# Service difficulty reports: N285WN

A list on [N285WN](https://openairdocs.org/aircraft/N285WN.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 7 · 318 reports

- [SDR SWAA2026101234484](https://openairdocs.org/sdr/SWAA2026101234484.md): Light · inoperative · Oct 6, 2026 · N285WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EMERGENCY EXIT, EXTERNAL EMERGENCY LIGHT NOT WORKING. REPLACED THE EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.
- [SDR SWAA2026080572858](https://openairdocs.org/sdr/SWAA2026080572858.md): Strut · cracked · Aug 1, 2026 · N285WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE TRF STRUT 1 WAS CRACKED AT C-1, 0.28 LONG. MERGED BOTH CRACKS TOGETHER ON ONE WRITE UP TTG8Q01DGQ1X.
- [SDR SWAA2026080594116](https://openairdocs.org/sdr/SWAA2026080594116.md): Strut · cracked · Aug 1, 2026 · N285WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > RIGHT ENGINE TRF STRUT NR 1 IS CRACKED AT C-1 0.28 LONG AND C-2 0.49 LONG. COMPLIED WITH M-21-172-00810 TO TRIGGER EO-7256-I-11716-C THE REPETITIVE INSPECTION INTERVAL OF 1300 CYCLES FOR THE RIGHT ENGINE TRF.
- [SDR SWAA2025100219639](https://openairdocs.org/sdr/SWAA2025100219639.md): Lens · missing · Sep 29, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > R-1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED A NEW LENS IAW MM 33-51-01 OPS CHKD NORMAL
- [SDR SWAA2025060276329](https://openairdocs.org/sdr/SWAA2025060276329.md): Handle · loose · May 30, 2025 · N285WN · Boeing 7377H4 · Galley Doors
  > LOOSE AFT SERVICE DOOR HANDLE. <[01] TIGHTENED LOOSE AFT SERVICE DOOR HANDLE IAW AMM 25-21-25-420-801. STEP 3.B(5); [02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.
- [SDR SWAA2025060276001](https://openairdocs.org/sdr/SWAA2025060276001.md): Battery Pack · inoperative · May 29, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP <[01]. REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTERY PACK IAW AMM 33-51-06-960-805.; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025060274803](https://openairdocs.org/sdr/SWAA2025060274803.md): Battery Pack · failed · May 24, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1670 FAIL<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1670 IAW AMM 33-51-06-960-805;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025060274804](https://openairdocs.org/sdr/SWAA2025060274804.md): Battery Pack · failed · May 24, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1675 FAIL<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1675 IAW AMM 33-51-06-960-805;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025060274802](https://openairdocs.org/sdr/SWAA2025060274802.md): Battery Pack · failed · May 24, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > LIGHT ASSOCIATED WITH EMERGENCY BATTERY PACK M1669 FAIL<[01] REMOVED AND REPLACED BATTERY PACK M1669 AND PERFORMED GOOD TEST IAW AMM 33-51-06-960-805;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025060274531](https://openairdocs.org/sdr/SWAA2025060274531.md): Skin · delaminated · May 23, 2025 · N285WN · Boeing 7377H4 · Trailing Edge Flaps
  > DELAMINATED LOWER SURFACE AFT TRAILING EDGE RH MAIN INB FLAP<[01] OK TO INSTALL;[02] REMOVED AFT TRAILING EDGE RH MAIN I/B FLAP AND INSTALLED NEW AFT TRAILING EDGE RH MAIN I/B FLAP (WEDGE ASSEMBLY) P/N 113A2500-14 IAW AIPC 27-51-11-01B AND AMM 20-50-11-910-801
- [SDR SWAA2025060272385](https://openairdocs.org/sdr/SWAA2025060272385.md): Strip · corroded · May 18, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB 140AF L/H CAPSTRIP CORRODED<[01] REMOVED AND INSTALLED NEW CAPSTRIP ITEM# 453A2611-8; S/N 7253311; PER SRM 51-40-02-0G-0; AMM 25-52-10-000-801; AMM 25-52-10-400-801;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025060272386](https://openairdocs.org/sdr/SWAA2025060272386.md): Strip · corroded · May 18, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB 140CF L/H CAPSTRIP CORRODED<[01] REMOVED AND INSTALLED NEW CAPSTRIP ITEM# 453A2611-4; LOT#1510184-1 PER SRM 51-40-02-0G-0; AMM 25-52-10-000-801; AMM 25-52-10-400-801;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025060272172](https://openairdocs.org/sdr/SWAA2025060272172.md): Light · damaged · May 17, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY CEILING EMERGENCY EXIT LIGHT HOUSING DAMAGED<[01] REMOVED DAMAGED AFT ENTRY CEILING EMERGENCY EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802.;[02] REPLACED AFT ENTRY CEILING EMERGENCY EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802 (PENDING OPERATIONAL CHEC
- [SDR SWAA2025060270164](https://openairdocs.org/sdr/SWAA2025060270164.md): Support Bracket · cracked · May 13, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON SUPPORT BRACKET OVER WHEEL AT BS 692.1 RBL 2 WL 208.1.<[01] REMOVED AND REPLACED SUPPORT BRACKET OVER WHEEL AT BS-692.1; RBL-2; WL-208.1 IAW SRM 51-40-02-0G-0 AND DWG# 273A9111
- [SDR SWAA2025060269360](https://openairdocs.org/sdr/SWAA2025060269360.md): Support Bracket · cracked · May 9, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ON CHORD BS695; RBL2; BELOW UPPER DECK<[01] REPAIRED PER EA 25-153-01245-WIP1;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2025060268958](https://openairdocs.org/sdr/SWAA2025060268958.md): Sign · broken · May 9, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > FWD LAV EMERGENCY EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802. <BR>OPS TEST WILL BE ACCOMPLISHED ON TASK CARD #TTG8Q0103YWN PERFORM OPS CHECK OF INTERIOR LIGHTING.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED;
- [SDR SWAA2025060268959](https://openairdocs.org/sdr/SWAA2025060268959.md): Sign · broken · May 9, 2025 · N285WN · Boeing 7377H4 · Emergency Lighting
  > G-1 EMERGENCY EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT SIGN IAW AMM 33-51-01-960-802. <BR>OPS TEST WILL BE ACCOMPLISHED ON TASK CARD #TTG8Q0103YWN PERFORM OPS CHECK OF INTERIOR LIGHTING.;[02] CORRECTIVE ACTION UPDATED:<BR><BR>REMO
- [SDR SWAA2025060269359](https://openairdocs.org/sdr/SWAA2025060269359.md): Access Panel · cracked · May 9, 2025 · N285WN · Boeing 7377H4 · Passenger/Crew Doors
  > CRACKED ON 831 ACCESS PANEL AT FWD ENTRY DOOR<[01] REMOVED 831DZ ACCESS PANEL IAW AMM 05-41-08-210-807;[02] OK TO CLOSE;[03] COMPLETED. INSTALLED 831DZ ACCESS PANEL IAW AMM 20-50-11-910-801 AND SRM 51-40-02. TOOL USED ID: ATS2248 DUE DATE: 12/2025.;[04] REMOVE
- [SDR SWAA2025060268960](https://openairdocs.org/sdr/SWAA2025060268960.md): Attach Fitting · excess play · May 9, 2025 · N285WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > EXCESSIVE PLAY IN BOTH FWD AND AFT GIRT BAR FLOOR ATTACH FITTINGS AT ASD.<[01] REMOVED AND REPLACED FWD AND AFT GIRT BAR FLOOR ATTACH FITTINGS AT ASD IAW AMM 25-66-02-000-801 (REMOVAL) AND AMM 25-66-02-400-801 (INSTALLATION).;[02] VERIFIED ITEM 1
- [SDR SWAA2025060268534](https://openairdocs.org/sdr/SWAA2025060268534.md): Strap · cracked · May 7, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > STABILIZER STRAP IS CRACKED AT BS312+10 BL0; WL198<[01] REMOVED AND REPLACED STABILIZER STRAP P/N 141A5410-31 BS312 - BS344 BL 0 WL198 IAW SRM 51-40-02 AND DWG 141A5400 REV:-
- [SDR SWAA2025060268109](https://openairdocs.org/sdr/SWAA2025060268109.md): Rib · deformed · May 7, 2025 · N285WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE 331B STIFFENER IS DEFORMED AT LE STA 114<[01] UPON FURTHER INVESTIGATION LIGHTLY DEFORMATION FOUND ON RIB STIFFENER AT L/E STA 114; AND STRAIGHTENED IAW SRM 51-10-02 STEP 5 B. NOT OTHER DEFECTS NOTED PER NDT.;[0
- [SDR SWAA2025060267171](https://openairdocs.org/sdr/SWAA2025060267171.md): Threshold Web · corroded · May 3, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACD; THRESHOLD HAS CORROSION BS 787+20 RBL 24 AND 787+24 RBL 29 (MARKED).<[01] REMOVED AND REPLACED ACB THRESHOLD WEB I.A.W SRM 51-40-02-0G-0 AND DWG 146A8340 ID:0028 REV: -;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025060267164](https://openairdocs.org/sdr/SWAA2025060267164.md): Stiffener · cracked · May 3, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB; ANGLE IS CRACK BEHIND TO WATER SERVICE PANEL BS 907+11 RBL 9 (MARKED).<[01] REMOVED AND INSATLLED NEW STIFFINER ITEM # 147A7221Y32 LOT# 1567118-1 BN 39 PER SRM 51-40-02; DWG# 147A7221 REV:- ALL FAULT COMPLETED;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1
- [SDR SWAA2025060267166](https://openairdocs.org/sdr/SWAA2025060267166.md): Angle · corroded · May 3, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB; ZEE ANGLE HAS SEVERAL SPOTS WITH CORROSION AT BS 727 TO 847 LBL 23 (MARKED).<[01] REMOVED AND REPLACED ON ACB FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 LBL23 IAW SRM 51-40-02 AND DWG 146A7500 ID: 0113 REV: -
- [SDR SWAA2025060267167](https://openairdocs.org/sdr/SWAA2025060267167.md): Angle · corroded · May 3, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB; ZEE ANGLE HAS SEVERAL SPOTS WITH CORROSION AT BS 727 TO 767 RBL 23 (MARKED).<[01] REMOVED AND REPLACED ON ACB; NEW FLOOR TO SIDEWALL SUPPORT LOCATED BTW. STA 727 - STA 767 RBL 23 IAW SRM 51-40-02. DWG. #146A7500 REV: -
- [SDR SWAA2025060267168](https://openairdocs.org/sdr/SWAA2025060267168.md): Shield · corroded · May 3, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB; SUBTHRESHOLD HAS CORROSION AT BS 767 TO 787+7 RBL 23.<[01] VERIFIED OUT OF LIMITS;[02] REMOVED AND REPLACED FWD SHIELD AT BS 767 TO 787+7 RBL 23 IAW SRM 51-40-02 AND DWG 146A0081.
- [SDR SWAA2025060266809](https://openairdocs.org/sdr/SWAA2025060266809.md): Sidewall Support · corroded · May 2, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON SIDEWALL SUPPORT BS500A+14; BS500B+6; BS500B+10; BS500B+18; 500C+2 RBL 24.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS400 TO BS500D LBL24.5 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV: -.;[02] VERIFIED
- [SDR SWAA2025060268108](https://openairdocs.org/sdr/SWAA2025060268108.md): Shield · corroded · May 2, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON AFT SHIELD BS500+9.5 RBL 22 WL 156 (MARKED)<[01] REMOVED AND REPLACED AFT SHIELD AT FCB BS492 TO BS 500A RBL22 WL156 IAW SRM 51-10-02-0G-0 PAR-9. C AND DWG#143A0080 ID: 0011 REV: -;[02] VERIFIED;[03] VERIFIED
- [SDR SWAA2025060266658](https://openairdocs.org/sdr/SWAA2025060266658.md): Fairing · delaminated · May 2, 2025 · N285WN · Boeing 7377H4 · Wing, Control Surfaces
  > PANEL 643EB (#7 CANOE FAIRING CONE) IS DELAMINATED.<[01] RECEIVED NEW PANEL 643EB LOCATED AND DRILLED IAW SRM 51-40-05 AND AIPC 27-51-28-04;;[02] RECEIVED NEW PANEL 643EB LOCATED AND DRILLED IAW SRM 51-40-05 AND AIPC 27-51-28-04; AND DWG 113A9252 REV A;[03] NE
- [SDR SWAA2025060266810](https://openairdocs.org/sdr/SWAA2025060266810.md): Sidewall Support · corroded · May 2, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON SIDEWALL SUPPORT BS500A+6; BS500A+10; BS500A+14; BS500A+18 LBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED FCB SIDEWALL SUPPORT FROM BS 480+10 <BR>BS 500D AND SPLICE REPAIR LBL 24.75 WL 156 I.A.W SRM 51-40-02-0G-0; DWG 143A7500 ID: 0071
- [SDR SWAA2025060266814](https://openairdocs.org/sdr/SWAA2025060266814.md): Floor Support · corroded · May 2, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON FLOOR SUPPORT AFT BULKHEAD BS500C+18 RBL 12; LBL 14.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED NEW FCB FLOOR SUPPORT AFT BULKHEAD BS500D RBL21 TO LBL21 IAW SRM 51-40-02 AND DWG 143A7902 ID: 0209 REV:-;[02] VERIFIED COMPLETION CORRECTIVE ACT
- [SDR SWAA2025060266423](https://openairdocs.org/sdr/SWAA2025060266423.md): Support Frame · cracked · May 1, 2025 · N285WN · Boeing 7377H4 · Aerodynamic Fairings
  > WING TO BODY PANEL SUPPORT HAS CRACK AT BS 500D STR 19R<[01] REMOVE AND REPLACED WING TO BODY PANEL SUPPORT FRAME IAW SRM 51-10-02-0G-0 AND DWG# 116A3118 ID: 0004 REV: A
- [SDR SWAA2025060266420](https://openairdocs.org/sdr/SWAA2025060266420.md): Floor Support · cracked · May 1, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FWD WET AREA BS321 LBL45 WL208. MARKED<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET ARE BS 312-BS328 LBL45 I.A.W. SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] COMPLETE;[03] COMPLETE
- [SDR SWAA2025060266419](https://openairdocs.org/sdr/SWAA2025060266419.md): Floor Support · corroded · May 1, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT FWD WET AREA BS291 BL0 WL208. MARKED<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET ARE BS 277-BS294 BL0 I.A.W. SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] COMPLETE;[03] COMPLETE
- [SDR SWAA2025060266042](https://openairdocs.org/sdr/SWAA2025060266042.md): Floor Panel · pulled · May 1, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241XF WITH AREAS OF PULLED UPPER STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1
- [SDR SWAA2025060266047](https://openairdocs.org/sdr/SWAA2025060266047.md): Floor Panel · pulled · May 1, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AAF WITH AREAS OF UPPER SURFACE PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 147A5810 ID:0008
- [SDR SWAA2025060266051](https://openairdocs.org/sdr/SWAA2025060266051.md): Floor Panel · cracked · May 1, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242XF LOWER SKIN IS CRACKED.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242XF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 220.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025060266041](https://openairdocs.org/sdr/SWAA2025060266041.md): Stub Frame · cracked · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR; BETWEEN S-8R AND S-9R; LENGTH 1.6' (MARKED)<[01] REMOVED AND REPLACED STUB FRAME AT FWD SERVICE DOOR UPPER FWD AREA PER SRM 51-40-02; SRM 53-10-01-2R-6 REP 6 AND DWG 141A8370 REV D;[02] CORRECTIVE
- [SDR SWAA2025060265864](https://openairdocs.org/sdr/SWAA2025060265864.md): Panel · cracked · Apr 30, 2025 · N285WN · Boeing 7377H4 · Elevator, Plate/Skin
  > RT. ELEVATOR HINGE PANEL 344LB CRACKED.<[01] REPAIR OF PANEL ACCOMPLISHED ON WORK ORDER #582623 CUSTOMER PO: P006WAPC;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025060266039](https://openairdocs.org/sdr/SWAA2025060266039.md): Skin · cracked · Apr 30, 2025 · N285WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26' FROM FWD EDGE;.40' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.9; 26' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11;[0
- [SDR SWAA2025060266038](https://openairdocs.org/sdr/SWAA2025060266038.md): Skin · cracked · Apr 30, 2025 · N285WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.40' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON RH HORIZONTAL STABILIZER LOWER SKIN STA 193.9; 18' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11;[0
- [SDR SWAA2025060266040](https://openairdocs.org/sdr/SWAA2025060266040.md): Bear Strap · cracked · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK FOUND ON INNER BEAR STRAP OF FWD GALLEY DOOR(R1); BS 294.5; RBL 52; WL 265 BETWEEN S-8R AND S-9R; LENGTH 2.2' (MARKED)<[01] 'DAMAGE REPAIRED AS PER 737-700 SRM 53-10-01-2R-6 REV 84 FIGURE 202 (REPAIR 6 - TEMPORARY REVISION TR 53-179) AND EA 25-153-01258.
- [SDR SWAA2025060265694](https://openairdocs.org/sdr/SWAA2025060265694.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR 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.
- [SDR SWAA2025060265695](https://openairdocs.org/sdr/SWAA2025060265695.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR 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.;[02] COMPLETED PARTS REMOVED/INST
- [SDR SWAA2025060265689](https://openairdocs.org/sdr/SWAA2025060265689.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF 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 SWAA2025060265690](https://openairdocs.org/sdr/SWAA2025060265690.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF 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 SWAA2025060265691](https://openairdocs.org/sdr/SWAA2025060265691.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 232SF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM 175.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025060265692](https://openairdocs.org/sdr/SWAA2025060265692.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF 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.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025060265693](https://openairdocs.org/sdr/SWAA2025060265693.md): Floor Panel · pulled · Apr 30, 2025 · N285WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 231ZF IAW SRM 51-10-02-0G-0 PAR A9 AND AIPC 53-21-00-42A ITEM 145.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025060265298](https://openairdocs.org/sdr/SWAA2025060265298.md): Scuff Plate · cracked · Apr 28, 2025 · N285WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR R1; SCUFF PLATE HAS A CRACK AT AFT UPPER EDGE AREA (MARKED).<[01] WELDED THE DAMAGED AREA ON SCUFF PLATE USING AMS4954 FILLER ROD LOT NUMBER M798431 PER SRM 53-10-15-2R-2 PARAGRAPH 4.B.(4) REFERRED TO BAC5975 CLASS B.<BR>SCUFF PLATE INSTALLED ON

Next page: https://openairdocs.org/aircraft/N285WN/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 = 'N285WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N285WN/reports

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