# Service difficulty reports: N228WN

A list on [N228WN](https://openairdocs.org/aircraft/N228WN.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 · 272 reports

- [SDR SWAA2026082684292](https://openairdocs.org/sdr/SWAA2026082684292.md): Lamp · inoperative · Aug 22, 2026 · N228WN · Boeing 7377H4 · Emergency Lighting
  > AREA LIGHTS AT SEAT 8 FED, 14 FED, AND 16 FED INOP AREA LIGHTS AT SEAT 8 FED 14 FED AND 16 FED INOP RELAMPED AREA LIGHTS AT 8 FED 14 FED AND 16 FED IAW AMM 33-51-03. OPS CHECK GOOD
- [SDR SWAA2026081780830](https://openairdocs.org/sdr/SWAA2026081780830.md): Glowstrip · damaged · Aug 13, 2026 · N228WN · Boeing 7377H4 · Emergency Equipment
  > PASSENGER CABIN SEAT ROW 27 PHOTOLUMINESCENT STRIPS, RT & LT SIDES HAVE MOISTURE UNDER LENS. R & R THE PHOTOLUMINESCENT STRIPS IAW AMM 33-51-15.
- [SDR SWAA2026080517620](https://openairdocs.org/sdr/SWAA2026080517620.md): Slide · unwanted deploy · Aug 1, 2026 · N228WN · Boeing 7377H4 · Escape Slide
  > RAMP DEPLOYED R1 DOOR ESCAPE SLIDE. R & R R1 DOOR ESCAPE SLIDE IAW AMM 25-66-01.
- [SDR SWAA2026080390993](https://openairdocs.org/sdr/SWAA2026080390993.md): Light · inoperative · Jul 28, 2026 · N228WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT EXTERNAL OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE, REQUIRES REPLACEMENT. REMOVED AND REPLACED THE RT EXTERNAL OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04-960-801 AND INSTALLATION TESTED GOOD.
- [SDR SWAA2026021269503](https://openairdocs.org/sdr/SWAA2026021269503.md): Coupling · broken · Feb 10, 2026 · N228WN · Boeing 7377H4 · Passenger/Crew Doors
  > MAIN DOOR EMERGENCY ASSIST HANDLE BROKEN. R & R ASSIST HANDLE LOWER THREADED COUPLING IAW AMM 52-11-31.
- [SDR SWAA2025081197141](https://openairdocs.org/sdr/SWAA2025081197141.md): Battery Pack · inoperative · Aug 1, 2025 · N228WN · Boeing 7377H4 · Emergency Lighting
  > ALL ASSOCIATED LIGHTS WITH M1674 EMERGENCY BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK POWER SUPPLY AND CHARGER M1674 PER AMM 33-51-06-960-806 AND TEST GOOD PER AMM 33-51-06-960-806;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025081197142](https://openairdocs.org/sdr/SWAA2025081197142.md): Battery Pack · inoperative · Aug 1, 2025 · N228WN · Boeing 7377H4 · Emergency Lighting
  > ALL ASSOCIATED LIGHTS WITH EMERGENCY BATTERY PACK M1675 INOPERATIVE REMOVED AND REPLACED EMERGENCY BATTERY PACK POWER SUPPLY AND CHARGER M1675 PER AMM 33-51-06-960-806 AND TEST GOOD PER AMM 33-51-06-960-806;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025081193106](https://openairdocs.org/sdr/SWAA2025081193106.md): Lens · broken · Jul 19, 2025 · N228WN · Boeing 7377H4 · Emergency Lighting
  > SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT LENS BROKEN<[01] REMOVED AND REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802 <BR>OPT. CHECK: GOOD;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025081191944](https://openairdocs.org/sdr/SWAA2025081191944.md): Skin · cracked · Jul 16, 2025 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACKED FASTENER HOLE FOUND ON R/W FIXED L/E UPPER SURFACE; 5' I/B OF PYLON (MARKED LOCATION AND DIRECTION)<[01] REMOVED DAMAGE IN FASTENER HOLE FOUND ON R/W FIXED L/E UPPER SURFACE; 5' I/B OF PYLON IAW SRM 51-10-02-OG-0 AND SRM 57-41-01-2R-7.;[02] VERIFIED CO
- [SDR SWAA2025081188945](https://openairdocs.org/sdr/SWAA2025081188945.md): Seat Track · cracked · Jul 7, 2025 · N228WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S SEAT TRACK'S WORN; CRACKED & CORRODED<[01] REMOVED AND REPLACED CAPTAIN'S SEAT TRACK'S PER AMM 25-11-11-400-801<BR>CAL:DATE:03/2025<BR>DUE:03/2026<BR>ID:ATS2842;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025081188944](https://openairdocs.org/sdr/SWAA2025081188944.md): Seat Track · cracked · Jul 7, 2025 · N228WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > F/O'S SEAT TRACK'S WORN; CRACKED & CORRODED<[01] REOMVED AND REPLACED F/O'S SEAT TRACK'S PER AMM 25-11-11-400-801<BR>CAL:DATE:08/2024<BR>DUE:08/2025<BR>ID:ATS2328.;[02] COMPLETE.;[03] UPDATED MEASUREMENTS TABLE.
- [SDR SWAA2025081188468](https://openairdocs.org/sdr/SWAA2025081188468.md): Panel · delaminated · Jul 5, 2025 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT ING L/E PANEL 521KB DELAMINATED AT CORNERS OF CUTOUT. LEFT WING L/E PANEL 521KB WITH DELAMINATIONS AT CORNERS OF CUTOUTS WAS REPAIRED PER SRM 51-70-05-2R-6.
- [SDR SWAA2025081188467](https://openairdocs.org/sdr/SWAA2025081188467.md): Panel · delaminated · Jul 5, 2025 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > LEFT WING L/E PANEL 521DB DELAMINATED AT CUTOUT CORNERS. REPAIRED PER SRM 51-70-05-2R-6-A00737 REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL.
- [SDR SWAA2025081188470](https://openairdocs.org/sdr/SWAA2025081188470.md): Panel · delaminated · Jul 5, 2025 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS. RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS; WAS REPAIRED IAW SRM 51-70-05-2R-6.
- [SDR SWAA2025081188472](https://openairdocs.org/sdr/SWAA2025081188472.md): Panel · delaminated · Jul 5, 2025 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > RIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER. RIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER; WAS REPAIRED IAW SRM 51-70-05-2R-6.
- [SDR SWAA2025081188085](https://openairdocs.org/sdr/SWAA2025081188085.md): Floor Support · cracked · Jul 3, 2025 · N228WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED FLOORBEAM AT PASSENGER COMPARTMENT BS 540 LBL 2 WL 208. REMOVED AND REPLACED FLOOR SUPPORT PANEL BREAK AT PASSENGER COMPARTMENT BS 540 LBL 2 WL 208 IAW SRM 51-40-02-0G-0 AND AIPC SWA D638A001-SWA-0102.
- [SDR SWAA2025081188094](https://openairdocs.org/sdr/SWAA2025081188094.md): Skin · delaminated · Jul 3, 2025 · N228WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING INBD MAIN FLAP O/B T/E WEDGE IS DELAMINATED. REMOVED AND REPLACED THE RIGHT WING INBD MAIN FLAP O/B T/E WEDGE IAW SOPM 20-50-01.
- [SDR SWAA2025081187638](https://openairdocs.org/sdr/SWAA2025081187638.md): Support · corroded · Jul 2, 2025 · N228WN · 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] EVALUATED; LOCATED AND DRILLED; REMOVED AND REPRACED AFT CARGO BAY NEW R/H FLOOR TO SIDEWALL SUPPORT PLATE BS727 TO BS767 RBL
- [SDR SWAA2025081187637](https://openairdocs.org/sdr/SWAA2025081187637.md): Support · corroded · Jul 2, 2025 · N228WN · 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] EVALUATED; REMOVED; LOCATED; DRILLED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE BS727 TO BS847 LBL22 WL156 IA
- [SDR SWAA2025081187635](https://openairdocs.org/sdr/SWAA2025081187635.md): Splice Strap · corroded · Jul 2, 2025 · N228WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS887 RBL11.5 WL168<[01] EVALUATED; REMOVED; LOCATED; DRILLED AND INSTALLED FLOOR SPLICE STRAP BS887 LBL 8 TO RBL 22 WL 168 IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 149A8104 REV: B.;[02] C
- [SDR SWAA2025081187636](https://openairdocs.org/sdr/SWAA2025081187636.md): Shield · corroded · Jul 2, 2025 · N228WN · 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] EVALUATED; LOCATED AND DRILLED; REMOVED AND REPRACED AFT CARGO BAY NEW SHIELD BS767 TO BS794 RBL22 WL156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0
- [SDR SWAA2025062785273](https://openairdocs.org/sdr/SWAA2025062785273.md): Battery Pack · inoperative · Jun 25, 2025 · N228WN · Boeing 7377H4 · Emergency Lighting
  > R1 ESCAPE SLIDE EMERG LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2024102552450](https://openairdocs.org/sdr/SWAA2024102552450.md): Lens · cracked · Oct 24, 2024 · N228WN · Boeing 7377H4 · Emergency Lighting
  > 12 DEF TO 24 DEF EMERGENCY LIGHT LENS ARE CRACKED AND CRAZED MULTIPLE LOCATIONS<[01] REPLACED MULTIPLE LIGHT LENS IAW AMM 33-51-00.
- [SDR SWAA2024102552435](https://openairdocs.org/sdr/SWAA2024102552435.md): Lens · cracked · Oct 24, 2024 · N228WN · Boeing 7377H4 · Emergency Lighting
  > 12 ABC TO 24 ABC EMERGENCY LIGHT LENS ARE CRACKED AND CRAZED MULTIPLE LOCATIONS<[01] REPLACED MULTIPLE LIGHT LENS IAW AMM 33-51-00.
- [SDR SWAA2024091738134](https://openairdocs.org/sdr/SWAA2024091738134.md): Guard · loose · Sep 15, 2024 · N228WN · Boeing 7377H4 · Emergency Lighting
  > AFT F/A EMERGENCY LIGHT SW GUARD IS LOOSE<[01] ADJUSTED SPRING ON GUARD REF AMM 25-25-11
- [SDR SWAA2023080481516](https://openairdocs.org/sdr/SWAA2023080481516.md): Intercostal · damaged · Jul 12, 2023 · N228WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI. FORWARD CARGO BAY INTERCOSTAL AT STA. 500 LBL 21 FORWARD FASTENER IS TOE NAILED AND HOLE IS NOT COMPLETELY FILLED. 2023-422641<[01] REPLACED FASTENERS ( 1 E/A) FORWARD CARGO BAY INTERCOSTAL AT STA. 500 LBL 21 IAW B737-700 SRM 51-40-02 AND DRAWING # 143A75
- [SDR SWAA2023080477922](https://openairdocs.org/sdr/SWAA2023080477922.md): Nut Plate · cracked · Jul 12, 2023 · N228WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > CRACK NUTPLATE RAIL 2E/A LOCATED ON FRONT SPAR INTERNAL STRUCTURE LOWER CHORD BTW STAB STA 175.50 TO STAB STA 193.90 AT LT HORIZONTAL STABILIZER 2023-422644<[01] REPLACED NUTPLATE RAIL (2E/A) LOCATED ON FRONT SPAR INTERNAL STRUCTURE LOWER CHORD BTW STAB STA 17
- [SDR SWAA2023080775373](https://openairdocs.org/sdr/SWAA2023080775373.md): Angle · cracked · Jul 5, 2023 · N228WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE LOCATED INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING 2023-422561<[01] REPLACED ANGLE LOCATED INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02. LENGTH OF CRACK:2.041?. TOOL USED CALIPER P/N: 500-752-20 S/N:B21015879 DUE DATE: 1
- [SDR SWAA2023080475374](https://openairdocs.org/sdr/SWAA2023080475374.md): Bracket · damaged · Jul 5, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ON SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING 2023-422560<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING IAW. B373-700 SRM 51-40-02-0G-0 AN
- [SDR SWAA2023080774863](https://openairdocs.org/sdr/SWAA2023080774863.md): Panel · broken · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing, Control Surfaces
  > BROKEN ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING 2023-422541<[01] REPLACED ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING I.A.W SRM 51-40-02.;[02] REPLACED ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING I.A.W SRM 51-40-02.
- [SDR SWAA2023080480713](https://openairdocs.org/sdr/SWAA2023080480713.md): Filler · missing · Jul 4, 2023 · N228WN · Boeing 7377H4 · Fuselage Structure (General)
  > MISSING FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A 2023-422544<[01] REPLACED FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A IAW B737-700 SRM 51-10-02 AND DWG AND DWG149A751
- [SDR SWAA2023080474849](https://openairdocs.org/sdr/SWAA2023080474849.md): Plate · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT LT WING 2023-422505<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED ON ORSS 261 AT LT WING IAW B737-700 SEM 51-40-02 AND DWG 115A2001 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORR
- [SDR SWAA2023080474850](https://openairdocs.org/sdr/SWAA2023080474850.md): Bracket · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK TRAILING EDGE ON SUPPORT BRACKET LOCATED ORSS275 AT LT WING 2023-422506<[01] REPLACED SUPPORT BRACKET LOCATED ORSS275 AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; DWG 115A3700 SHEET: 3 REV. B. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED SUPPORT
- [SDR SWAA2023080474851](https://openairdocs.org/sdr/SWAA2023080474851.md): Angle · damaged · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING 2023-422507 IAW DWG NAME OF PART IS CLIP ASSY DWG114A5300 REV:A<[01] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A5300; S
- [SDR SWAA2023080474858](https://openairdocs.org/sdr/SWAA2023080474858.md): Support Bracket · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING 2023-422516<[01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED SUP
- [SDR SWAA2023080474857](https://openairdocs.org/sdr/SWAA2023080474857.md): Plate · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING 2023-422518<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 REV:-. LENGTH OF CRACK:0.807?. TOOL USED CALIPER P/N: 500-752
- [SDR SWAA2023080474856](https://openairdocs.org/sdr/SWAA2023080474856.md): Plate · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING 2023-422520<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 115A2001 REV-. SEE INDIVIDUAL SIG
- [SDR SWAA2023080474854](https://openairdocs.org/sdr/SWAA2023080474854.md): Angle · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING 2023-422530PART INSTALLEDP/N: 115A2953-2 PO# 2022 196669<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-4
- [SDR SWAA2023080474853](https://openairdocs.org/sdr/SWAA2023080474853.md): Angle · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING 2023-422532<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING IAW SRM B737-700 51-40-02 SRM 51-10-02 PARAGRAPH 9;[02] STEP 1 COR
- [SDR SWAA2023080474852](https://openairdocs.org/sdr/SWAA2023080474852.md): Angle · cracked · Jul 4, 2023 · N228WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING 2023-422526 IAW DGW NAME PART IS CLIP ASSY 115A2000 REV-<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING; MEASURE CRACK IS L=0.817? TOOL USED CALIPER P/N: 500-193-30; S/N: 0039393; DUE DATE: 02-
- [SDR SWAA2023080774547](https://openairdocs.org/sdr/SWAA2023080774547.md): Angle · cracked · Jul 3, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ANGLE ENTRY DOOR CUT OUT LOC BS 294.5 AND BTW STR 13 TO STR 14 FWD GALLEY AND LAV 2023-422454<[01] REPLACED ANGLE ENTRY DOOR CUT OUT LOC BS 294.5 AND BTW STR 13 TO STR 14 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. SEE IN
- [SDR SWAA2023080474844](https://openairdocs.org/sdr/SWAA2023080474844.md): Bracket · damaged · Jul 3, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > ELONGATED HOLE BRACKET ON BS 1016 UPPER AREA AFT GALLEY AND LAV 2023-422464<[01] REPLACED BRACKET ON BS 1016 UPPER AREA AFT GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 148A2230 REV. C. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED BRA
- [SDR SWAA2023080274848](https://openairdocs.org/sdr/SWAA2023080274848.md): Access Panel · cracked · Jul 3, 2023 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING 2023-422499<[01] REPLACED ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 113A9350; SHEET 1; REV.F.;[02] REPLACED ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING I.A.W B7
- [SDR SWAA2023080274846](https://openairdocs.org/sdr/SWAA2023080274846.md): Access Panel · cracked · Jul 3, 2023 · N228WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ACCESS PANEL 651GB TRAILING EDGE SUPPORT PLATE RT WING 2023-422502<[01] REPLACED ACCESS PANEL 651GB TRAILING EDGE SUPPORT PLATE AT RT WING I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON S
- [SDR SWAA2023080474163](https://openairdocs.org/sdr/SWAA2023080474163.md): Stub Frame · cracked · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR 2023-422409<[01] REPLACED STUB FRAME LOC. BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR IAW SRM B737-700 51-10-02. SRM 51-40-02; DRAWING: 141A8370 REV. D. SEE IND
- [SDR SWAA2023080474160](https://openairdocs.org/sdr/SWAA2023080474160.md): Floorbeam · corroded · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-422400<[01] TOOL USED: THICKNESS GAGE. P/N: 45MG; S/N: 130060401; DUE DATE: 20-MAR-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 220273012. DUE DATE: 17-DEC-23.;[03] REP
- [SDR SWAA2023080474162](https://openairdocs.org/sdr/SWAA2023080474162.md): Strap · corroded · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE ON STRAP LOCATED BS1040 BETWEEN BL0 TO LBL 43 AND WL 208.1 AT AFT GALLEY AREA 2023-422406<[01] REPLACED STRAP LOCATED BS1040 BETWEEN BL0 TO LBL 43 AND WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A
- [SDR SWAA2023080474169](https://openairdocs.org/sdr/SWAA2023080474169.md): Strap · corroded · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE ON STRAP LOCATED BS1040 BETWEEN BL 0 TO RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-422404<[01] REPLACED STRAP LOCATED BS1040 BETWEEN BL 0 TO RBL 43 WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A9870 S
- [SDR SWAA2023080474168](https://openairdocs.org/sdr/SWAA2023080474168.md): Bracket · cracked · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL RBL6 AT LOWER FUSELAGE 2023-422410<[01] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL RBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 212A1101 SHEET 3 REV
- [SDR SWAA2023080474170](https://openairdocs.org/sdr/SWAA2023080474170.md): Bracket · cracked · Jul 2, 2023 · N228WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL LBL6 AT LOWER FUSELAGE 2023-422411<[01] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL LBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 212A1101 SHEET 3

Next page: https://openairdocs.org/aircraft/N228WN/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 = 'N228WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N228WN/reports

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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.