# Service difficulty reports: N293WN A list on [N293WN](https://openairdocs.org/aircraft/N293WN.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 6 · 269 reports - [SDR SWAA2026051904055](https://openairdocs.org/sdr/SWAA2026051904055.md): Girt Bar · unsecure · May 17, 2026 · N293WN · Boeing 7377H4 · Emergency Equipment > FWD SERVICE DOOR SLIDE WILL NOT STAY IN THE STOWED POSITION. RESECURED FWD SERVICE DOOR SLIDE GIRT BAR IN THE STOWED POSITION. REF AMM 25-66-01. OK FOR SERVICE. - [SDR SWAA2026021971705](https://openairdocs.org/sdr/SWAA2026021971705.md): Battery Pack · no test · Feb 18, 2026 · N293WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY BATTERY PACK FAILED TIMED CHECK AT 14 ABC. R & R THE BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2025052072088](https://openairdocs.org/sdr/SWAA2025052072088.md): Hook · out of adjust · May 17, 2025 · N293WN · Boeing 7377H4 · Emergency Equipment > FWD SERVICE DOOR FORWARD GIRT BAR STOWAGE HOOK DOES NOT STOW GIRT BAR SECURELY <[01]. ADJUSTED FORWARD SERVICE DOOR; FORWARD GIRT BAR STOWAGE HOOK PER SIP. OPS CHECKS OK. - [SDR SWAA2025051467110](https://openairdocs.org/sdr/SWAA2025051467110.md): Light · damaged · May 4, 2025 · N293WN · Boeing 7377H4 · Emergency Lighting > FWD LAV EMERGENCY EXIT LIGHT DAMAGED<[01] REPLACED FWD LAVATORY 'A' EXIT LIGHT WITH NEW ASSEMBLY IAW AMM 33-51-01-960-802.;[02] ADDITION: SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED;[03] VERIFIED - [SDR SWAA2025051366262](https://openairdocs.org/sdr/SWAA2025051366262.md): Floor Support · corroded · May 1, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB FLOOR SUPPORT INTERCOSTAL STA 767+5; RBL 25<[01] REMOVED AND REPLACED ACB FLOOR SUPPORT INTERCOSTAL AT STA 767 TO STA 787; RBL 25 LOT 1602576-1 I.A.W SRM 51-40-02-0G-0 AND DWG 146A0081 REV: A. ALL WORK ACCOMPLISHED ON FAULT TTG8Q00ZV5ZZ;[02] V - [SDR SWAA2025051465016](https://openairdocs.org/sdr/SWAA2025051465016.md): Scuff Plate · cracked · Apr 28, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD CAREGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] JOB CARD COMPLETED AND INSTALLED ON CUSTOMER CARD TTG8Q00ZSUFL;[02] REPAIRED FCB FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1; NDI NO CRACKS NOTED.;[03] VERIFIED ACTION 2.
JOB COMPLETE. - [SDR SWAA2025051464309](https://openairdocs.org/sdr/SWAA2025051464309.md): Plate · corroded · Apr 25, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > LWR FUSELAGE - ANTENNA COVER PLATE AREA HAS EVIDENCE OF CORROSION AND FILLET SEAL DETERIORATED AT STA 410; STR 27L.<[01] REMOVED AND REPLACED THE LWR FUSELAGE - ANTENNA COVER PLATE STA 410; STR 27L; IAW SRM 51-40-02 AND DWG #143A3230 REV A.;[02] VERIFIED ACTIO - [SDR SWAA2025051456877](https://openairdocs.org/sdr/SWAA2025051456877.md): Floorbeam · cracked · Apr 25, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-64 LOT 1601361-1 AT STA 540; BL 0 TO RBL 24.75 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -.;[02] UPDATED MEASUREMENTS TAB - [SDR SWAA2025051456875](https://openairdocs.org/sdr/SWAA2025051456875.md): Floorbeam · cracked · Apr 25, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-63 LOT 1602100-2 AT STA 540; BL 0 TO LBL 24.75 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -.;[02] UPDATED MEASUREMENTS TAB - [SDR SWAA2025051456870](https://openairdocs.org/sdr/SWAA2025051456870.md): Panel · delaminated · Apr 24, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Structure > PANEL 193D HAS DELAMINATION ON INNER SURFACE CORE<[01] DELAMINATION TO INNER SURFACE CORE OF PANEL 193D WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051356866](https://openairdocs.org/sdr/SWAA2025051356866.md): Support Angle · corroded · Apr 21, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT ANGLE ACB STA-767 TO 790 RBL-25 COMMON TO FWD SHIELD.<[01] REMOVED AND REPLACED NEW ON SUPPORT ANGLE ACB BS767 TO BS 787 RBL 25 IAW SRM 51-40-02 AND DWG 146A8123 ID: 0016 REV: -;[02] VERIFIED CORECTIVE ACTION;[03] VERIFIED CORECTIVE ACTION - [SDR SWAA2025051456818](https://openairdocs.org/sdr/SWAA2025051456818.md): Floorbeam · corroded · Apr 16, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLES AT RBL 27.5; RBL31.5; RBL35.5 AND RBL 43 WL208.1<[01] REPAIRED PASSENGER CABIN FLOOR BEAM BS 986 IAW SRM 53-70-51-2R-4 REPAIR-4;[02] COMPLETE;[03] VERIFY JOB COMPLETE;[04] COMPLETE - [SDR SWAA2025051441158](https://openairdocs.org/sdr/SWAA2025051441158.md): Vapor Barrier · cracked · Apr 16, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Bulkhead > R/H VAPOR BARRIER CRACKED AT BS 663<[01] R/H VAPOR BARRIER CRACK AT BS 663 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051441159](https://openairdocs.org/sdr/SWAA2025051441159.md): Vapor Barrier · cracked · Apr 16, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Bulkhead > L/H VAPOR BARRIER CRACKED AT BS 663<[01] L/H VAPOR BARRIER CRACK AT BS663 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051456819](https://openairdocs.org/sdr/SWAA2025051456819.md): Seal · cracked · Apr 16, 2025 · N293WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.
USED TOOL: SCREW GUN
ID: PER2472
CAL DUE: 08/2025;[02] VERIFIED COMPLETION ACTION 1 - [SDR SWAA2025051456782](https://openairdocs.org/sdr/SWAA2025051456782.md): Support Angle · cracked · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > WATER SERVICE PAN AFT SUPPORT ANGLE CRACKED AT APPROX. STA 907+15 (MARKED)<[01] REMOVED AND REPLACED WATER SERVICE PAN AFT SUPPORT ANGLE AT APPROX. STA 907+15 PER B737-700 SRM 51-40-02-OG AND BOEING DWG 147A7221 REV. F.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; - [SDR SWAA2025051456786](https://openairdocs.org/sdr/SWAA2025051456786.md): Web · canning · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB SUB THRESHOLD WEB AT MULTIPLE AREAS<[01] REMOVED AND REPLACED ACB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340; ID: 0024 REV: A.;[02] VERIFIED ACTION 1.
JOB COMPLETE. - [SDR SWAA2025051456780](https://openairdocs.org/sdr/SWAA2025051456780.md): Support · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT STA 747+10; LBL 25<[01] THIS CARD WILL BE ACCOMPLISHED ON TASK CARD # TTG8Q00ZV5YL
FOR REPLACEMENT PART.;[02] VERIFIED;[03] VERIFIED - [SDR SWAA2025051456791](https://openairdocs.org/sdr/SWAA2025051456791.md): Shield · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY DOOR CUT-OUT FWD SHIELD AT STA 420+2; 420+9; 420+17; WL 156; RBL 24.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY DOOR CUT-OUT FWD SHIELD FROM BS420 TO BS440 RBL24 IAW SRM 51-40-02 AND DWG 143A0080 ID:0023 REV: -;[02] CORRECTIVE AC - [SDR SWAA2025051456783](https://openairdocs.org/sdr/SWAA2025051456783.md): Shield · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA 500+12 AND 500+16; WL 156; RBL 24.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD FROM BS492 TO BS500A RBL24 IAW SRM 51-40-02 AND DWG 143A0080 ID: 0023 REV: -;[02] VERIFIED ACTIO - [SDR SWAA2025051456800](https://openairdocs.org/sdr/SWAA2025051456800.md): Web · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO SUB-THRESHOLD WEB FROM STA 440+6 TO 480+9 RBL 25 TO RBL 28; WL 156.<[01] REMOVED AND REPLACED NEW ON FWD CARGO SUB-THRESHOLD WEB BS440 TO BS492.4 RBL 25 TO RBL28 WL 156 IAW SRM 51-40-02 AND DWG 143A8330 ID: 0042 REV: A;[02] CORRECTIVE AC - [SDR SWAA2025051456766](https://openairdocs.org/sdr/SWAA2025051456766.md): Floor Support · cracked · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL AT STA 324; RBL 30; WL 208.1<[01] REMOVED AND INSTALLED AT DISCREPANCY AREA NEW INTERCOSTAL PN:141A5410U140ATSMRO; LOT#1598453-1 PER DWG#141A5410; DWG141A5400 REV:_ SRM 51-40-05-0G-0; SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025051456815](https://openairdocs.org/sdr/SWAA2025051456815.md): Seal · cracked · Apr 15, 2025 · N293WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > LT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL
PER AMM 53-31-31-000-802. (REMOVAL)
PER AMM 53-31-31-400-802. (INSTALLATION)
SCREW GUN ID: PER2469 DUE DATE:08/2025;[02] VERIFIED COMPL - [SDR SWAA2025051356788](https://openairdocs.org/sdr/SWAA2025051356788.md): Sidewall Support · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > DAMAGE ON ACB FLOOR TO SIDEWALL SUPPORT STA 787; LBL 25<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT P/N 146A7502-27; LOT 1601300-2 AT ACB BS727 - BS847 LBL25 WL 156 IAW SRM 51-10-02 AND DWG# 146A7500 ID:0085 REV: A.;[02] VERIFIED CORRECTIVE ACTION. CAR - [SDR SWAA2025051356802](https://openairdocs.org/sdr/SWAA2025051356802.md): Floor Panel · pulled · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 222DF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)] - [SDR SWAA2025051356798](https://openairdocs.org/sdr/SWAA2025051356798.md): Floor Panel · pulled · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 222CF FLOOR PANEL UPPER SKIN 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)] - [SDR SWAA2025051356801](https://openairdocs.org/sdr/SWAA2025051356801.md): Floor Panel · pulled · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF 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. - [SDR SWAA2025051356781](https://openairdocs.org/sdr/SWAA2025051356781.md): Shield · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Cargo Compartments > CORROSION ON ACB FWD SHEILD STA 767-792; RBL 25<[01] REMOVED AND REPLACED ACB FWD SHEILD STA 767-794; RBL 25 IAW SRM 51-10-02-0G-0 AND DWG# 146A0081 ID: 0040 REV: A.;[02] VERIFIED INSTALLATION - [SDR SWAA2025051356779](https://openairdocs.org/sdr/SWAA2025051356779.md): Sidewall Support · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT STA 727B+17; 727C+10; 727E+8; 727E+12; 727E+16; 747+7 - 767; RBL 25<[01] REMOVED AND REPLACED AT ACB FLOOR TO SIDE WALL SUPPORT
BETWEEN BS 727 TO BS 767 RBL 25 WL 156
IAW SRM 51-40-02; DWG# 146A7500 REV: A;[02 - [SDR SWAA2025051356789](https://openairdocs.org/sdr/SWAA2025051356789.md): Sidewall Support · corroded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 460 TO 500D; LBL 24; WL 156.<[01] REMOVED AND REPLACED NEW ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS400 TO BS500D LBL24 TO IAW SRM 51-40-02 AND DWG 143A7500 ID: OO71 REV: -;[02] VERIFIED CORRECT - [SDR SWAA2025051356771](https://openairdocs.org/sdr/SWAA2025051356771.md): Floor Panel · pulled · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241ZF FLOOR PANEL UPPER SKIN 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)] - [SDR SWAA2025051356769](https://openairdocs.org/sdr/SWAA2025051356769.md): Floor Panel · debonded · Apr 15, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > AFT FLOOR PANEL 241XF UPPER SKIN HAS A PREVIOUS REPAIR THAT IS DISBONDED. (MARKED)<[01] 241XF FLOOR PANEL UPPER SKIN 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)] - [SDR SWAA2025051456764](https://openairdocs.org/sdr/SWAA2025051456764.md): Stub Frame · cracked · Apr 14, 2025 · N293WN · Boeing 7377H4 · Service Doors > CRACK FOUND ON FSD STUB FRAME AT BS 291.5+8;.2' ABOVE SEAL DEPRESSOR; 1.6' IN LENGTH<[01] EVALUATED DAMAGE; NO ALLOWABLE DAMAGE FOUND AT SRM; UPPER STUB FRAME TO BE REPAIRABLE BY REPLACEMENT PER SRM 51-10-02; STEP 9. REMOVED FWD SERVICE DOOR UPPER STUB FRAME - [SDR SWAA2025051456759](https://openairdocs.org/sdr/SWAA2025051456759.md): Floorbeam · corroded · Apr 14, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLE RBL 43; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACTION COMPLETED.;[03] CHANGED MEASUREMENTS FIELD ON RII TO NO AND MAJOR REPAIR TO NO DAMAGE REPAIRED O - [SDR SWAA2025051456760](https://openairdocs.org/sdr/SWAA2025051456760.md): Floorbeam · corroded · Apr 14, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 35.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACTION COMPLETED. - [SDR SWAA2025051456761](https://openairdocs.org/sdr/SWAA2025051456761.md): Floorbeam · corroded · Apr 14, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 31.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACTION COMPLETED. - [SDR SWAA2025051456762](https://openairdocs.org/sdr/SWAA2025051456762.md): Floorbeam · corroded · Apr 14, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CORROSION ON BS986 FLOOR BEAM AT BOTTOM SIDE OF NUTPLATE HOLE RBL 27.5; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACTION COMPLETED. - [SDR SWAA2025051456690](https://openairdocs.org/sdr/SWAA2025051456690.md): Vapor Barrier · cracked · Apr 11, 2025 · N293WN · Boeing 7377H4 · Wing Main, Frame Structure > R/H VAPOR BARRIER CRACKED AT BS 663<[01] REMOVED; REINSTALLED AND RAPAIRED VAPOR BARRIER IAW B737-7 SRM 51-40-02-0G-0 DWG 111A1000 ID: 0259 REV: A AND REINSTALLED ALL PARTS TO FOM.;[02] COMPLETE;[03] COMPLETE;[04] VERIFIED;[05] ALL REPAIR WORK ACCOMPLISHED ON - [SDR SWAA2025051456694](https://openairdocs.org/sdr/SWAA2025051456694.md): Vapor Barrier · cracked · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Main, Bulkhead > L/H VAPOR BARRIER CRACKED AT BS 663<[01] L/H VAPOR BARRIER BS663 REPAIRED IN TTG8Q00ZWLU7;[02] REMOVED AND REINSTALLED L/H VAPOR BARRIER AT BS 663 LBL6-LBL70 IAW SRM 51-40-02 & DWGS 111A1000 ID:0259 REV: A;[03] VERIFIED ACTION 2.
JOB COMPLETE. - [SDR SWAA2025051356692](https://openairdocs.org/sdr/SWAA2025051356692.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 242PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242PF 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. - [SDR SWAA2025051356691](https://openairdocs.org/sdr/SWAA2025051356691.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241WF 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. - [SDR SWAA2025051356688](https://openairdocs.org/sdr/SWAA2025051356688.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241VF 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. - [SDR SWAA2025051356687](https://openairdocs.org/sdr/SWAA2025051356687.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR 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. - [SDR SWAA2025051356682](https://openairdocs.org/sdr/SWAA2025051356682.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE. - [SDR SWAA2025051356681](https://openairdocs.org/sdr/SWAA2025051356681.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF WAS REPLACED. FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0 & BOEING DWG 144A5810 ID 0189.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025051356680](https://openairdocs.org/sdr/SWAA2025051356680.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)] - [SDR SWAA2025051356679](https://openairdocs.org/sdr/SWAA2025051356679.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0. - [SDR SWAA2025051356678](https://openairdocs.org/sdr/SWAA2025051356678.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232RF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0. - [SDR SWAA2025051356677](https://openairdocs.org/sdr/SWAA2025051356677.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231ZF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)] - [SDR SWAA2025051356684](https://openairdocs.org/sdr/SWAA2025051356684.md): Floor Panel · pulled · Apr 11, 2025 · N293WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231YF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)] Next page: https://openairdocs.org/aircraft/N293WN/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 = 'N293WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N293WN/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.