# Service difficulty reports: N257WN

A list on [N257WN](https://openairdocs.org/aircraft/N257WN.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 · 305 reports

- [SDR SWAA2026072026224](https://openairdocs.org/sdr/SWAA2026072026224.md): Crossbeam · cracked · Jun 24, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, Structure
  > PANEL BRAKE AT BS 540 RBL 1 TO RBL 25 WL 208 IS CRACK. REMOVED AND REPLACED THE BREAK PANEL AT BS 540 RBL 1 TO RBL 25 WL IAW SRM 51-40--02-0G-0, AND DWG 143A0060, SHEET 46, REV -.
- [SDR SWAA2026071943097](https://openairdocs.org/sdr/SWAA2026071943097.md): Isolator · damaged · Jun 22, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, Structure
  > LEFT EMERGENCY EXIT UPPER LINER ATTACH ISOLATOR IS DAMAGED. R & R LT EMERGENCY EXIT UPPER LINER ATTACH ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2026072063670](https://openairdocs.org/sdr/SWAA2026072063670.md): Crossbeam · cracked · Jun 15, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED PANEL BRAKE AT LBL 1 BS 540 WL 208. REMOVED AND REPLACED BREAK PANEL AT LBL 1 BS 540 WL 208 IAW SRM 51-40-02-OG-0 AND DWG 143A0060 SHEET:46 REV-.
- [SDR SWAA2026072077412](https://openairdocs.org/sdr/SWAA2026072077412.md): Bulkhead · cracked · Jun 12, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACKED LOWER RT COMPOSITE BULKHEAD, BS 663, RBL 33, WL 164. CRACK AT LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL33 WL164 WAS FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS. PERMANENTLY SEALED AND REFINISHED CRACK IAW SRM 57-10-10-1A-2.
- [SDR SWAA2026072003003](https://openairdocs.org/sdr/SWAA2026072003003.md): Seat Track · corroded · Jun 12, 2026 · N257WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 846 - 850 ON CROWN AND WELL, BS 858 ON CROWN AND WELL, BS 887 ON CROWN LBL45 WL208. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52-1A-1, SRM 51-10-02-0G-0. SEAT TRACK FOUND TO BE IN LIMITS IAW S
- [SDR SWAA2026072060924](https://openairdocs.org/sdr/SWAA2026072060924.md): Seat Track · corroded · Jun 12, 2026 · N257WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 500C+8 ON CROWN, BS 500B+9 ON CROWN, BS 561 ON CROWN, BS 581 ON CROWN & WELL, BS 611 ON CROWN, BS 632 ON CROWN, BS 685-693 IN WELL, RBL45, WL 208. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52-1
- [SDR SWAA2026072012087](https://openairdocs.org/sdr/SWAA2026072012087.md): Seat Track · corroded · Jun 12, 2026 · N257WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 400-404 ON CROWN AND BS 432-434 ON CROWN LBL25 WL208. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 400-404 ON CROWN AND BS 432-434 ON CROWN LBL25 WL208 IAW SRM 53-00-52-1A-1 SRM 51-10-02-0G-0. SEAT TRACK
- [SDR SWAA2026072093568](https://openairdocs.org/sdr/SWAA2026072093568.md): Skin · bulged · Jun 11, 2026 · N257WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB UPPER SKIN BULGING AT OTBD T/E PANEL. REPAIRED IAW EA 26-155-01648 WITH AN INSPECTION THRESHOLD DEFINED IN 26-155-01648-DTI..
- [SDR SWAA2026072024604](https://openairdocs.org/sdr/SWAA2026072024604.md): Rib · cracked · Jun 11, 2026 · N257WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB, CRACKED AT INSPAR RIB 4, STAB STA 120.30, STIFFENER 4 LOWER AREA. REMOVED, REPAIR, AND REINSTALLED RT STAB 4 RIB SS 120.30 IAW SRM 51-40-02-0G-0, SRM 55-10-09-2R-5, REP 5, DWG 182A3001, REV F, DWG 182A4001, REV D, AND DWG 182A1500, RE
- [SDR SWAA2026072093453](https://openairdocs.org/sdr/SWAA2026072093453.md): Wedge · debonded · Jun 11, 2026 · N257WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT INBD MID FLAP OTBD T/E WEDGE TRAILING EDGE, DISBONDED. REMOVED AND REPLACED LEFT, INBD MID FLAP OTBD T/E EDGE WEDGE IAW SRM 51-40-02-0G-0, CMM 20-50-11-910-801, SRM 51-40-05-0G-0, AND DWG 113A2100, REV C, AND AMM 51-31-00.
- [SDR SWAA2026072024158](https://openairdocs.org/sdr/SWAA2026072024158.md): Floor Panel · delaminated · Jun 11, 2026 · N257WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232SF HAS AREA OF DELAMINATION. FABRICATION OF NEW 232SF PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026072080575](https://openairdocs.org/sdr/SWAA2026072080575.md): Shield · corroded · Jun 10, 2026 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. CORROSION ON AFT CARGO BAY SHIELD FWD OF CARGO DOOR; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-
- [SDR SWAA2026072028123](https://openairdocs.org/sdr/SWAA2026072028123.md): Sidewall Support · corroded · Jun 10, 2026 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A7500, REV A.
- [SDR SWAA2026072062760](https://openairdocs.org/sdr/SWAA2026072062760.md): Sidewall Support · corroded · Jun 10, 2026 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AND DWG 146A
- [SDR SWAA2026072081615](https://openairdocs.org/sdr/SWAA2026072081615.md): Pressure Deck · cracked · Jun 10, 2026 · N257WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK IN MID PASSENGER CABIN AT BS 663, RBL 41. REPAIRED THE HORIZONTAL PRESSURE DECK BS 663 - 675, RBL 40 AND RBL 60. APPLIED CUP SEAL A FILLET SEAL AND CIC IAW SRM 53-40-51-2R-2, REPAIR 2.
- [SDR SWAA2026072018354](https://openairdocs.org/sdr/SWAA2026072018354.md): Threshold Web · corroded · Jun 10, 2026 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS 440+5' - 490, RBL 26, WL156. CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A NEW FWD CARGO BAY SUB THRESHOLD WEB IAW
- [SDR SWAA2026072001893](https://openairdocs.org/sdr/SWAA2026072001893.md): Scuff Plate · cracked · Jun 9, 2026 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFFPLATE AFT CORNER IS CRACKED. WELDED FWD SERVICE DOOR SCUFFPLATE AFT CORNER PER SRM 53-10-15-2R-2.
- [SDR SWAA2026060207248](https://openairdocs.org/sdr/SWAA2026060207248.md): Isolator · cracked · May 29, 2026 · N257WN · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR CRACKED. R&R AFT ENTRY DOOR FWD UPPER SLIDE ISOLATOR IAW SRM 51-40-02.
- [SDR SWAA2025090510629](https://openairdocs.org/sdr/SWAA2025090510629.md): Glowstrip · unsecure · Sep 3, 2025 · N257WN · Boeing 7377H4 · Emergency Equipment
  > PASSENGER CABIN SEAT ROW 24ABC PHOTOLUMINESCENT STRIP DISBONDED FROM FLOOR. SECURED LOOSE PHOTOLUMINESCENCE STRIP PER AMM 33-51-15.
- [SDR SWAA2025041423519](https://openairdocs.org/sdr/SWAA2025041423519.md): Girt Bar · out of adjust · Apr 11, 2025 · N257WN · Boeing 7377H4 · Emergency Equipment
  > AFT GALLEY SERVICE DOOR GIRT HANGING TOO LOW.<[01] RE-PACKED AFT GALLEY SERVICE DOOR GIRT REF AMM 25-66-01.
- [SDR SWAA2025041423518](https://openairdocs.org/sdr/SWAA2025041423518.md): Light · inoperative · Apr 11, 2025 · N257WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN; EMERGENCY LIGHT ABOVE SEAT 9ABC INOP.<[01] R&R PASSENGER CABIN AREA EMERGENCY LIGHT ABOVE SEAT 9ABC IAW AMM 33-51-03.
- [SDR SWAA2025041423528](https://openairdocs.org/sdr/SWAA2025041423528.md): Handle · loose · Apr 11, 2025 · N257WN · Boeing 7377H4 · Service Doors
  > R2 DOOR INTERIOR OPEN/CLOSE HANDLE LOOSE.<[01] RE-SECURED CAM ASSEMBLY NUT ON R2 DOOR INTERIOR HANDLE REF AMM 20-50-11.
- [SDR SWAA2025032609546](https://openairdocs.org/sdr/SWAA2025032609546.md): Girt Bar · out of adjust · Mar 26, 2025 · N257WN · Boeing 7377H4 · Emergency Equipment
  > PERFORM PERMANENT REPAIR OF L1 GIRT BAR RETAINING CLIP MISSING FASTNER. REFERENCE M-23-125-01839-TLD (SWA - REPAIR - NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP MISSING FASTENERS - PERMANENT<[01] INSTALLED SOLID RIVET PER SRM 51-40-02.
- [SDR SWAA2025032408538](https://openairdocs.org/sdr/SWAA2025032408538.md): Hook · loose · Mar 23, 2025 · N257WN · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE GIRT BAR J HOOK IS LOOSE<[01] REPAIRED PER EA M-23-125-01839. REF AMM 26-66-00
- [SDR SWAA2025012790033](https://openairdocs.org/sdr/SWAA2025012790033.md): Handle · broken · Jan 27, 2025 · N257WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR ASSIST HANDLE BROKEN<[01] SWAPPED AFT LAV ASSIST HANDLE TO THE FWD ENTRY DOOR POSITION. AFT LAV ASSIST HANDLE IS OK TO CONTINUE PER MEL 25-10-01 SP# 1B AUTH# 234562. REMOVED AND REPLACED BROKEN ASSIST HANDLE REF AMM 25-21-25.
- [SDR SWAA2024112561328](https://openairdocs.org/sdr/SWAA2024112561328.md): Handle · broken · Nov 19, 2024 · N257WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR UPPER ASSIT HANDLE BROKEN<[01] REMOVED AND REPLACED FWD ENTRY DOOR UPPER ASSIST HANDLE PER AMM 52-11-31.
- [SDR SWAA2024112161334](https://openairdocs.org/sdr/SWAA2024112161334.md): Isolator · cracked · Nov 19, 2024 · N257WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR LOWER AFT SLIDE ISOLATOR IS CRACKED<[01] R&R FWD SERVICE DOOR LOWER AFT SLIDE ISOLATOR PER SRM 51-40-02
- [SDR SWAA2024111157562](https://openairdocs.org/sdr/SWAA2024111157562.md): Flap System · locked · Nov 7, 2024 · N257WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > NO FLAP RESPONSE WHEN FLAP HANDLE SET TO 5. ALTERNATE EXTENSION WORKED PROPERLY. FLAPS 15 LANDING.<[01] CHECKED FSEU FOR LOGGED FAULTS. NONE FOUND. OPERATED FLAPS REF. AMM 27-51-00 USING PRIMARY HYDRAULIC POWER. FLAPS WORKED NORMALLY. UNABLE TO VERIFY FAILED C
- [SDR SWAA2024101446415](https://openairdocs.org/sdr/SWAA2024101446415.md): Lens · missing · Oct 8, 2024 · N257WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT RH EMERGENCY EXIT FLOOR LEVEL LENS MISSING<[01] R&R?D LIGHT ASSAY PER AMM 33-51-01
- [SDR SWAA2024100444000](https://openairdocs.org/sdr/SWAA2024100444000.md): Slide · out of position · Oct 1, 2024 · N257WN · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE OUT OF POSITION<[01] REPOSITIONED FWD SERVICE DOOR SLIDE IAW MT725-611-06.;[02] REPOSITIONED FWD SERVICE DOOR SLIDE IAW MT725-61-06. CORRECTION MADE FOR INCORRECT AMM REF. ENTERED FOR E117006.;[03] CERTIFY
- [SDR SWAA2024092741366](https://openairdocs.org/sdr/SWAA2024092741366.md): Flashlight · inoperative · Sep 25, 2024 · N257WN · Boeing 7377H4 · Emergency Equipment
  > AFT GALLEY FLASHLIGHT NOT CHARGING. R&R FLASHLIGHT ASSY REF AMM 25-64-00. CKS GOOD.
- [SDR SWAA2024081322544](https://openairdocs.org/sdr/SWAA2024081322544.md): Bulb · inoperative · Aug 5, 2024 · N257WN · Boeing 7377H4 · Emergency Lighting
  > L/H OWE AFT EMERGENCY EXIT WINDOW BULB INOP<[01] RELAMPED L/H OWE AFT EMERGENCY EXIT WINDOW LIGHT BULB IAW AMM 33-21-00-960-801 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-00-710-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024081322545](https://openairdocs.org/sdr/SWAA2024081322545.md): Battery Pack · inoperative · Aug 5, 2024 · N257WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED TO BATTERY PACK M1674 INOP<[01] VERIFIED STEPS 1-3;[02] VERIFIED STEP 3.;[03] UPDATED PARTS INFO;[04] REMOVED AND REPLACED BATTERY PACK M1674. OP CHECK GOOD. PER AMM 33-51-06-960-805;[05] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024081322546](https://openairdocs.org/sdr/SWAA2024081322546.md): Bulb · inoperative · Aug 5, 2024 · N257WN · Boeing 7377H4 · Emergency Lighting
  > R/H OWE AFT LOCATOR HAS MULTIPLE BULBS INOP 3 TOTAL INOP<[01] RELAMPED R/H EMERGENCY OWE AFT LOCATOR AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024081321931](https://openairdocs.org/sdr/SWAA2024081321931.md): Scuff Plate · cracked · Aug 3, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB DOOR AFT CORNER SCUFF PLATE CRACKED<[01] REMOVED; REPAIRED AND REINSTALLED SCUFF PLATE IAW SRM 53-60-15 AND AMM 53-11-02<BR>LEAK CHECK ACCOMPLISHED ON TTG8Q00DCW18 STEP 11;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2024081321424](https://openairdocs.org/sdr/SWAA2024081321424.md): Bracket · corroded · Aug 1, 2024 · N257WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET AT STA 312; LBL 55; WL 208.5<[01] FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET AT STA 312; LBL 55; WL 208.5 WAS REPLACED ON CUSTOMER CARD# TTG8Q00UD398.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.
- [SDR SWAA2024081320827](https://openairdocs.org/sdr/SWAA2024081320827.md): Wire · damaged · Aug 1, 2024 · N257WN · Boeing 7377H4 · Light System Wiring
  > WIRE W2214-0021-20 FOUND DAMAGED ABOVE L1 DOOR (MARKED).<[01] SPLICED WIRE W2214-0021-20 AND SECURED PER SWPM 20-30-12 AND 20-10-13. AND PERFORMED GOOD CONTINUITY CHECK PER WDM 33-51-11. OPERATIONAL TEST OF EMERGENCY LIGHTS WILL BE PERFORMED ON TTG8Q00U9K7S.;[
- [SDR SWAA2024081316718](https://openairdocs.org/sdr/SWAA2024081316718.md): Strap · corroded · Jul 25, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR PNL T-STRAP HAS CORROSION BS 727D+5 LBL 20 - RBL 20<[01] RECIVED 'T' STRAP 146A9401-8ATSMRO; GOING TO BE INSTALL ON W/C TTG8Q00U29VL;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.
- [SDR SWAA2024081315972](https://openairdocs.org/sdr/SWAA2024081315972.md): Intercostal · cracked · Jul 24, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL COMMON TO FLOOR TO SIDEWALL SUPPORT AT ACB CRACK AT BS747-767; BETWEEN STR25-STR26 RBL21-23.<[01] REMOVED AND REMPLACED INTERCOSTAL AT ACB BETWEEN BS 747 TO BS 767; STR 25- STR 26 RBL 21- 23 PER SRM 51-40-02 AND DWG:146A7500 ID:0044 REV:C;[02
- [SDR SWAA2024081314768](https://openairdocs.org/sdr/SWAA2024081314768.md): Fairing · delaminated · Jul 21, 2024 · N257WN · Boeing 7377H4 · Trailing Edge Flaps
  > #3 FLAP MOVEABLE FAIRING; FORWARD INBOARD EDGE DELAMINATED 542BB<[01] VERIFIED THE REPAIR AT THE FORWARD EDGE OF FAIRING 542BB IS COMPLETE IAW EA 24-157-02035;[02] VERIFIED
- [SDR SWAA2024081314296](https://openairdocs.org/sdr/SWAA2024081314296.md): Stub Frame · cracked · Jul 19, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Frame
  > R1 DOOR FWD CUTOUT HAS CRACKED FRAME AND DEPRESSOR<[01] REMOVED AND REPLACED R1 DOOR FWD CUTOUT STUB FRAME AND DEPRESSOR ER SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV: D.<BR><BR>SEE INDIVIDUAL STEP SIGN OFF FOR DETAILS. TASK CARD COMPLETED;[02] VERIFIED COR
- [SDR SWAA2024081313771](https://openairdocs.org/sdr/SWAA2024081313771.md): Intercostal · cracked · Jul 17, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT MOISTURE SEAL INTERCOSTAL CRACKED BS 1021 RBL 37 WL 209<[01] REMOVED AND REPLACED INTERCOSTAL FROM RBL 26 TO RBL 44 BS 1021 WL 209 PER SRM 51-40-02-0G-0 AND BOEING DWG 148A0922.;[02] REMOVED AND REPLACED INTERCOSTAL FROM RBL 26 TO RBL 44 BS 1021 WL 209 PER
- [SDR SWAA2024081312036](https://openairdocs.org/sdr/SWAA2024081312036.md): Skin · corroded · Jul 12, 2024 · N257WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE SKIN - FWD ANTENNA COVER PLATE AND SKIN HAVE EVIDENCE OF CORROSION AT STA 410; STR 27L.<[01] PARTIAL UPDATED STEPS 1 AND 2.;[02] JOB COMPLETE.
- [SDR SWAA2024080912038](https://openairdocs.org/sdr/SWAA2024080912038.md): Intercostal · cracked · Jul 12, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN; L-1 DOOR; FWD SIDE; STRUCTURAL INTERCOSTAL HAS CRACK BTW STA 294.5 & 303.9; STR 16L. MARKED.<[01] INSTALLED NEW INTERCOSTAL AT L1 DOOR FWD SIDE BS 294.5 TO 309.9; STR 16L PER SRM 51-40-02-0G-0 AND DWG 141A8180;[02] REMOVED REVEAL PANEL TO BE I
- [SDR SWAA2024080910332](https://openairdocs.org/sdr/SWAA2024080910332.md): Door · out of adjust · Jul 8, 2024 · N257WN · Boeing 7377H4 · Passenger/Crew Doors
  > ADJUST FED AS REQUIRED<[01] PERFORMED FED ADJUSTMENT AS REQUIRED IAW AMM 52-11-00-820-801;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024081309762](https://openairdocs.org/sdr/SWAA2024081309762.md): Support · corroded · Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY RH FLOOR TO SIDEWALL SUPPORT SECTION 2 BS 767-727D-10; RBL 21; WL 156 MULTIPLE CORROSION AFT CARGO BAY RH FLOOR TO SIDEWALL SUPPORT SECTION 2 BS 767-727D-10 RBL 21 WL 156<[01] UPDATED STEP 11;[02] UPDATED MEASUREMENTS PARAMETERS ITEM 21
- [SDR SWAA2024081309767](https://openairdocs.org/sdr/SWAA2024081309767.md): Support · corroded · Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE CORROSION ON AFT CARGO BAY LH FLOOR TO SIDEWALL SUPPORT SECTION 4;767+5 TO 767-3; RBL 21; WL 156<[01] THIS TASK ACCOMPLISHED ON TTG8Q00UDXCA;[02] VERIFIED CORRECTIVE ACTION ITEMS AND STEPS; CARD COMPLETE.
- [SDR SWAA2024081309930](https://openairdocs.org/sdr/SWAA2024081309930.md): Strap · corroded · Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON AFT CARGO BAY T-STRAP BS 767+5; RBL 17.70 TO LBL 3; WL 156<[01] T-STRAP WILL BE INSTALL ON CUSTOMER CARD NR: TTG8Q00U29VL;[02] EVALUATED MULTIPLE AREAS OF CORROSION ON AFT CARGO BAY T-STRAP BS 767+5; RBL 17.70 TO LBL 3; WL 156. F
- [SDR SWAA2024081309756](https://openairdocs.org/sdr/SWAA2024081309756.md): Web · corroded · Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY THRESHOLD BS 787-10 TO 794; RBL 27; WL 156.<[01] UPDATED STATUS STEP 5 AND 6 TO PARTIAL.;[02] REMOVED AND REPLACED ACB THRESHOLD WEB BETWEEN BS 794 TO BS 847; RBL 27; WL 156 PER SRM 51-40-02 AND DWG:146A8340; ID:0024; REV: A.;[03] VERIF
- [SDR SWAA2024081309933](https://openairdocs.org/sdr/SWAA2024081309933.md): Shield · corroded · Jul 6, 2024 · N257WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO DOOR AFT SHIELD BS 500A-6 TO 500A -10; RBL 21; WL 156.<[01] REMOVED AND REPLACED SHIELD AT FCB BETWEEN BS 480+12' TO BS 500A; RBL 21; WL 156 PER SRM 51-40-02 AND DWG:143A0080.;[02] EDITED STATEMENT;[03] VERIFIED;[04] REMOVED AND REPLACED S

Next page: https://openairdocs.org/aircraft/N257WN/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 = 'N257WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N257WN/reports

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