# Service difficulty reports: N203WN

A list on [N203WN](https://openairdocs.org/aircraft/N203WN.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 · 295 reports

- [SDR SWAA2026090493713](https://openairdocs.org/sdr/SWAA2026090493713.md): Floor Panel · cracked · Sep 3, 2026 · N203WN · Boeing 7377H4 · Fuselage Floor Panel
  > RAMP FOUND A CRACK IN FWD CARGO BIN FLOOR PANEL ( METAL). ADJACENT TO CARGO DOOR. OK TO CONTINUE IAW MEL 25-16-01 SP1B. R & R THE FWD CARGO FLOOR PANEL 120BF IAW AMM 25-52-10. CLEARED MEL
- [SDR SWAA2026032782681](https://openairdocs.org/sdr/SWAA2026032782681.md): Slide · loose · Mar 24, 2026 · N203WN · Boeing 7377H4 · Escape Slide
  > MAIN CABIN DOOR EMERGENCY ESCAPE SLIDE J-HOOK LOOSE<[01] INSTALLED NEW RIVET IN MAIN CABIN DOOR EMERGENCY ESCAPE SLIDE J-HOOK PER SRM 51-40-02. J-HOOK NOW TIGHT.
- [SDR SWAA2026022674268](https://openairdocs.org/sdr/SWAA2026022674268.md): Girt Bar · unsecure · Feb 25, 2026 · N203WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR STOWAGE HOOK IS UNATTACHED. REATTACHED THE BRACKET FOR FORWARD SERVICE DOOR IAW SRM 51-40-02
- [SDR SWAA2025092919181](https://openairdocs.org/sdr/SWAA2025092919181.md): Trim Motor · loose · Sep 29, 2025 · N203WN · Boeing 7377H4 · Stabilizer Control System
  > ELECTRIC STABILIZER TRIM INOP AFTER TAKE OFF. FOUND STABILIZER TRIM MOTOR ELECTRICA CONNECTOR D700 LOOSE. AS PRECAUTION, R&R STABILIZER TRIM MOTOR PER AMM 27-41-71. OPS CHECK GOOD
- [SDR SWAA2025070387817](https://openairdocs.org/sdr/SWAA2025070387817.md): Seal · cracked · Jul 3, 2025 · N203WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER UPPER RIGHT FORWARD SLIDER CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)] HORIZONTAL STABILIZER UPPER RIGHT FORWARD SLIDER
- [SDR SWAA2025062384178](https://openairdocs.org/sdr/SWAA2025062384178.md): Brake · fluctuates · Jun 20, 2025 · N203WN · Boeing 7377H4 · Brake
  > BRAKE SHAKE ENTIRE AIRCRAFT AT SLOW SPEED WHEN APPLYING BRAKES <[01]. R&R #3 BRAKE PER AMM 32-41-41.
- [SDR SWAA2025031003007](https://openairdocs.org/sdr/SWAA2025031003007.md): Megaphone · inoperative · Mar 7, 2025 · N203WN · Boeing 7377H4 · Emergency Equipment
  > AFT CABIN MEGAPHONE INOP <[01]. 01 - REMOVED AND REPLACED AFT GALLEY MEGAPHONE PER [AMM 25-64-00-SWA-804-NG-01 (REMOVE AND REPLACE MEGAPHONE - PERMANENT)].
- [SDR SWAA2025012188042](https://openairdocs.org/sdr/SWAA2025012188042.md): Circuit Breaker · tripped · Jan 20, 2025 · N203WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > TRAILING EDGE FLAP DISAGREE WITH. FLAP HANDLE SET TO 5. IN ALTERNATE FLAP MODE SPLIT FLAP DISAGREE.<[01] CLOSED L/H TE FLAP POS SKEW SNSR & IND C/B P6-2 A 12 PER MM 27-58-00. PERFORMED OPS CK OF PRIMARY AND ALT FLAP CONTROL SYS MULTIPLE TIMES PER MM 27-51-0. O
- [SDR SWAA2024121676161](https://openairdocs.org/sdr/SWAA2024121676161.md): Battery · failed · Dec 11, 2024 · N203WN · Boeing 7377H4 · Emergency Equipment
  > FWD LOWER CABIN FLASHLIGHT NOT BLINKING<[01] REPLACED FLASH LIGHT BATTERY AS PER AMM 25-64-00 OPS CK NORMAL.
- [SDR SWAA2024121259893](https://openairdocs.org/sdr/SWAA2024121259893.md): Handle · deteriorated · Nov 14, 2024 · N203WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED LINING ENTRY DOOR NUT ON ASSIST HANDLE AT FWD GALLEY AREA (4 EA) 2024-701531<[01] REPLACED LINING ENTRY DOOR NUT ON ASSIST HANDLE AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3. G. (2) (A) (B) (C) (D);[02] REPLACED LINING ENTRY
- [SDR SWAA2024121258700](https://openairdocs.org/sdr/SWAA2024121258700.md): Splice · corroded · Nov 11, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION SPLICE LOCATED BS360 STR28L AND WL148.8 AT EQUIPMENT ELECTRONIC COMP 2024-701509<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE:
- [SDR SWAA2024121258072](https://openairdocs.org/sdr/SWAA2024121258072.md): Nut Plate · corroded · Nov 9, 2024 · N203WN · Boeing 7377H4 · Wing, Attach Fittings
  > CORROSION RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS291 LEADING EDGE AT LT WING 2024-701496<[01] REPLACED RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS291 LEADING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV-;[02] CERTIFIED COMPLETE
- [SDR SWAA2024121258270](https://openairdocs.org/sdr/SWAA2024121258270.md): Support Angle · cracked · Nov 9, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED 1016 BTW STR 3L TO STR 3R AT VERTICAL STABILIZER 2024-701498<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED 1016 BTW STR 3L TO STR 3R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 176A3101 SHEET
- [SDR SWAA2024121258073](https://openairdocs.org/sdr/SWAA2024121258073.md): Angle · cracked · Nov 9, 2024 · N203WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ON ANGE LOCATED SLAT 1 AT LT WING 2024-701494<[01] REPLACED ON ANGE LOCATED SLAT 1 AT LT WING I.A.W SRM B737-700 51-40-02 AND CMM 57-43-01;[02] REPLACED ON ANGE LOCATED SLAT 1 AT LT WING I.A.W SRM B737-700 51-40-02 AND CMM 57-43-01
- [SDR SWAA2024121258271](https://openairdocs.org/sdr/SWAA2024121258271.md): Angle · cracked · Nov 9, 2024 · N203WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK ANGLE LOCATED ON SLAT 8 AT RT WING 2024-701499<[01] REPLACED ANGLE LOCATED ON SLAT 8 AT RT WING I.A.W SRM B737-700 51-40-02 AND CMM 57-43-01;[02] REPLACED ANGLE LOCATED ON SLAT 8 AT RT WING I.A.W SRM B737-700 51-40-02 AND CMM 57-43-01
- [SDR SWAA2024121257994](https://openairdocs.org/sdr/SWAA2024121257994.md): Support Angle · cracked · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR 26R TO STR 27 AFT POSITION AT AFT CARGO COMPARTMENT 2024-701471<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 907 TO BS 927 AND BTW STR 26R TO STR 27R AFT POSITION AT AFT CARGO COMPARTM
- [SDR SWAA2024121257995](https://openairdocs.org/sdr/SWAA2024121257995.md): Support Angle · cracked · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR 26R TO STR 27 FWD POSITION AT AFT CARGO COMPARTMENT 2024-701472<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 907 TO BS 927 AND BTW STR 26R TO STR 27R FWD POSITION AT AFT CARGO COMPARTM
- [SDR SWAA2024121257993](https://openairdocs.org/sdr/SWAA2024121257993.md): Fitting · cracked · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-701473<[01] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SMR 51-10-02 ITEM 9 AND DWG 1149A8103 SHEET 6 REV - SEE INDIVIDUAL SIGN OFF BE
- [SDR SWAA2024121057992](https://openairdocs.org/sdr/SWAA2024121057992.md): Intercostal · cracked · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-701470<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9
- [SDR SWAA2024121057998](https://openairdocs.org/sdr/SWAA2024121057998.md): Support · corroded · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-701475<[01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7
- [SDR SWAA2024121057997](https://openairdocs.org/sdr/SWAA2024121057997.md): Support · corroded · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 767 TO BS 807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-701474<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00WY873. SEE INDIVUAL SIGN OF BELOW;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00WY873. SEE INDIVUAL SIGN OF BE
- [SDR SWAA2024121057999](https://openairdocs.org/sdr/SWAA2024121057999.md): Support · corroded · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-701476<[01] REPLACED SUPPORT ZEE LOCATED BTW BS 727+4 IN TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-01 P; SRM 51-40-02 AND DWG: 146
- [SDR SWAA2024121057996](https://openairdocs.org/sdr/SWAA2024121057996.md): Angle · cracked · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727B TO BS 727E LBL 52 AT AFT CARGO COMPARTMENT 2024-701479<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727A TO BS 747 LBL 52 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02
- [SDR SWAA2024121058066](https://openairdocs.org/sdr/SWAA2024121058066.md): Strap · corroded · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP LOCATED BS 794.37 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT 2024-701482<[01] REPLACED STRAP LOCATED BS 794.37 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 146A8340 SHEET: 21 REV - SEE INDIVI
- [SDR SWAA2024121058070](https://openairdocs.org/sdr/SWAA2024121058070.md): Web · corroded · Nov 8, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON WEB LOCATED BTW BS 847 TO BS 867 LBL19 WL 156.1 AT AFT CARGO COMPARTMENT 2024-701484<[01] REPLACED WEB LOCATED BTW BS 847 TO BS 867 LBL19 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 146A7500 SHEET 86 REV A
- [SDR SWAA2024121257600](https://openairdocs.org/sdr/SWAA2024121257600.md): Gusset · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2024-701435<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND S-19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902 SHEET:174 REV: - SEE INDIVID
- [SDR SWAA2024121257604](https://openairdocs.org/sdr/SWAA2024121257604.md): Support Angle · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-701441<[01] REPLACED SUPPORT ANGLE LOCATED AFT FACE BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 2 REV B<B
- [SDR SWAA2024121257809](https://openairdocs.org/sdr/SWAA2024121257809.md): Intercostal · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL LOCATED BTW BS 685 TO BS 706 AT LEVEL STR 14L AT PASSENGER CABIN 2024-701457<[01] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS 685 TO BS 706 AT LEVEL STR 14L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9
- [SDR SWAA2024121257810](https://openairdocs.org/sdr/SWAA2024121257810.md): Frame · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-701458<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] HIGH FREQUENCY EDDY CURRENT INSPECTION DONE ON FRAME LOC BS 727B BTW STR 8L TO STR
- [SDR SWAA2024121257804](https://openairdocs.org/sdr/SWAA2024121257804.md): Support Bracket · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-701450<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV A.<BR>
- [SDR SWAA2024121057598](https://openairdocs.org/sdr/SWAA2024121057598.md): Floor Panel · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2024-701431<[01] FABRICATED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2610 SHEET: 20 REV: E. SEE INDIVIDUAL SIGN OFF BELOW.;[02] FABRICATED FLOOR PANEL 140BF AT
- [SDR SWAA2024121057599](https://openairdocs.org/sdr/SWAA2024121057599.md): Intercostal · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-701434<[01] STEP 5. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 210138103 AND DUE DATE: 10-JUN-25;[02] TOOL USED STEP 9 EDDY CURRENT EQUIPMENT PN: NORTE
- [SDR SWAA2024121057601](https://openairdocs.org/sdr/SWAA2024121057601.md): Intercostal · cracked · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS 500B TO BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-701436<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 500B TO BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG:143A7505 SHE
- [SDR SWAA2024121057602](https://openairdocs.org/sdr/SWAA2024121057602.md): Web · corroded · Nov 7, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R WL 156.1 AT FWD CARGO COMPARTMENT 2024-701438<[01] REPLACED SHIELD WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R WL 156.1 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-
- [SDR SWAA2024121257100](https://openairdocs.org/sdr/SWAA2024121257100.md): Pressure Web · cracked · Nov 6, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.187 INCH 2024-701393<[01] ON STEPS 6 AND 7; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210136503; DUE DATE: 24-JUL-25.;[02] PERFORMED PERMANENT
- [SDR SWAA2024121257103](https://openairdocs.org/sdr/SWAA2024121257103.md): Intercostal · cracked · Nov 6, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT PASSENGER CABIN 2024-701403<[01] REPLACED BREAK ASSY PANEL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG
- [SDR SWAA2024121257104](https://openairdocs.org/sdr/SWAA2024121257104.md): Intercostal · cracked · Nov 6, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-701404<[01] REPLACED BREAK ASSY PANEL LOCATED FLOOR STRUCTURE BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DW
- [SDR SWAA2024121257105](https://openairdocs.org/sdr/SWAA2024121257105.md): Support Angle · cracked · Nov 6, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2024-701405<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[
- [SDR SWAA2024121057351](https://openairdocs.org/sdr/SWAA2024121057351.md): Web · cracked · Nov 6, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON WEB LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-701412<[01] REPLACED WEB LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 143A7902; SHEET: 126;
- [SDR SWAA2024121257098](https://openairdocs.org/sdr/SWAA2024121257098.md): Stringer · cracked · Nov 5, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT LT WING 2024-687464<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25;[02] PERFORMED REPAIR CATEGORY A ON STRINGE
- [SDR SWAA2024121256719](https://openairdocs.org/sdr/SWAA2024121256719.md): Support Angle · cracked · Nov 4, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA 2024-687174<[01] REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR<BR>13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9<BR>DWG: 141A1311 SHEET: 1 REV: C SEE INDIVIDUAL SIGN OF
- [SDR SWAA2024121056510](https://openairdocs.org/sdr/SWAA2024121056510.md): Frame · cracked · Nov 4, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME LOCATED BS 259.5 AT LEVEL STRINGER 9L AT COCKPIT 2024-687094<[01] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED STA 259.5 BETWEEN STR 6R TO 11R AT PASSENGER CABIN IAW EA 24-153-03134-WIP1<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 <BR>P
- [SDR SWAA2024121256343](https://openairdocs.org/sdr/SWAA2024121256343.md): Rib · cracked · Nov 3, 2024 · N203WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB LE STA 114.55 OF ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER 2024-687053<[01] REPLACED RIB ON LE STA 114.55 OF ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 11 REV. A SEE INDIVIDUAL SIGN OFFS BELOW.;
- [SDR SWAA2024121256345](https://openairdocs.org/sdr/SWAA2024121256345.md): Rib · cracked · Nov 3, 2024 · N203WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB LE STA 151.75 OF ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER 2024-687064<[01] REPLACED RIB LE AND FASTENERA STA 151.75 OF ACCESS PANEL 331B AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A<BR>SEE INDIVIDU
- [SDR SWAA2024121256344](https://openairdocs.org/sdr/SWAA2024121256344.md): Skin · debonded · Nov 3, 2024 · N203WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST - DEBONDED OB AFT FLAP UPPER AND LOWER SURFACE AT LT WING 2024-687057<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED STEP 3: BOND TESTER; P/N: BONDMASTER 600M; S/N: 230106912; DUE DATE: 09 JAN 25.;[
- [SDR SWAA2024121255939](https://openairdocs.org/sdr/SWAA2024121255939.md): Web · cracked · Nov 2, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB SUPPORT BETWEEN BS 291.5 TO BS 303.9 AND SRINGER 16L AT PASSENGER CABIN 2024-687005<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED REPAIR CATEGORY B ON WEB SUPPORT BETWEEN BS 291.5 TO BS 303.9
- [SDR SWAA2024121255938](https://openairdocs.org/sdr/SWAA2024121255938.md): Tie Clip · cracked · Nov 2, 2024 · N203WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP BS 277 AND STRINGER 10R AT PASSENGER CABIN 2024-687004<[01] REMOVED TIE CLIP BS 277 AND STRINGER 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMADE. TIE CLIP MUST BE REPLACED DUE TO NO FO
- [SDR SWAA2024121255942](https://openairdocs.org/sdr/SWAA2024121255942.md): Support Angle · cracked · Nov 2, 2024 · N203WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK BODY FAIRING SUPOORT ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE 2024-686987<[01] REPLACED SUPOORT ANGLE ON BODY FAIRING BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG 116A3010 SHEET 21 REV A. SEE INDIVIDUAL S
- [SDR SWAA2024121055937](https://openairdocs.org/sdr/SWAA2024121055937.md): Frame · cracked · Nov 2, 2024 · N203WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FRAME BS 259.5 AND STRINGER 9R AT COCKPIT 2024-687003<[01] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED STA 259.5 BTW STR 6R TO 11R AT PASSENGER CABIN IAW EA 24-153-03139-WIP1 AND EA # 24-153-031349. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORMED PERMANE
- [SDR SWAA2024121055941](https://openairdocs.org/sdr/SWAA2024121055941.md): Fitting · deteriorated · Nov 2, 2024 · N203WN · Boeing 7377H4 · Escape Slide
  > DETERIORATED HARDWARE ON GIRTBART FITTING FWD AND AFT POSITION FWD ENTRY DOOR AT FWD GALLEY AREA 2024-687002<[01] REPLACED HARDWARE ON GIRTBART FITTING FWD AND AFT POSITION FWD ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED HARDW

Next page: https://openairdocs.org/aircraft/N203WN/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 = 'N203WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N203WN/reports

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