# Service difficulty reports: N432WN, cancelled Oct 4, 2024

A list on [N432WN, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N432WN-2024-10-04.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 5 · 237 reports

- [SDR SWAA2023122031843](https://openairdocs.org/sdr/SWAA2023122031843.md): Light · inoperative · Dec 14, 2023 · N432WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT ENTRY DOOR EMERGENCY LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION ENTRY AND MEASUREMENT TABLE.
- [SDR SWAA2023122031515](https://openairdocs.org/sdr/SWAA2023122031515.md): Battery Pack · failed · Dec 8, 2023 · N432WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS RELATED TO M1675 FAILED TEST.<[01] REMOVED AND REPLACED M1675 EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06-960-805. TEST STILL REQUIRED.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.;[03] PERFORMED GOOD TEST OF EMERGENCY BATTERY PAC
- [SDR SWAA2023122031516](https://openairdocs.org/sdr/SWAA2023122031516.md): Battery Pack · failed · Dec 8, 2023 · N432WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS RELATED TO M1674 FAILED TEST.<[01] REMOVED AND REPLACED M1674 EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06-960-805. TEST STILL REQUIRED.;[02] PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK PER AMM 33-51-06-960-805.;[03] VERIFIED CORRECTIVE ACTI
- [SDR SWAA2023122031517](https://openairdocs.org/sdr/SWAA2023122031517.md): Battery Pack · failed · Dec 8, 2023 · N432WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS RELATED TO M1673 FAILED TEST.<[01] REMOVED AND REPLACED M1673 EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06-960-805. TEST STILL REQUIRED.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.;[03] PERFORMED GOOD TEST OF EMERGENCY BATTERY PAC
- [SDR SWAA2022090247442](https://openairdocs.org/sdr/SWAA2022090247442.md): Tailpipe · fire · Aug 28, 2022 · N432WN · Boeing 737 · Engine (Turbine/Turboprop)
  > AIRCRAFT BEHIND US REPORTED TAILPIPE FIRE AS WE TOOK THE RUNWAY. #1 ENGINE. / [01] FOUND OIL PUDDLING IN THE CENTER PLUG CAVITY. PERFORMED FIM 71-05 TASK 811. CLEANED WET AREA AND PERFORMED IDLE RUN. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2022081843243](https://openairdocs.org/sdr/SWAA2022081843243.md): Retaining Clip · loose · Aug 17, 2022 · N432WN · Boeing 7377H4 · Emergency Equipment
  > FORWARD ENTRY GIRT BAR RETAINING CLIP LOOSE / [01] SECURED CLIP REF SIP
- [SDR SWAA2022051307349](https://openairdocs.org/sdr/SWAA2022051307349.md): Battery Pack · failed · May 13, 2022 · N432WN · Boeing 7377H4 · Emergency Lighting
  > AFT SERVICE DOOR OVERHEAD EXIT SIGN FAILS TO ILLUMINATE DURING E-LIGHT CHECK / [01] R/R'D M1672 E-LIGHT BATTERY PACK REF AMM 33-51-06
- [SDR SWAA2021121350803](https://openairdocs.org/sdr/SWAA2021121350803.md): None · cracked · Dec 7, 2021 · N432WN · Boeing 737 · Aerodynamic Fairings
  > SUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD TEE CLIP.; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD TEE CLIP. / [01] INSTALLED NEW TEE CLIP PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED NEW TEE CLIP PER SRM 51-40-02 AND
- [SDR SWAA2021121350802](https://openairdocs.org/sdr/SWAA2021121350802.md): Support Angle · cracked · Dec 7, 2021 · N432WN · Boeing 737 · Aerodynamic Fairings
  > SUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD VERTICAL SUPPORT ANGLE.; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD VERTICAL SPPORT ANGLE. / [01] INSTALLED NEW VERTICAL ANGLE PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED
- [SDR SWAA2021121350799](https://openairdocs.org/sdr/SWAA2021121350799.md): Panel · elongated · Dec 7, 2021 · N432WN · Boeing 737 · Aerodynamic Fairings
  > SUPPLEMENTAL INFORMATION: 194E PANEL HAS ELONGATED HOLES WITH CRACKS EXTENDING FROM HOLES AT SEVERAL PLACES. / [01] DRILLED; COUNTERSUNK; TRIMMED NEW 194 E PANEL <BR>REF SRM 51-20-07
- [SDR SWAA2021112244910](https://openairdocs.org/sdr/SWAA2021112244910.md): Web · corroded · Nov 17, 2021 · N432WN · Boeing 737* · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT DOORWAY LOWER SILL WEB HAS CORROSION ON SURFACE; / [01] BLENDED CORROSION AND VERIFIED WITH 10X MAG IAW SRM 53-60-15-1A-1; [02] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG.045'; LOSS.008'; REMAINING.037'. TOOL#40084; DUE 11AUG22; [0
- [SDR SWAA2021111944476](https://openairdocs.org/sdr/SWAA2021111944476.md): None · corroded · Nov 17, 2021 · N432WN · Boeing 737* · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOORWAY LOWER SILL WEB HAS CORROSION ON SURFACE; / [01] BLENDED CORROSION AND VERIFIED WITH 10X MAG IAW SRM 53-60-15-1A-1; [02] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG.045'; LOSS.008'; REMAINING.037'. TOOL#40084; DUE 11AUG22; [0
- [SDR SWAA2021110840212](https://openairdocs.org/sdr/SWAA2021110840212.md): Skin · cracked · Nov 4, 2021 · N432WN · Boeing 737* · Horizontal Stabilizer, Plate/Skin
  > L/H HORIZONTAL LOWER INSPAR SKIN CRACKED AT STAB STA.193.90; APPROX. 16' AFT OF FRONT SPAR. VERIFIED BY HFEC. 1' IN LENGTH.; / [01] EA SUMMARY ADDED TO THE FAULT.; [02] EA 21-155-03259WIP1 COMPLETED
- [SDR SWAA2021090714113](https://openairdocs.org/sdr/SWAA2021090714113.md): Megaphone · inoperative · Sep 1, 2021 · N432WN · Boeing 7377H4 · Emergency Equipment
  > MEGA PHONE INOP; / [01] R/R'D MEGA PHONE PER AMM 25-64-00. OPS CHECK @ THIS TIME.
- [SDR SWAA2020121034413](https://openairdocs.org/sdr/SWAA2020121034413.md): Light · inoperative · Dec 5, 2020 · N432WN · Boeing 7377H4 · Emergency Lighting
  > R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERABLE. RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT, AS PER BOEING B737 AMM 33-51-04-960-801 AND OPERATIONAL TEST OK.
- [SDR SWAA2020121034414](https://openairdocs.org/sdr/SWAA2020121034414.md): Connector · inoperative · Dec 5, 2020 · N432WN · Boeing 7377H4 · Light System Wiring
  > INTERIOR OVERWING EXIT SIGN RIGHT SIDE INOPERABLE. CONNECTED INTERIOR RIGHT OVERWING EXIT SIGN CONNECTORS D12392 AND D12394, AS PER BOEING B737 AMM 33-51-010-960-802. OPERATIONAL CHECK NORMAL.
- [SDR SWAA2021072733848](https://openairdocs.org/sdr/SWAA2021072733848.md): Angle · cracked · Dec 3, 2020 · N432WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING L/E I/B ON TOP OF FUEL BOOST PUMP FOUND ANGLE CRACKED. P/N 116A3939-2 / REMOVED AND REPLACED CRACK ANGLE ON R/H WING L/E I/B ON BOOST PUMP AREA PER REF SRM 57-20-10-1A-3; ANGLE P/N 116A3939-2
- [SDR SWAA2021072733621](https://openairdocs.org/sdr/SWAA2021072733621.md): Angle · cracked · Dec 2, 2020 · N432WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING L/E I/B ON TOP OF BOOST PUMP FOUND ANGLE CRACKED P/N 116A3939-1 / REMOVED AND REPLACED LEFT WING L/E I/B ANGLE ON TOP OF BOOST PUMP P/N 116A3939-1 REF B737-7 SRM 57-20-10-1A-3 ALLOWABLE DAMAGE
- [SDR SWAA2021071631746](https://openairdocs.org/sdr/SWAA2021071631746.md): Baffle · cracked · Nov 18, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP BAFFLE ASSY CRACKED BETWEEN BS 500B AND 500C RBL-21 / REPLACED BAFFLE @ FWD CARGO COMP BETWEEN STA 500B & 500C @ RBL21 AS PER B737-700 SRM 51-40-02-0G-0
- [SDR SWAA2021071631747](https://openairdocs.org/sdr/SWAA2021071631747.md): Baffle · cracked · Nov 18, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMP BAFFLE ASSY CRACKED BETWEEN BS 500B AND 500C LBL-21. / REPLACED BAFFLE ASSY @ FWD CARGO COMP. BETWEEN STA 500B AND 500C LBL-21/ AS PER B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2021072930141](https://openairdocs.org/sdr/SWAA2021072930141.md): Rib · cracked · Nov 12, 2020 · N432WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > DORSAL FIN RIB AT STA 867; RIB CRACK / REMOVED AND REPLACED DAMAGED RIB DORSAL FIN STA 867' PER REF B737 SRM 51-40-02-0G-0
- [SDR SWAA2021081029619](https://openairdocs.org/sdr/SWAA2021081029619.md): Tie Down · corroded · Nov 11, 2020 · N432WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPT;SHOWS NET TIE-DOWN PLATE WITH SURFACE CORROSION;JUST AFT OF B.S.787 STR.25L.(MKD 26-002) / RECEIVED NEW TIE DOWN PLATE P/N 41901-102; NEW NET TIE DOWN PLATE TO BE INSTALLED ON T/C 753-105-01-01
- [SDR SWAA2021021129736](https://openairdocs.org/sdr/SWAA2021021129736.md): Channel · corroded · Nov 11, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS FOUND FWD CARGO COMPARTMENT RH 'Z' CHANNEL FROM STA 500A TO STA 500D RBL 21 @ WL 153.5 / REPLACED R/H 'Z' CHANNEL @ FWD CARGO COMP. FROM STA 500A TO STA 500D RBL 21 @ WL 153.5 AS PER B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2021021129508](https://openairdocs.org/sdr/SWAA2021021129508.md): Support Angle · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS FOUND AT FWD CARGO AT STA 500D LOWER ANGLE SUPPORT AT LBL 10 AND LBL 21 AT WL 153.5 / REMOVED AND REPLACED LWR SUPPORT ANGLE AT FWD CARGO ON STA 500D BETWEEN LBL21 AND RBL 21 WL 153.5 REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481.
- [SDR SWAA2021021129506](https://openairdocs.org/sdr/SWAA2021021129506.md): Channel · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS FOUND AT FWD CARGO LH 'Z' CHANNEL FROM STA 400 TO STA 500D LBL 21 AT WL 153.5 / FWD CARGO L/H Z CHANNEL FROM STA 400 TO STA 500D CORROSION FOUND OUT OF LIMITS REF B737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED AND REPLACED Z CHANNEL BETWE
- [SDR SWAA2021021129503](https://openairdocs.org/sdr/SWAA2021021129503.md): Channel · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS FOUND FWD CARGO COMPARTMENT RH 'Z' CHANNEL FROM STA 500 TO STA 500A AND WL153.5 @ RBL 21. / REPLACED RH Z CHANNEL @ FWD CARGO COMPARTMENT FROM STA 500 TO 500A RBL 21 & WL 153.5 AS PER B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2021021129504](https://openairdocs.org/sdr/SWAA2021021129504.md): Strap · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SPOTS FOUND AT FWD CARGO STA 500 RBL 21 AND WL 153.5 / REMOVED CORROSION AT FWD CARGO STA 500 RBL 21 AND WL 153.5 OROGINAL MAT.100'; MAT LOSS.014'; MAT REMAINING.086' FOUND OUT OF LIMITS REMOVED AND REPLACED STARP AS PER B737-7 SRM 51-40-02-0G-0;
- [SDR SWAA2021021129497](https://openairdocs.org/sdr/SWAA2021021129497.md): Support Angle · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > L1 DOOR THRESHOLD @ STA328 - STA344 LBL 60 WL 208 L ANGLE SUPPORT HAS CORROSION. / REPLACED L ANGLE SUPPORT @ L1 DOOR THERSHOLD @ STA 328 - STA 344 LBL 60 WC 208 AS PER B737-700 SRM 51-40-02-06-0
- [SDR SWAA2020121429498](https://openairdocs.org/sdr/SWAA2020121429498.md): Crease Beam · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION, MAIN CABIN FLOOR CREASE BEAM INNER CHORD AT FASTENERS HEAD RBL 55 STA 616 &STA 639, MARKED DOTS 60-023. REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD AT MAIN CABIN FLOOR BETWEEN STA 626 TO STA 673 RBL 55', REF B737-7 SRM 51-40-0G-0 AND DWG NR 1
- [SDR SWAA2020121029301](https://openairdocs.org/sdr/SWAA2020121029301.md): Channel · corroded · Nov 10, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION R2 DOOR Z-CHANNEL HAS CORROSION BETWEEN STA 951 TO STA 992 RBL 51 (203-011). REMOVED AND REPLACED R2 DOOR INNER CHORD, PER REF B737-700 SRM51-40-02-0G-0 AND DWG 147A8501.
- [SDR SWAA2021040729136](https://openairdocs.org/sdr/SWAA2021040729136.md): Floor Panel · cracked · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > R/H CABIN FLOOR PANEL 232SF UPPER FWD I/B CORNER CRACKED. (18-034) / CLEANED AND REPAIRED PANEL #232SF AT I/B CORNER IN ACCORDANCE TO B737-7 SRM 53-00-50-2R-0. MATERIALS USED PO# 1693338 COMPOUND
- [SDR SWAA2020121429138](https://openairdocs.org/sdr/SWAA2020121429138.md): Floor Panel · damaged · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 232HF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-039). REMOVED AND REPLACED FLOOR BOARD PANEL AT MAIN CABIN NR 232HF, IN REF B737-700 AMM 53-21-00-000-801 AND AMM 53-21-00-400-801 PO NR 169444 AAR ISSUE TAG FL3269.
- [SDR SWAA2020121429139](https://openairdocs.org/sdr/SWAA2020121429139.md): Floor Panel · damaged · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 232GF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-040). REMOVED AND REPLACED RT CABIN FLOOR PANEL 232GF, REF B737-700 AMM 53-21-00-000-801 AND 53-21-00-400-801.
- [SDR SWAA2020121429140](https://openairdocs.org/sdr/SWAA2020121429140.md): Floor Panel · damaged · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 232EF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-041). REMOVED AND REPLACED RT CABIN FLOOR PANEL 232EF, REF B737-7 AMM 53-21-00-000-801 AND 53-21-00-400-801.
- [SDR SWAA2020121429493](https://openairdocs.org/sdr/SWAA2020121429493.md): Frame · corroded · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Main, Frame
  > RT FWD WET AREA FLOOR AT STA 328 RBL 48-RBL 56 FRAME UPPER AND LOWER SURFACES HAS CORROSION (18-047). ACCOMPLISHED THIS N/R ON EA NR 1-A53-8530 REV.
- [SDR SWAA2020121029145](https://openairdocs.org/sdr/SWAA2020121029145.md): Floor Support · cracked · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LT FWD WET AREA FLOOR AT STA 294.5-STA 312 LBL 55 INNER CHORD UPPER SURFACE CRACKED (18-046). REPLACED INNER CHORD AT LT FWD WET AREA FLOOR AT STA 312-394.5 LBL 55, AS PER B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2020121029141](https://openairdocs.org/sdr/SWAA2020121029141.md): Floor Support · cracked · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR AT STA 344-STA 360 BL 0 INTERCOSTAL UPPER SURFACE CRACKED (18-042). REPLACED INTERCOSTAL AT FWD WET AREA FLOOR AT STA 344-STA 360 BL, AS PER B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR SWAA2020121029147](https://openairdocs.org/sdr/SWAA2020121029147.md): Floor Support · cracked · Nov 9, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RT FWD WET AREA FLOOR AT STA 312-STA 328 RBL 30.5 INTERCOSTAL CRACKED (18-049). REMOVED AND INSTALLED NEW INTERCOSTAL AT RT FWD AREA BETWEEN STA 312-328 RBL 30.5', REF B737-7 SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR SWAA2021040728828](https://openairdocs.org/sdr/SWAA2021040728828.md): Pressure Deck · damaged · Nov 8, 2020 · N432WN · Boeing 7377H4 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR DAMAGED / INSTALLED REPAIR AT FLIGHT DECK FLOOR FABRICATED TWO (2) DOUBLERS MAT USED 2024 T3.050 PO# 1484683 AND ONE WEB MAT USED 2024 T3.040 PO# 1691232; TREATED AND PRIMED REPAIR AS PER B737-7 SRM 51-40-02-0G-0; 51-20-13-0G-0; 51-30-01; 5
- [SDR SWAA2021011129134](https://openairdocs.org/sdr/SWAA2021011129134.md): Floor Panel · peeling · Nov 8, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > CENTER CABIN FLOOR PANEL 241DF UPPER SURFACE HAS MATERIAL PEELING (18-038). REPAIRED PANEL 241DF IN ACCORDANCE WITH B737-7 SRM 53-00-50-2R-1. REPAIRED TOP SURFACE. MATERIALS USED RESIN PO 1691358.
- [SDR SWAA2021011129130](https://openairdocs.org/sdr/SWAA2021011129130.md): Floor Panel · peeling · Nov 8, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 232RF UPPER SURFACE HAS MATERIAL PEELING (18-032). REPAIRED PANEL NR 232RF AT UPPER SURFACE IN ACCORDANCE TO B737-700 SRM 53-00-50-2R1 MATERIAL USED RESIN PO 1691358.
- [SDR SWAA2020121029133](https://openairdocs.org/sdr/SWAA2020121029133.md): Floor Panel · peeling · Nov 8, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 242CF UPPER SURFACE HAS MATERIAL PEELING (18-037). REPAIRED FLOOR PANEL 242CF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1. MATERIAL USED PO: 1688495 AND PO3 1480720.
- [SDR SWAA2020121029132](https://openairdocs.org/sdr/SWAA2020121029132.md): Floor Panel · peeling · Nov 8, 2020 · N432WN · Boeing 7377H4 · Fuselage Floor Panel
  > RT CABIN FLOOR PANEL 242DF UPPER SURFACE HAS MATERIAL PEELING (18-036). REPAIRED RT CABIN FLOOR PANEL NR 242DF UPPER SURFACE, IN ACCORDANCE TO B737-7 SRM 53-00-50-2R-1. MATERIALS USED RESIN PO 1691358.
- [SDR SWAA2021052528807](https://openairdocs.org/sdr/SWAA2021052528807.md): Gusset · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AT STA 500D S-21L GUSSET BRACKET CRACK. 227-009 / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP AT STA 500D S-21L IN REF B737-700 SRM 51-40-02-0G-0 AND DWG #143A9481.
- [SDR SWAA2021052528808](https://openairdocs.org/sdr/SWAA2021052528808.md): Gusset · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT RH SIDE AT STA 500D S-19R GUSSET BRACKET CRACK. 227-010 / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP FROM STA 500D S-19R IN REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481
- [SDR SWAA2021052528806](https://openairdocs.org/sdr/SWAA2021052528806.md): Gusset · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AT STA 500D S-19L GUSSET BRACKET CRACK. 227-008 / REMOVED ANS REPLACED GUSSET AT FWD CARGO COMP FROM STA 500D S-19L IN REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481
- [SDR SWAA2020121028804](https://openairdocs.org/sdr/SWAA2020121028804.md): Stiffener · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER RIB NR 4 HAS A CRACK. REPAIRED LEFT HORIZONTAL STABILIZER MACHINED INSPAR RIB NR 4 STIFFENER NR 3, PER REF B737-700 SRM 55-10-09-2R-4 REPAIR 4.
- [SDR SWAA2020121028810](https://openairdocs.org/sdr/SWAA2020121028810.md): Stiffener · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER RIB NR 4 STIFFENER NR 3 CRACK. REPAIRED HORIZONTAL STAB MACHINED INSPAR RIB NR 4 STIFFENER NR 3, PER REF B737-700 SRM 55-10-09-2R-4. RIGHT HORIZONTAL STAB.
- [SDR SWAA2020121028801](https://openairdocs.org/sdr/SWAA2020121028801.md): Angle · cracked · Nov 6, 2020 · N432WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > LT LOWER FUSELAGE AT STA 663.75 LBL 44 VAPOR BARRIER ANGLE HAS SUSPECT CRACK. ACCOMPLISHED REPLACEMENT ANGLE AT LT LOWER FUSELAGE STA 663 BETWEEN LBL 20' TO LBL 60' VAPOR BARRIER ANGLE, REF B737-7 SRM 57-10-10-2R-5 FIG 202 AND DWG 111A1000. LEAK CHECK BEING
- [SDR SWAA2021072628562](https://openairdocs.org/sdr/SWAA2021072628562.md): Skin · cracked · Nov 4, 2020 · N432WN · Boeing 7377H4 · Leading Edge Devices
  > L/H WING #4 SLAT LOWER SURFACE AT ACTUATOR RIB HAS A CRACK AROUND 1 FASTENER. / REPAIRED L/H WING #4 SLAT LEADING EDGE NOSE SKIN LOWER SURFACE AT ACTUATOR RIB PER REF B737-700 SRM 57-42-01-2R-8; REPAIR 8. AND EA NO. 20-157-02240 REV IR

Next page: https://openairdocs.org/deregistered/N432WN-2024-10-04/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 = 'N432WN' AND deregistration_id = 'N432WN-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N432WN-2024-10-04/reports

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