N7742B

Service difficulty reports · 228

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 = 'N7742B' 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 SWAA2025021085576Floor Panel · pulledPANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085569Floor Panel · pulledPANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231ZF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085570Floor Panel · pulledPANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 232SF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALLDAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085571Floor Panel · pulledPANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS ON UPPER SURFACE WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0127;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085572Floor Panel · pulledPANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085577Floor Panel · pulledPANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085573Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085574Floor Panel · pulledPANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2025021085904Shield · corrodedFWD CARGO; FWD SHIELD BS 420 TO 440 RBL 23 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED FCB FWD SHIELD BS 420 TO BS 440 RBL 23<BR>IAW SRM 51-40-02 SRM 51-40-05 AND DWG # 143A0080 REV:-;[02] VERIFIED ITEM 1Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2025021085905Shield · corrodedFWD CARGO; AFT SHIELD BS 480 TO 500A RBL 23 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED FCB AFT SHIELD BS 492 TO BS 500A RBL 23 WL 156 IAW SRM 51-40-02 SRM 51-40-05 AND DWG # 143A0080 REV:-Jan 14, 2025 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024121878324Battery Pack · failedL/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.Dec 17, 2024 · N7742B · Boeing 7377BD · Emergency LightingSDR SWAA2024121878314Seal · delaminatedLEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER RUB STRIP DELAMINATING<[01] R/R LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER PER AMM 53-31-31Dec 17, 2024 · N7742B · Boeing 7377BD · Horizontal Stabilizer StructureSDR SWAA2023122033546Unknown · unknownGEAR HANDLE WAS MOVED FROM UP TO OFF; 3 RED LIGHT AND GEAR PARTIALLY EXTENDED AT 296 KNOTS.<[01] NO PREVIOUS HISTORY. PERFORMED TEST OF LANDING GEAR POSITION INDICATING AND WARNING SYSTEM PER AMM 32-61-00. ALL INDICATIONS AND FUNCTIONS ARE NORMAL.Dec 15, 2023 · N7742B · Boeing 7377BD · Landing Gear Position and WarningSDR SWAA2023112724566Doubler · crackedGPU DOOR LOWER SURROUND DOUBLER CRACK.<[01] CUT OUT DAMAGE; FAB; DRILLED UP DOUBLER AND FILLER PER SRM 53-10-15-2R-4;[02] ACCOMPLISHED HFEC OF CUT OUT AREA PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] INSTALLED REPAIR PARTS PER SRM 53-10-15-2RNov 23, 2023 · N7742B · Boeing 7377BD · Fuselage Main, Plate/SkinSDR SWAA2023110815396Vapor Barrier · crackedBS 663 LEFT WHEEL WELL VAPOR BARRIER IS CRACKED LBL 31.83 TO 45.84; LENGTH OF CRACK MEASURES 20.5'.<[01] REPAIRED DAMAGE AREA AT LEFT WHEEL WELL VAPOR BARRIER AS PER SRM 51-70-04-2R-10. MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMS9-3-120 CL7 PO#1690463.APPLIEOct 26, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023110815397Vapor Barrier · crackedBS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; CRACK MEASURES 17' LENGTH.<[01] REPAIRED DAMAGE AREA AT RIGHT WHEEL WELL VAPOR BARRIER AS PER SRM 51-70-04-2R-10.MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMS9-3-120TYD CL7 PO#1690463.APPLIED TEFLOOct 26, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023082994075Vapor Barrier · crackedAT BS 663 LEFT WHEEL WELL VAPOR BARRIER IS CRACKED LBL 31.83 TO 45.84; LENGTH OF CRACK MEASURES 20.5'.<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.Aug 27, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023082994076Vapor Barrier · crackedAT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; CRACK MEASURES 17' LENGTH.<[01] ACCOMPLISHED EA 23-157-02635 TO NOTED AREA.;[02] VERIFIED.Aug 27, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023082994077Vapor Barrier · crackedAT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 40 TO RBL 45.64; WL 169; CRACK MEASURES 12'<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.Aug 27, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023082994078Vapor Barrier · crackedAT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 40 AT WL 164; CRACK MEASURES 2.5' LENGTH.<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.Aug 27, 2023 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023082893034Seal · crackedRIGHT HORIZONTAL STABILIZER- UPPER FORWARD SLIDER CRACKED.<[01] R&R RH HORIZONTAL UPPER FWD SLIDER REF. AMM 53-31-31.Aug 24, 2023 · N7742B · Boeing 7377BD · Horizontal Stabilizer StructureSDR SWAA2023082893019Bracket · cracked-RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET CRACKED AT STA 500.<[01] REMOVED AND REPLACED RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET PER SRM 51-40-02.Aug 24, 2023 · N7742B · Boeing 7377BD · Aerodynamic FairingsSDR SWAA2023032720601Slide · out of adjustL1 DOOR EMERGENCY SLIDE HANGING OUT OF COMPARTMENT TSR# 2023002221<[01] ADJUSTED Z-FOLD REF MT 725-61-06 NO OTHER DEFECTS NOTED AC OK FOR SERVICEMar 24, 2023 · N7742B · Boeing 7377BD · Escape SlideSDR SWAA2023013094904Hinge · crackedAFT ENTRY DOOR; AFT DOOR STOP HINGE; 3RD FROM THE TOP; HAS EVIDENCE OF A CRACK. AFT ENTRY DOOR AFT DOOR STOP 3RD FROM THE TOP HAS EVIDENCE OF A CRACK.<[01] PERFORMED HFEC CRACK VERIFICATION ON AFT ENTRY DOOR; AFT DOOR STOP HINGE; 3RD FROM THE TOP; IAW NDT MANUJan 25, 2023 · N7742B · Boeing 7377BD · Fuselage, Door HingeSDR SWAA2023010985371Battery Pack · no testSEVERAL EMERGENCY LIGHTS BY MID-CABIN SECTION FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY AT M1669 AND M1668 I.A.W AMMM 33-51-06-960-805 SEPT 4.A TO E; AND POWER SUPPLY AT M1669 AND M1668 I.A.W AMM 33-51-06-960-806 STEP 5.A TO E; INSTALLATION TEST Dec 27, 2022 · N7742B · Boeing 7377BD · Emergency LightingSDR SWAA2023010989866Power Supply · failedSEVERAL EMERGENCY LIGHTS BY MID-CABIN SECTION FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY AT M1669 AND M1668 I.A.W AMMM 33-51-06-960-805 SEPT 4.A TO E; AND POWER SUPPLY AT M1669 AND M1668 I.A.W AMM 33-51-06-960-806 STEP 5.A TO E; INSTALLATION TEST Dec 27, 2022 · N7742B · Boeing 7377BD · Emergency LightingSDR SWAA2023010985369Light · inoperativeL-1 DOOR EXTERIOR FUSELAGE EMERGENCY LIGHT INOP.<[01] REPLACED LAMP AT L-2 DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04-960-801.<BR>TOOL ID 6699 CAL DUE 06/08/23<BR>AAR TAG A129955;[02] VERIFIED STEP 1Dec 27, 2022 · N7742B · Boeing 7377BD · Emergency LightingSDR SWAA2023010985370Light · inoperativeL-2 DOOR EXTERIOR FUSELAGE EMERGENCY LIGHT INOP.<[01] REPLACED LAMP AT L-1 DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04-960-801.<BR>TOOL ID 6699 CAL DUE 06/08/23<BR>AAR TAG A129955;[02] VERIFIED STEP 1Dec 27, 2022 · N7742B · Boeing 7377BD · Emergency LightingSDR SWAA2023011079098Rib · crackedRH HORIZONTAL STABILIZER RIB 5 AFT LOWER END FASTENER HOLES CRACKED IN THE MID SECTION 0.500' IN LENGTH. RH HORIONTAL STABILIER RIB 5 AFT LOWER END FASTENER HOLES CRACKED IN THE MID SECTION 0.500&#34; IN LENGTH.<[01] PERFORMED HFEC INSP ON STAB RIB 5 PER B737 Dec 7, 2022 · N7742B · Boeing 7377BD · Horizontal Stabilizer, Spar/RibSDR SWAA2023011078638Floorbeam · corrodedCORROSION AT AFT CABIN WET AREA FLOORBEAM FWD FLANGE FASTENER HOLES BS 986.5, LBL 45. REMOVED CORROSION IAW SRM 51-40-02-0G-0, INSTALLED A REPAIR ANGLE AND STRAP IAW SRM 53-70-51-2R-6, ALTERNATIVE 4, FIGURE 205, SRM 51-40-02-0G, SRM 51-40-02-0G-0, AND SRM 5Dec 6, 2022 · N7742B · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2023011078637Panel · crackedLEFT WING LEADING EDGE ACCESS PANEL 521MB CRACKED. PREPARED DAMAGE AREA FOR REPAIR AT LT WING LEADING EDGE PANEL 521MB IAW SRM 51-70-04-2R-6. REPAIRED THE DAMAGE AREA IAW SRM 51-70-04-2R-6. RESTORED ORIGINAL FINISHED IAW AMM 51-21-99-300-801.Dec 5, 2022 · N7742B · Boeing 7377BD · Wing, Plate/SkinSDR SWAA2022122178247Panel · corrodedWASTE TANK DOOR 145AL FOUND CORROSION AT BONDING JUMPER TERMINAL CONNECTION<[01] REMOVED WASTE TANK SERVICE PANEL AS PER AMM 52-49-07-000-801.;[02] VERIFIED STEP 1. OK TO INSTALL NEW WASTE TANK SERVICE PNL 145AL.;[03] INSTALLED NEW WASTE TANK SERVICE PANEL 145Dec 3, 2022 · N7742B · Boeing 7377BD · Fluid Service DoorsSDR SWAA2023011077891Rib · crackedDORSAL FIN ACCESS PANEL 321A FWD RIB #8 ASSY CRACKED P/N 174A1008-2<[01] LOCATED & DRILLED NEW RIB P/N: 174A1108-2; AS PER DWG. 174A1008 & SRM 51-40-02-0G-0.(JOB ACCOMPLISHED BY: W.C.#372).;[02] LATE ENTRY: REMOVED DAMAGE RIB #8 AT DORSAL FIN PANEL 321A; AS PEDec 2, 2022 · N7742B · Boeing 7377BD · Vertical Stabilizer, Spar/RibSDR SWAA2023011077893Vapor Barrier · cracked2 CRACKS FOUND AT EXTERNAL LOWER LT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION LBL 6 AND LBL 7; MARKED. 2 CRACKS FOUND AT EXTERNAL LOWER LT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION LBL 6 AND LBL 7 MARKED.<[01] FORMED REPLACEMENT ANGLE & SPLICE ANGLE FOR Dec 2, 2022 · N7742B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2023011077894Angle · crackedCRACK FOUND AT EXTERNAL LOWER RT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION RBL 7. CRACK FOUND AT EXTERNAL UPPER RT VAPOR BARRIER WEB ATTACH ANGLE STA 663 OPEN HOLE LOCATION RBL 7.<FORMED REPLACEMENT ANGLE & SPLICE ANGLE FOR REPAIR AT VAPOR BARRIER ATTACH ANDec 2, 2022 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023011077399Cargo Track · corrodedAFT CARGO COMP CARGO TRACK CORROSION BETWEEN STA 787-847 RBL 14' AFT CARGO COMPARTMENT TRACK CORROSION BETWEEN STA 787 + 7 AND STA 847 - 6 RBL 13.8'<[01] FOUND EXFOLIATING CORROSION AT AFT CARGO COMPARTMENT CARGO TRACK BETWEEN STA 787 TO STA 847 RBL 14. THIS CDec 1, 2022 · N7742B · Boeing 7377BD · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023010977412Bracket · crackedL2 DOOR PANEL 834DZ FWD BRACKET CRACKED<[01] REMOVED AND REPLACED BRACKET AT L2 DOOR PANEL 834DZ REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1Dec 1, 2022 · N7742B · Boeing 7377BD · Passenger/Crew DoorsSDR SWAA2022122177411Strap · corrodedAFT CARGO COMP STRAP UNDER FLOOR SUPPORT CORROSION STA 767+14 RBL 20'<[01] FOUND EXFOLIATING CORROSION AT AFT CARGO COMPARTMENT STRAP UNDER FLOOR SUPPORT AT STA 767+ 14 RBL 20. THIS CORROSION IS OUT OF LIMITS AS PER REF SRM 53-00-53-1A-2. PART NEEDS REPLACEMENDec 1, 2022 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023012093411Seal · damagedR/H HORIZONTAL STABILIZER CENTER BOX FWD HINGE LOWER SLIDING SEAL MISSING RUB STRIPS. REMOVED R/H HORIZONTAL STABILIZER CENTER BOX FWD HINGE LOWER SLIDING SEAL REF AMM-53-31-31-000-803;[02] VERIFIED STEP 1 REMOVAL OF LOWER SLIDING SEAL. OK TO INSTALL NEW LOWENov 30, 2022 · N7742B · Boeing 7377BD · Horizontal Stabilizer StructureSDR SWAA2023010976879Angle · crackedFWD CARGO COMP STA 500C STR 26L CLIP UNDER ZEE CHANNEL CRACKED<[01] REMOVED CLIP AT FWD CARGO COMP STA 500C STR 26L AS PER REF SRM 51-40-02;[02] RREMOVED AND REPLACED 1 EA CLIP ; STA 500C STR26L SRM51-40-02 AND DWD #143A7505.;[03] VERIFIED STEPS 1 AND 2Nov 30, 2022 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2022122176583Intercostal · crackedMAIN CABIN BETWEEN STA 380-400 RBL 12' INTERCOSTAL CRACKED<[01] REMOVED & REPLACED INTERCOSTAL ANGLE P/N: 143A5410-170; AS PER SRM 51-40-02-0G-0 & DWG. 143A5400.;[02] VERIFIED STEP 1Nov 30, 2022 · N7742B · Boeing 7377BD · Fuselage Main, StructureSDR SWAA2022122176584Intercostal · crackedMAIN CABIN BETWEEN STA 380-400 LBL 14' INTERCOSTAL CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400 AS PER REF SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW INTERCOSTAL;[03] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400 ASNov 30, 2022 · N7742B · Boeing 7377BD · Fuselage Main, StructureSDR SWAA2023011076581Not Reported · damagedMAIN CABIN FWD WET AREA STA 360-4 LBL 61' INNER CHORD HOLE ELONGATED<[01] MEASURED DIAMETER OF ELONGATED HOLE: 0.339'.;[02] CORRECTION ON STEP #1: MEASURED DIAMETER OF ELONGATED HOLE: 0.320'.;[03] MEASURED DIMENSIONS TO 3EA. NEAREST FASTENERS: HOLE #1:(AFT O/BNov 29, 2022 · N7742B · Boeing 7377BD · Fuselage Structure (General)SDR SWAA2023011076558Seat Track · corrodedCORROSION FWD WET AREA L/H O/B SEAT TRACK CROWN LBL 45.5 STA 360+10'. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, FIG.103, DETAIL A. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0, AMM 51-21-72. SRM 51-40-02Nov 29, 2022 · N7742B · Boeing 7377BD · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023011076549Seat Track · corrodedCORROSION FWD WET AREA L/H I/B SEAT TRACK CROWN LBL 24.5 STA 360+10. REMOVED THE SEAT TRACK BS 360+10 - 480, LBL 24.5 IAW SRM 51-40-02-0G-0. FABRICATED A NEW SEAT SECTION IAW SRM 53-00-52-2R-4 FIGURE 202 DETAIL B-B. LOCATED AND DRILLED THE NEW SEAT TRACK IANov 29, 2022 · N7742B · Boeing 7377BD · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2023011076567Floorbeam · corrodedCORROSION AT AFT CABIN WET AREA FLOOR BEAM FWD FLANGE FASTENER HOLES STA 986.5 LBL24 TO LBL 45. REMOVED CORROSION AT AFT CABIN WET AREA FLOOR BEAM FWD FLANGE FASTENER HOLE STA 986.5 AND LBL45 REF SRM 51-40-02-0G-0.<OUT OF LIMITS REF. SRM 53-70-51-1A-1; FIGURENov 29, 2022 · N7742B · Boeing 7377BD · Fuselage Main, Floor BeamSDR SWAA2023011076173Bracket · crackedLEFT WING TRAILING EDGE FIX PANEL JUST O/B OF SPOILER #6 LOWER BRACKET CRACKED<[01] REMOVED BRACKET AT LEFT WING TRAILING EDGE FIX PANEL O/B OF SPOILER #6 AS PER SRM 41-40-02-0G-0-A00729;[02] CORRECTION ON STEP #1:<BR>REMOVED BRACKET AT LEFT WING TRAILING EDGENov 29, 2022 · N7742B · Boeing 7377BD · Wing Miscellaneous StructureSDR SWAA2023011076565Bracket · crackedAFT CABIN WET AREA AFT PRESSURE BULKHEAD LT CORNER BRACKET CRACKED, BS 1016. REMOVED THE BRACKET IAW SRM 51-40-02, FABRICATED A NEW BRACKET IAW DWG 69-43232. LOCATED AND DRILLED THE BULKHEAD BRACKET IAW SRM 51-40-05. INSTALLED THE BULKHEAD BRACKET IAW SRNov 29, 2022 · N7742B · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2023011076573Floor Support · crackedMAIN CABIN FWD WET AREA BETWEEN BS 344-360 RBL 35 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0. LOCATED AND DRLLING A NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5410.Nov 29, 2022 · N7742B · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2023010976564Floor Panel · crackedMAIN CABIN FLOOR PANEL 221BF CRACKED<[01] RECEIVED NEW PANEL. WILL BE INSTALLED ON TTG8Q00FGHSR;[02] VERIFIED STEP 1Nov 29, 2022 · N7742B · Boeing 7377BD · Fuselage Floor Panel
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