# Service difficulty reports: N430WN, cancelled Oct 4, 2024

A list on [N430WN, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N430WN-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 6 · 270 reports

- [SDR SWAA2023102712945](https://openairdocs.org/sdr/SWAA2023102712945.md): Light · inoperative · Oct 21, 2023 · N430WN · Boeing 7377H4 · Emergency Lighting
  > L/H EXTERIOR OVERWING EMERGENCY LIGHT INOP.<[01] RELAMPED L/H EXTERIOR OVERWING EMERGENCY LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023102712946](https://openairdocs.org/sdr/SWAA2023102712946.md): Light · inoperative · Oct 21, 2023 · N430WN · Boeing 7377H4 · Emergency Lighting
  > L/H EXTERIOR GROUND EMERGENCY LIGTH INOP.<[01] RELAMPED L/H EXTERIOR GROUND EMERGENCY LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023103010385](https://openairdocs.org/sdr/SWAA2023103010385.md): Battery Pack · failed · Oct 12, 2023 · N430WN · Boeing 7377H4 · Emergency Lighting
  > ALL EMERGENCY LIGHTS FAILS TEST; DUE TO STORAGE OF THE AIRCRAFT ALL EMERGENCY LIGHTS FAILS TEST DUE TO STORAGE OF THE AIRCRAFT<[01] REMOVED AND REPLACED SERVICEABLE BATTERY PACKS M1668; M1669; M1670; M1672; M1673; M1674 AND M1675.;[02] VERIFIED CORRECTIVE ACTI
- [SDR SWAA2022040490280](https://openairdocs.org/sdr/SWAA2022040490280.md): Flashlight · inoperative · Mar 31, 2022 · N430WN · Boeing 7377H4 · Emergency Equipment
  > ALL 4 EMERGENCY FLASHLIGHTS INOP. ALL NOT BLINKING. / [01] REMOVED AND REPLACED 4 EACH BATTERIES REF AMM 25-64-00
- [SDR SWAA2022040490865](https://openairdocs.org/sdr/SWAA2022040490865.md): Flashlight · inoperative · Mar 31, 2022 · N430WN · Boeing 7377H4 · Emergency Equipment
  > ALL 4 EMERGENCY FLASHLIGHTS INOP. ALL NOT BLINKING. / [01] REMOVED AND REPLACED 4 EACH BATTERIES REF AMM 25-64-00
- [SDR SWAA2021121350797](https://openairdocs.org/sdr/SWAA2021121350797.md): Panel · delaminated · Dec 7, 2021 · N430WN · Boeing 737 · Nacelle/Pylon Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: 444BR AFT STRUT FAIRING DELAM.; / [01] REMOVED AND REPLACED AFT STRUT FAIRING PANEL 444BR PER SRM 51-40-02
- [SDR SWAA2021110540208](https://openairdocs.org/sdr/SWAA2021110540208.md): Transmitter · failed · Nov 4, 2021 · N430WN · Boeing 7377H4 · Trailing Edge Flap Control System
  > FLAPS WOULD NOT MOVE TO COMMANDED POSITION WITH THE LEVER. FLAPS WENT TO APPROX 13 DEGREES AND HAD TO EXTEND TO 15 WITH ALTERNATE EXTENSION; / [01] REMOVED AND REPLACED RIGHT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK NORMAL.
- [SDR SWAA2021092119275](https://openairdocs.org/sdr/SWAA2021092119275.md): Slide · loose · Sep 17, 2021 · N430WN · Boeing 7377H4 · Escape Slide
  > AFT LEFT ESCAPE SLIDE CASE HAS LOOSE SCREW; / [01] RESECURED SLIDE CASE REF AMM 25-66-01
- [SDR SWAA2021072095004](https://openairdocs.org/sdr/SWAA2021072095004.md): Rivet · sheared · Jul 16, 2021 · N430WN · Boeing 7377H4 · Emergency Equipment
  > CABIN L1 FWD. ENTRY DOOR GIRT BAR AFT STOW BRACKET NOT SECURE.(MARKED) / [01] FOUND RIVET SHEARED ON BRACKET. R&R FASTENER PER SRM 51-40-02
- [SDR SWAA2021071592870](https://openairdocs.org/sdr/SWAA2021071592870.md): Bulb · inoperative · Jul 11, 2021 · N430WN · Boeing 7377H4 · Passenger Compartment Lighting
  > FLT ATTDT REPORTS AFT GALLEY LIGHT BURNT OUT WITH SCORCH MARKS AND ELECTRICAL SMELL.; / [01] REMOVED AND REPLACED RH AFT GALLEY WORK LIGHT BULB PER MM 33-26-01; OPS CHECK GOOD. INSPECTED SOCKET ASSY WITH NO DEFECTS NOTED. PERFORMED SMOKE OR FUMES IN CABIN CON
- [SDR SWAA2021051349505](https://openairdocs.org/sdr/SWAA2021051349505.md): Fairing · damaged · Feb 17, 2021 · N430WN · Boeing 7377H4 · Aerodynamic Fairings
  > 193 FAIRING PANEL HAS MULITPLE ELONGATED HOLES (LOCATIONS 30-38) / REMOVED AND REPLACED PNL 193B REF SRM 51-40-02; AMM 53-51-21
- [SDR SWAA2020102725392](https://openairdocs.org/sdr/SWAA2020102725392.md): Bracket · corroded · Oct 22, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION, THREE AFT ENTRY AND GALLEY GRIT BAR FLOOR BRACKETS IS CORRODED. THREE AFT ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS FOUND TO BE OUT OF LIMITS AND THEY WERE REPAIRABLE BY REPLACEMENT, IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED AND RELACED BRACKETS, IAW
- [SDR SWAA2020102725272](https://openairdocs.org/sdr/SWAA2020102725272.md): Light · inoperative · Oct 22, 2020 · N430WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT EMERGENCY SLIDE GROUND LIGHT. L548 DOES NOT ILLUMINATE. RELAMPED RIGHT EMERGENCY SLIDE GROUND LIGHT L548. PERFORMED A GOOD FUNCTIONAL CHECK, PER AMM 33-51-04-960-801. 59234U 23OCT20.
- [SDR SWAA2021052522536](https://openairdocs.org/sdr/SWAA2021052522536.md): Bushing · corroded · Oct 12, 2020 · N430WN · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > ***CORROSION*** RMLG FWD TRUNNION SUPPORT FITTING BUSHING O/B FACES ALL FOUR LOCATION S / REPAIRED BUSHING O/B FACES 4EA PER CC# 1-A57-3246; WORKED ACCOMPLISHED BY OUTSIDE VENDOR FAA FORM 8130-3 TRACKING # 805315 SWA WO# 31165
- [SDR SWAA2021051321292](https://openairdocs.org/sdr/SWAA2021051321292.md): Plate · broken · Oct 6, 2020 · N430WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING T/E WIGGLE PLATE AT ORSS 375 HAS BROKEN PHENOLIC / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 375 P/N.115A3760-49 IAW.SRM 51-40-02 AND DWG 115A3700 88920U 10OCT20
- [SDR SWAA2021051321291](https://openairdocs.org/sdr/SWAA2021051321291.md): Plate · cracked · Oct 5, 2020 · N430WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING WIGGLE PLATE AT ORSS 404.0 IS BENT AND PHENOLIC IS CRACKED / REMOVED AND REPLACED LEFT WING WIGGLE PLATE AT ORSS 404.0 P/N 115A3760-13 IAW SRM 51-40-02 AND DWG 115A3700 AND DWG 115A3711 88920U 13OCT20
- [SDR SWAA2020102720887](https://openairdocs.org/sdr/SWAA2020102720887.md): Shear Web · cracked · Oct 3, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > SHEAR WEB CRACKED BS 986.5, LBL 45, WL 208. REMOVED AND REPLACED SHEAR WEB FROM BS 986.5 TO BS 1016 LBL 45, WL 208, IAW SRM 51-40-02 AND DWG 147A5600.
- [SDR SWAA2021081320882](https://openairdocs.org/sdr/SWAA2021081320882.md): Web · cracked · Oct 1, 2020 · N430WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING FIXED T/E PANEL AFT OF NO.1 PYLON LOWER WEB HAS A CRACK AROUND FASTENER ORSS277. MARKED / REMOVED AND REPLACED L/H FIXED T/E UPPER PANEL LOWER WEB ORSS 277 IAW SRM 51-40-02-0G-0 57083U 03OCT20
- [SDR SWAA2021051320885](https://openairdocs.org/sdr/SWAA2021051320885.md): Plate · cracked · Oct 1, 2020 · N430WN · Boeing 7377H4 · Wing Main, Frame Structure
  > FOUND R/H WIGGLE PLATE AT ORSS261 LWR FLANGE TO BE CRACKED / REMVOED AND REPLACED R/H WIGGLE PLATE AT ORSS261 LWR FRAMES P/N 115A2781-14 IAW. SRM 51-40-02 AND AIPC 57-50-00-30. 88920U 10OCT20.
- [SDR SWAA2021051320883](https://openairdocs.org/sdr/SWAA2021051320883.md): Plate · cracked · Oct 1, 2020 · N430WN · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING T/E WIGGLE PLATE IS CRACKED ORSS261. / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE @ ORSS 261 COMMON TO T/E ACCESS PANEL 551GB IAW SRM 51-40-02-0G-0 CHEMICAL CONVERSION COATING APPLIED TO BARE METAL AREAS IAW AMM 51-21-41-370-802 PRIMER & DECORAT
- [SDR SWAA2020102820352](https://openairdocs.org/sdr/SWAA2020102820352.md): Stiffener · cracked · Oct 1, 2020 · N430WN · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LT HORIZONTAL STAB RIB 120.30 HAS A CRACK ON THE 2ND VERTICAL STIFFENER FROM FWD AT LOWER END. TRIMMED OUT THE DAMAGE PART AT LT HORIZONTAL STAB RIB 120.30 2ND VERTICAL STIFFENER LOWER END AND INSTALLED REPAIR PARTS, IAW SRM 55-10-09-2R-4 88920U 06OCT20.
- [SDR SWAA2021081620276](https://openairdocs.org/sdr/SWAA2021081620276.md): Shear Web · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON SHEAR WEB AT B.S. 1028; L.B.L. 4; W.L. 208.1. / SHEAR WEB AT B.S. 1028 LBL 4 REPAIRED IAW ATS ER 20-03382; REV IR; DATED 09-OCT-2020 AND PER EA NO: 20-153-01983 REV IR 55981U 20OCT20
- [SDR SWAA2021081620275](https://openairdocs.org/sdr/SWAA2021081620275.md): Shear Web · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON SHEAR WEB AT B.S. 1016; L.B.L. 5; W.L. 208.1. / SHEAR WEB AT B.S. 1016; LBL 5 REPAIRED IAW ATS ER 20-03382; REV IR; DATED 09-OCT-2020 AND PER EA NO: 20-153-01983 REV IR. 55981U 20OCT20
- [SDR SWAA2021081620307](https://openairdocs.org/sdr/SWAA2021081620307.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON STRAP AT PASSENGER CABIN BS713 LBL65 WL202. MARKED / PAX CABIN STRAP AT BS 713 LBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20
- [SDR SWAA2021081620312](https://openairdocs.org/sdr/SWAA2021081620312.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON STRAP AT PASSENGER CABIN BS708 RBL65 WL202. / PAX CABIN STRAP AT BS 708 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20
- [SDR SWAA2021081620313](https://openairdocs.org/sdr/SWAA2021081620313.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON STRAP AT PASSENGER CABIN BS713 RBL65 WL202. / PAX CABIN STRAP BS 713 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20
- [SDR SWAA2021081620309](https://openairdocs.org/sdr/SWAA2021081620309.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON STRAP AT PASSENGER CABIN BS694 LBL65 WL202. MARKED / PAX CABIN STRAP AT BS 694 LBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20
- [SDR SWAA2021081620314](https://openairdocs.org/sdr/SWAA2021081620314.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON STRAP AT PASSENGER CABIN BS719 RBL65 WL202. / PAX CABIN STRAP AT BS 719 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR 55981U 14OCT20
- [SDR SWAA2021081620280](https://openairdocs.org/sdr/SWAA2021081620280.md): Channel · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT SERVICE DOOR MOP SILL AT B.S. 950-995; R.B.L. 52; W.L. 208.1. / REMOVED AND INSTALLED NEW AFT SERVICE DOOR MOP SILL AT B.S. 907- BS 995; RBL 52 WL 208.1 ITEM #7530246 IAW SRM 51-40-02-0G-0; SRM 53-70-15-1A-1; SRM 53-70-15-01-1; SRM 51-40
- [SDR SWAA2021081620335](https://openairdocs.org/sdr/SWAA2021081620335.md): Cargo Track · cracked · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ACB CARGO FLOOR TRACK IS CRACKED. BS 767; LBL 17; WL 156 / REMOVED AND REPLACED ON ACB CARGO FLOOR TRACK BS727 TO BS 867 LBL17 WL156. RECEIVED NEW TRACK ITEM 7531208 PO# 804224. LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02; DWG 146A7500 AND DWG 149A8102
- [SDR SWAA2021081520282](https://openairdocs.org/sdr/SWAA2021081520282.md): Channel · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT ENTRY DOOR MOP SILL AT B.S. 950-986; L.B.L. 52; W.L. 208.1. / REMOVED CORROSION ON AED MOPSILL BS 950-986 LBL 52 ORIGINAL THICKNESS.080' MAT LOSS MORE THAN 30% IN AN AREA OF 30' X-2'.0 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1; RE
- [SDR SWAA2021081520288](https://openairdocs.org/sdr/SWAA2021081520288.md): Channel · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FORWARD ENTRY DOOR MOP SILL AT B.S. 312-344; L.B.L. 55; W.L. 208.1. / REMOVED CORROSION ON FWD ENTRY DOOR MOPSILL; THE LOST MATERIAL IS MORE THAN 10% REMAINING THICKNESS IS.050' ORIGINAL THICKNESS IS.080' THEREFORE FOUND TO BE OUT OF LIMIT
- [SDR SWAA2021081520323](https://openairdocs.org/sdr/SWAA2021081520323.md): Support · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727- 767; RBL 20; WL 157 / EVALUATED DAMAGE ON FLOOR TO SIDEWALL SUPPORT BS 727 - 767 RBL 20 WL 157 MORE THAN 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB FLOOR TO
- [SDR SWAA2021081320334](https://openairdocs.org/sdr/SWAA2021081320334.md): Angle · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ACB WATER SERVICE PAN; FWD ANGLE HAS CORROSION AND AFT ANGLE IS CRACKED. BS 907- 927; RBL 8- 18; WL 170 / REMOVED AND REPLACED 2EA ANGLES AT ACB WATER SERVICE PAN PER SRM 51-40-02; SRM 51-40-05 AND DWG. 147A7221. 91195U 10-9-20
- [SDR SWAA2021081323168](https://openairdocs.org/sdr/SWAA2021081323168.md): Strap · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON TENSION STRAP AT B.S. 1017-1030; L.B.L. 3; W.L. 208.1. / REMOVED AND REPLACED TENSION STRAP BS1006 TO 1030 LBL3; WL208.1 DUE TO NO ALLOWABLE LIMIT; FOUND ON SRM FOR THIS PART IAW SRM 51-40-02 & REF DWG 147A5600 REV H DATED 03/04/08
- [SDR SWAA2021081220293](https://openairdocs.org/sdr/SWAA2021081220293.md): Gate · cracked · Sep 30, 2020 · N430WN · Boeing 7377H4 · Service Doors
  > ASD LOWER GATE SKIN HAS A CRACK AT THE AFT EDGE / REMOVED AND REPLACED ASD LOWER GATE PER AMM 52-41-31-000-802 AMM 52-41-31-400-802; AMM 52-09-12-000-801; AMM 52-09-12-400-801; AMM 52-41-61-400-801; AMM 52-41-61-000-801; AMM 52-41-00-820-801; AMM 52-09-00-700-
- [SDR SWAA2021080320324](https://openairdocs.org/sdr/SWAA2021080320324.md): Support · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727- 727E; LBL 20; WL 157 REJECTED DUE TO FASTENER NOT INSTALLED AT BS. 727 AT FWD END; LOWER SIDE AND B.S 747 FWD OF FRAME. / REMOVED - ACB FLOOR TO SIDEWALL SUPPORT INSTALLED FASTENER AT BODY STATION 727 AT FW
- [SDR SWAA2021072120333](https://openairdocs.org/sdr/SWAA2021072120333.md): Floorbeam · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > ***CORROSION*** ACB IN FLOOR SUPPORT 'T' ANGLE; AT FASTENER; BS 794; RBL 18; WL 157 / REMOVED AND REPLACED ON ACB IN FLOOR SUPPORT 'T' ANGLE AT FASTENER BS794; RBL18; WL157. IAW SRM 51-40-02 AND DWG 146A7500 80641U 05OCT20
- [SDR SWAA2021072020328](https://openairdocs.org/sdr/SWAA2021072020328.md): Attach Angle · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > ***CORROSION*** ON ATTACH ANGLE AT MAIN EBAY BS320 LBL53 WL182. / REMOVED AND INSTALLED NEW ATTACH ANGLE AT MAIN EBAY BS320 LBL53 FROM BAC1490-2503# 7075T62C PO# 804408 LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 141A8143. APPLIED CHEMICAL CONVERSION COATING
- [SDR SWAA2021072020322](https://openairdocs.org/sdr/SWAA2021072020322.md): Attach Angle · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACH ANGLE AT MAIN EBAY BS328 LBL53 WL182. / REMOVED AND INSTALLED NEW ON ATTACH ANGLE AT MAIN EBAY BS328 LBL53 FROM BAC 1490-2503 #7075T62C PO# 804408 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-20-01; AND DWG 141A8140
- [SDR SWAA2021072020317](https://openairdocs.org/sdr/SWAA2021072020317.md): Attach Angle · cracked · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT PASSENGER CABIN BS692 RBL1 WL207. / REMOVED & REPLACED ATTACH ANGLE AT PASSANGER CABIN BS692 RBL1 WL207 PER SRM 51-40-02-0G-0 & DWG# 273A9112
- [SDR SWAA2021071620337](https://openairdocs.org/sdr/SWAA2021071620337.md): Shield · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ACB SIDE SHIELD AT FASTENER HOLE BS 854; RBL21; WL 167 / REMOVED AND REPLACED ACB AFT SHIELD PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A0081. 91195U 10-6-20 SHIELD REPLACED AT STA.847-867 R/H SIDE WL167. 91195U 10-6-20
- [SDR SWAA2021071620326](https://openairdocs.org/sdr/SWAA2021071620326.md): Shield · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ACB FLOOR SIDE SHIELD BS 767- 787; RBL 22; WL 157 / REMOVED AND REPLACED AT ACB FLOOR SIDE SHIELD BS 767-787 RBL 22 P/N 146A8127U12 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 146A0081 80641U 8OCT20
- [SDR SWAA2021071420330](https://openairdocs.org/sdr/SWAA2021071420330.md): Support Angle · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ACB ON INTERCOSTAL SUPPORT ANGLE BELOW SIDE SHIELD; BS 767- 787; RBL 21; WL 157 / REMOVED AND REPLACED ACB ON INTERCOSTAL SUPPORT ANGLE BELOW SIDE SHIELD BS 767-787 RBL 21 WL 157 IAW SRM 51-40-02 REF DWG 146A8123 89004U 06OCT20
- [SDR SWAA2021071420331](https://openairdocs.org/sdr/SWAA2021071420331.md): Support Angle · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ACB AT FASTENER IN THRESHOLD INTERCOSTAL SUPPORT ANGLE; BS 794; RBL 19; WL 155 / REMOVED AND REPLACED ON ACB AT FASTENER IN THRESHOLD INTERCOSTAL SUPPORT ANGLE. BS794; RBL19 WL155 IAW SRM 51-40-02 AND DWG 146A0082. 05OCT20
- [SDR SWAA2021071420290](https://openairdocs.org/sdr/SWAA2021071420290.md): Floor Support · cracked · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > DAMAGED FLOOR SUPPORT AT B.S. 312-328; L.B.L. 47; W.L. 208.1. / FLOOR SUPPORT IS ELONGATED HOLE AND CRACKED THEREFORE FOUND TO BE OUT OF LIMIT PER REF B737 SRM 53-10-51-1A-1 PARAGRAPH IB. REMOVED AND REPLACED INTERCOSTAL PER REF SRM 51-40-02-0G AND DWG NBR 141
- [SDR SWAA2020102820292](https://openairdocs.org/sdr/SWAA2020102820292.md): Support Fitting · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION, FORWARD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 344 LBL 55 WL 208.1. THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE. THEREFORE, WILL BE REPAIRED BY REPLACEMENT, PER SRM 51-10-02-0G-0 PARAGRAPH 9. 92462R 02OCT20 INSP 46 02OCT20. REMOVED FWD ENTRY DOO
- [SDR SWAA2020102820291](https://openairdocs.org/sdr/SWAA2020102820291.md): Support Fitting · corroded · Sep 30, 2020 · N430WN · Boeing 7377H4 · Emergency Equipment
  > CORROSION, FORWARD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 312 LBL 53 WL 208.1. THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE. THEREFORE, WILL BE REPAIRED BY REPLACEMENT, PER SRM 51-10-02-0G-0 PARAGRAPH 9. 92462R 02OCT20 INSP 46 02OCT20. REMOVED FWD ENTRY DOO
- [SDR SWAA2020102824708](https://openairdocs.org/sdr/SWAA2020102824708.md): Skin · dented · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT AT BS 887+16.5; 2.5' ABOVE S-9R. REPAIRED FUSELAGE SKIN DENT AT BS 887+16.5; 2.5' ABOVE S-9R, PER ER 20-03388 REV IR DATED 10-14-20 AND EA 20-153-01938 REV IR.
- [SDR SWAA2020102823169](https://openairdocs.org/sdr/SWAA2020102823169.md): Skin · dented · Sep 30, 2020 · N430WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT ON THE PREVIOUS REPAIR FASTENER AT BS 500D+10'; 2' BELOW S-R7. REPAIRED FUSELAGE SKIN DISCREPANCY AREA OF BS 500D+10'; 2' BELOW STR 7R, IAW SRM.53-00-01-2R-3 88302U 05OCT20.

Next page: https://openairdocs.org/deregistered/N430WN-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 = 'N430WN' AND deregistration_id = 'N430WN-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N430WN-2024-10-04/reports

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