N7741C

Service difficulty reports · 233

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 = 'N7741C' 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 SWAA2026022473255Girt Bar · unsecureRAMP REPORTS L2 SLIDE GIRT BAR NOT STOWED. STOWED L2 DOOR SLIDE GIRT BAR IAW AMM25-66-01.Feb 22, 2026 · N7741C · Boeing 7377BD · Emergency EquipmentSDR SWAA2025122955405Sense Line · brokenAT 30000 CABIN ALT WARNING HORN CAME ON. THE CABIN ALT REACHED 10;000 FEET. STARTED QRH PROCEDURES AND DESCENDED TO 10;000. NO PAX MASKS DROPPED. FOUND SENSE LINE FROM BLEED AIR REGULATOR ON NR 1 ENG BROKEN. REPLACED THE LINE IAW SIP. FOUND SENSE LINE FRODec 23, 2025 · N7741C · Boeing 7377BD · Pneumatic Distribution SystemSDR SWAA2025032408178Slide · detachedFWD ENTRY DOORESCAPE SLIDE DETACHED FROM DOOR AFTER OPENING<[01] R/R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FEMar 21, 2025 · N7741C · Boeing 7377BD · Escape SlideSDR SWAA2025031003497Slide · dislodgedFWD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REPACKED SLIDE INTO BOX PER 25-66-00. NO DEFECTS NOTEDMar 9, 2025 · N7741C · Boeing 7377BD · Escape SlideSDR SWAA2025011384827Lamp · inoperativeONE EMERGENCY LIGHT INOP BELOW AFT ENTRY DOOR<[01] RELAMPED ONE EMERGENCY LIGHT BELOW AFT ENTRY DOOR REF AMM 33-51-04. OPS CHECK GOOD.Jan 10, 2025 · N7741C · Boeing 7377BD · Emergency LightingSDR SWAA2024121776126Cabin Air Sys · odorSHORTLY BEFORE DESCENT CABIN CREW REPORTED A BURN POPCORN SMELL MID CABIN. SMELL DISSIPATED AND DID NOT RETURN<[01] PERFORMED FIM 21-00 TASK 806 AND SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER AMM 05-51-56. NO DEFECTS NOTED.Dec 10, 2024 · N7741C · Boeing 7377BD · Air Distribution SystemSDR SWAA2024112561272Light · inoperativeFWD SERVICE DOOR SLIDE LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR SLIDE LIGHT IAW AMM 33-51-04-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Nov 19, 2024 · N7741C · Boeing 7377BD · Emergency LightingSDR SWAA2024112560649Battery Pack · failedEMERGENCY BATERY PACK M1668 FAIL TEST<[01] REMOVED AND REPLACED EMERGENCY BATERY PACK M1668 AND TESTED GOOD PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.Nov 16, 2024 · N7741C · Boeing 7377BD · Emergency LightingSDR SWAA2024112553044Support · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED MAIN CABIN FLOOR STRUCTURE WITH NEW SUPPORT AT STA 540; BL 0 TO RBL 24.75 IAW SRM 51-40-02 AND BOEING DWG 143A0060 REV:-; AMM 20-60-07-913-801;[02] VERIFIED Oct 24, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112151884Floor Panel · delaminatedCABIN FLOOR PANEL 221BF TOP SURFACE IS DELAMINATED.<[01] 221BF 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 TO THIS FAULT.Oct 23, 2024 · N7741C · Boeing 7377BD · Fuselage Floor PanelSDR SWAA2024112551348Frame · crackedFWD SERVICE DOOR FRAME BS 294 CRACKED AT LOWER END RBL 56 WL 208.<[01] REFER TO FAULT TTG8Q00WJ92N FOR REPAIR RESOLUTION;[02] VERIFIED CORRECTIVE ACTION 1Oct 21, 2024 · N7741C · Boeing 7377BD · Fuselage Main, FrameSDR SWAA2024112551351Frame · crackedCRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282.<[01] REMOVED CRACK ON BS 312 FRAME COMMON TO STR 5L LBL 33 WL 282 PER M-22-153-01244 ON FAULT# TTG8Q00WKNT8.;[02] VERIFIED CORRECTIVE ACTION 1Oct 21, 2024 · N7741C · Boeing 7377BD · Fuselage Main, FrameSDR SWAA2024112150854Stub Frame · crackedCRACK ON R1 DOORWAY FWD STUB FRAME IB SURFACE; BS 295 STR 17R<[01] NDT HFEC INSPECTED SURFACE PER 737 NDTM PART 6; 51-00-00; PROC 23; VERIFIED 1 INCH LONG CRACK FOUND; MARKED. <BR>EQUIP ID IS000680 DUE 07/25;[02] REMOVED DAMAGE PART OF THE R1 DOORWAY FWD STUB Oct 19, 2024 · N7741C · Boeing 7377BD · Fuselage Main, FrameSDR SWAA2024112150857Skin · corrodedL/W FRONT SPAR - PITTING CORROSION ON UPPER ROLLER SURFACE AT INB MAIN SLAT TRACK #3 SLAT (MARKED)<[01] FAULT WILL BE RESOLVED ON CUSTOMER CARD:TTG8Q00WJA0T;[02] DISREGARD CORRECTIVE ACTION BLOCK 1;[03] REMOVED AND REPLACED DAMAGED I/B MAIN SLAT TRACK ON #3 SLOct 19, 2024 · N7741C · Boeing 7377BD · Leading Edge DevicesSDR SWAA2024112550123Threshold · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 53-60-15-2R-1;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Oct 18, 2024 · N7741C · Boeing 7377BD · Cargo CompartmentsSDR SWAA2024112550607Support Angle · crackedRIGHT WING UPPER T/E PANEL BULB SEAL SUPPORT ANGLE IS CRACKED AT RSS 274<[01] REMOVED; REPLACED; AND INSTALLED A NEW BULB SEAL SUPPORT ANGLE AT R/W UPPER T/E PANEL AT RSS 274 IAW SRM 51-40-02 AND IPC 57-50-00-25.;[02] VERIFIED CORRECTIVE ACTION 1Oct 18, 2024 · N7741C · Boeing 7377BD · Trailing Edge FlapsSDR SWAA2024112550614Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON ORSS 269. MARKED<[01] REMOVED AND REPLACED BULB SEAL RETAINER SUPPORT FITTING P/N 115A2953-1; PO # 1000542/1; IAW SRM 51-40-02-0G-0 AND DWG. 115A2930; REV. -;[02] VERIFIEDOct 18, 2024 · N7741C · Boeing 7377BD · Trailing Edge FlapsSDR SWAA2024112150125Track · crackedAFT CARGO BAY CARGO TRACK IS CRACKED AT BS767 AND BS747 RBL13 WL156<[01] REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK FROM BS727+4 - BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500; DWG 147A7500 AND 146A0061. ALSO INSTALLED ALL REPAIR PARTS ON AFT CARGOct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112150124Shield · corrodedCORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED AND REMPLACED SHIELD BS500A? TO BS500+19? RBL22 WL156 PER SRM 51-40-02 AND DWG 143A0080; REV:-;[02] VERIFIED STEP 2 COMPLETE;[03] ALL STEPOct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112150126Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] LINE ITEM 2 ON PART REQUIREMENTS FOR P/N 146A7502-27 WAS BAD FROM STOCK AND NOT ISSUED TO N7741C FOR USE; THAT PART WAS RETURNED Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112150127Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED FWD SHIELD BETWEEN BS767 TO BS787 RBL 22 WL 156 ACB PER SRM 51-40-02 AND BOEING DWG 146A0081.;[02] ADDED REV LEVEL TO DWG; SOct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112150128Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SUPPORT AS PER SRM 51-40-02-0G-0; DWG 146A7500 REV: AOct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2024112550083Attach Angle · crackedATTACH ANGLE CRACKED BS 294 FWD SIDE OF STUB FRAME RBL 54 WL 208.<[01] REMOVED DAMAGE CLIP I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0; FABRICATION AND INSTALLATION TO BE ACCOMPLISHED ON CCN TTG8Q00WJ92N DUE TO CRACK ON STUB FRAME;[02] VERIFIED CORRECTIVE ACOct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach FittingsSDR SWAA2024112550108Strap · corrodedCORROSION ON L/H REINFORCEMENT STRAP BS 1017-1020 LBL 27 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND INSTALLED NEW LH REINFORCEMENT STRAP BS1006-1020 LBL27 WL208 IAW SRM 51-40-02-0G-0. APPLIED PRIMER TO LH REINFORCEMENT STRAP REPLACEMENT BS1017-1020 LBL 27Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, StructureSDR SWAA2024112550109Strap · corrodedCORROSION ON L/H REINFORCEMENT STRAP BS 1017 LBL 19 WL 208.<[01] REMOVED LH REINFORCEMENT STRAP AND REPLACED WITH NEW LH REINFORCEMENT STRAP BS1006-1025 LBL19 WL208 IAW SRM 51-40-02-0G-0. APPLIED PRIMER TO LH REINFORCEMENT STRAP REPLACEMENT BS1017-1020 LBL 19 Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, StructureSDR 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 Panel
Back to N7741C