# Service difficulty reports: N935WN, cancelled Oct 3, 2025 A list on [N935WN, cancelled Oct 3, 2025](https://openairdocs.org/deregistered/N935WN-2025-10-03.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 · 237 reports - [SDR SWAA2025011384955](https://openairdocs.org/sdr/SWAA2025011384955.md): Scuff Plate · cracked · Jan 11, 2025 · N935WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FSD SCUFF PLATE IS LEAKING DURING PRESSURIZATION AFT THE AFT EDGE (SCUFF PLATE IS CRACKED)<[01] UPDATED STEPS 1.2.;[02] COMPLETED STEPS 2;[03] FSD SCUFF PLATE LEAK CHECK WILL BE ACCOMPLISHED ON FAULT# TTG8Q00Y3RXH - [SDR SWAA2025010983903](https://openairdocs.org/sdr/SWAA2025010983903.md): Battery Pack · inoperative · Jan 8, 2025 · N935WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674 AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805. - [SDR SWAA2025010983904](https://openairdocs.org/sdr/SWAA2025010983904.md): Battery Pack · inoperative · Jan 8, 2025 · N935WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1675 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1675 AND PERFORMED SATISFACTORY INSTALLATION TEST PER AMM 33-51-06-960-805. - [SDR SWAA2025010983902](https://openairdocs.org/sdr/SWAA2025010983902.md): Drip Tray · cracked · Jan 8, 2025 · N935WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure > HORIZONTAL STAB FWD DRUM DRIP SHIELD CRACKED. DRIP SHIELD WILL BE INSTALLED ON TASK CARD. - [SDR SWAA2025010979623](https://openairdocs.org/sdr/SWAA2025010979623.md): Floorbeam · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED CRACKED PART.
LOCATED AND DRILLED NEW PART;[02] REJECT - CORRECTIVE ACTION ENTRY 1.; NO REFERENCE DOCUMENTED FOR REMOVAL OF PART; NO DOCUMENTATION OR REFERENCE FOR INSTALLATION OF PLATE (143A52 - [SDR SWAA2025010979603](https://openairdocs.org/sdr/SWAA2025010979603.md): Stringer Clip · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727B STR 6L<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727B STR 6L IAW SRM 51-40-02-0G-0 AND DWG 146A1102;[02] REMOVED AND REPLACED STRINGER CLIP AT BS 727B STR 6L IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV:-;[03] VERIFIED CORREC - [SDR SWAA2025010979610](https://openairdocs.org/sdr/SWAA2025010979610.md): Stringer Clip · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727B STR 5L<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727B STR 5L IAW SRM 51-40-02-0G-0 AND DWG 146A1102;[02] REMOVED AND REPLACED STRINGER CLIP AT BS 727B STR 5L IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV:-;[03] VERIFIED CORREC - [SDR SWAA2025010979614](https://openairdocs.org/sdr/SWAA2025010979614.md): Stringer Clip · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727E STR 6L<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E STR 6L IAW SRM 51-40-02-0G-0 AND DWG 146A1112;[02] REMOVED AND REPLACED STRINGER CLIP AT BS 727E STR 6L IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV:-;[03] VERIFIED CORREC - [SDR SWAA2025010979616](https://openairdocs.org/sdr/SWAA2025010979616.md): Stringer Clip · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727E STR 5L<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E STR 5L IAW SRM 51-40-02-0G-0 AND DWG 146A1112;[02] REMOVED AND REPLACED STRINGER CLIP AT BS 727B STR 5L IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV:-;[03] REMOVED AND REP - [SDR SWAA2025010979618](https://openairdocs.org/sdr/SWAA2025010979618.md): Stringer Clip · cracked · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP AT BS 727E STR 6R<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E STR 6R IAW SRM 51-40-02-0G-0 AND DWG 146A1112;[02] REMOVED AND REPLACED STRINGER CLIP AT BS 727E STR 6R IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV:-;[03] VERIFIED CORREC - [SDR SWAA2025010879253](https://openairdocs.org/sdr/SWAA2025010879253.md): Strap · corroded · Dec 19, 2024 · N935WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 767+5 RBL 10 TO LBL 14 WL 156<[01] EVALUATED CORROSION ON FLOOR T STRAP BS 767+5 RBL 10 TO LBL 14 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] RECE - [SDR SWAA2025010978992](https://openairdocs.org/sdr/SWAA2025010978992.md): Bulkhead · cracked · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Bulkhead > 663 COMPOSITE BULKHEAD RH WHEEL WELL CRACKED (MARKED)<[01] R/H COMPOSITE BULKHEAD PANEL BS663 CRACK WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025010979239](https://openairdocs.org/sdr/SWAA2025010979239.md): Web · corroded · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED AND REPLACED SUB THRESHOLD WEB AT BS 794 TO 847 RBL 26 WL 156 PER SRM 51-40-02-0G-0 AND DWG 146A8340 REV: -.;[02] VERIFIED CORRECTIVE ACTIO - [SDR SWAA2025010979245](https://openairdocs.org/sdr/SWAA2025010979245.md): Skin · cracked · Dec 18, 2024 · N935WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17.5' FROM FWD EDGE;.4' IN LENGTH (MARKED)<[01] REPAIRED RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17.5' FROM FWD EDGE IAW SRM 10-01-2R-11 REPAIR 11.;[02] VERIFIED ACTION ITEMS A - [SDR SWAA2025010879212](https://openairdocs.org/sdr/SWAA2025010879212.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231XF TOP SURFACE IS DELAMINATING<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 231XF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-21.;[02] VERIFIED CORRECTIVE ACTION 1 - [SDR SWAA2025010879213](https://openairdocs.org/sdr/SWAA2025010879213.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231ZF TOP SURFACE IS DELAMINATING<[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)]

ATTACHED CURE SHEET TO THIS FAULT.;[02] - [SDR SWAA2025010879227](https://openairdocs.org/sdr/SWAA2025010879227.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241BF TOP SURFACE IS DELAMINATING<[01] REPLACED PASSENGER CABIN FLOOR PANEL 241BF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025010879215](https://openairdocs.org/sdr/SWAA2025010879215.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241DF TOP SURFACE IS DELAMINATING<[01] FLOOR PANEL 241DF WITH TOP SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0128 - [SDR SWAA2025010879216](https://openairdocs.org/sdr/SWAA2025010879216.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 232RF TOP SURFACE IS DELAMINATING<[01] UPDATED STEP 1.;[02] STEP 1;[03] COMPLETED STEP 1;[04] DAMAGE FOUND TO BE OUT OF LIMITS; REPLACED CABIN FLOOR PANEL 232RF PER SRM 53-00-50-2R-0;[05] VERIFIED CORRECTIVE ACTION ITEM 4. - [SDR SWAA2025010879217](https://openairdocs.org/sdr/SWAA2025010879217.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 232SF TOP SURFACE IS DELAMINATING<[01] REPLACED PASSENGER CABIN FLOOR PANEL 232SF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. - [SDR SWAA2025010879218](https://openairdocs.org/sdr/SWAA2025010879218.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242DF TOP SURFACE IS DELAMINATING<[01] PANEL 242DF WAS REPLACED DUE TO EXCESSIVE TOP SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 AND AIPC 53-21-00-42A ITEM 135;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE. - [SDR SWAA2025010879219](https://openairdocs.org/sdr/SWAA2025010879219.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242CF TOP SURFACE IS DELAMINATING<[01] PASSENGER CABIN FLOOR PANEL 242CF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM #125.;[02] VERIFIED JOB COMPLETE - [SDR SWAA2025010879228](https://openairdocs.org/sdr/SWAA2025010879228.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242BF TOP SURFACE IS DELAMINATING<[01] PASSENGER CABIN FLOOR PANEL 242BF WAS REPLACED DUE TO EXCESSIVE TOP SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM #85.;[02] VERIFIED JOB COMPLETE - [SDR SWAA2025010879220](https://openairdocs.org/sdr/SWAA2025010879220.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242AF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 242AF IAW AMM 53-21-00-000-801;[02] REPLACED PASSENGER CABIN FLOOR PANEL 242AF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] R - [SDR SWAA2025010879221](https://openairdocs.org/sdr/SWAA2025010879221.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231AF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 231AF IAW AMM 53-21-00-000-801;[02] REMOVED AND REPLACED CABIN FLOOR PANEL 231AF TOP SURFACE IS DELAMINATING PER AMM 53-21-00-400-801; TORQUE INFO: CAL. DATE: JULY 24 2024 CAL. - [SDR SWAA2025010879222](https://openairdocs.org/sdr/SWAA2025010879222.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231KF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 231KF IAW AMM 53-21-00-000-801;[02] FABRICATION OF NEW 231KF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT - [SDR SWAA2025010879229](https://openairdocs.org/sdr/SWAA2025010879229.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231DF TOP SURFACE IS DELAMINATING<[01] UPDATED STEP 1;[02] OK TO RE-INSTALL;[03] COMPLETED STEP 1;[04] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED. - [SDR SWAA2025010879223](https://openairdocs.org/sdr/SWAA2025010879223.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 231GF TOP SURFACE IS DELAMINATING<[01] UPDATED STEP 1;[02] UPDATED STEP 1;[03] REMOVED; FABRICATED AND INSTALLED CABIN FLOOR PANEL 241KF IAW AMM 53-21-00-000-801 SRM 53-00-50-2R-0 AND AMM 53-21-00-400-801.;[04] VERIFIED CARD COMPLETE - [SDR SWAA2025010879224](https://openairdocs.org/sdr/SWAA2025010879224.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242HF TOP SURFACE IS DELAMINATING<[01] REMOVEDCABIN FLOOR PANEL 242HF IAW AMM 53-21-00-000-801;[02] REMOVED CABIN FLOOR PANEL 242HF IAW AMM 53-21-00-000-801;[03] UPDATED STEP 2;[04] PASSENGER CABIN FLOOR PANEL 242HF WAS REPLACED DUE TO EXCESS - [SDR SWAA2025010879230](https://openairdocs.org/sdr/SWAA2025010879230.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241KF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 241KF IAW AMM 53-21-00-000-801;[02] FABRICATION OF NEW 241KF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - [SDR SWAA2025010879231](https://openairdocs.org/sdr/SWAA2025010879231.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242MF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 242MF IAW AMM 53-21-00-000-801;[02] REPLACED PASSENGER CABIN FLOOR PANEL 242MF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] U - [SDR SWAA2025010879225](https://openairdocs.org/sdr/SWAA2025010879225.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 242NF TOP SURFACE IS DELAMINATED. REMOVED CABIN FLOOR PANEL 242NF IAW AMM 53-21-00-000-801. REPLACED CABIN FLOOR PANEL 242NF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-63A ITEM 265 AND MAINTENANCE WAS ACCOMPLISHED ON STEPS 1-2 - [SDR SWAA2025010879232](https://openairdocs.org/sdr/SWAA2025010879232.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241RF TOP SURFACE IS DELAMINATED. REMOVED CABIN FLOOR PANEL 241RF IAW AMM 53-21-00-000-801. FABRICATION OF NEW 241RF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938. REMOVED; FABRICATED AND INSTALLED CABIN FLOO - [SDR SWAA2025010879233](https://openairdocs.org/sdr/SWAA2025010879233.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241SF TOP SURFACE IS DELAMINATING. REMOVED CABIN FLOOR PANEL 241SF IAW AMM 53-21-00-000-801; REPLACED PASSENGER CABIN FLOOR PANEL 241SF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9 AND REMOVED AND RE-INSTALLED NEW CABIN FLOOR PANEL - [SDR SWAA2025010879226](https://openairdocs.org/sdr/SWAA2025010879226.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241UF TOP SURFACE IS DELAMINATING<[01] REMOVED CABIN FLOOR PANEL 241UF IAW AMM 53-21-00-000-801;[02] REPLACED PASSENGER CABIN FLOOR PANEL 241UF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] O - [SDR SWAA2025010879214](https://openairdocs.org/sdr/SWAA2025010879214.md): Floor Panel · delaminated · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Floor Panel > CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATING<[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)]

ATTACHED CURE SHEET TO THIS FAULT.;[02] - [SDR SWAA2025010879236](https://openairdocs.org/sdr/SWAA2025010879236.md): Attach Angle · corroded · Dec 18, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED; REPLACED AND IN - [SDR SWAA2025010879238](https://openairdocs.org/sdr/SWAA2025010879238.md): Shield · corroded · Dec 18, 2024 · N935WN · Boeing 7377H4 · 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 INSTALLED AFT CARGO BAY SHIELD FWD BS767 TO BS794 RBL22 LW156 PER SRM 51-40-02-0G-0 AND DWG. 146A0081 REV:-.;[02] VERIFIED CORRECTIVE - [SDR SWAA2025010879240](https://openairdocs.org/sdr/SWAA2025010879240.md): Sidewall Support · corroded · Dec 18, 2024 · N935WN · Boeing 7377H4 · 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] REMOVED AND INSTALLED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE AT BS 727 TO BS 847 LBL 22 WL 156 PER SRM 51-40-02-0G-0 A - [SDR SWAA2025010879242](https://openairdocs.org/sdr/SWAA2025010879242.md): Support · corroded · Dec 18, 2024 · N935WN · Boeing 7377H4 · 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] REMOVED AND INSTALLED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE AT BS 727 TO BS 767 RBL 22 WL 156 PER SRM 51-40-02-0G - [SDR SWAA2025010978575](https://openairdocs.org/sdr/SWAA2025010978575.md): Attach Angle · cracked · Dec 17, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] REMOVED DAMAGE AND INSTALLED A REPAIR AS PER SRM 57-10-10-2R-5.;[02] VERIFIED CORRECTIVE ACTION STEP 1. - [SDR SWAA2025010978781](https://openairdocs.org/sdr/SWAA2025010978781.md): Doubler · cracked · Dec 17, 2024 · N935WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > EGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] TRIMMED; FABRICATED PARTS AND REPAIRED THE EGPR SURROUND DOUBLER BS233 WL175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARG 4(B-M) AND SRM 51-40-02-0G-0 - [SDR SWAA2024121074770](https://openairdocs.org/sdr/SWAA2024121074770.md): Power Supply · inoperative · Dec 7, 2024 · N935WN · Boeing 7377H4 · Emergency Lighting > R/H OVERWING EXT EMERGENCY LIGHT INOP.<[01] R/R R/H EMERGENCY EXIT ROW LIGHTS POWER SUPPLY IAW AMM 33-51-06. - [SDR SWAA2024101146173](https://openairdocs.org/sdr/SWAA2024101146173.md): Isolation Mount · cracked · Oct 8, 2024 · N935WN · Boeing 7377H4 · Escape Slide > FWD SERVICE DOOR AFT UPPER SLIDE MOUNT ISOLATOR CRACKED<[01] R&R FWD SERVICE DOOR AFT UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.;[02] INSP C/W - [SDR SWAA2024052287809](https://openairdocs.org/sdr/SWAA2024052287809.md): Bulb · inoperative · May 20, 2024 · N935WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY AREA LIGHT AT SEAT 8D IS INOP.<[01] R&R EMERGENCY AREA LIGHT BULB AT SEAT 8D PER AMM 33-51-03 - [SDR SWAA2023060956323](https://openairdocs.org/sdr/SWAA2023060956323.md): Light · inoperative · Jun 6, 2023 · N935WN · Boeing 7377H4 · Emergency Lighting > R/H OVERWING EXIT FWD EMERGENCY LIGHT INOP<[01] R&R R/H OVERWING EXIT LIGHT PER AMM 33-51-01 - [SDR SWAA2023052451027](https://openairdocs.org/sdr/SWAA2023052451027.md): Lens · missing · May 23, 2023 · N935WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT LENS COVER MISSING AT 1 ABC<[01] OK TO CONT PER MEL 33-15-02 SP1 AUTH 135907;[02] INSTALLED NEW LENS AS REQUIRED PER MM 33-51-03 - [SDR SWAA2023052451327](https://openairdocs.org/sdr/SWAA2023052451327.md): Lens · missing · May 23, 2023 · N935WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT LENS COVER AT 1ABC MISSING<[01] REPLACED MISSING LENS AT 1 ABC IAW AMM 33-51-02 - [SDR SWAA2023022409406](https://openairdocs.org/sdr/SWAA2023022409406.md): Cover · loose · Feb 23, 2023 · N935WN · Boeing 7377H4 · Emergency Lighting > 14/15/16DEF OVERHEAD BIN BULLNOSE IS HANGING DOWN AND EMERGENCY LIGHT LENS IS NOT SECURED IN PLACE.<[01] SECURED BULLNOSE PANEL TO STRUCTURE AND SECURED EMER LIGHT LENS COVER @ LOCATION 14-16DEF IAW AMM 25-24-31.;[02] C/W - [SDR SWAA2023010386055](https://openairdocs.org/sdr/SWAA2023010386055.md): Connector · loose · Dec 28, 2022 · N935WN · Boeing 7377H4 · Light System Wiring > MAIN CABIN EMRGENCY LIGHTS L2 DOOR OFF<[01] RE-SECURED CONNECTOR BATTERY PACK M1672 AS PER REFERENCE AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST EMERGENCY LIGHT DOOR L2. TEST NORMAL OPERATION.;[02] VERIFIED STEP 1 Next page: https://openairdocs.org/deregistered/N935WN-2025-10-03/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 = 'N935WN' AND deregistration_id = 'N935WN-2025-10-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N935WN-2025-10-03/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.