# Service difficulty reports: N557WN, cancelled Oct 4, 2024

A list on [N557WN, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N557WN-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 · 247 reports

- [SDR SWAA2023072481068](https://openairdocs.org/sdr/SWAA2023072481068.md): Light · inoperative · Jul 21, 2023 · N557WN · Boeing 737790 · Emergency Lighting
  > LH OVERWING EMERGENCY LIGHT INOP<[01] RELAMPED LH OVERWING EMERGENCY LIGHT<BR>LIGHT IAW AMM 33-51-04
- [SDR SWAA2023060253837](https://openairdocs.org/sdr/SWAA2023060253837.md): Shield · broken · May 30, 2023 · N557WN · Boeing 737790 · Emergency Equipment
  > FWD FLASHLIGHT SHIELDS BROKEN<[01] R+R?D FWD FLASHLIGHT SHIELDS IAW S.I.P.
- [SDR SWAA2023042530472](https://openairdocs.org/sdr/SWAA2023042530472.md): Cowling · pulled · Apr 22, 2023 · N557WN · Boeing 737790 · Nacelle/Pylon, Main Frame
  > #2 ENGINE INLET COWL LEFT UPPER SKIN AFT ROW OF FASTENERS HAS MULTIPLE MISSING; LOOSE OR PULLED FASTENERS FROM 12:00 TO INBOARD STRAKE.<[01] COMPLIED WITH EA 23-171-01335
- [SDR SWAA2022111670997](https://openairdocs.org/sdr/SWAA2022111670997.md): Lamp · inoperative · Nov 13, 2022 · N557WN · Boeing 737790 · Emergency Lighting
  > EMERGENCY LIGHT OUT 11FED / [01] RELAMPED EMERGENCY LT AT ROW 11DEF REF AMM 33-51-03
- [SDR SWAA2022061618173](https://openairdocs.org/sdr/SWAA2022061618173.md): Panel · elongated · Jun 14, 2022 · N557WN · Boeing 737790 · Aerodynamic Fairings
  > PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND OVERSIZED COUNTERSINKS. / [01] REPLACED PANEL 193B PER SRM 51-40-02
- [SDR SWAA2022022376194](https://openairdocs.org/sdr/SWAA2022022376194.md): Bustle · loose · Feb 20, 2022 · N557WN · Boeing 737790 · Escape Slide
  > FWD ENTRY DOOR SLIDE BUSTLE NOT SECURE / [01] SECURED PER MT 725-61-06-FE
- [SDR SWAA2021110428618](https://openairdocs.org/sdr/SWAA2021110428618.md): Floor Panel · corroded · Oct 8, 2021 · N557WN · Boeing 737* · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PNL 140DF HAS CORROSION ALONG AFT EDGE BS 947 RBL 22 - LBL 22 WL 157; / [01] FABRICATED NEW ACB FLOOR PNL 140DF FROM 2024T3#0.071X48SH-C; LOT# 1461004-1 IAW BOING DWG 435A2610 AND BOEING DWG 435A2600; [02] PRIOR TO MAINTENANCE; BLENDED DAM
- [SDR SWAA2021110427411](https://openairdocs.org/sdr/SWAA2021110427411.md): Frame · cracked · Oct 7, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACK ON FRAME BS 500C STR 8L AIR CONDITIONING RAIL BRACKET OUTBD ATTACH HOLE. CRACK EXTENDS UP.300' AND DOWN.300' FROM INBD EDGE OF HOLE. NOT IN FRAME RADIUS.; / [01] REPAIRED ON CARD TTG8Q006QK4S; [02] VERIFIED BS500C STR8L REWORK PERFORMED ON CC# TTG8Q00
- [SDR SWAA2021110426401](https://openairdocs.org/sdr/SWAA2021110426401.md): Support Angle · cracked · Oct 4, 2021 · N557WN · Boeing 737* · Galley Doors
  > AFT SERVICE DOOR LOWER HINGE PANEL # 844DZ HAS CRACKED FWD SUPPORT ANGLE CRACKED.; / [01] REMOVED AND REPLACED AFT SERVICE DOOR LOWER HINGE PANEL #844DZ FWD SUPPORT ANGLE IAW SRM 51-40-02; [02] VERIFIED REPLACEMENT OF THE AFT SERVICE DOOR LOWER HINGE PANEL SU
- [SDR SWAA2021110425666](https://openairdocs.org/sdr/SWAA2021110425666.md): Skin · cracked · Oct 3, 2021 · N557WN · Boeing 737790 · Horizontal Stabilizer, Plate/Skin
  > WHILE ACCOMPLISHING HFEC INSPECTION ON CCN: 5510-I-15029-NG #2; FOUND 1 INCH CRACK ON R/H HORIZONTAL STABILIZER LOWER SKIN AT RIB STATION 193.90; 18 INCHES AFT OF THE THE FWD EDGE.; / [01] REQUEST HFEC FOR CRACK VERIFICATION ON R/H HORIZONTAL STAB ON LOWER SK
- [SDR SWAA2021110425651](https://openairdocs.org/sdr/SWAA2021110425651.md): Baffle · cracked · Oct 1, 2021 · N557WN · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CRACKED AT FASTENER HOLE BS 500C - BS 500D RBL 23 WL 156; / [01] REMOVED FWD CARGO BAY BAFFLE CRACKED BS 500C - 500D RBL23 WL 156 IAW SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FCB BAFFLE BS 500C-500D RBL23 WL156 AS PER DWG 143A7505 AND
- [SDR SWAA2021110425653](https://openairdocs.org/sdr/SWAA2021110425653.md): Baffle · cracked · Oct 1, 2021 · N557WN · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CRACKED AT FASTENER HOLE BS 500B - BS 500C RBL 23 WL 156; / [01] EVALUATED CRACK AT FWD CARGO BAFFLE BS 500B-500C. BAFFLE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED FWD CARGO BAY BAFFLE CRACKED BS 500B-500C RBL 23 WL 1
- [SDR SWAA2021110425657](https://openairdocs.org/sdr/SWAA2021110425657.md): None · cracked · Oct 1, 2021 · N557WN · Boeing 737* · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500C LBL 23 WL 154 AFT SIDE OF FRAME; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP BS 500C LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500C LBL
- [SDR SWAA2021110425658](https://openairdocs.org/sdr/SWAA2021110425658.md): Structure · cracked · Oct 1, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500C LBL 23 WL 154 FWD SIDE OF FRAME; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP BS 500C LBL 23 WL 154 FWD SIDE OF FRAME P/N 143A7502-13 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500C LBL
- [SDR SWAA2021110425659](https://openairdocs.org/sdr/SWAA2021110425659.md): Structure · cracked · Oct 1, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 500B LBL23 WL 154 FWD SIDE OF FRAME; / [01] REMOVED AT FWD CARGO BAY BAFFLE ATTACH CLIP B/S 500B LBL 23 WL 154 FWD SIDE OF FRAME P/N 143A7502-13 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 500B
- [SDR SWAA2021110425660](https://openairdocs.org/sdr/SWAA2021110425660.md): Structure · cracked · Oct 1, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 440 LBL 23 WL 154 AFT SIDE OF FRAME; / [01] REMOVED FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 440 LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 440
- [SDR SWAA2021110425661](https://openairdocs.org/sdr/SWAA2021110425661.md): Structure · cracked · Oct 1, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE ATTACH CLIP CRACKED BS 400 LBL 23 WL 154 AFT SIDE OF FRAME; / [01] REMOVED AT FWD CARGO BAY BAFFLE ATTACH CLIP B/S 400 LBL 23 WL 154 AFT SIDE OF FRAME P/N 143A7502-5 IAW SRM 51-40-02; [02] LOCATED AND DRILLED BAFFLE ATTACH CLIP BS 400 LBL
- [SDR SWAA2021110425654](https://openairdocs.org/sdr/SWAA2021110425654.md): Web · cracked · Oct 1, 2021 · N557WN · Boeing 737790 · Fuselage Main, Structure
  > FWD CARGO WEB CRACKED AT FASTENER HOLE BS 500 - BS 500A RBL 22 WL 154; / [01] REMOED WEB AT FWD CARGO BS 500 - BS 500A RBL 22 WL 154 IAW SRM 51-40-02-0G-0; [02] WEB FORMING AND HEAT TREATMENT ACCOMPLISHED ON PO#839725/1.; [03] LOCATED AND DRILLED REPLACEMENT
- [SDR SWAA2021110425655](https://openairdocs.org/sdr/SWAA2021110425655.md): None · cracked · Oct 1, 2021 · N557WN · Boeing 737* · Wing, Control Surfaces
  > RIGHT WING T/E WIGGLE PLATE IS CRACKED AT ORSS 261; / [01] REMOVED R/W T/E WIGGLE PLATE IAW AMM 51-40-02-0G-0 STEP 4. FIG 8; [02] VERIFIED; [03] INSTALLED NEW WIGGLE PLATE O/ R/W T/E ORSS 261 IAW SRM 51-40-02-0G-0 STEP 4; [04] INSTALLED NEW WIGGLE PLATE ON R/
- [SDR SWAA2021110425662](https://openairdocs.org/sdr/SWAA2021110425662.md): None · cracked · Oct 1, 2021 · N557WN · Boeing 737* · Wing, Control Surfaces
  > LEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED; / [01] REMOVED AND REPLACED L/W T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0 STEP 4; [02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2021110424702](https://openairdocs.org/sdr/SWAA2021110424702.md): Frame · cracked · Sep 30, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > INTERIOR; BS 867 FRAME; IN-BETWEEN STR 9L AND STR8L; WL 273; IS CRACKED AT I/B FASTENER HOLE. (AREA WHERE THE SUPPORT BRACKET IS REMOVED).; / [01] CRACK AT BS 867 BETWEEN 8-9 L/H TO BE REPAIRED ON TTG8Q006Q5L5; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD CO
- [SDR SWAA2021110424699](https://openairdocs.org/sdr/SWAA2021110424699.md): Frame · cracked · Sep 30, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACK IN FRAME BS 747 STR 8R OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP.300 IN AND DOWN.300 IN. MARKED ENDS FO CRACKS IN RED; / [01] FAULT TO BE REPAIRED ON TTG8Q006QAGC; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110425170](https://openairdocs.org/sdr/SWAA2021110425170.md): Doubler · corroded · Sep 30, 2021 · N557WN · Boeing 737790 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER BS 1016-1040 LBL 6- LBL 9 W/L 306.5; / [01] REMOVED CORROSION AT DOUBLER BS.1016+20 TO BS.1040 LBL.5 TO LBL.9 REWORK DIMENSION L:7' X W:3' IAW SRM 51-10--02; [02] REMOVER 5EA RIVETS AT DUOBLER IAW SRM 51-40-02; [03] REMOVED CORROSION AT D
- [SDR SWAA2021100425171](https://openairdocs.org/sdr/SWAA2021100425171.md): Support Angle · corroded · Sep 30, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE BS 1016+23' RBL 6 - RBL 12 W/L 306.5<REMOVED 3EA FASTENERS AT SUPPORT ANGLE BS.1016+23 RBL.9 TO RBL.12 IAW SRM 51-40-02 REMOVED CORROSION AT SUPPORT ANGLE BS.1016+23 RBL.9 TO RBL.12 REWORKED DIMENSION L:3' X W:0.750' IAW SRM 51-10-02
- [SDR SWAA2021100424700](https://openairdocs.org/sdr/SWAA2021100424700.md): Frame · cracked · Sep 30, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > CRACK IN FRAME BS 747 STR 8L OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP.400 IN AND DOWN.250 IN. MARKED ENDS OF CRACKS IN RED.; / [01] CORRECTION TO FAULT - DISCREPANCY SHOULD BE BS 867 NOT 747.; [02] REPA
- [SDR SWAA2021100424701](https://openairdocs.org/sdr/SWAA2021100424701.md): Frame · cracked · Sep 30, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > CRACK IN FRAME BS 747 STR 8L OUTBD ATTACH HOLE FOR AIR CONDITIONING RAIL BRACKET. CRACKS PROPAGATE FROM INBD EDGE OF HOLE UP.300 IN AND DOWN.300 IN. MARKED ENDS OF CRACKS IN RED.; / [01] REPAIRED ON TTG8Q006Q5KY; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CAR
- [SDR SWAA2021110424035](https://openairdocs.org/sdr/SWAA2021110424035.md): Frame · cracked · Sep 29, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME DURING MFEC INSPECTION BS 500C STR 8R AT AIR CONDITIONING BRACKET INBD FASTENER HOLE; / [01] CORRECTION TO ORIGINAL DISCREPANCY SHOULD BE STRINGER 8 LEFT.; [02] DISPLACED INSULATION BLANKETS FOR ACCESS AT BS 500B - 500D; STR 7 - 10 L
- [SDR SWAA2021110424673](https://openairdocs.org/sdr/SWAA2021110424673.md): Stringer · cracked · Sep 29, 2021 · N557WN · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL156. MARKED; / [01] EVALUATED CRACK AT STRINGER 25RH; BS 540 WL 156- STRINGER FOUND OUT OF LIMIT PER SRM 53-00-03-1A-1 PARAGRAPH 4 A(2)(A)1; [02] REMOVED FASTENERS FROM STRINGER 26R BS 500D+6'- 540; IAW SRM 51
- [SDR SWAA2021110424672](https://openairdocs.org/sdr/SWAA2021110424672.md): Stringer · cracked · Sep 29, 2021 · N557WN · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED; / [21] INSTALLED REPLACEMENT STRINGER SECTION BS 500D+12 TO 540 AND HAT SECTION REPAIR BS 500D+4 TO 500D+16 STR 23R/H WL 164 IAW SRM 53-00-03-2R-1 AND SRM 51-40-02 AND EA NO: 21-153-02931 REV A; [
- [SDR SWAA2021110424674](https://openairdocs.org/sdr/SWAA2021110424674.md): Stringer · cracked · Sep 29, 2021 · N557WN · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED; / [09] FABRICATED AND LOCATED AND DRILLED NEW STRINGER REPAIR SECTION BS 500D+12' TO 540; APPLIED CHEMICAL CONVERSION ON STR REPAIR 26 R/H. ITEM: HFAB53-STR-011; LOT: 1470602-1; P.O.# 839549/1. I
- [SDR SWAA2021110424034](https://openairdocs.org/sdr/SWAA2021110424034.md): Frame · cracked · Sep 29, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME FOUND ON MFEC INSPECTION. BS 747 STR 8R AT AIR CONDITIONING BRACKET INBD ATTACH FASTENER; / [01] REPAIRED ON TTG8Q006QGJW; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110424692](https://openairdocs.org/sdr/SWAA2021110424692.md): Shield · corroded · Sep 29, 2021 · N557WN · Boeing 737790 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY; R/H FLOOR TO SIDE WALL SHIELD HAS SEVERAL AREAS OF CORROSION AND HAS BEEN PREVIOUSLY BLENDED; BS 767 TO 787; RBL 21; WL 156;; / [01] NOT FOUND ALLOWABLE DAMAGE ON THE SRM;REPAIR BY REPLACEMENTE PART IAW SRM 51-10-02-0G- 0 STEP 9.REMOVED SHIELD
- [SDR SWAA2021110424678](https://openairdocs.org/sdr/SWAA2021110424678.md): Stiffener · cracked · Sep 29, 2021 · N557WN · Boeing 737790 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; 129.50; 3RD VERTICAL STIFFENER IS CRACKED.; / [01] REQUEST NDI TO VERIFY RH RIB AT STAB STA 129.50;3RD VERTICAL STIFFENER CRACKED.;[11] FABRICATED REPAIR PARTS -1 T SECTION FROM 7075-T76511 0.063 INCH LOT#1463116-1
- [SDR SWAA2021110424013](https://openairdocs.org/sdr/SWAA2021110424013.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 480.; / [01] TO BE REPAIRED ON TTG8Q006Q8B7; [02] VERIFIED BS480 STR8L FRAME WAS REPAIRED ON CC# TTG8Q006Q8B7
- [SDR SWAA2021110424012](https://openairdocs.org/sdr/SWAA2021110424012.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 400.; / [01] TO BE REPAIRED ON TTG8Q006Q91V; [02] VERIFIED FAULT REPAIRED ON CC# TTG8Q006Q91V
- [SDR SWAA2021110424020](https://openairdocs.org/sdr/SWAA2021110424020.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 400.; / [01] TO BE REPAIRED ON TTG8Q006Q8C6; [02] VERIFIED CRACKED FRAME AT BS 400 STR8R WAS REPAIRED ON CC# TTG8Q006Q8C6
- [SDR SWAA2021110424021](https://openairdocs.org/sdr/SWAA2021110424021.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727D.; / [01] REPAIRED ON TTG8Q006Q934; [02] VERIFIED BS727D STR8L REWORK PERFORMED ON CC# TTG8Q006Q934
- [SDR SWAA2021110424023](https://openairdocs.org/sdr/SWAA2021110424023.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 827.; / [01] TO BE REPAIRED ON TTG8Q006Q93G; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2021110424010](https://openairdocs.org/sdr/SWAA2021110424010.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727D.; / [01] REPAIR COMPLETED ON CUSTOMER CARD NO. TTG8Q006Q91P.; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110424014](https://openairdocs.org/sdr/SWAA2021110424014.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 747.; / [01] REPAIRED ON TTG8Q006Q8BH; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110424015](https://openairdocs.org/sdr/SWAA2021110424015.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 LEFT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 867.; / [01] REPAIRED ON TTG8Q006Q924; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110424017](https://openairdocs.org/sdr/SWAA2021110424017.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 480.; / [01] REFER TO FAULT TTG8Q006QSFD WHERE EA 21-153-02907 WAS ADDED AS A SUBTASK; [02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021110424018](https://openairdocs.org/sdr/SWAA2021110424018.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 500A.; / [01] REPAIR ACCOMPLISHED ON TTG8Q006Q92Z; [02] REPAIR FRAME AT B.S 500A R/H STRINGER 8 AIR CONDITIONING BRACKET ACCOMPLISHED ON CUST SYSTEM ID: TTG8Q006Q92Z; [03] VERIFIE
- [SDR SWAA2021110424019](https://openairdocs.org/sdr/SWAA2021110424019.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 727B.; / [01] INSTALLED EWIS PROTECTION IN WORK AREA IAW AMM 20-60-07; [02] VERIFIED INSTALLATION OF EWIS PROTECTION PER AMM 20-60-07; [03] CERTIFY; [04] REMOVED EWIS PER AMM 20-6
- [SDR SWAA2021110424022](https://openairdocs.org/sdr/SWAA2021110424022.md): Frame · cracked · Sep 28, 2021 · N557WN · Boeing 737* · Fuselage Main, Frame
  > CRACKED FRAME AT STRINGER 8 RIGHT AIR CONDITIONING BRACKET ATTACH POINT AT B.S. 787.; / [01] REPAIR COMPLETED ON CUSTOMER CARD NO TTG8Q006Q8CK; [02] CERTIFY; [03] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2021100424002](https://openairdocs.org/sdr/SWAA2021100424002.md): Former · none · Sep 28, 2021 · N557WN · Boeing 737790 · Fuselage Main, Plate/Skin
  > FAIRING FORMER FOR FWD EDGE OF PANEL 192BR AT BS 540 HAS BARE METAL AND HAS FRETTING WEAR.REMOVED TAPERED SHIM AT FAIRING FORMER FWD EDGE OF PANEL 192BR IAW SRM 51-40-02-0G-0. CHEMICAL CONVERSION AT NEW SHIM IAW BAC5719 TYPE II CLASS A AND PRIME. INSTALLED
- [SDR SWAA2021110423989](https://openairdocs.org/sdr/SWAA2021110423989.md): Battery · failed · Sep 27, 2021 · N557WN · Boeing 737* · Emergency Lighting
  > M1675 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST; / [01] REMOVED M1675 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] PERFORMED GOOD INSTALLATION TEST OF M167
- [SDR SWAA2021110423988](https://openairdocs.org/sdr/SWAA2021110423988.md): Battery · failed · Sep 27, 2021 · N557WN · Boeing 737* · Emergency Lighting
  > M1674 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST; / [01] REMOVED M1674 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERIFIED CORRECTIVE ACTIONS STEP 1.; [03] PERFORMED GOOD INSTALLATION TEST OF M167
- [SDR SWAA2021110423987](https://openairdocs.org/sdr/SWAA2021110423987.md): Battery · failed · Sep 27, 2021 · N557WN · Boeing 737* · Emergency Lighting
  > M1669 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST; / [01] REMOVED AIR RETURN GRILL AT STA 603 RBL 67 PER CMM 25-23-01 PARA. 1.2 AND REMOVED M1669 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VER
- [SDR SWAA2021110423986](https://openairdocs.org/sdr/SWAA2021110423986.md): Battery · failed · Sep 27, 2021 · N557WN · Boeing 737* · Emergency Lighting
  > M1670 EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST; / [01] REMOVED AIR RETURN GRILL AT STA 727C+13 LBL 68 PER CMM 25-23-01 PARA. 1.2 AND REMOVED M1670 EMERGENCY BATTERY AND REPLACED WITH SERVICEABLE BATTERY PER AMM 33-51-06-960-805 STEP 4.D.(1)-(5); [02] VERI

Next page: https://openairdocs.org/deregistered/N557WN-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 = 'N557WN' AND deregistration_id = 'N557WN-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N557WN-2024-10-04/reports

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