# Service difficulty reports: N226WN

A list on [N226WN](https://openairdocs.org/aircraft/N226WN.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 · 290 reports

- [SDR SWAA2026081114863](https://openairdocs.org/sdr/SWAA2026081114863.md): Engine · no discrepancy · Aug 7, 2026 · N226WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE SLOW TO SPOOL ON TAKEOFF. EGT 60 SPLIT FROM NR 1 ENGINE. TROUBLESHOT IAW FIM 73-05 TASK 814. PERFORMED TEST 8, ACCELERATION CHECK OF NR 2 ENGINE IAW AMM 71-00-00. TEST PASSED WITH ACCELERATION OF 4.5 SECS. NO EEC FAULTS. NO EGT EXCEEDANCES OBSER
- [SDR SWAA2026041387896](https://openairdocs.org/sdr/SWAA2026041387896.md): Slide · out of position · Apr 9, 2026 · N226WN · Boeing 7377H4 · Escape Slide
  > AFT LEFT EMERG SLIDE UN STOWED WHEN PROVO CLOSED AFT LEFT DOOR<[01] C/W MT 725-61-06 REINSTALLED PER MT
- [SDR SWAA2025052072014](https://openairdocs.org/sdr/SWAA2025052072014.md): Rivet · loose · May 17, 2025 · N226WN · Boeing 7377H4 · Emergency Equipment
  > LOOSE RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER BAR <[01]. REMOVED AND REPLACED RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER BAR I.A.W SRM 51-40-02-0G-0 AND AIPC 25-66-00-13.; [02] REMOVED AND REPLACED RIVETS ON FED EMERGENCY ESCAPE SLIDE AFT HOLDER B
- [SDR SWAA2025052071600](https://openairdocs.org/sdr/SWAA2025052071600.md): Fitting · loose · May 16, 2025 · N226WN · Boeing 7377H4 · Emergency Equipment
  > FED AFT GIRT BAR FITTING IS LOOSE. <[01] SECURED FED AFT GIRT BAR FITTING PER AMM 25-66-02-400-801; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025052071603](https://openairdocs.org/sdr/SWAA2025052071603.md): Handle · loose · May 16, 2025 · N226WN · Boeing 7377H4 · Emergency Equipment
  > AED ASSIST HANDLE LOOSE ON DOOR. <[01] TIGHTENED AED ASSIST HANDLE PER AMM 25-21-25-420-801; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025052071248](https://openairdocs.org/sdr/SWAA2025052071248.md): Charger · inoperative · May 14, 2025 · N226WN · Boeing 7377H4 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHTS INOP <[01] REMOVED; REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTERY CHARGER PER AMM 33-51-06-960-806; [02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025052066290](https://openairdocs.org/sdr/SWAA2025052066290.md): Hook · corroded · May 1, 2025 · N226WN · Boeing 7377H4 · Emergency Equipment
  > LH EMERGENCY EXIT HATCH ESCAPE LIFE LINE HAS WORN AREAS AND KEEPER SNAP HOOK WITH CORROSION. <[01] REMOVED AND INSTALLED HATCH; IAW AMM 25-21-20-000-801 AND AMM 25-21-20-400-801 AND REMOVED AND INSTALLED L/H EMERGENCY EXIT HATCH ESCAPE LIFE LINE; IAW AMM 25-61
- [SDR SWAA2025052065697](https://openairdocs.org/sdr/SWAA2025052065697.md): Scuff Plate · cracked · Apr 29, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT SCUFF PLATE IS CRACKED<[01] THIS SCUFF PLATE WAS INSTALLED ON CUSTOMER CARD:TTG8Q005QZ2P;[02] CORRECTION TO ACTION 1: REPAIRED SCUFF PLATE IAW SRM 53-60-15-2R-1. SCUFF PLATE RE-INSTALLED ON TASK CARD TTG8Q005QZ2P.;[03] VERIFIED CORRECTIVE ACT
- [SDR SWAA2025052164584](https://openairdocs.org/sdr/SWAA2025052164584.md): Bracket · cracked · Apr 26, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RT AC BAY BRACKET ASSY PN: 212A1116-1 IS CRACKED (MARKED) <[01]. REMOVED AND REPLACED RT AC BRACKET ASSY I.A.W. B737 AMM 20-50-11-910-801; TABLE 204. T/W ID: ATS348 DATE:11/2025; [02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025052158370](https://openairdocs.org/sdr/SWAA2025052158370.md): Seat Track · cracked · Apr 23, 2025 · N226WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S FWD I/B SEAT TRACK CRACKED <[01]. CAPTAIN'S FWD I/B SEAT TRACK CRACKED WAS REPLACED PER IPC 25-11-01-55. THIS COMPONENT WILL BE INSTALLED IN TASKCARD TTG8Q003JZYU; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025052058363](https://openairdocs.org/sdr/SWAA2025052058363.md): Door Frame · cracked · Apr 22, 2025 · N226WN · Boeing 7377H4 · Fuselage Main, Frame
  > PASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L)<BR>'EA-GENERAL' REPAIR REFERENCE IS SELECTED.
- [SDR SWAA2025052058351](https://openairdocs.org/sdr/SWAA2025052058351.md): Shield · corroded · Apr 18, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON ACB FWD SHIELD BETWEEN BS767-BS792 RBL21; WL156 <[01] REMOVED AND REPLACED ACB FWD SHIELD BETWEEN BS767-BS792 RBL21; WL156 IAW SRM 51-40-02 AND DWG# 146A0081 REV:A; [ 02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025052058346](https://openairdocs.org/sdr/SWAA2025052058346.md): Panel · cracked · Apr 18, 2025 · N226WN · Boeing 7377H4 · Wing Main, Frame Structure
  > PANEL 192CR O/B LATCH 2ND FROM AFT END IS CRACKED. (MARKED)<[01] REMOVED AND REPLACED PANEL 192CR O/B LATCH 2ND FROM AFT IAW SOPM 20-50-01.<BR>CALIBRATED TOOL USED:<BR>ID:ATS2427<BR>DATE:02/2025<BR>DUE:02/2026;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025052058348](https://openairdocs.org/sdr/SWAA2025052058348.md): Scuff Plate · cracked · Apr 18, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FSD SCUFF PLATE IS CRACKED.<[01] REMOVED AND INSTALLED SCUFF PLATE GALLERY SERVICE DOOR
- [SDR SWAA2025052058352](https://openairdocs.org/sdr/SWAA2025052058352.md): Stringer Clip · cracked · Apr 18, 2025 · N226WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP ITEM# 143A1010U1; LOT#1602791-1 AT DISCREPANCY AREA PER SRM 51-40-05; SRM 51-40-02; DWG# 146A1102 REV:-. ALL WORK COMPLETED.;[02] JOB COMPLETE
- [SDR SWAA2025052058345](https://openairdocs.org/sdr/SWAA2025052058345.md): Skin · debonded · Apr 18, 2025 · N226WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 194FR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194FR OUTER SKIN DIS BOND WAS REPAIRED IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025052025724](https://openairdocs.org/sdr/SWAA2025052025724.md): Floor Panel · pulled · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FABRICATION OF NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025052025722](https://openairdocs.org/sdr/SWAA2025052025722.md): Floor Panel · pulled · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 241DF 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 FO ALL DAMAGE.
- [SDR SWAA2025052025723](https://openairdocs.org/sdr/SWAA2025052025723.md): Floor Panel · pulled · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 241EF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025052058308](https://openairdocs.org/sdr/SWAA2025052058308.md): Floor Panel · pulled · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 242DF 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 FO ALL DAMAGE.
- [SDR SWAA2025052025721](https://openairdocs.org/sdr/SWAA2025052025721.md): Floor Panel · pulled · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FABRICATION OF NEW 242CF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025052058337](https://openairdocs.org/sdr/SWAA2025052058337.md): Shield · corroded · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON AFT CARGO BAY RH FLOOR SHIELD - BS [727B+5; 727B+12; 727C+10; 727D-787]; WL 156; RBL 21<[01]. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO SIDEWAL SUPPORT FROM BS727 TO BS767 RBL21 WL156 IAW SRM 51-40-02; SRM 51-40-05 A
- [SDR SWAA2025052058334](https://openairdocs.org/sdr/SWAA2025052058334.md): Support · corroded · Apr 17, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON AFT CARGO LH SHIELD - BS [727A-727B; 727B+2; 727B+6; 727B+18; 727C+2; 727C+5; 727D-787]; LBL 21; WL 156. <[01] REMOVED AND REPLACED AFT CARGO L/H FLOOR-TO-SIDEWALL SUPPORT FROM STA 727- STA 847; LBL 21; WL 156 IAW SRM 51-40-02-0G
- [SDR SWAA2025052025719](https://openairdocs.org/sdr/SWAA2025052025719.md): Floor Panel · pulled · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] FLOOR PANEL 231ZF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025052025720](https://openairdocs.org/sdr/SWAA2025052025720.md): Floor Panel · failed · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF A FAILED PREVIOUS REPAIR. <[01] FLOOR PANEL 241AF WAS REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A NOTE:; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.
- [SDR SWAA2025052025711](https://openairdocs.org/sdr/SWAA2025052025711.md): Support · corroded · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON SIDEWALL SUPPORT BS 400+10 RBL 23 WL 156.5 (MARKED) <[01]. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB FROM BS 400 TO BS420 RBL 23 WL 156.5 IAW SRM 51-40-02 & DWG# 143A7500 REV: -. ID: 0071.
- [SDR SWAA2025052026660](https://openairdocs.org/sdr/SWAA2025052026660.md): Shield · corroded · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON FWD SHIELD BS 420+17 RBL 23 WL 156.5 (MARKED) <[01] REMOVED AND REPLACED FWD SHIELD AT FCB BS420-BS440 RBL23 WL156.5 IAW SRM 51-40-02-0G-0 AND DWG 143A0080.
- [SDR SWAA2025052058295](https://openairdocs.org/sdr/SWAA2025052058295.md): Support · corroded · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON SIDEWALL SUPPORT BS 440+2; BS440+10; BS440+18; BS460+6; BS460+10; BS460+14; BS460+18 LBL 24.5 AND BS440+2 LBL23.5 WL 156.5 (MARKED) <[01]. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FCB BETWEEN BS 396 TO BS 500D RBL 25 WL 156 IAW SRM
- [SDR SWAA2025052025713](https://openairdocs.org/sdr/SWAA2025052025713.md): Floorbeam · cracked · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT CROSSBEAMS AT MID CABIN ABOVE FWD SPAR CRACKED - BS 539; LBL 1 AND RBL 1.<[01] REMOVED AND REPLACED 2EA PANEL BREAK. P/N: 143A5240U33 LOT: 1602183-5 AND P/N: 143A5240U34 LOT: 1591872-1 AND 2EA PLATE P/N 143A5240U12 LOT: 1598027-6 AND P/N: 143A524
- [SDR SWAA2025052025715](https://openairdocs.org/sdr/SWAA2025052025715.md): Support · corroded · Apr 16, 2025 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB - CORROSION ON SIDEWALL SUPPORT BS 500+10; BS500+14; BS500+18; BS500A+2; BS500A+6; BS500A+10; BS500C+2; BS500C+6; BS500C+10 LBL 24.5 WL 156.5 (MARKED)<[01] THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00ZWH9X.
- [SDR SWAA2025021093875](https://openairdocs.org/sdr/SWAA2025021093875.md): Battery Pack · no test · Feb 7, 2025 · N226WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1673 FAILED CAPACITY TEST<[01] R&R EMERGENCY LIGHTS BATTERY PACK M1673 IAW AMM 33-51-06.
- [SDR SWAA2025021093874](https://openairdocs.org/sdr/SWAA2025021093874.md): Battery Pack · no test · Feb 7, 2025 · N226WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R EMERGENCY LIGHTS BATTERY PACK M1675 IAW AMM 33-51-06.
- [SDR SWAA2024100343331](https://openairdocs.org/sdr/SWAA2024100343331.md): Power Supply · inoperative · Sep 29, 2024 · N226WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE R/H OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY FUSE REF AMM 33-51-06. OPS TEST GOOD.
- [SDR SWAA2024090934917](https://openairdocs.org/sdr/SWAA2024090934917.md): Bracket · out of adjust · Sep 6, 2024 · N226WN · Boeing 7377H4 · Emergency Equipment
  > BRACKET THAT HOLDS GIRT BAR ON FORWARD SERVICE DOOR; NOT SECURE<[01] RESECURED BRACKET ON FWD SERVICE DOOR GIRT BAR BRACKET PER SRM 51-40-02
- [SDR SWAA2024083031427](https://openairdocs.org/sdr/SWAA2024083031427.md): Charger · inoperative · Aug 28, 2024 · N226WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS FWD AND TOP OF FO EMERGENCY EXIT DOOR INOP<[01] R/R EMERGENCY LIGHT CHARGER ASSY AT FO SIDE EMERGENCY DOOR IAW AMM 33-51-06
- [SDR SWAA2023080485448](https://openairdocs.org/sdr/SWAA2023080485448.md): Landing Gear · failed · Aug 3, 2023 · N226WN · Boeing 7377H4 · Landing Gear System
  > LEFT MLG FAILED TO RETRACT AFTER TAKE-OFF, GEAR PINS INSTALLED & ALTERNATE MLG DOWN SWITCH IN ALTN POSITION. OK TO CONTINUE IAW MEL 32-16-01. SP1 C/W. REMOVED LT MLG DOWNLOCK ACT IAW AMM 32-32-51. C/BS PULLED & COLLARED IAW AMM 32-09-00-840-801. HYD SYS
- [SDR SWAA2023060248065](https://openairdocs.org/sdr/SWAA2023060248065.md): Web · cracked · May 12, 2023 · N226WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK WEB TRAILING EDGE ORSS 278 AT RT WING 2023-295602<[01] REPLACED WEB LOCATED ON TRAILING EDGE ORSS 278 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 115A2512 SHEET 13 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLET
- [SDR SWAA2023060248064](https://openairdocs.org/sdr/SWAA2023060248064.md): Angle · cracked · May 12, 2023 · N226WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORRSS 279 AT LT WING 2023-295600<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE LOCATED AT LEVEL ORRSS 279 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A6200 REV:-.;[02] TASK CARD COMPLETED
- [SDR SWAA2023060147131](https://openairdocs.org/sdr/SWAA2023060147131.md): Plate · corroded · May 10, 2023 · N226WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER LOBE- ANTENNA AT STA 450 S-28L HAS EVIDENCE OF CORROSION AAI:2023-295599<[01] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403;[02] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE STA 450 S-28L
- [SDR SWAA2023060147132](https://openairdocs.org/sdr/SWAA2023060147132.md): Plate · corroded · May 10, 2023 · N226WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER LOBE - ANTENNA AT STA 410 S-28L HAS EVIDENCE OF CORROSION AAI:2023-295598<[01] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700 SRM-51-40-02-0G-0 AND DGW- 143N3403;[02] REPLACED COVER PLATE AT LOWER FUSELAGE LOWER LOBE IAW B737-700
- [SDR SWAA2023060145782](https://openairdocs.org/sdr/SWAA2023060145782.md): Frame · cracked · May 4, 2023 · N226WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 947.5 LOCATED LBL10 AND WL178 AFT CARGO COMPARTMENT 2023-295529<[01] REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R LBL10 AND WL178 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG 147A1047; SHEET: 107; REV: ?. DWG 147A002; SH
- [SDR SWAA2023060145778](https://openairdocs.org/sdr/SWAA2023060145778.md): Support · cracked · May 4, 2023 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS947.5 LBL10 AND WL178 AT AFT CARGO COMPARTMENT 2023-295522<[01] REPLACED ANGLE-SUPPORT LOCATED BS947.5 LBL10 AND WL178 AT AFT CARGO COMPARTMEN IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV:A. SEE INDIVIDUAL SIGNOFFS BELOW.;[02]
- [SDR SWAA2023060145777](https://openairdocs.org/sdr/SWAA2023060145777.md): Web · cracked · May 4, 2023 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS947.5 RBL21 AND WL178 AT AFT CARGO COMPARTMENT 2023-295524<[01] REPLACED INTERCOSTAL-WEB LOCATED BS947.5 RBL21 AND WL178 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7500; SHEET 24 AND REV -:; SEE INDI
- [SDR SWAA2023060145780](https://openairdocs.org/sdr/SWAA2023060145780.md): Angle · cracked · May 4, 2023 · N226WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS907 PLUS 11 INCH RBL13 AND WL171 AT AFT CARGO COMPARTMENT 2023-295523<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] REPLACED FASTENER 1 E/A ON ANGLE LOCATED BS907 PLUS 11 INCH RBL13 AND WL
- [SDR SWAA2023060245393](https://openairdocs.org/sdr/SWAA2023060245393.md): Angle · cracked · May 3, 2023 · N226WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > CRACK LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2023-295520<[01] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 176A3101 REV: -. DWG: 176A3001 REV:
- [SDR SWAA2023060245104](https://openairdocs.org/sdr/SWAA2023060245104.md): Plate · cracked · May 3, 2023 · N226WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 233 AT LT WING 2023-295510<[01] REPLACED CORRUGATED PLATE LOC. TRAILING EDGE ORSS 233 AT LT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 115A3700 SHEET: 39 REV: - SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPLACED
- [SDR SWAA2023060245105](https://openairdocs.org/sdr/SWAA2023060245105.md): Plate · cracked · May 3, 2023 · N226WN · Boeing 7377H4 · Wing, Control Surfaces
  > CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING 2023-295508<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING I.A.W SRM B737-700 51-40-0 115A2001 REV:-;[02] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING I.A.W SRM B737-700
- [SDR SWAA2023060245106](https://openairdocs.org/sdr/SWAA2023060245106.md): Plate · cracked · May 3, 2023 · N226WN · Boeing 7377H4 · Wing, Control Surfaces
  > CRACK CORRUGATED PLATE TRAILING EDGE IRSS 217 AT RT WING 2023-295514<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE IRSS 217 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1 <BR>R
- [SDR SWAA2023060144015](https://openairdocs.org/sdr/SWAA2023060144015.md): Fairing · cracked · May 1, 2023 · N226WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CRACK INBOARD THRUST REVERSE ON PANEL UPPER AREA RT ENGINE 2023-295411<[01] REPLACED ACCESS PANEL FAIRING INBOARD THRUST REVERSE UPPER AREA RT ENGINE IAW B737-700 AMM 78-31-09-010-801-F00 AND IAW B737-700 AMM 78-31-09-420-801-F00. SEE INDIVIDUAL SIGN OFF BELOW
- [SDR SWAA2023060143546](https://openairdocs.org/sdr/SWAA2023060143546.md): Cover · broken · Apr 30, 2023 · N226WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT COVER ON HEADER PANEL RH SIDE AT FWD GALLEY AREA (1 EA) 2023-295361<[01] REPLACED EMERGENCY EXIT LIGHT COVER ON HEADER PANEL RH SIDE AT FWD GALLEY AREA (1 EA) IAW B737 AMM 33-51-01-960-802 STEP 3.C (5)(A) AND (7)(10).;[02] TASK CARD

Next page: https://openairdocs.org/aircraft/N226WN/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 = 'N226WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N226WN/reports

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