N8656B

Service difficulty reports · 168

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 = 'N8656B' 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 SWAA2022082538743Attach Angle · corrodedCORROSION ON FSD THRESHOLD ATTACH ANGLE BS308-318 RBL 58 WL208 / [01] REMOVED COROSION ON FSD THRESHOLD ATTACH ANGEL AT BS 308 RBL 58 WL 208; 1''X1''X.015'' FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2.;[02] CERTIFY;[03] VERIFIED OUT OF LIMITS.;[04] REMOVEDAug 4, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082538748Web · corrodedCORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 440+8; BS 440+14; BS 460+2; BS 460+4; BS 460+9; BS 460+11; BS 460+18; BS 480+2; BS 480+4. / [01] REMOVED CORROSION FROM FCD THRESHOLD WEB AT BS 440+8 MEASURED 1.8'W X 1.8'L AND 0.004' DEEP; ORIGINAL THICKNESS OAug 4, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022082538749Shield · corrodedCORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 23 BS 500+18. / [01] UPDATED MEASUREMENTS;[02] FIXED MEASUREMENTS 7-12;[03] REMOVED DAMAGE IN A 0.5'X0.5'DEPTH 0.005. AT BS500+18 RBL23. SHIELD IS OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMIT. REPAIR BY REPLAAug 4, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082538754Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500D+15; BS 500D+20; BS 500E+2; BS 500E+7; BS 500E+11; BS 500E+20; BS 500F+2; BS 500F+7; BS 500F+2; BS 500F+7. / [01] REMOVED CORROSION FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS 500D+20 RBL 2Aug 4, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022091538093Stringer Clip · crackedREJECT STRINGER 10R CLIP AT B S 927 IS CRACKED / [01] UPDATED MEASUREMENT TABLE;[02] SRM DOES NOT HAVE REPAIR LIMITS FOR CRACKED STR CLIPS. OUT OF LIMITS AND TO BE REPLACED IAW SRM 51010-02-0G-0 STEP 9.;[03] REFERENCE IS SRM 51-10-02-0G-0 STEP 9;[04] CERTIFY;[Aug 3, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2022082437843Floor Panel · pulledCABIN FLOOR PANEL 232CF UPPER SKIN HAS PULLED STRANDS AT THE AFT O/B CORNER. (MARKED) / [01] IDENTIFIED PANEL 232CF IAW SRM 53-00-50-0I-1 TABLE 3 FIG 3.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>TO BE REPAIRED IAug 3, 2022 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022082437844Floor Panel · pulledFLOOR PANEL 232DF UPPER SKIN HAS PULLED STRANDS ALONG THE AFT EDGE. (MARKED) / [01] IDENTIFIED PANEL 232DF IAW SRM 53-00-50-0I-1 TABLE 3 FIG 3.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B OK TO POT EXPOSED CORE IAW SRM 5Aug 3, 2022 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2022082537833Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727F+6; BS 727F+16; BS 727G+8; BS 727G+10; BS 727G+19; BS 727H; BS 727H+6. / [01] REMOVED CORROSION FROM ACB L/H FLOOR TO SIDEWALL SUPPORT AT BS 727H LBL 21 MEASURED 2'W X 1'L AND 100% MATERIAL Aug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082537831Rail · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 13 BS 767+5. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;;[15] INSTALLED NEW REINFORCING CHANNEL IAW SRM 53-00-53-2R-3 REPAIR 3;[16] EDITED MEASUREMENTS;[17] VERIFIED CORRECTIVE ACTION #15; 16 AND MEASUREMENT TABLEAug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082537830Channel · corrodedCORROSION ON AFT CARGO BAY RAIL AT RBL 8 BS 767+5. / [01] ENTERED MEASUREMENTS;[09] LOCATED AND DRILLED NEW REINFORCING CHANNEL LOT #1487793-1 IAW SRM 53-00-53-2R-2 REPAIR 2 TABLE 205 ALTERNATIVE 5. OK TO APPLY PRIMER;[10] VERIFIED CORRECTIVE ACTION #1 OK TO AAug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082537820Shield · corrodedCORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+5; BS 847+11; BS 847+14. / [01] REMOVED AFT DOOR SHIELD AT ACB RBL 21 BS 847 TO BS 867 IAW SRM 51-40-02;[02] SRM 53-00-53-1A-2 IS EFFECTIVE FOR THIS EVALUATION. NO ALLOWABLE DAMAGE FOUND FOR THIS PARAug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082537819Support · corrodedCORROSION ON AFT CARGO BAY AFT LOWER BULKHEAD SUPPORT AT BS 947 RBL 10; RBL 12; RBL 15. / [01] REMOVED AFT LWR BULKHEAD SUPPORT AT BS 947.5 RBL 22 TO LBL10 IAW SRM 51-40-02;[02] THERE IS NO SRM ALLOWABLE DAMAGE FOR ACB AFT LOWER BULKHEAD SUPPORT AT BS947. PARTAug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2022082537832Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+5; BS 767+9; BS 767+12; BS 767+16. / [01] ENTERED MEASUREMENTS;[02] SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 IS EFFECTIVE FOR THIS EVALUATION.<BR>NO ALLOWABLE GIVEN IN B737-800 SRM. REPAIR BY REPLACEMENT Aug 2, 2022 · N8656B · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022082537841Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727I+1; BS 727I+3; BS 727I+6-727I+11; BS 727I+12-727J+4; 727J+5-727J+16; BS 727J+18; BS 747-747+12; BS 747+14-747+19. / [01] ENTERED MEASUREMENTS;[06] FABRICATED AND LOCATED AND DRILLED NEW SIDEAug 2, 2022 · N8656B · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022082437816Intercostal · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT LBL 11 BS 344+9. / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL AT BS344 TO BS360 BL0 FOR ACCESS IAW SRM 51-40-02-0G-0;[03] CRACK ON UPPER FLANGE OF INTERCOSTAL EXCEEDS REPAIRABLE LIMIT IN SRM 53-10-51-1A-Aug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082437814Intercostal · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT RBL 12 BS 344+5; BS 344+9. / [01] UPDATED CHART.;[02] REMOVED INTERCOSTAL AT RBL 12 BS 344+5 - BS 344+9 IAW <BR>SRM 51-40-02-0G-0.;[03] EVALUATED CRACK ON UPPER FLANGE OF INTERCOSTAL EXCEEDS REPAIRABLE LIMIT IN SRM 5Aug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082437825Attach Angle · crackedCRACK ON AFT CARGO BAY AFT BULKHEAD SUPPORT ATTACH ANGEL AT LBL 10 BS 847+18. / [01] REMOVED AND REPLACED ACB AFT BULKHEAD SUPPORT ATTACH ANGLE AT LBL 10 BS 847+18 IAW SRM 51-40-02 AND BOEING DWG 149A8102;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03Aug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022082237821Web · corrodedCORROSION ON AFT CARGO BAY THRESHOLD AT RBL 21 BS 787+8; RBL 26 BS 787+14-807+6; RBL 26 BS 807+8; RBL 26 BS 807+12; RBL 26 BS 807+19; RBL 26 BS 827+1-827+11. / 02] 1.- REMOVED CORROSION FROM ACB THRESHOLD AT RBL 21; BS 787+8; IS FOUND IN LIMITS IAW SRM 53-60-1Aug 2, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022092220224Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS970 - BS887 S-4R TO S-6R. MARKED. BS887 - BS960 S-6R TO S-8R. MARKED. BS887 - BS947 S-8R TO S-11R. MARKED. BS887 - BS928 S-11R TO S-13R. MARKED. BS887 - BS908 S-13R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST INJun 18, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092220225Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS858 - BS887 S-4R - S-10R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 858 TO 887 S-4R TO S-10R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+5.5' 3.5' BELOW STR 9R<BR>Jun 18, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092220227Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS887 - BS987 S-2R TO S-4R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 987 S-2R TO S-4R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 907+10' 4' BELOW STR 3R<BR>2) BJun 18, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092220228Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS845 - BS887 S-10R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 845 TO 887 S-10R TO S-14R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+13' 1.5' BELOW STR 13R<Jun 18, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092218943Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-2L TO S-4L BS887 - BS947+5. MARKED / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 1016 S-2L TO S-4L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 887-907 S-2L TO S-3L<BR>2) BJun 15, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092218944Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-4L TO S-6L BS887 - BS947+6. MARKED S-6L TO S-9L BS927 - BS947. MARKED S-9L TO S-11L BS887 - BS927. MARKED. S-9L TO S-10L BS927 - BS927+15. MARKED. S-11L TO S-14L BS887 - BS907. MARKED. / [01] PERFORMED CLAD PENETRATION TEST Jun 15, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092218946Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-10L TO S-14L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-10L TO S-14L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 827-847 S-13L TO S-14L<BR>Jun 15, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092218948Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-16L TO S-19L BS787 - BS827. MARKED. / [01] EVALUATED ANOMALIES ON FUSELAGE SKIN AT BS 787+14.5 6.5'BELOW STR 19L D=.0006'; BS 787+12 1'BELOW STR 18L D=.0005'; BS 787+11 6'BELOW STR 17L D=.001'; BS 807+6 6'BELOW STR 18L D=.00Jun 15, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092218947Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-14L TO S-16L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-14L TO S-23L LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 807-827 S-16L TO S-17L<BR>2Jun 15, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022092217456Skin · corrodedSKIN PITTING AND ANOMALIES BS 907 - BS 927 STR 6L - STR 7L / [01] REMOVED SKIN PITTING AND ANOMALIES FROM FUSELAGE SKIN AT BS 907-927; STR 6L-7L IAW SRM 51-10-02-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ACCOMPLISHED UT INSPECTION OF BLENDED AREA LOWEST TJun 10, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2022091517245None · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK AT M1673 / [01] REMOVED AND REPLACED BATTERY PACK M1673 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS REQUIREMENT BLOCK;[03] CERTIFIED ITEM 1 AND 2Jun 10, 2022 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2022091517244None · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK AT M1670 WILL NOT CHARGE / [01] REMOVED AND REPLACED BATTERY PACK M1670 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS REQUIREMENT BLOCK;[03] CERTIFIED ITEM 1 AND 2Jun 10, 2022 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2022091517243None · inoperativeEMERGENCY LIGHT PATTERY PACK AT M1672 WILL NOT CHARGE / [01] REMOVED AND REPLACED BATTERY PACK M1672 PER AMM 33-51-06-960-805 STEPS 4. E. (1)-(5);[02] UPDATED PARTS INFORMATION;[03] CERTIFIED ITEM 1Jun 10, 2022 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2022050200066Skin · corrodedTRANSFERRED FROM FAULT TTG8Q00AP7ZC. AFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATELY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN /Apr 27, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022020869405Skin · corrodedAFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATLY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN ; /Feb 4, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022013164829Skin · corrodedAFTER PAINT STRIP FOUND SOME SKIN PITTING AND SKIN ANOMALIES FROM APPROXIMATELY STA 867 TO 928 STR 14 TO 14 OVER THE CROWN.Jan 27, 2022 · N8656B · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2021080298125Light · brokenCENTER CABIN OVERJEAD EMERGECNY EXIT LIGHT BROKEN ( MX NOTE ) / REMOVED AND REPLACED CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN PER AMM 33-51-02. CLR # 91927Jul 27, 2021 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2021030452790Battery Pack · failedFWD RIGHT REAR BATT PACK FAILED / REPLACED FWD RIGHT BATT PACK PER 33-51-06 OF THE AMMMar 3, 2021 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2021081326528Bracket · crackedRH WING BRACKET O/B OF DEFLECTION CONTROL RIB TO WEB IS CRACKED / REMOVED AND REPLACED R/H WING BRACKET O/B OF DEFLECTION CONTROL RIB TO WEB IAW SRM 51-40-02-0G-0 AND DWG 115A6200 REV A MPN 115A6260-2 A TAG A90889Oct 28, 2020 · N8656B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021072126773Panel · crackedPASSENGER CABIN; EXPANSION PNL CRACKED AT STA 540; LBL1; WL208. / REMOVED CRACKED PASSENGER CABIN EXPANSION PNL AT STA 540 LBL 1 WL 208 AND REPLACED WITH NEW EXPANSION PNL P/N 143A5240-35 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REV - ATAG WN8693Oct 28, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021072126772Panel · crackedPASSENGER CABIN; EXPANSION PNL CRACKED AT STA 540; RBL1; WL 208. / REMOVED CRACKED PASSENGER CABIN EXPANSION PNL AT STA 540 RBL 1 WL 208 AND REPLACED WITH NEW EXPANSION PNL P/N 143A5240-36 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 REV - ATAG WN8998Oct 28, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021071626530Rib · corrodedPANEL 424 #2 ENGINE OB COWL HAS CRACK AT ACCESS DOOR CUTOUT ON INTERIOR RIB SUPPORT AT LATCH SIDE / REMOVED CRACKED SHIELD AT # 2 ENG O/B COWL PNL 424 IAW SRM 51-40-02-0G-0 DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0 AND CMM 71-13-30 INSTALLED NEW SHIELD IAW SRM Oct 28, 2020 · N8656B · Boeing 7378H4 · Nacelle/Pylon, Main FrameSDR SWAA2020111026527Lens · crackedRIGHT AFT OVERWING ILLUMINATION LIGHT LENSE CRACKED. REPLACED RIGHT AFT SLIDE/OVERWING LIGHT LENS, IAW AMM 33-51-04-960-801 STEPS 2F (1) (A) AND (D) A TAG A91524.Oct 28, 2020 · N8656B · Boeing 7378H4 · Emergency LightingSDR SWAA2021071526503Angle · corrodedFWD PIT STA 418 FLOOR SUPPORT SHIELD UPPER SURFACE CORRODED AT RBL24 AND W/L157 / REMOVED CORROSION ON R/H Z-ANGLE AT STA 418 IN FWD CARGO COMPARTMENT IAW SRM 51-10-02-0G-0. VERIFIED LIMITS ORIGINAL THICKNESS .040'; LOSS OF .006' REMAINING .034' OUT OF LIMITS Oct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021071526492Shield · corrodedFWD PIT STA 438 FLOOR SUPPORT SHIELD UPPER SURFACE CORRODED STA RBL24 AND W/L157 / REMOVED CORROSION ON FWD SHIELD IN FWD CARGO COMPARTMENT AT STA 438; RBL 24 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS ORIGINAL THICKNESS .032; LOSS OF .013; REMAINING .019' OUT OF Oct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021071526496Rail · corrodedFWD PIT STA 500I LATERAL FLOOR SUPPORT UPPER SURFACE CORRODED FROM LBL24 TO RBL24 AND W/L157 / EVALUATED CORROSION AT FWD PIT STA 500I FLOOR SUPPORT RAIL LBL 24 RBL 24 W/L 157 100% MATERIAL LOSS FOUND. NO PUBLICATION OF LIMITS WAS FOUND. REMOVED AND REPLACED FOct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021071526099Support Angle · bentLEFT WING TRAILING EDGE PANEL 551FB WIRE BUNDLE SUPPORT ANGLE DAMAGED/BENT. MARKED. / REMOVED AND INSTALLED NEW LEFT WING TRAILING EDGE PANEL 551FB WIRE BUNDLE SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG # 115A2710 REV - A TAG # A90358Oct 27, 2020 · N8656B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021071426497Support · corrodedFWD PIT STA 500I SIDEWALL SUPPORT UPPER SURFACE CORRODED AT RBL25 AND W/L157 / REMOVED CORROSION ON FWD PIT STA 500I; RBL 25 SIDE WALL SUPPORT ANGLE ORIGINAL MATERIAL THICKNESS .071 LOSS OF .003 WITH .068 REMAINING FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHEDOct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021040826499Angle · corrodedAFT CARGO COMPARTMEMT R/H Z-ANGLE; RBL 20; WL 156; BS 727C + 16' - 767 CORRODED IN MULTIPLE PLACES / BLENDED AND REMOVED CORROSION AFT CARGO COMPARTMENT R/H Z ANGLE RBL 20 WL 156 BS 727C+16 - 767 AND VERIFIED WITH 10X MAGNIFYING IAW SRM 51-10-02-0G-0 ORIGINAL Oct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021040726092Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120AF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON FWD CARGO COMPT FLOOR PANEL 120AF TOTAL ACCUMULATED DAMAGE FOUND TO BE MORE THAN THE 20' MAXIMUM ALLOWED OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL 120AFOct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021040726091Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120BF HAS CORROSION AROUND EDGES ALSO MISALIGNED HOLES ON ONE SIDE / EVALUATED CORROSION AS OUT OF LIMITS DAMAGE GREATER THAN 20' IAW SRM SRM 53-00-53-1A-1 FIGURE 102. VERIFIED NEW MATERIAL AS 2024 T3 0.071' ATAG# GO6775 IAW AMM 25Oct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021040726088Floor Panel · corrodedFWD CARGO COMPT. FLOOR PANEL 120CF HAS CORROSION AROUND EDGES / REMOVED CORROSION AT FWD CARGO COMPT FLOOR PANEL 120CF CORROSION EXCESS MORE THAN 20' INCHES IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 VERIFIED NEW MATERIAL AND FABRICATED NEW PNL 120CF IAW SRM 51-40Oct 27, 2020 · N8656B · Boeing 7378H4 · Fuselage Floor Panel
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