# Service difficulty reports: N258WN

A list on [N258WN](https://openairdocs.org/aircraft/N258WN.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 · 283 reports

- [SDR SWAA2026091701651](https://openairdocs.org/sdr/SWAA2026091701651.md): Lens · missing · Sep 13, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN MID CABIN ON THE CEILING IS MISSING ON ONE SIDE FOUND AND INSTALLED MID CABIN EMERGENCY EXIT SIGN LENS IN REFERENCE TO AMM 33-51-01.
- [SDR SWAA2026051903314](https://openairdocs.org/sdr/SWAA2026051903314.md): Elec Connector · disconnected · May 15, 2026 · N258WN · Boeing 7377H4 · Light System Wiring
  > RIGHT OVERWING EXIT SLIDE LIGHT DOES NOT ILLUMINATE. REPLACED LAMP, VERIFIED GOOD FUSES, AND PERFORMED FUNCTIONAL TEST OF RIGHT OVERWING EXIT SLIDE LIGHT IAW AMM 33-51-04-960-801 AND AMM 33-51-06-06-960-804. LIGHT STILL INOPERATIVE. PERFORMED POWER AND GRO
- [SDR SWAA2026051903315](https://openairdocs.org/sdr/SWAA2026051903315.md): Cover · missing · May 15, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > FORWARD SERVICE DOOR EXIT INDICATOR SIGN MISSING COVER UPPER LAMP INOPERATIVE. REMOVED; REPLACED LAMPS; INSTALLED COVER; AND PERFORMED GOOD INSTALLATION TEST OF FWD SERVICE DOOR EXIT INDICATOR IAW AMM 33-51-01-960-801.
- [SDR SWAA2026051997372](https://openairdocs.org/sdr/SWAA2026051997372.md): Bulb · inoperative · May 10, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 23CBA DOES NOT ILLUMINATE. REPLACED LIGHT BULB IN EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 23CBA AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-03-960-801.
- [SDR SWAA2026051996232](https://openairdocs.org/sdr/SWAA2026051996232.md): Scuff Plate · cracked · May 6, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FSD SCUFF PLATE IS CRACKED. WELDED THE SCUFF PLATE IAW SRM 53-10-15-2R-2 STEP 4.B.(4). INSTALLED FSD SCUFF PLATE IAW AMM 53-11-01-420-801, SRM 53-10-15-2R-2, AND CUSTOMER CARD TTG8Q003P50Z STEP 10.
- [SDR SWAA2026051994317](https://openairdocs.org/sdr/SWAA2026051994317.md): Baffle · cracked · Apr 30, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB BAFFLE BS 500 - 500A, LBL 21 CRACKED. REMOVED AND REPLACED ON FCB BAFFLE IAW SRM 51-40-02, AND DWG 143A7505 0117, REV -.
- [SDR SWAA2026051994319](https://openairdocs.org/sdr/SWAA2026051994319.md): Baffle · damaged · Apr 30, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB BAFFLE BS 500A - 500B, LBL 21 HAS ELONGATED FASTENER HOLES. REMOVED AND REPLACED ON FCB BAFFLE IAW SRM 51-40-02 AND DWG 143A7505 0118, REV -.
- [SDR SWAA2026051993853](https://openairdocs.org/sdr/SWAA2026051993853.md): Vapor Barrier · cracked · Apr 28, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > BS 663 VAPOR BARRIER RH UPPER ATTACH FILLER IS CRACKED. REMOVED AND FABRICATED FILLER IAW SRM 51-40-05 AND DWG 111A1601 REV-.
- [SDR SWAA2026051993854](https://openairdocs.org/sdr/SWAA2026051993854.md): Doubler · cracked · Apr 28, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Structure
  > BS 663 VAPOR BARRIER RT UPPER ATTACH DOUBLER IS CRACKED. REMOVED AND FABRICATED DOUBLER IAW SRM 51-40-05 AND DWG 111A1521 REV -.
- [SDR SWAA2026051993490](https://openairdocs.org/sdr/SWAA2026051993490.md): Stub Frame · cracked · Apr 28, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Frame
  > FSD STUB FRAME IS CRACKED AT BS 296; BETWEEN STR 8 AND 9 RT; CRACK IS 0.6' LONG LOCATED IN THE FRAME JOGGLE AREA LOCATED ABOVE THE TOP END OF THE SEAL DEPRESSOR; CONTACT ENGINEERING VIA THE TSR POLICY NOTE THE CRACK WAS FOUND USING HFEC. REMOVED AND REPLACED
- [SDR SWAA2026051992975](https://openairdocs.org/sdr/SWAA2026051992975.md): Support Angle · cracked · Apr 25, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ECS BAY TEE SUPPORT ANGLE IS CRACKED AT BS 650, RBL 41, WL 143. REMOVED AND REPLACED TEE SUPPORT ANGLE BS 650 RBL41; WL143 IAW SRM 51-40-02 AND DWG 149A7210 REV -.
- [SDR SWAA2026051992753](https://openairdocs.org/sdr/SWAA2026051992753.md): Skin · cracked · Apr 24, 2026 · N258WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED RH LOWER HORIZONTAL STAB SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE;.6' IN LENGTH. REMOVED THE DAMAGED PART ON RH HORIZONTAL STAB LOWER SKIN HSS 193.90 18' FROM FWD EDGE; CUT OUT DIMENSIONS 1.7' X 1.0' AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-
- [SDR SWAA2026051992505](https://openairdocs.org/sdr/SWAA2026051992505.md): Support Angle · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT BS 500A+14.5, WL 156, RBL 25. REMOVED AND REPLACED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE RT SIDE IAW SRM 51-40-02-0G-0, AND DWG 143A7500 0058, REV -.
- [SDR SWAA2026051992501](https://openairdocs.org/sdr/SWAA2026051992501.md): Support · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT BS 400+3, 400+7, 440+14, 440+18, 500+5, AND 500A+18, LBL 25, WL 156. REMOVED AND REPLACED FCB L/H SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A7500 0058, REV -.
- [SDR SWAA2026051992757](https://openairdocs.org/sdr/SWAA2026051992757.md): Support · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB LT FLOOR TO SIDEWALL SUPPORT, BS 727 - 847 HAS AREAS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT BS 727 TO 847, LBL 24, WL 158 IAW SRM 51-40-02-0G-0 AND DWG 146A7502, REV -.
- [SDR SWAA2026051992502](https://openairdocs.org/sdr/SWAA2026051992502.md): Threshold Web · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT SUB-THRESHOLD WEB FROM BS 440+8 TO 480+7, RBL 27 - RBL 29, WL 155. REMOEVED AND REPLACED FWD CARGO DOOR CUT-OUT SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A8330 0006, REV B.
- [SDR SWAA2026051992755](https://openairdocs.org/sdr/SWAA2026051992755.md): Sidewall Support · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB FLOOR TO SIDEWALL SUPPORT R/H BS 727-767 HAS AREAS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT BS 727 TO 767, RBL 24, WL 158 IAW SRM 51-40-02-0G-0 AND DWG 146A7502, REV -. REJECTION OF STEP 6 ITEM 3: FLOOR TO SIDEWALL SUPPORT AT RBL 24 HAS 1EA BA
- [SDR SWAA2026051992503](https://openairdocs.org/sdr/SWAA2026051992503.md): Shield · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM BS 420 TO 440, RBL 24, WL 156. REMOVED AND REPLACED ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD BS420 TO BS440 RBL24 IAW SRM 51-40-02 AND DWG 143A0080 0010, REV A.
- [SDR SWAA2026051992504](https://openairdocs.org/sdr/SWAA2026051992504.md): Shield · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD AT STA 500+10; RBL 24; WL 156. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 0027, REV -.
- [SDR SWAA2026051992754](https://openairdocs.org/sdr/SWAA2026051992754.md): Threshold Web · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB SUB THRESHOLD WEB HAS AREAS OF CORROSION. REMOVED AND REPLACED ON ACB SUB THRESHOLD WEB FROM BS 794 TO 847, RBL 22 IAW SRM 51-40-02 AND DWG 146A8340, 0028, REV -.
- [SDR SWAA2026051992756](https://openairdocs.org/sdr/SWAA2026051992756.md): Shield · corroded · Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > R/H FLOOR TO SIDEWALL SUPPORT BS 767-787 HAS AREAS OF CORROSION. REMOVED AND REPLACED SHIELD BS 767 TO 787, RBL 22, WL 158 IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV-.
- [SDR SWAA2026051992495](https://openairdocs.org/sdr/SWAA2026051992495.md): Crossbeam · cracked · Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED PANEL BREAK, BS 540, RBL 2, WL 208. REMOVED AND INSTALLED PANEL BREAK IAW SRM 51-40-02, AND DWG 143A0060, REV-.
- [SDR SWAA2026051992496](https://openairdocs.org/sdr/SWAA2026051992496.md): Crossbeam · cracked · Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED CROSSBEAM BS 540, RBL 26, WL 208. REMOVED AND INSTALLED CROSSBEAM IAW SRM 51-40-02 AND DWG 143A0060, REV-.
- [SDR SWAA2026051992497](https://openairdocs.org/sdr/SWAA2026051992497.md): Attach Angle · cracked · Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED FLOORBEAM ATTACH ANGLE, BS 693, RBL 2, WL 208. REMOVED AND INSTALLED FLOORBEAM ATTACH ANGLE IAW SRM 51-40-02 AND DWG 273A9111, REV-.
- [SDR SWAA2026051991844](https://openairdocs.org/sdr/SWAA2026051991844.md): Stringer · cracked · Apr 22, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-24L WL162. REPAIRED FCB STR 24L BETWEEN BS 500D AND 540 WL162; APPLIED A FILLET SEAL AND CIC IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2026051991842](https://openairdocs.org/sdr/SWAA2026051991842.md): Stringer · cracked · Apr 22, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 535, S26L, WL 153. REPAIRED FCB STR 26L BETWEEN BS 500D AND 540 WL162; APPLIED A FILLET SEAL AND CIC IAW SRM 53-00-03-2R-1 REPAIR 1.
- [SDR SWAA2026051991843](https://openairdocs.org/sdr/SWAA2026051991843.md): Stringer · cracked · Apr 22, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 535 S26R, WL 153. PERFORMED REPAIR AT STR 26L BETWEEN BS 500D - 540 IAW SRM 53-00-03-2R-1, REP 1.
- [SDR SWAA2026051992082](https://openairdocs.org/sdr/SWAA2026051992082.md): Tail Cone · debonded · Apr 22, 2026 · N258WN · Boeing 7377H4 · Aerodynamic Fairings
  > TAIL CONE OUTER SKIN IS DISBONDED 4' FWD OF ACCESS PANEL 318BR, FWD LOWER CORNER. REPAIRED DISBOND TO TAILCONE OUTER SKIN 4' FWD OF ACCESS PANEL 318BR LOWER CORNER IAW SRM 51-70-04-2R-2.
- [SDR SWAA2026051991430](https://openairdocs.org/sdr/SWAA2026051991430.md): Floor Panel · pulled · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2026051991431](https://openairdocs.org/sdr/SWAA2026051991431.md): Floor Panel · pulled · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026051991428](https://openairdocs.org/sdr/SWAA2026051991428.md): Floor Panel · pulled · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026051991429](https://openairdocs.org/sdr/SWAA2026051991429.md): Floor Panel · pulled · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW 241EF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026051991737](https://openairdocs.org/sdr/SWAA2026051991737.md): Seat Track · corroded · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 AT BS480+17; BS500+8; BS500A+7; BS500A+18; BS500B+19; BS500D+9. SEAT TRACK WILL BE REPLACED ON FAULT# TTG8Q01BUUY6. REMOVED DAMAGE ON TOP SURFACE OF SEAT TRACK AT DISCREPANCY AREA; REWORKED AREA: L= 1.5'; W= 0.6'; MAX. MATERIA
- [SDR SWAA2026051991730](https://openairdocs.org/sdr/SWAA2026051991730.md): Seat Track · corroded · Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 25 AT BS480+17; BS500+8; BS500A+7; BS500A+18; BS500B+19; BS500D+9. SEAT TRACK WILL BE REPLACED ON FAULT# TTG8Q01BUUYA. REMOVED DAMAGE ON TOP SURFACE OF SEAT TRACK AT DISCREPANCY AREA; REWORKED AREA: L= 1.5'; W= 0.6'; MAX. MATERI
- [SDR SWAA2026051991424](https://openairdocs.org/sdr/SWAA2026051991424.md): Vapor Barrier · cracked · Apr 20, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > LEFT BS 663 VAPOR BARRIER IS CRACKED. REPAIRED PER SRM 51-70-04-2R-10-A00755, REPAIR 10, REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES.
- [SDR SWAA2026051991425](https://openairdocs.org/sdr/SWAA2026051991425.md): Vapor Barrier · cracked · Apr 20, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > R/H B.S. 663 VAPOR BARRIER IS CRACKED. REPAIRED PER SRM 51-70-04-2R-10-A00755, REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES.
- [SDR SWAA2026042190268](https://openairdocs.org/sdr/SWAA2026042190268.md): Battery Pack · failed · Apr 17, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK LT FAILED CAPACITY CHECK M01669. R & R CABIN EMERGENCY BATTERY PER AMM 33-51-06. INSPECTION C/W, R & R CABIN EMERGENCY BATTERY IAW AMM 33-51-06.
- [SDR SWAA2026042190267](https://openairdocs.org/sdr/SWAA2026042190267.md): Battery Pack · failed · Apr 17, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT BATTERY PACK LT FAILED CAPACITY CHECK M01668. R & R CABIN EMERGENCY BATTERY PER AMM 33-51-06. INSPECTION C/W R&R CABIN EMERGENCY BATTERY PER AMM 33-51-06.
- [SDR SWAA2026042090269](https://openairdocs.org/sdr/SWAA2026042090269.md): Battery · no test · Apr 17, 2026 · N258WN · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR LT EMERGENCY BATTERY PACK FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PER AMM 33-51-06. INSPECTION C/W, R & R CABIN EMERGENCY BATTERY IAW AMM 33-51-06
- [SDR SWAA2025020492875](https://openairdocs.org/sdr/SWAA2025020492875.md): Sign · out of adjust · Feb 3, 2025 · N258WN · Boeing 7377H4 · Emergency Lighting
  > FA'S REPORTED FWD EXIT SIGN FELL OFF AND FA'S REATTACHED IT<[01]. RESECURED FWD CABIN EMERGENCY EXIT SIGN PER SIP.
- [SDR SWAA2024091638132](https://openairdocs.org/sdr/SWAA2024091638132.md): Window · arced · Sep 15, 2024 · N258WN · Boeing 7377H4 · Flight Compartment Windows
  > AT FL 350 FIRST OFFICERS WINDSCREEN STARTED TO ARC AT UPPER RIGHT CORNER. SHORTLY AFTER WINDSCREEN CRACKED FROM UPPER RIGHT CORNER TO LOWER LEFT CORNER.<[01] REMOVED AND REPLACED R! FLIGHT COMPARTMENT WINDOW. REF AMM 56-11-11. OPS NORMAL.
- [SDR SWAA2024061398904](https://openairdocs.org/sdr/SWAA2024061398904.md): Battery Pack · inoperative · Jun 6, 2024 · N258WN · Boeing 7377H4 · Emergency Lighting
  > REFERENCE[TTG8Q00TRMXN]FOUND 3 EMERGENCY LIGHTS INOP EXTERIOR OF AIRCRAFT DURING OPS CHECK<[01] RELAMPED FWD ENTRY DOOR SLIDE LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801<BR><BR>UPON FURTHER INVESTIGATION; FOUND EMERGENCY BATTERY PACK M1
- [SDR SWAA2024061390688](https://openairdocs.org/sdr/SWAA2024061390688.md): Scuff Plate · cracked · May 28, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB FWD CORNER SCUFF PLATE IS CRACKED<[01] EDIT: ADDED CALIBRATED WELDING EQUIPMENT USED IN STEP 2;[02] REPAIRED ACB FWD CORNER SCUFF PLATE PER BAC5975 PT INSPECTED WELDED AREA IAW SOPM 20-20-02. NO DEFECTS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF THE
- [SDR SWAA2024061489708](https://openairdocs.org/sdr/SWAA2024061489708.md): Floor Support · cracked · May 25, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT ANGLE STA-380 TO 400 BL-0 WL-208<[01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE P/N 143A5410-170 LOT: 1563147-3. LOCATED BETWEEN BS 380 - BS 400 BL.0 WL 208. IAW B-737-700 SRM 51-40-02. 7 DWG# 143A5400.;[02] VERIFIED COMPLETE STEP 3; CARD
- [SDR SWAA2024061489907](https://openairdocs.org/sdr/SWAA2024061489907.md): Floor Support · cracked · May 25, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT ANGLE STA-380 TO 400 RBL 9.5' WL-208<[01] REMOVED AND REPLACED FLOOR SUPPORT ANGLE P/N 143A5410-170 LOT: 1563147-2. LOCATE BETWEEN BS 380 - BS 400 RBL 9.5 WL 208. IAW B-737-700 SRM 51-10-02 SRM 51-40-02. AND DWG# 143A5400.;[02] UPDATED M
- [SDR SWAA2024061489457](https://openairdocs.org/sdr/SWAA2024061489457.md): Panel · cracked · May 24, 2024 · N258WN · Boeing 7377H4 · Wing, Plate/Skin
  > RT WING L/E PANEL 621YB CORNER IS CRACKED (MARKED)<[01] CRACKED CORNER ON RT WING L/E PANEL 621YB WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024061388950](https://openairdocs.org/sdr/SWAA2024061388950.md): Floorbeam · cracked · May 22, 2024 · N258WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75<[01] REMOVED AND REPLACED PANEL BREAK ASSY P/N 143A5240-63 LOT 1563941-1 IAW B-737-700; SRM 51-10-02 SRM 51-40-02; DWG# 143A0060.;[02] REMOVED AND REPLACED PANEL BREAK ASSY P/N 14
- [SDR SWAA2024061388949](https://openairdocs.org/sdr/SWAA2024061388949.md): Intercostal · cracked · May 22, 2024 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED FWD OF FWD ENTRY DOOR; BS 295; STR 16L<[01] REMOVED AND REPLACED INTERCOSTAL ON FWD OF FWD ENTRY DOOR BS 295 TO BS 303.9 STR 16L IAW SRM 51-40-02 AND DWG 141A8180 REV.C SHEET 27
- [SDR SWAA2024061498230](https://openairdocs.org/sdr/SWAA2024061498230.md): Frame · worn · May 19, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Frame/Spar/Rib
  > #2 ENGINE STRUT FORWARD FAIRING FRAME HAS WORN AREA (COMMON TO THUMBNAIL UPPER AFT LATCH)<[01] VERIFIED STEP 5 COMPLETE.;[02] VERIFIED STEPS 6 COMPLETE; STEP 7 IN PARTIAL.;[03] VERIFIED STEP 7 COMPLETE AND MEASUREMENT FIELD.;[04] VERIFIED RII STEP COMPLETE.;[0
- [SDR SWAA2024061487783](https://openairdocs.org/sdr/SWAA2024061487783.md): Rub Strip · debonded · May 19, 2024 · N258WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE PYLON UPPER WEB PANEL CUT OUT RUB STRIP DISBONDED (COMMON TO PANEL 433AT)<[01] UPDATED MEASUREMENTS.;[02] REMOVED AND REINSTALLED #1 ENGINE PANEL 433AT CUT OUT RUB STRIP PER AMM 51-51-00-340-803.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2; CARD COMPLE

Next page: https://openairdocs.org/aircraft/N258WN/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 = 'N258WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N258WN/reports

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