Boeing 737-7BD

Service difficulty reports · 7,528

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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 aircraft_model_key = '7377BD'
  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 SWAA2024112549565Former · crackedR/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] EVALUATED CRACK ON FAIRING FORMER AT BS 500D BETWEEN STRINGER 18R/H AND 19R/H FOUND TO BE OUT OF LIMITS THEREFORE FAIRING FORMER WILL BE REPAIRED BY REPLACEMENT OF PART PER 53-30-71-Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2024112550098Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS685 S-3L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 685 S-3L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1106 REV. A.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2024112550099Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-2L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 706 S-2L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1107 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2024112550093Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2024112550094Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727A S-3R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727A S-3R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1101 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2024112550095Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727B S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1102 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550100Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727C S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1103 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550096Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-4L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-4L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550097Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550101Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727C S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550102Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-7L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-7L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550103Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 767 S-6L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550104Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS767 S-5L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP FROM BS 767 S-5L PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1132 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112549904Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL25 BS500B+12 WL208. MARKED<[01] REMOVED CORROSION ON SEAT TRACK LBL25 BS500B+12 AND APPLIED CHEMICAL CONVERSION AND PRIMER ON BLENDED AREAS IAW AMM 51-21-41-370-801 AND AMM 51-21-72-370-804;[02] VERIFIED TASK COMPLETEOct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Internal Mounting StructureSDR SWAA2024112150107Floorbeam · corrodedCORROSION AROUND FASTENER HOLE BS 986 FLOOR BEAM RBL 45 WL 208. CORROSION AROUND FASTENER HOLE PREVIOUS REPAIR BS 986 FLOOR BEAM RBL 45 WL 208<[01] REMOVED AND REPLACED BS986 LBL50-RBL50 WL206-WL208 UPPER T-CHORD REPAIR PARTS PER 737-700 SRM 51-40-02-0G-0 AS SOct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2024112150092Floorbeam · crackedBS 294 FLOOR BEAM IS CRACKED ON UPPER FLANGE RBL 52 WL 208.<[01] REMOVED DAMAGE PART OF THE FLOOR BEAM BS294 RBL24-RBL60 WL208 AND REPAIRED I.A.W SRM 53-10-51-2R-16 REPAIR 16 TASK COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2024112149568Floor Panel · crackedCABIN FLOOR PANEL 221GF FWD O/B CORNER TANG IS CRACKED.<[01] CABIN FLOOR PANEL 221GF FWD O/B CORNER TANG WITH CRACK WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112150081Floor Panel · delaminatedCABIN FLOOR PANEL 232AF TOP SURFACE DELAMINATED.<[01] CABIN FLOOR PANEL 232AF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112549551Floor Panel · delaminatedCABIN FLOOR PANEL 242VF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 242VF WITH TOP SURFACE DELAMINATION WAS REPAIRED AND CORRODED INSERTS WERE REPLACED IAW SRM 53-00-50-2R-1AND DWG 147A5810 ID:0350; DWG D1040M003-309.;[02] JOB COMPLETOct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112549553Floor Panel · delaminatedCABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] TOP SURFACE DAMAGE WAS REPAIRED AND DAMAGED INSERTS WERE REMOVED AND REPLACED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112549378Rib · crackedFOUND CRACK ON R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB LEADING EDGE RIB AT L/E STA 95.96<BR>I.A.W SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED CORRECTIVE ACTION STEP 1.Oct 16, 2024 · N7741C · Boeing 7377BD · Horizontal Stabilizer, Spar/RibSDR SWAA2024112149549Floor Panel · delaminatedCABIN FLOOR PANEL 241ZF HAS TOP SURFACE DELAMINATION.<[01] TOP SURFACE DELAMINATION ON CABIN FLOOR PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149548Floor Panel · delaminatedCABIN FLOOR PANEL 241XF HAS TOP SURFACE DELAMINATION.<[01] 241XF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149367Floor Panel · delaminatedCABIN FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 222CF WITH TOP SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149362Floor Panel · delaminatedCABIN FLOOR PANEL 221BF CORRODED INSERTS; BROKEN TAB AND TOP SURFACE DELAMINATION.<[01] 221BF FLOOR PANEL DAMAGED AREAS HAVE BEEN REPAIRED PER [SRM 53-00-50-2R-6-A00944 (REPAIR 6 - REPAIR OF DAMAGE LESS THAN 10 SQUARE INCHES IN AREA TO TWO FACESHEETS AND THE COct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149364Floor Panel · delaminatedCABIN FLOOR PANEL 221EF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 221EF WITH CORRODED INSERTS AND TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Main, StructureSDR SWAA2024112149370Floor Panel · delaminatedCABIN FLOOR PANEL 222BF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 222BF WITH CORRODED INSERTS AND TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149371Floor Panel · delaminatedCABIN FLOOR PANEL 222AF CORRODED INSERTS AND TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 222AF WITH CORRODED INSERTS AND TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149376Floor Panel · debondedCABIN FLOOR PANEL 241CF TOP SURFACE IS DISBONDED.<[01] CABIN FLOOR PANEL 241CF TOP SURFACE WITH DISBONDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149545Floor Panel · delaminatedCABIN FLOOR PANEL 241UF HAS TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 241UF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149552Floor Panel · delaminatedCABIN FLOOR PANEL 241AAF HAS TOP SURFACE DELAMINATION.<[01] CABIN FLOOR PANEL 241AAF WITH TOP SURFACE DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112548844Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] REMOVED; REPLACED; AND INSTALLED NEW B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02-0G-0; AND DWG 111A1000 REV: A.;[02] VERIFIED ACTION ITEMS AND TASK CARDOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112548845Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] REMOVED; REPLACED; AND INSTALLED NEW B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02-0G-0; AND DWG 111A1000 REV: A.;[02] VERIFIED ACTION ITEMS AND TASK CARDOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112548846Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 165.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF907.;[02] VERIFIED CORRECTIVE ACTION 1.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2024112548843Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 165.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF8ZU.;[02] VERIFIED CORRECTIVE ACTION 1.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112148790Vapor Barrier · delaminatedL/H 663 VAPOR BARRIER HAS A PREVIOUS REPAIR THAT IS DELAMINATING 'MARKED'<[01] L/H BS 663 VAPOR BARRIER WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2024112149043Floor Panel · delaminatedCABIN FLOOR PANEL 231DF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1.;[03] REMOVED AND INSTALLED NEW FLOOR PANEL 231DF IAW AMM 53-21-00-000-801 AND AMM 53-21-00-400-801.;[04] VERIFIED ITEM 3 AND TASK CARD COMPLETED.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149044Floor Panel · delaminatedCABIN FLOOR PANEL 231GF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1.;[03] REMOVED AND INSTALLED NEW FLOOR PANEL 231GF IAW AMM 53-21-00-000-801 AND AMM 53-21-00-400-801.;[04] VERIFIED ITEM 3 AND TASK CARD COMPLETED.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149040Floor Panel · delaminatedCABIN FLOOR PANEL 231KF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1.;[03] REMOVED AND INSTALLED NEW FLOOR PANEL 231KF IAW AMM 53-21-00-000-801 AND AMM 53-21-00-400-801.;[04] VERIFIED ITEM 3 AND TASK CARD COMPLETED.Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149045Floor Panel · delaminatedCABIN FLOOR PANEL 231XF UPPER SURFACE IS DELAMINATED.<[01] REMOVED AND INSTALLED NEW FLOOR PANEL 231XF IAW AMM TASK 53-21-00-000-801 PAR. 2. E.; AMM 53-21-00-400-801;[02] REMOVED AND INSTALLED NEW FLOOR PANEL 231XF IAW AMM TASK 53-21-00-000-801 PAR. 2. E.; AMMOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149042Floor Panel · delaminatedCABIN FLOOR PANEL 241DF UPPER SURFACE IS DELAMINATED.<[01] REMOVED AND INSTALLED NEW FLOOR PANEL 241DF IAW AMM 53-21-00-400-801; AMM TASK 53-21-00-000-801 PAR. 2. E.;[02] REMOVED AND INSTALLED NEW FLOOR PANEL 241DF IAW AMM 53-21-00-400-801; AMM TASK 53-21-00-0Oct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149041Floor Panel · delaminatedCABIN FLOOR PANEL 241AF UPPER SURFACE IS DELAMINATED.<[01] CABIN FLOOR PANEL 241AF IS TO BE INSTALLED ON CARD TTG8Q00VS4JJ;[02] REMOVED AND FABRICATED NEW CABIN FLOOR PANEL DUE TO DAMAGE IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4; SRM 53-00-50-1A-1 PARA 2. A. NOTE: SOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149046Floor Panel · delaminatedCABIN FLOOR PANEL 241KF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] COMPLETE.;[03] UPDATED STEP 1.;[04] COMPLETED STEP 1.;[05] REMOVED AND INSTALLED NEW FLOOR PANEL 241KF PER AMM 53-21-00-000-801 AND PER AMM 53-21-00-400-801.;[06] VERIFIED ITEM 5 ANOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149048Floor Panel · delaminatedCABIN FLOOR PANEL 241RF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1.;[03] UPDATED STEP 1;[04] REMOVED OLD FLOOR PANEL AND INSTALLED NEW FLOOR PANEL 241RF PER AMM 53-21-00-000-801 AND AMM 53-21-00-400-801;[05] VERIFIED STEP 1 CORRECTIOOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112149047Floor Panel · delaminatedCABIN FLOOR PANEL 241NF UPPER SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1.;[03] COMPLETED STEP 1.;[04] REMOVED AND INSTALLED NEW FLOOR PANEL 241NF PER AMM 53-21-00-000-801 AND PER AMM 53-21-00-400-801.;[05] VERIFIED ITEM 4 AND TASK CARD COMOct 15, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112548619Vapor Barrier · crackedDELAMINATING VAPOR BARRIER BS 663 LBL 24.92 (MARKED)<[01] CRACK DAMAGE ON L/H BS 663 VAPOR BARRIER TO BE ACCOMPLISHED ON FAULT#TTG8Q00WF5TG.;[02] VERIFIED JOB COMPLETEOct 14, 2024 · N7741C · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2024112548620Vapor Barrier · crackedCRACKED ANGLE ATTACH VAPOR BARRIER WING CENTER SECTION REAR SPAR AT BS 663 RBL 45. CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF907.;[02] VERIFIED CORRECTIVE ACTION 1.Oct 14, 2024 · N7741C · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2024112148618Vapor Barrier · crackedCRACKED PREVIOUS REPAIR VAPOR BARRIER BS 663 RBL 25 TO RBL 40 (MARKED)<[01] CRACK DAMAGE ON BS 663 VAPOR BARRIER TO BE ACCOMPLISHED ON FAULT#TTG8Q00WF5TG.;[02] CORRECTION TO ITEM 1: WRITTEN IN ERROR.;[03] CRACKED VAPOR BARRIER WAS REPAIRED AT BS 663 RBL 25 - 4Oct 14, 2024 · N7741C · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2024112148621Plate · damagedASD AFT GRIT BAR FITTING PLATE DAMAGED.<[01] COMPLETED REPLACED ASD AFT GIRT BAR FITTING PLATE IAW AMM 25-66-02-400-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 14, 2024 · N7741C · Boeing 7377BD · Escape SlideSDR SWAA2024112148622Bracket · looseFSD SLIDE COVER GRIT BAR FITTING ATTACHMENT FWD & AFT BRACKET RIVETS LOOSE<[01] REMOVED AND REPLACED FWD & AFT BRACKET RIVETS ON FSD SLIDE COVER GRIT BAR FITTING ATTACHMENT IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Oct 14, 2024 · N7741C · Boeing 7377BD · Escape Slide
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