[03] C/W RII INSPECTION OF C/A #1;[04] INSTALLED REPAIR PER SRM 5May 8, 2025 · N8685B · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025021294473Unknown · fumesFLIGHT ATTENDANTS REPORT PLASTIC BURNING FUMES AT ROWS 2-4. RAN SMOKE; FIRE OR FUMES QRH. FUMES EXTINGUISHED. RESTORED PWR TO ALL SWITCHES NO FUMES NOTED REMAINDER OF FLIGHT WAS NORMAL<[01] ACCOMPLISHED SMOKE/FUMES IN CABIN CONDITIONAL INSPECTION REF AMM 05-51Feb 8, 2025 · N8685B · Boeing 7378H4 · Air Distribution SystemSDR SWAA2024060597735Seat · lockedPASSENGER EMERGENCY EXIT SEAT 15C; 15B RECLINE NOT LOCKED OUT<[01] LOCKED OUT EMR EXIT SEATS 15C AND 15B RFE AMM 25-22-00Jun 3, 2024 · N8685B · Boeing 7378H4 · Passenger Compartment EquipmentSDR SWAA2024043077020Battery Pack · inoperativeCABIN EMERGENCY LIGHTS L/H FWD CABIN STA 500C BATTERY PACK INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[03] OPS CHECKED GOOD PER AMM 33-51-06.;[04] REMOVED ANDApr 19, 2024 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2024043077021Battery Pack · inoperativeFWD CABIN R/H OVERWING EMERGENCY LIGHTS AT STA 565 BATTERY PACK IS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06.;[02] OPS CHECK GOOD PER AMM 33-51-06.;[03] REMOVED AND REPLACED BATTERY CHARGER ASSY PER AMM 33-51-06. <BR>OPS CHECK GOOD PER AMM 3Apr 19, 2024 · N8685B · Boeing 7378H4 · Emergency LightingSDR SWAA2024050275843Bracket · corrodedR/H WING FUELING PANEL BRACKET FOR CENTER FUEL TANK HAS CORROSION.<[01] REPLACED P15 REFUELING PANEL PLATE PER SOPM 20-50-01 AND MM 28-41-61. P15 REFUELING PANEL OPS CHECKED GOOD PER MM 28-21-00-400-801;[02] VERIFIED INSTALLATION OF P15 REFUELING PANEL PLATE PApr 16, 2024 · N8685B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2024050277222Angle · corrodedREPLACE LH AFT CARGO SIDE PLATE FORM STA 727H +11 TO 800 DUE TO CORROSION<LOCATED; DRILLED AND COUNTERSUNKED NEW LH SIDE PLATE FROM STA 727H + 11 TO 800 PER SRM 51-40-05 ; 51-40-08 AND 53-00-53-2R-6;[03] CW INSP STEP #2;- REMOVED AND REPLACED PER [SRM 51-40-02Apr 15, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024043074100Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT CRACKED AT ATTACH FASTENER STA. 540 RBL 1.<[01] REMOVED BROKEN CABLIN FLOOR SUPPORT BRAKE ASSY AT STA. 540 RBL1;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME -Apr 12, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024043074101Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT CRACKED AT ATTACH FASTENER STA.540 LBL 1.<[01] REMOVED BROKEN CABLIN FLOOR SUPPORT BRAKE ASSY AT STA. 540 LBL 1.;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME Apr 12, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050273653Support Angle · corrodedWALL SUPPORT STA. 986.5 + 4 HAS CORROSION ON UPPER SURFACE I/B END<[01] CORROSION AT Z-ANGLE(WALL SUPPORT) AT APPROXIMATELY STA. 987+5' ; LBL 33' IS OUT OF LIMITS PER SRM 53-70-51-1A-1. PARENT THICKNESS IS .050'. REMAINING THICKNESS IS .000'. REMOVED ANGLE PERApr 11, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272575Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 767-787+2 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED) AFT CARGO SIDE PLATE CHANNEL AT LBL 21 STA 767-787+2 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON L/H SApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272576Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 767-787 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] 01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] REMOVED CORROSION ON Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272569Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 747-767 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO L/H SIDE PLATE CHANNEL PER SRM 51-10-02; FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272577Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 747-767 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 747-767 PER SRM 51-10-02. REMANNING THICKNESS .030; FOUND TO BE OUT OF LIApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272578Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 727J-747 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO L/H SIDE PLATE CHANNEL PER SRM 51-10-02; FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272579Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727J-747 HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727J-747 PER SRM 51-10-02. REMANNING THICKNESS .033; FOUND TO BE OUT OF Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272580Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727I-727J HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727I-727J PER SRM 51-10-02. REMANNING THICKNESS .033; FOUND TO BE OUT OApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272571Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT LBL 21; STA 727H-727I HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON L/H SIDE PLATE FROM STA 727I-727J LBL21 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 MATERIAL Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272586Channel · corrodedAFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727D-727E HAS VARIOUS AREAS OF SURFACE CORROSION VISIBLE. (MARKED)<[01] REMOVED SURFACE CORROSION ON AFT CARGO SIDE PLATE CHANNEL AT RBL 21; STA 727D-727E PER SRM 51-10-02. REMAINING THICKNESS .035'. FOUND TO BE OUT Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272596Web · corrodedFWD CARGO DOOR LOWER SILL THRESHOLD WEB HAS CORROSION.<[01] REMOVED CORROSION MATERIAL LOSS .005 AND FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS .040. PER SRM 53-00-53. REMOVED FORWARD CARGO THRESHOLD WEB FOR REPLACEMENT PER SRM 51-40-02.;[02] VERIFIED WEB Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050272964Floorbeam · corrodedSTA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND FLOOR PANEL ATTACH HOLE AT LBL 30.5.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS=.150?; REMAINING THICKNESS=.125?.;[02] BLENDApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024050272963Floorbeam · corrodedSTA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND NUTPLATE HOLE AT LBL 43.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF Apr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024050272966Fitting · corrodedAFT GALLEY LAV E O/B AND AFT TIE DOWN FITTING POSSIBLE CORROSION UNDER FITTING. (MARKED)<BLENDED CORROSION PER SRM 51-10-02. MAX MATERIAL REMOVED 0.075?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1;REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER FLANGE PApr 9, 2024 · N8685B · Boeing 7378H4 · Fuselage, Equipment Attach FittingsSDR SWAA2024043072965Skin · delaminatedL/H O/B AFT FLAP DELAMINATED LOWER I/B CORNER LOWER SURFACE<[01] REMOVED L/H O/B AFT FLAP IAW AMM 27-51-22;[02] OK TO INSTALL;[03] INSTALLED L/H OB AFT FLAP PER AMM 27-51-22 THROUGH STEP 3.(5)(G).;[04] C/W RII INSPECTION OF OUTBD FLAP INSTALL;[05] REMOVED AND Apr 9, 2024 · N8685B · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2024043072601Handle · looseAFT GALLEY SERVICE DOOR (R2) HANDLE CAM PLATE LOOSE<[01] SECURED CAM PLATE ATTACHING HARDWARE PER M/M REF 52-41-11;[02] SECURED CAM PLATE ATTACHING HARDWARE PER M/M REF 52-41-11Apr 9, 2024 · N8685B · Boeing 7378H4 · Galley DoorsSDR SWAA2024043071858Intercostal · crackedBETWEEN STATION 380 AND 400; THE INTERCOSTAL AT LBL 14 HAS EVIDENCE OF CRACKS AT BOTH THE FASTENER HOLES AND THE UPPER ANGLE INNER RADIUS.<[01] REMOVED AND REPLACED UPPER ANGLE PER SRM 51-40-02.;[02] RII C/W INSPECTION AS REQUIREDApr 8, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050271685Plate · corrodedFWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500 TO 500A RBL 24.<[01] BLENDED AREAS; REMOVED .030' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AND REPLACED SHIELD PER SRM 51-40-02.;[03] 02 Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050271668Plate · corrodedFWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500A TO 500D LBL 24.<[01] BLENDED AREAS; REMOVED .008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS; REMOVED .008' MATERIAL. FOUND TO BE OUTApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050271688Plate · corrodedFWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500D TO 500F LBL 24.<[01] THIS SECTION TO BE REPLACED FROM STA 500B + 10 TO 500I ON NR # TTG8Q00SLBEU;[02] BLENDED AREAS; REMOVED .009' MATERIAL FOUND TO BE OUT OF LIMITS PApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050271690Plate · corrodedFWD CARGO FLOOR STRUCTURE SIDE PLATE HAS LIGHT CORROSION AROUND FASTENER HOLES FROM STA 500F TO 500I LBL 24.<[01] BLENDED AREAS; REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED FROM STA 500B + 10 TO 500I ON Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050171842Floorbeam · corrodedAFT WET AREA- CORROSION ON FLOOR BEAM AT STA 947 +4; LBL +25. BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. BLENDING WAS DONE ON INTERCOSTAL WHICH IS OUT OF LIMITS. REMOVED DAMAGED INTERCOSTAL FROM STAApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024050171841Web · corrodedAFT WET AREA- CORROSION ON FLOOR PAN WEB AT STA 1006 +8; LBL +38. DRILLED UP NEW WEB PER SRM 51-40-02. BLENDED CORROSION ON FLOOR PAN WEB AT STA. 1006+8'; LBL 38' PER SRM 51-10-02. REMOVED .008' OF MATERIAL. REMAINING THICKNESS IS .032. DAMAGE REMOVAL OUT Apr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024050171840Web · corrodedAFT WET AREA- CORROSION ON FLOOR PAN WEB AT STA 1006 +3; LBL +38. DRILLED UP NEW WEB PER SRM 51-40-02.;[02] BLENDED CORROSION ON FLOOR PAN WEB AT STA. 1006+3'; LBL 38' IAW SRM 51-10-02. REMOVED .012' OF MATERIAL. REMAINING THICKNESS IS .028. DAMAGE REMOVAL OUApr 7, 2024 · N8685B · Boeing 7378H4 · Fuselage Miscellaneous Structure
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