N8651A

Service difficulty reports · 181

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 = 'N8651A' 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 SWAA2022100571982None · crackedMOPSILL INNER CHORD CRACKED BS 303.9 LBL 55 WL 209 / [01] UPDATED MEASUREMENTS. REMOVED FWD ENTRY DOOR MOPSILL IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FED MOP SILL IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A8110 APPLIED CHEMICAL CONVERSION COAT AND PRIMEDSep 14, 2022 · N8651A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022100571983Floor Support · crackedFLOOR SUPPORT CRACKED BS 312+9 LBL 43 WL 208 / [01] REMOVED CRACKED FLOOR SUPPORT BS 312+9 LBL 43 WL 208 PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05; DRW # 141A5400. REQUEST OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION #2<BRSep 14, 2022 · N8651A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2022100552547None · corrodedFORWARD CARGO BAY SUBTHRESHOLD WEB HAS CORROSION BS 440+15 RBL 28 WL 156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB; AT BS 440+15 RBL 28 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DSep 13, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552820Angle · damagedCORROSION ON L/H FWD EMERGENCY EXIT DOOR LOWER HINGE SUPPORT ANGLE AT LBL 67 WL 221 BS 580+9; BS 580+15. / [01] REMOVED L/H FWD EMERGENCY EXIT DOOR LOWER CLOSEOUT LINING ASSEMBLY AT BS 578 TO BS 601 LBL 67 WL 221 IAW AMM 25-21-20-000-801 STEP 6 (A) AND (B) REMSep 13, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552821Angle · corrodedCORROSION ON R/H FWD EMERGENCY EXIT DOOR LOWER HINGE SUPPORT ANGLE AT RBL 67 WL 221 BS 580+9; BS 580+15. / [01] REMOVED R/H FWD EMERGENCY EXIT DOOR LOWER CLOSEOUT LINING ASSEMBLY AT BS 578 TO BS 601 RBL 67 WL 221 IAW AMM 25-21-20-000-801 STEP 6 (A) AND (B) REMSep 13, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552540Bracket · brokenAFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166 / [01] REMOVED ACB LAV TANK LOWER BULKHEAD SUPPORT BRACKET BS867; LBL10; WL166 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW ACB LAV TANK LOWER BULKHEAD SUPPORT BRACKET BS867; LBL10Sep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2022100552534Sidewall Support · corrodedFWD CARGO BAY R/H FLOOR TO SIDEWALL HAS MULTIPLE AREAS OF CORROSION BS500A TO BS500I RBL24 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT FOUND DEEPEST LOCATION TO BE AT BS 500C+10 RBL 24 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.Sep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552537Support Plate · corrodedFWD CARGO BAY L/H FLOOR SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION BS500 TO BS500I LBL24 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT FOUND DEEPEST LOCATION TO BE AT BS 500D+10 LBL 24 WL 156; FOUND 0.015 REMOVED FRSep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552543Shield · corrodedFWD CARGO BAY SHIELD AFT OF CARGO DOOR HAS CORROSION BS500+10 RBL24 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 500+10 RBL 24 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVSep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552536Sidewall Support · corrodedAFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AT BS867+15; RBL21; WL168 / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 867+15 RBL 21 WL 168; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-0Sep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552544Shield · corrodedAFT CARGO BAY SHIELD AFT OF CARGO DOOR HAS CORROSION BS847+15; WL164 RBL21 / [01] EVALUATED CORROSION ON SHIELD BS 847+15 RBL 21 WL 164; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTISep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552535None · corrodedAFT CARGO BAY SUBTHRESHOLD HAS MULTIPLE AREAS OF CORROSION 792 TO 847 RBL26 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF SUBTHRESHOLD WEB; FOUND DEEPEST LOCATION TO BE AT BS 787+10 RBL 26 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN NUMEROUS 1'X1' ARSep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552538Shield · corrodedAFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLE BS767 TO BS794 RBL22 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO 794 RBL 22 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACESep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552539Attach Angle · corrodedAFT CARGO BAY LOWER ATTACH ANGLE COMMON TO SHIELD HAS CORROSION AROUND MULTIPLE NUT PLATE HOLES BS767 TO BS787 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD ATTACH ANGLE BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND Sep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552546Sidewall Support · corrodedAFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION BS727I TO BS807 LBL21.5 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT FOUND DEEPEST LOCATION TO BE AT BS 767+10 LBL 21 WL 156 IN; FOUND 0.015 REMSep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100552545Support · corrodedAFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES BS727I TO BS767 RBL21.5 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT FOUND DEEPEST LOCATION TO BE AT BS 747+10 RBL 21 WL Sep 12, 2022 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2022100551440Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED AT VAPOR BARRIER LBL8 WL167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[02] INSTALLED EWIS PROTECTION AT REPAIR AREA BS 663 LBL 6-45 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA AND FASTENERS AT REPAIER AREA BSep 8, 2022 · N8651A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022100551463Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED AT VAPOR BARRIER RBL8 WL167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[02] INSTALLED EWIS PROTECTION AT REPAIR AREA BS 663 RBL 6-45 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA AND FASTENERS AT REPAIER AREA BSep 8, 2022 · N8651A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022020969404Sign · brokenCENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT HOUSING BROKEN ; / [01] REMOVED AND REPLACED CENTER AISLE EMERGENCY EXIT SIGN IAW AMM 33-51-01.Feb 5, 2022 · N8651A · Boeing 7378H4 · Emergency LightingSDR SWAA2022020969403Fairing · crackedNO 2 ENG STRUT AFT FAIRING STRUCTURE CRACK 313A2752-1 PERMANENT REPAIR REQUIRED ; REMOVED NO 2 ENG AFT FAIRING AND OTER EXHAST NOZZLE FOR ENG STRT AFT FAIRING REPAIR PER AMM 54-52-04 / [01] REMOVED #2 ENGINE FAIRING AFT PANEL PER EA 22-154-00275; [02] LOCATED Feb 5, 2022 · N8651A · Boeing 7378H4 · Nacelle/Pylon, Attach FittingsSDR SWAA2022013164721Fitting · cracked#2 ENGINE AFT PYLON SUPPORT FITTING CRACKED ; / [01] REMOVED #2 ENGINE PYLON AFT FAIRING TO FOM PER AMM 54-52-04.; [02] REINSTALLED #2 ENGINE PYLON AFT FAIRING AS PER AMM 54-52-04Jan 27, 2022 · N8651A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2021100425119Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDSep 30, 2021 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021072696676Floor Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDJul 21, 2021 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021071292590Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDJul 8, 2021 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021070791543Lamp · inoperativeR2 DOOR EXTERIORE EMERGCY. LT. INOP / RELAMPED PER AMM 33-51-04. OPS-OK.Jul 7, 2021 · N8651A · Boeing 7378H4 · Emergency LightingSDR SWAA2021062486107Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDJun 20, 2021 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021061480905Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDJun 8, 2021 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021061480904Panel · crackedFWD CARGO PANEL 120ZAC HAS A 2' LONG CRACK 27' FROM LH EDGE OF PANELPERFORMED INTERIM REPAIR PER EA 1-A25-3722 REV 5 EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTEDJun 8, 2021 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021051069305Slide · out of positionFORWARD GALLEY SERVICE DOOR SLIDE PACK IS SLIPPING OUT FROM CASING / REPOSITIONED & SECURED SLIDE PER AMM 25-66-01May 5, 2021 · N8651A · Boeing 7378H4 · Escape SlideSDR SWAA2021051070731Mount · brokenFORWARD SERVICE DOOR ASSIST HANDLE IS BROKEN / INSTALLED NEW HANDLE MOUNT PER S.I.PApr 27, 2021 · N8651A · Boeing 7378H4 · Galley DoorsSDR SWAA2020102024353Sign · unsecureEXIT SIGN FOR OVERWING EXITS FELL DOWN. RESECURED IN REF TO SIP.Oct 17, 2020 · N8651A · Boeing 7378H4 · Emergency LightingSDR SWAA2021080314216Splice Strap · corrodedAFT CRAGO FLOOR PANEL SPLICE STRAP AT STA 727D + 4'; WL 156; RBL 8 HAS CORROSION AT FASTENER HOLE / REPLACED AFT CARGO FLOOR PANEL SPLICE STRAP STA 727 + D WL 156 P/N 146A9401-8 TAG# A78407 IAW B737 DWG 146A7500 REV. -Sep 4, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021081014103Support Bracket · crackedLEFT WING - APPROX. 1' ABOVE AFT SAIL TAIL TIP - 'L' ANGLE THAT ATTACHES TO SUPPORT BRACKET IS CRACKED / BROKEN / REMOVED AND REPLACED SUPPORT BRACKET ON LEFT WING 1' ABOVE AFT SAIL TAIL TIP IAW BOEING 737-800 SRM 51-40-02-0G-0 BOEING DWG 115A6200 REV - P/N 11Sep 3, 2020 · N8651A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021081313528Angle · corrodedAFT CARGO COMPARTMENT BULKHEAD SIDEWALL R/H ANGLE BS947; RBL22; WL156; CORRODED / REMOVED DAMAGE ON AFT CARGO AFT R/H BULKHEAD ANGLE FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS 50% MATERIAL LOSS IAW SRM 51-10-02-0G-0. REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWG Sep 2, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021081313527Angle · corrodedAFT CARGO COMPARTMENT BULKHEAD FLOOR ANGLE BS947; RBL22-LBL12; WL156; CORRODED / REMOVED DAMAGE ON AFT CARGO AFT BULKHEAD FLOOR ANGLE FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS 50% MATERIAL LOSS IAW SRM 51-10-02-0G-0. REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWGSep 2, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021080313437Splice · corrodedAFT CARGO; FLOOR PANEL SPICE TEE AT STATION 772; WL 150;RBL15 HAS AREAS OF CORROSION. / REPLACED AFT CARGO PANEL SPLICE TEE STA 772 RBL 15 WL 150 P/N 146A9401-4 TAG# WN9492 (3530573) IAW B737 IPC 53-42-11-26Sep 2, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2020091713522Angle · corrodedAFT CARGO COMPARTMENT FLOOR RT Z-ANGLE SECTION BS 727-767; RBL 22; WL 156; MULTIPLE AREAS OF CORROSION. REMOVED CORROSION AFT CARGO COMPARTMENT FLOOR RT Z-ANGLE STA 727 - 767 RBL 22, IAW B737 SRM 51-40-02-0G-0. ITEM IS ORIGINAL 'T' .040 REMAINING .032 LOSS .Sep 2, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2020091713529Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 231FF, UPPER SURFACE HAS FIBERS PULLED THE WHOLE LENGTH OF THE BOARD APPROX 3 INCHES FROM INBOARD SIDE. REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACE OF FLOORBOARD 231FF, IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1 REV 70 AND SRM 53-0Sep 2, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021081713280Support · corrodedFWD PIT STA 500I LBL 24 SIDEWALL LOWER SUPPORT FLANGE CORRODED AT WL157 / REMOVED CORROSION ON FWD PIT STA 500I LBL 24 SIDEWALL SUPPORT ORIGINAL THICKNESS .071 LOSS .008 REMAINING THICKNESS .063 OUT OF LIMITS DUE TO NO PUBLISHED LIMITS COMPLIED WITH EA 200474 Sep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2021081713153Channel · crackedRIGHT WING; TRAILING EDGE PANEL STRUCTURE AT ORSS 290 (BELOW DEFLECTION RIB) ATTACH FITTING AND CHANNEL CRACKED. / REMOVED + REPLACED ATTACH FITTING + CHANNEL ON R/H WING; TRAILING EDGE AT ORSS 290 BELOW DEFLECTION RIB IAW SRM 51-40-02-0G-0 + DEG 115A3712 SHT Sep 1, 2020 · N8651A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021081708063Attach Fitting · crackedRIGHT WING; TRAILING EDGE PANEL STRUCTURE AT ORSS 290 (BELOW DEFLECTION RIB) ATTACH FITTING AND CHANNEL CRACKED. / REMOVED + REPLACED ATTACH FITTING + CHANNEL ON R/H WING; TRAILING EDGE AT ORSS 290 BELOW DEFLECTION RIB IAW SRM 51-40-02-0G-0 + DEG 115A3712 SHT Sep 1, 2020 · N8651A · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2021080313152Floor Panel · corrodedAFT CARGO; FLR PNL 140AF IS CORRODED ALONG MULTIPLE EDGES. / FOUND TOTAL ACCUMULATED LENGTH OF CORROSION MORE THAN 20'. FOUND FLOOR PANEL 140AF OUT OF LIMITS. FABRICATED NEW FLOOR PANEL FROM 2024-T3 .071' ATAG A76431. ALODINED AND PRIMED NEW FLOOR PANEL IAW AMSep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021080313148Floor Panel · corrodedAFT CARGO FLR PNL 140CF IS CORRODED ALONG MULTIPLE EDGES. / MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE GREAYTER THAN 20'. FOUND FLOOR PANEL 140CF OUT OF LIMITS. VERIFIED MATERIAL FOR NEW FLOOR PANEL TO BE 2024 T3 .071' A-TAG A76436; LOCATED; DSep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021080313151Floor Panel · corrodedAFT CARGO; FLR PNL 140BF IS CORRODED ALONG BOTH OUTER EDGES. / EVALUATED AFT CARGO FLOOR PANEL 140BF; CORROSION EXCEED THE 20 INCH IN LENGTH. OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 SECTION F AND BOEING Sep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021080313149Floor Panel · corrodedAFT CARGO; FLR PNL 140EF IS CORRODED ALONG BOTH OUTER EDGES. / EVALUATED CORROSION ON AFT CARGO FLOOR PANEL 140EF; CORROSION EXXEEDES 10' IN LENGTH; OUT OF LIMITS IAW SRM 53-00-53-1A-1; FIGURE 102. FABRICATED NEW PANEL IAW AMM 25-52-01-201-801 AND BOEING DWG# Sep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021080313150Floor Panel · corrodedAFT CARGO; FLR PNL 140DF IS CORRODED ALONG MULTIPLE EDGES. / EVALUATED CORROSION ON AFT CARGO PIT FLOOR PANEL 140DF; VERIFIED TOTAL LENGTH OF CORROSION EXCEEDES 20 IN. OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801. TRSep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2021071513288Angle · crackedRIGHT WING T/E UPPER FIXED T/E PANEL JUST INBD OF DEFLECTION CONTROL RIB; PANEL SUPPORT ANGLE CRACKED @ OTBD END; MRK'D. / REMOVED CRACKED ANGLE AT RH WING T/E UPPER FIXED T/E PANEL JUST I/B OF DEFLECTION CONTROL RIB AND INSTALLED NEW ANGLE ALL IAW SRM 51-40-0Sep 1, 2020 · N8651A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021071513282Support Angle · crackedLEFT WING FIXED TRAILING EDGE PANEL SUPPORT ANGLE JUST INBOARD OF THE DEFLECTION CONTROL RIB IS CRACKED / REMOVED CRACKED LEFT WING FIXED TRAILING EDGE PANEL SUPPORT ANGLE AND REPLACED WITH NEW SUPPORT ANGLE P/N 115A1567-7 IAW SRM 51-40-02-0G-0Sep 1, 2020 · N8651A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2021071513281Support Angle · corrodedFWD PIT STA 500I LATERAL FLOOR SUPPORT CORRODED FROM LBL 23 TO RBL 23 AT WL 157 / FWD PIT STA 500I LATERAL FLOOR SUPPORT CORROSION FROM LBL 23 - RBL 23 WL 157 FOUND TO BE 'OUT OF LIMITS' DUE TO NO PUBLISHED LIMITS. REPLACED FLOOR SUPPORT ANGLE WITH PN: 143A948Sep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2020091713284Angle · corrodedFWD PIT STA 500A TO 500I FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED AT RBL 24 AND WL 157. REMOVED CORROSION, IAW SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-2. VERIFIED WITH 10X MAGNIFICATION. ORIGINAL THICKNESS .040' AFTER REWORK .029', .011' MATERIAL LOSS, OUSep 1, 2020 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous Structure
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