# Service difficulty reports: N7741C A list on [N7741C](https://openairdocs.org/aircraft/N7741C.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 5 · 233 reports - [SDR SWAA2026022473255](https://openairdocs.org/sdr/SWAA2026022473255.md): Girt Bar · unsecure · Feb 22, 2026 · N7741C · Boeing 7377BD · Emergency Equipment > RAMP REPORTS L2 SLIDE GIRT BAR NOT STOWED. STOWED L2 DOOR SLIDE GIRT BAR IAW AMM25-66-01. - [SDR SWAA2025122955405](https://openairdocs.org/sdr/SWAA2025122955405.md): Sense Line · broken · Dec 23, 2025 · N7741C · Boeing 7377BD · Pneumatic Distribution System > AT 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 FRO - [SDR SWAA2025032408178](https://openairdocs.org/sdr/SWAA2025032408178.md): Slide · detached · Mar 21, 2025 · N7741C · Boeing 7377BD · Escape Slide > FWD ENTRY DOORESCAPE SLIDE DETACHED FROM DOOR AFTER OPENING<[01] R/R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FE - [SDR SWAA2025031003497](https://openairdocs.org/sdr/SWAA2025031003497.md): Slide · dislodged · Mar 9, 2025 · N7741C · Boeing 7377BD · Escape Slide > FWD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REPACKED SLIDE INTO BOX PER 25-66-00. NO DEFECTS NOTED - [SDR SWAA2025011384827](https://openairdocs.org/sdr/SWAA2025011384827.md): Lamp · inoperative · Jan 10, 2025 · N7741C · Boeing 7377BD · Emergency Lighting > ONE EMERGENCY LIGHT INOP BELOW AFT ENTRY DOOR<[01] RELAMPED ONE EMERGENCY LIGHT BELOW AFT ENTRY DOOR REF AMM 33-51-04. OPS CHECK GOOD. - [SDR SWAA2024121776126](https://openairdocs.org/sdr/SWAA2024121776126.md): Cabin Air Sys · odor · Dec 10, 2024 · N7741C · Boeing 7377BD · Air Distribution System > SHORTLY 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. - [SDR SWAA2024112561272](https://openairdocs.org/sdr/SWAA2024112561272.md): Light · inoperative · Nov 19, 2024 · N7741C · Boeing 7377BD · Emergency Lighting > FWD 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.
JOB COMPLETE. - [SDR SWAA2024112560649](https://openairdocs.org/sdr/SWAA2024112560649.md): Battery Pack · failed · Nov 16, 2024 · N7741C · Boeing 7377BD · Emergency Lighting > EMERGENCY 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. - [SDR SWAA2024112553044](https://openairdocs.org/sdr/SWAA2024112553044.md): Support · cracked · Oct 24, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > MAIN 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 - [SDR SWAA2024112151884](https://openairdocs.org/sdr/SWAA2024112151884.md): Floor Panel · delaminated · Oct 23, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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)]

ATTACHED CURE SHEETS TO THIS FAULT. - [SDR SWAA2024112551348](https://openairdocs.org/sdr/SWAA2024112551348.md): Frame · cracked · Oct 21, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Frame > FWD 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 1 - [SDR SWAA2024112551351](https://openairdocs.org/sdr/SWAA2024112551351.md): Frame · cracked · Oct 21, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Frame > CRACK 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 1 - [SDR SWAA2024112150854](https://openairdocs.org/sdr/SWAA2024112150854.md): Stub Frame · cracked · Oct 19, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Frame > CRACK 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.
EQUIP ID IS000680 DUE 07/25;[02] REMOVED DAMAGE PART OF THE R1 DOORWAY FWD STUB - [SDR SWAA2024112150857](https://openairdocs.org/sdr/SWAA2024112150857.md): Skin · corroded · Oct 19, 2024 · N7741C · Boeing 7377BD · Leading Edge Devices > L/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 SL - [SDR SWAA2024112550123](https://openairdocs.org/sdr/SWAA2024112550123.md): Threshold · cracked · Oct 18, 2024 · N7741C · Boeing 7377BD · Cargo Compartments > AFT 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. - [SDR SWAA2024112550607](https://openairdocs.org/sdr/SWAA2024112550607.md): Support Angle · cracked · Oct 18, 2024 · N7741C · Boeing 7377BD · Trailing Edge Flaps > RIGHT 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 1 - [SDR SWAA2024112550614](https://openairdocs.org/sdr/SWAA2024112550614.md): Support · cracked · Oct 18, 2024 · N7741C · Boeing 7377BD · Trailing Edge Flaps > BULB 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] VERIFIED - [SDR SWAA2024112150125](https://openairdocs.org/sdr/SWAA2024112150125.md): Track · cracked · Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > AFT 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 CARG - [SDR SWAA2024112150124](https://openairdocs.org/sdr/SWAA2024112150124.md): Shield · corroded · Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION 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 STEP - [SDR SWAA2024112150126](https://openairdocs.org/sdr/SWAA2024112150126.md): Plate · corroded · Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION 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 - [SDR SWAA2024112150127](https://openairdocs.org/sdr/SWAA2024112150127.md): Shield · corroded · Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION 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; S - [SDR SWAA2024112150128](https://openairdocs.org/sdr/SWAA2024112150128.md): Support · corroded · Oct 18, 2024 · N7741C · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION 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: A - [SDR SWAA2024112550083](https://openairdocs.org/sdr/SWAA2024112550083.md): Attach Angle · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > ATTACH 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 AC - [SDR SWAA2024112550108](https://openairdocs.org/sdr/SWAA2024112550108.md): Strap · corroded · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Structure > CORROSION 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 27 - [SDR SWAA2024112550109](https://openairdocs.org/sdr/SWAA2024112550109.md): Strap · corroded · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Structure > CORROSION 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 - [SDR SWAA2024112549565](https://openairdocs.org/sdr/SWAA2024112549565.md): Former · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/Skin > R/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- - [SDR SWAA2024112550098](https://openairdocs.org/sdr/SWAA2024112550098.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/Skin > CRACKED 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. - [SDR SWAA2024112550099](https://openairdocs.org/sdr/SWAA2024112550099.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/Skin > CRACKED 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. - [SDR SWAA2024112550093](https://openairdocs.org/sdr/SWAA2024112550093.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/Skin > CRACKED 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. - [SDR SWAA2024112550094](https://openairdocs.org/sdr/SWAA2024112550094.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Plate/Skin > CRACKED 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. - [SDR SWAA2024112550095](https://openairdocs.org/sdr/SWAA2024112550095.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550100](https://openairdocs.org/sdr/SWAA2024112550100.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550096](https://openairdocs.org/sdr/SWAA2024112550096.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550097](https://openairdocs.org/sdr/SWAA2024112550097.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550101](https://openairdocs.org/sdr/SWAA2024112550101.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550102](https://openairdocs.org/sdr/SWAA2024112550102.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550103](https://openairdocs.org/sdr/SWAA2024112550103.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112550104](https://openairdocs.org/sdr/SWAA2024112550104.md): Stringer Clip · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Attach Fittings > CRACKED 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. - [SDR SWAA2024112549904](https://openairdocs.org/sdr/SWAA2024112549904.md): Seat Track · corroded · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Internal Mounting Structure > CORROSION 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 COMPLETE - [SDR SWAA2024112150107](https://openairdocs.org/sdr/SWAA2024112150107.md): Floorbeam · corroded · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Floor Beam > CORROSION 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 S - [SDR SWAA2024112150092](https://openairdocs.org/sdr/SWAA2024112150092.md): Floorbeam · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Main, Floor Beam > BS 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 1 - [SDR SWAA2024112149568](https://openairdocs.org/sdr/SWAA2024112149568.md): Floor Panel · cracked · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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 1 - [SDR SWAA2024112150081](https://openairdocs.org/sdr/SWAA2024112150081.md): Floor Panel · delaminated · Oct 17, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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. - [SDR SWAA2024112549551](https://openairdocs.org/sdr/SWAA2024112549551.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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 COMPLET - [SDR SWAA2024112549553](https://openairdocs.org/sdr/SWAA2024112549553.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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. - [SDR SWAA2024112549378](https://openairdocs.org/sdr/SWAA2024112549378.md): Rib · cracked · Oct 16, 2024 · N7741C · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib > FOUND 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
I.A.W SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED CORRECTIVE ACTION STEP 1. - [SDR SWAA2024112149549](https://openairdocs.org/sdr/SWAA2024112149549.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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. - [SDR SWAA2024112149548](https://openairdocs.org/sdr/SWAA2024112149548.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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)]

ATTACHED CURE SHEETS - [SDR SWAA2024112149367](https://openairdocs.org/sdr/SWAA2024112149367.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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 #1 - [SDR SWAA2024112149362](https://openairdocs.org/sdr/SWAA2024112149362.md): Floor Panel · delaminated · Oct 16, 2024 · N7741C · Boeing 7377BD · Fuselage Floor Panel > CABIN 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 C Next page: https://openairdocs.org/aircraft/N7741C/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N7741C/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.