N8679A

Service difficulty reports · 109

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 = 'N8679A' 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 SWAA2024021547235Sidewall Support · corrodedFWD CARGO FOUND DAMAGE ON RH SIDEWALL TO SUPPORT SECTION 2 FW OF DOOR CUT OUT BS 420-440; WL 150; RBL 20.<[01] REMOVED AND REPLACED NEW FCB FWD SHIELD IAW SRM 51-40-02 AND BOEING DWG 143A0080;[02] VERIFIED CORRECTIVE ACTION 1Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021546796Floor Panel · pulledAFT FLOOR PANEL 242D UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242D IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-46 ITEM 180.;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024021546799Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024021546800Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] FWD FLOOR PANEL 222AF WITH UPPER SKIN HAS AN AREA OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024021546802Floor Panel · debondedFWD FLOOR PANEL 222BF UPPER SKIN IS DISBONDED APPROX 11' FROM O/B EDGE AND 7' FROM FWD EDGE. (MARKED)<[01] FLOOR PANEL 222BF WITH DISBONDED UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] REPAIR COMPLETED.;[03] VERIFIED CORRECTIVE ACTION #1Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024021547064Shield · corrodedFOUND CORROSION ON AFT CARGO FWD SHIELD NUTPLATES BS 767 TO BS 787; RBL 21; WL 150<[01] REMOVED AND INSTALLED NEW AFT CARGO FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081; ID: 0049; REV: A;[02] VERIFIED STEP 3 COMPLETE; ALL STEPS MEASUREMENT TABLE AND CARD Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547061Sidewall Support · corrodedAFT CARGO RH SUPPORT BEAM SECTION # 2 HAS MULTIPLE CORROSION AROUND NUTPLATES BS 727I TO 767<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727G+10' TO BS 767;RBL 21 AT ACB IAW SRM 51-40-02 AND DWG 146A7500.;[02] CUSTOMER CARD COMPLETE AND VERIJan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547062Support Beam · corrodedAFT CARGO LH SUPPORT BEAM SECTION 1 FROM BS 727D TO 727F HAS MULTIPLE CORROSION AROUND NUTPLATE HOLES; WL 150.6; LBL 21.0 CORRECTION- FAULT DETAILS AFT CARGO LH FLOOR TO SIDEWALL SUPPORT SECTION 1 FROM BS 727D TO 727F HAS MULTIPLE CORROSION AROUND NUTPLATE HOLJan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547068Shield · corrodedFOUND CORROSION AROUND NUTPLATES ON AFT SHIELD BS 847 TO BS 867; WL; 150; RBL 21<[01] FIXED P/N IN MEASURMENT FIELS;[02] REMOVED AND INSTALLED NEW AFT CARGO AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081; ID: 0049; REV: A;[03] VERIFIED STEP 4 COMPLETE; ALL Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547071Support Beam · corrodedAFT CARGO- FOUND CORROSION AROUND NUTPLATES ON FLOOR TO SIDEWALL SUPPORT BEAM 867 TO 887 ; LBL 21; WL 128 CORRECTION-AFT CARGO; FOUND CORROSION AROUND NUTPLATES ON FLOOR TO SIDEWALL SUPPORT BEAM BS 867 TO 887 WL 150 RBL 21.<[01] VERIFIED STEP 1;3 COMPLETE.;[02Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547240Sidewall Support · corrodedRH FWD CARGO SEC 3 FLOOR TO SIDEWALL SUPPORT CORRODED AROUND NUTPLATE HOLES BS 500C TO 500I ; WL 150; RBL 20.<[01] REMOVED CORROSION AT R/H FLOOR TO SIDE WALL SUPPORT; AREA FOUND OUT IF LIMITS IAW SRM 53-00-53-1A-2. FLOOR TO SIDE WALL SUPPORT GOING TO REPLACE Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547241Sidewall Support · corrodedLH FWD CARGO SEC 1 AFT END FLOOR TO SIDEWALL SUPPORT CORRODED AROUND NUTPLATE HOLES BS 500A TO 500B; WL 150; RBL 20<[01] REMOVED CORROSION AT R/H FLOOR TO SIDE WALL SUPPORT; AREA FOUND OUT IF LIMITS IAW SRM 53-00-53-1A-2. FLOOR TO SIDE WALL SUPPORT GOING TO REJan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021547242Cargo Track · corrodedCOROSSION FOUND ON FWD CARGO BS 500I FROM LBL 20 TO RBL 20; WL 150<[01] REPLACED LOWER RAIL AT FCB ;BS 500I FROM LBL 20 TO RBL 20; WL 150 IAW SRM 51-40-02 AND DWG:143A9481.;[02] VERIFIED CORRECTIVE ACTION 1Jan 31, 2024 · N8679A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024021946775Angle · crackedAED LOWER PAN 834DZ FWD ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED AED LOWER PAN 834DZ FWD ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 411A2119 REV: A;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLEJan 30, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021546789Sidewall Support · corrodedCORROSION FOUND AROUND NUTPLATES ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BEAM BS 767-787<[01] GENERAL FAULT RESOLVED ON OTHER FAULT (FAULT WAS RESOLVED ON ANOTHER FAULT) #TTG8Q00R9J93;[02] VERIFIEDJan 30, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021546788Web · corrodedCORROSION AFT CARGO BAY SUBTHRESHOLD: BS794+2 TO 3; RBL27; BS794+6; RBL26; BS794+8 TO 10; RBL26; BS794+11; RBL26; BS807+3 TO 4; RBL26; BS807+12; BS827+3; RBL26; BS827+5 TO 6; BS827+8; RBL26; WL156 ALL<[01] SRM 53-60-15-1A-1 IS APPLICABLE FOR THIS ALLOWABLE DAMJan 30, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021945782Bracket · looseR/H EMERGENCY EXIT SURROUND HAS SEVERAL BRACKETS LOOSE/DISBONDED<[01] RE-BONDED BRACKETS ON R/H EMERGENCY EXIT SURROUND PER BOEING DWG 411A2810 AND BAC 5010 TYPE 89. CURE TIME 24 HOURS; BONDED AT 1817UTC 02/02/24;[02] VERIFIED.Jan 28, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021945783Bracket · looseR/H AFT EMERGENCY EXIT SURROUND HAS SEVERAL BRACKETS LOOSE/DISBONDED<[01] RE-BONDED BRACKETS ON R/H AFT EMERGENCY EXIT SURROUND PER BOEING DWG 411A2810 AND BAC 5010 TYPE 89. CURE TIME 24 HOURS; BONDED AT 1817UTC 02/02/24;[02] VERIFIED.Jan 28, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021945786Bracket · looseL/H AFT EMERGENCY EXIT SURROUND HAS SEVERAL BRACKETS LOOSE<[01] RE-BONDED BRACKETS ON L/H AFT EMERGENCY EXIT SURROUND PER BOEING DWG 411A2810 AND BAC 5010 TYPE 89;[02] CURE TIME 24 HR. BONDED AT 1814 UTC 02/02/24;[03] UPDATED SUB TASK;[04] VERIFIED.Jan 28, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024021945781Bracket · debondedL/H FWD EMERGENCY EXIT SURROUND HAS SEVERAL BRACKETS DISBONDED<[01] RE-BONDED BRACKETS ON L/H FWD EMERGENCY EXIT SURROUND PER BOEING DWG 411A2810 AND BAC 5010 TYPE 89. CURE TIME 24 HOURS; BONDED AT 1817UTC 02/02/24;[02] VERIFIED.Jan 28, 2024 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023122835807Cradle · inoperativeEMERGENCY FLASHLIGHT IN AFT GALLEY AREA INOP<[01] REMOVED AND REPLACED AFT L/H INBOARD ATTENDANT SEAT FLASH LIGHT MOUNTING BRACKET AND BATTERY PER AMM 25-64-00. OPS CHECK GOOD.Dec 28, 2023 · N8679A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2023122835809Battery · inoperativeEMERGENCY FLASHLIGHT IN AFT GALLEY AREA INOP<[01] REMOVED AND REPLACED AFT L/H INBOARD ATTENDANT SEAT FLASH LIGHT MOUNTING BRACKET AND BATTERY PER AMM 25-64-00. OPS CHECK GOOD.Dec 28, 2023 · N8679A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2023101108822Bracket · brokenFWD R/H (SERVICE DOOR) EMERGENCY SLIDE COMPARTMENT ASSY QUICK RELEASE BRACKET BROKEN<[01] REMOVED AND REPLACED R1 DOOR EMERGENCY SLIDE COVER BRACKET HINGE PER SRM 51-40-02Oct 7, 2023 · N8679A · Boeing 7378H4 · Escape SlideSDR SWAA2023090595992Seal · crackedRH HORIZONTAL UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] R&R RH HORIZONTAL UPPER FRONT SPAR SLIDING SEAL. IAW AMM 53-31-31Sep 1, 2023 · N8679A · Boeing 7378H4 · Horizontal Stabilizer StructureSDR SWAA2023090195995Battery Pack · failedEMX BATT PACK M01670 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK AT POSITION M01670 PER AMM 33-51-06Sep 1, 2023 · N8679A · Boeing 7378H4 · Emergency LightingSDR SWAA2023081689171Battery Pack · inoperativeEMER. LIGHTS ON M2816; M1675 AND M1671 INOP<[01] REMOVED BATTERY PACKS FORM EMER POWER SUPPLY # M2816; M1675 AND M1671PER AMM 33-51-06;[02] REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT POWER SUPPLY M2816; M1675 AND M1671. OPS CHECKS NORMALLY AT THIS TIME.Aug 14, 2023 · N8679A · Boeing 7378H4 · Emergency LightingSDR SWAA2023051147620Sign · missingEXIT SIGN MISSING OVER RIGHT AFT ENTRY DOOR (R2)<[01] INSTALLED NEW COVER FOR EXIT SIGN ABOVE RIGHT AFT SERVICE DOOR PER AMM 33-51-01.May 10, 2023 · N8679A · Boeing 7378H4 · Emergency LightingSDR SWAA2022071126835Megaphone · faultyCREW REPORTED MEGAPHONE INTERMITTENT / [01] R&RD MEGAPHONE & OPS CHK GOOD PER AMM 25-64-00Jul 7, 2022 · N8679A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022031681828Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK ASSEMBLY M1676 FAILS TO CHARGE / [01] REPLACED AND TESTED EMERGENCY LIGHT BATTERY PACK M1676 STA 500C+7 RBL 67 PER AMM 33-51-06-960-805. TEST PASSED.;[02] VERIFIED STEP 1; JOB COMPLETE; AUDIT C/WMar 9, 2022 · N8679A · Boeing 7378H4 · Emergency LightingSDR SWAA2022031681827Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK ASSEMBLY M1672 FAILS TO CHARGE / [01] REPLACED AND TESTED EMERGENCY LIGHT BATTERY PACK M1672 AFT RIGHT CEILING PER AMM 33-51-06-960-805. TEST PASSED.;[02] VERIFIED STEP 1 JOB COMPLETE; AUDIT C/WMar 9, 2022 · N8679A · Boeing 7378H4 · Emergency LightingSDR SWAA2022031677292Stiffener · crackedFWD CARGO DOOR STIFFENER FOUND CRACKED P/N 143A6124-1 / [01] REMOVED STIFFENER IAW B737 SRM 51-40-02-0G-0;[02] VERIFIED ROBED CARGO DOOR STIFFENER AS 143A6124-1 ROBED FROM A/C 8680 FWD CARGO DOOR ON N/R TTG8Q00B4L5E PER CUSTOMER REQUEST;[03] VERIFIED STEP 2 ANFeb 24, 2022 · N8679A · Boeing 7378H4 · Cargo/Baggage DoorsSDR SWAA2022031676260Shield · corrodedDOT A-24-10 AFT PIT FORWARD RH SHIELD CORRODED ON UPPER SURFACE BETWEEN STATIONS 767-787. / [01] REMOVED CORROSION FROM AFT CARGO RH FWD OF DOOR FLOOR SHIELD AND VERIFIED WITH 10X MAG GLASS IAW SRM 53-60-15-1A-1 STEP 2A;[02] VERIFIED MATERIAL LOSS: ORIGINAL T=Feb 21, 2022 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022031676261Angle · corrodedDOT A-24-20 AFT PIT. RH 'Z-ANGLE' CORRODED ON UPPER SURFACE BETWEEN STATIONS 727H-767. / [01] REMOVED CORROSION DAMAGE FROM UPPER SURFACE OF AFT CARGO RH ZEE ANGLE STA 727H TO 767 AND VERIFIED WITH 10X MAG GLASS IAW SRM 53-00-53-1A-2 STEP 2D.;[02] VERIFIED MATFeb 21, 2022 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022031676257Angle · corrodedDOT A-24-30 AFT PIT. LH 'Z-ANGLE' CORRODED ON UPPER SURFACE BETWEEN STATIONS 727F-807. / FOUND Z-ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL# 36306 DUE 14JUN22;[05] CHANGED TO OUT OF LIMITS & UPGRADED TO MAJOR REPAIR; LEVEL 2.;[06] VERIFIED STEP 5Feb 21, 2022 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022031675171Bracket · crackedAFT CARGO COMPARTMENT BULKHEAD LOWER SUPPORT ANGLE BRACKET AT STA 867 LBL 12 CRACKED. DOT# A193-19 / [01] REMOVED CRACKED BULKHEAD LOWER SUPPORT ANGLE AND REPLACED WITH NEW BULKHEAD LOWER SUPPORT ANGLE; PN 149A8109-114 ATAG A108783; IAW SRM 51-40-02-0G-0 AND BFeb 18, 2022 · N8679A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022031673890None · crackedEXTERNAL POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT CRACKED / [01] PREFORMED CUTOUT AT POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT IAW SRM 53-10-15-2R-4;[02] VERIFIED STEP 1.;[03] VERIFIED NEW MATERIAL AS P/N 2024-T3-050/ 2024-T3-040 ATAG# A12631/A5Feb 17, 2022 · N8679A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022031673880Splice Plate · corrodedDOT#44-186 FWD CARGO COMPARTMENT FWD SPLICE PLATE CORRODED / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. FWD CARGO BAY FLOOR SPLICE PLATE IS OUT OF LIMITS.;[02] VERIFIED AND REPLACED ON SHELF: NEW FWD CARGO FLOOR SPLICE PLATE MPN: 453A1611-25 ATAG: A115564 IFeb 17, 2022 · N8679A · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022031673883Angle · corrodedDOT#40-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 500C+6' TO 500I LBL24 WL 156 / [01] REMOVED CORROSION FROM STA 500C+6 -500G IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .008 MATERIAL REMOVED OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL NO. 36647 Feb 17, 2022 · N8679A · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022031673875Angle · corrodedDOT#35-186 FWD CARGO COMPARTMENT Z ANGLE CORRODED STA 460+6' TO 500C LBL 24 WL 156 / [01] REMOVED CORROSION FROM STA 460+ 6 - STA 500 B IAW SRM 51-10-02 10X MAGNIFY ORIGINAL THICKNESS .040 .003 MATERIAL REMOVED .037 MATERIAL REMAINS FOUND TO BE IN LIMITS IAW SFeb 17, 2022 · N8679A · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022031673157Floor Panel · peelingCABIN FLOOR PANEL 241 AF HAS FIBERS PEELING UPPER SURFACE CENTER A225-006 / [01] EVALUATED UPPER SURFACE DAMAGED FIBERS ON FLOORBOARD PANEL (241-AF) AND FOUND DAMAGE TO BE IN REPAIRABLE LIMITS I/A/W B737-800 SRM 53-00-50-2R-1 (3) A-N <BR>(REV 74);[02] CLEANED Feb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673153Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120DF HAS AREAS OF CORROSION ALONG EDGES OF PANEL. DOT#A193-14 / [01] CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW <BR>SRM 553-00-53-1A-1 5. A.(1). (B) FIG. 102;[02] VERIFIED STEP 1 IS COMPLETE;[03] UPDATED P/N;[04] SRM REFEFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673154Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120AF HAS AREA OF CORROSION ALONG EDGE OF PANEL. DOT#A193-15 / [01] EVALUATE DAMAGE FROM FLOOR PNL # 120AF ; FOUND TO BE OUT OF LIMITS DUE CORROSION LENGTH IS MORE THAN 20'. IAW SRM 53-00-53-1A-1. FIG 102.;[02] IDENTIFIED MATEFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673344Floor Panel · corroded(DOT 67-21) AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS AREAS OF CORROSION ALONG TOP EDGES. / [01] MEASURED TOTAL ACCUMULATED CORROSION DAMAGE TO BE = 83'. LIMIT = 20'. FLOOR PANEL 140AF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102.;[02] VERIFIED NEW FLOOR PFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673343Floor Panel · corroded(DOT 67-20) AFT CARGO COMPARTMENT FLOOR PANEL 140EF HAS AREAS OF CORROSION ALONG TOP EDGES. / [01] EVALUATED CORRASION DAMAGE FOUND TO BE OUT OF LIMITS IAW <BR>SRM 53-00-53-1A-1 5.A.(1)(B) FIG 102;[02] VERIFIED STEP COMPLETE;[03] VERIFIED MATERIAL IAW<BR>AMM 2Feb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673342Floor Panel · corroded(DOT 67-17) AFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS AREAS OF CORROSION ALONG TOP EDGES. / [01] REMOVED DAMAGE FROM AFT CARGO FLOOR PANEL 140BF. ORIGINAL T= .071' LOSS OF .006' REMAINING T= .065' TOTAL ACCUMULATED DAMAGE EXCEEDS 20' FOUND TO BE OUT OF LIMITFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673341Floor Panel · corroded(DOT 67-19) AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS AREAS OF CORROSION ALONG TOP EDGES. / [01] EVALUATED DAMAGE ON PANEL 140CF. FOUND CORROSION TO EXCEED 20' IN LENGTH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. MEASRURED WITH STEEL RULE. <BRFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673340Floor Panel · corroded(DOT 67-18) AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS AREAS OF CORROSION ALONG TOP EDGES. / [01] EVALUATED DAMAGE TO FLOOR PANEL 140DF; FOUND DAMAGE EXCEEDS 20' IN LENGTH; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102; MEASURED WITH STEEL RULE. WORFeb 16, 2022 · N8679A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022031673517Panel · corrodedA-061 DOT 015 R/H WING FUEL QTY PNL UNDER PANEL 621GB CORRODED AROUND GAUGES AND SCREWS / [01] REMOVED CORROSION FROM R/H WING FUEL QTY PANEL IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED WITH 10X MAGNIFICATION.;[02] VERIFIED STEP 1.;[03] ACCOMPLISHED UT IAW B737Feb 16, 2022 · N8679A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022031673339Angle · crackedRIGHT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED. / [01] REMOVED DAMAGED SECTION OF ANGLE RBL 6-17 IAW SRM 57-10-10-2R-5 VERIFIED -1 REPLACFeb 16, 2022 · N8679A · Boeing 7378H4 · Wing, Center BoxSDR SWAA2022031673338Angle · crackedLEFT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 LBL 10 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED. / [01] VERIFIED -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP W/O 43216-5100-0001 AND -2 SPFeb 16, 2022 · N8679A · Boeing 7378H4 · Wing, Center Box
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