# Service difficulty reports: N769SW, cancelled Oct 30, 2024

A list on [N769SW, cancelled Oct 30, 2024](https://openairdocs.org/deregistered/N769SW-2024-10-30.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 7 · 319 reports

- [SDR SWAA2024040168796](https://openairdocs.org/sdr/SWAA2024040168796.md): Bottle · low pressure · Mar 28, 2024 · N769SW · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE PRESSURE INDICATOR IN RED<[01] R&R FWD ENTRY DOOR EMER. SLIDE PER MT 725-61-06.
- [SDR SWAA2023092002221](https://openairdocs.org/sdr/SWAA2023092002221.md): Slide · out of position · Sep 19, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE NOT SEEN IN WINDOW<[01] REMOVED AND REPLACED FS-ASSY PER MT 725-61-06 FS;CK;S GOOD (76286)
- [SDR SWAA2023091499429](https://openairdocs.org/sdr/SWAA2023091499429.md): Slide · out of adjust · Sep 12, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE MANUAL INFLATION HANDLE EXPOSED<[01] RESECURED COVER FLAP VELCRO ATTACHMENT TO OTHER SIDE OF VELCRO TO CONCEAL SLIDE MANUAL INFLATION HANDLE. REF SIP.
- [SDR SWAA2023090196242](https://openairdocs.org/sdr/SWAA2023090196242.md): Slide · out of adjust · Sep 1, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > FORWARD RIGHT SIDE EMERGENCY EXIT SLIDE IS HANGING DOWN FROM BOTTOM.<[01] PERFORMED FORWARD SERVICE DOOR ESCAPE SLIDE REPACK PER MT 725-61-06-FS.
- [SDR SWAA2023090196235](https://openairdocs.org/sdr/SWAA2023090196235.md): Slide · out of adjust · Sep 1, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE SLIPPING OUT OF POSITION<[01] REPOSITIONED FWD SVC. DOOR ESCAPE SLIDE PER M/T 725-61-06. CK OK @ THIS TIME.
- [SDR SWAA2023071076317](https://openairdocs.org/sdr/SWAA2023071076317.md): Slide · out of adjust · Jul 7, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > CREW REPORTS THAT FWD SERVICE DOOR ESCAPE SLIDE PRESSURE GAUGE IS DIFFICULT TO READ DUE TO SITTING LOW IN INSPECTION WINDOW<[01] VERIFIED SLIDE ASSY IS CORRECT AND SERVICEABLE INSTALLED PART NUMBER. ADJUSTED SLIDE IN CONTAINER PER AMM 25-66-01 AND MT 725-61-06
- [SDR SWAA2023051146920](https://openairdocs.org/sdr/SWAA2023051146920.md): Battery Pack · inoperative · May 9, 2023 · N769SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS AT 3DEF; 5DEF; EXTERIOR SERV DOOR LIGHT; AND OVER DOOR EXIT SIGN INOP<[01] REMOVED AND INSTALLED NEW BATTERY PACK IAW AMM 33-51-06.OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR SWAA2023020197065](https://openairdocs.org/sdr/SWAA2023020197065.md): Slide · out of adjust · Jan 30, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE HAS DROPPED 4 INCHES<[01] REF AMM 25-66-01 REPACKED SLIDE AS REQUIRED. OK FOR SERVICE
- [SDR SWAA2023013197070](https://openairdocs.org/sdr/SWAA2023013197070.md): Slide · out of adjust · Jan 30, 2023 · N769SW · Boeing 7377H4 · Escape Slide
  > MOC REQUEST -REPOSTION FWD SEV DOOR SLIDE<[01] RE-POSITIONED FWD SEV DOOR SLIDE;CK;S GOOD REF AMM 25-66-01 (69675)
- [SDR SWAA2022122183438](https://openairdocs.org/sdr/SWAA2022122183438.md): Intercostal · cracked · Dec 20, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Structure
  > FLOOR BEAM INTERCOSTAL IS CRACKED BETWEEN STA 312-328 AT LBL 45<[01] R & R INTERCOSTAL PER SRM 51-10-02 & SRM 51-40-02.;[02] C/W INSPECTION PER SRM 51-10-02 & SRM 51-40-02
- [SDR SWAA2022122183439](https://openairdocs.org/sdr/SWAA2022122183439.md): Intercostal · cracked · Dec 20, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Floor Beam
  > FLOOR BEAM INTERCOSTAL IS CRACKED BETWEEN STA 328-344 AT LBL 45<[01] R & R INTERCOSTAL PER SRM 51-10-02 & 51-40-02.;[02] C/W INSPECTION PER SRM 51-10-02 & SRM 51-40-02
- [SDR SWAA2022122183877](https://openairdocs.org/sdr/SWAA2022122183877.md): Light · failed · Dec 20, 2022 · N769SW · Boeing 7377H4 · Emergency Lighting
  > FWD L/H AND MID R/H EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1675 AND M1669 REFERENCING AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2022122083452](https://openairdocs.org/sdr/SWAA2022122083452.md): Battery Pack · no test · Dec 20, 2022 · N769SW · Boeing 7377H4 · Emergency Lighting
  > FWD L/H; AND MID R/H EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1675 AND M1669 REFERENCING AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2022100349426](https://openairdocs.org/sdr/SWAA2022100349426.md): Handle · cracked · Sep 29, 2022 · N769SW · Boeing 7377H4 · Emergency Exits
  > RIGHT OVERWING EMERGENCY EXIT HANDLE IS CRACKED. / [01] REMOVED AND REPLACED RIGHT OVERWING HANDLE PER AMM 52-22-51. OPS CK OK
- [SDR SWAA2022042095134](https://openairdocs.org/sdr/SWAA2022042095134.md): Plate · cracked · Apr 17, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT ANCHOR PLATE CRACKED / [01] REMOVED AND REPLACED ACB AFT ANCHOR PLATE IAW AMM 25-52-10-400-801 STEPS 3.F.(10);[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2022042594318](https://openairdocs.org/sdr/SWAA2022042594318.md): Angle · cracked · Apr 14, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Structure
  > L/H MWW ATTACH CLIP 149A7692-15 CRACKED BS 727 LBL 19 WL 145 L/H MWW SUPPORT RING CLIP IS CRACKED BS 727 LBL 20.5 W/L 148. P/N 149A7678-7 / [01] UPDATED MEASUREMENTS;[02] ATTACH CLIP HAS NO LIMITS FOR A CRACK. PART FOUND TO BE OUT OF LIMITS IAW SRM 53-40-71-1A
- [SDR SWAA2022042193523](https://openairdocs.org/sdr/SWAA2022042193523.md): Panel · delaminated · Apr 12, 2022 · N769SW · Boeing 7377H4 · Aerodynamic Fairings
  > PANEL 193AR HAS 2 DELAMINATED AREAS ON OUTER SURFACE SKIN AS NOTED ON FAULT TTG8Q00BMNQU / [01] IDENTIFIED PANEL 193AR MATERIAL IAW SRM 53-40-70-0I-1 TABLE 2 FIGURE 2 ITEM 18. DELAMINATED SKIN AT DISCREPANT LOCATIONS OVER HONEYCOMB CORE EXCEED ALLOWABLE DAMAGE
- [SDR SWAA2022042593165](https://openairdocs.org/sdr/SWAA2022042593165.md): Support Ring · cracked · Apr 11, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Structure
  > L/H MWW SUPPORT RING CLIP IS CRACKED BS 727; LBL 20.5; W/L 148. P/N 149A7678-7 / [01] REMOVED CLIP AT L/H MWW SUPPORT BS 727; LBL 20.5; W/L 148. IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP P/N 149A7678U9 PO# 864333 IAW SRM 51-40-05-0G-0 AND DWG 149
- [SDR SWAA2022042590342](https://openairdocs.org/sdr/SWAA2022042590342.md): Flap · delaminated · Apr 1, 2022 · N769SW · Boeing 7377H4 · Trailing Edge Flaps
  > R/W O/B AFT FLAP I/B END UPPER SURFACE IS DELAMINATED / [01] REMOVED R/W O/B AFT FLAP IAW AMM 27-51-22-000-801 STEPS 2.D.;[02] VERIFIED;[03] ACCOMPLISHED PARTS REMOVAL TABLE;[04] R/W O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED AREA WAS REPAIRED ON ATS WORK
- [SDR SWAA2022042590177](https://openairdocs.org/sdr/SWAA2022042590177.md): Scuff Plate · cracked · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR; FWD SCUFF PLATE IS CRACKED / [01] WELDED 1EA CRACKED AREA ON ACB; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N; KJ256554;[02] VERIFIED WE
- [SDR SWAA2022042590005](https://openairdocs.org/sdr/SWAA2022042590005.md): Web · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB AT STA 440+14 TO STA 460+19; WL 156; RBL 28 TO RBL 29. / [01] REMOVED CORROSION AT<BR><BR>STA 440+14 0.003'<BR>STA 440+15 0.001'<BR>STA 440+16 0.002'<BR>STA 460 0.006'<BR>STA 460+3 0.002'<BR>STA 460+5 0.002'<BR>STA
- [SDR SWAA2022042590003](https://openairdocs.org/sdr/SWAA2022042590003.md): Support · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 420+4 TO STA 500C+14; LBL 24; WL 156. / [01] REMOVED CORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT BTW BS 480+7' TO 500D REWORKED AREA BTW BS 500B TO 500C' IN L=1' X W=1' X D=.002' FROM ORIGIN
- [SDR SWAA2022042590011](https://openairdocs.org/sdr/SWAA2022042590011.md): Support · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727+4 TO STA 847; LBL 24; WL 156 TO WL 160. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847 LBL 24 WL 156;TO WL 160 IA
- [SDR SWAA2022042590016](https://openairdocs.org/sdr/SWAA2022042590016.md): Angle · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ATTACH ANGLE AT STA 787+2; RBL 24; WL 156. / [01] REMOVED CORROSION ON ATTACH ANGLE AT STA 787+2; RBL 24; WL 156.; DIMENSIONS L:0.400' W:0.320' DEPTH: 0.045' ORIGINAL MATERIAL 0.063' TOOL USED: MICROMETER ID:ATS 601 DATE DUE: 05/2022 IAW SRM 51
- [SDR SWAA2022042590021](https://openairdocs.org/sdr/SWAA2022042590021.md): Support · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB R/H FLOOR TO SIDEWALL FROM STA 867+7; TO STA 927+17; RBL 22; WL 165 TO WL 178. / [01] REMOVED CORROSION FROM ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS867+7 MEASURED 1.2'L X 0.6'W AND 0.001'DEEP ORIGINAL THICKNESS OF 0.040' FOUND IN LIMITS PER SR
- [SDR SWAA2022042590017](https://openairdocs.org/sdr/SWAA2022042590017.md): Support · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR SUPPORT AT STA927; LBL 2; WL 179. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS927; LBL 2; WL 179 IN AREA OF L=2'XW=2'XD=.006' REMAINING THICKNESS OF.074' OF ORIGINAL THICKNESS OF.080'; FOUND TO BE IN LIMITS IAW SRM 53-70-53-0I-2; S
- [SDR SWAA2022042190002](https://openairdocs.org/sdr/SWAA2022042190002.md): Shield · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO STA 440; RBL 24; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD P/N:143A8126U21ATSMRO; LOT:1481125-1 AND
- [SDR SWAA2022042190006](https://openairdocs.org/sdr/SWAA2022042190006.md): Strap · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY TENSION STRAP AT STA 440+4 TO STA 480+5 RBL 22; WL 156. / [01] REMOVED CORROSION AT<BR><BR>STA 440+4 0.005'<BR>STA 440+9 0.006'<BR>STA 440+13 0.004'<BR>STA 440+17 0.003'<BR>STA 460+1 0.002'<BR>STA 460+5 0.002'<BR>STA 460+9 0.003'<BR>
- [SDR SWAA2022042190007](https://openairdocs.org/sdr/SWAA2022042190007.md): Shield · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT SHIELD AT STA 500+10; WL 156; RBL 24. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD P/N:143A8126U31; LOT:1484884-1 AND LOCATED AND DRILLED
- [SDR SWAA2022042190008](https://openairdocs.org/sdr/SWAA2022042190008.md): Support · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT AT STA 500A+5 TO STA 500C+15; RBL 24; WL 156. / [01] VERIFIED APPLICABILITY FOR ALLOWABLA DAMAGE LIMITS OF FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 500A+5 TO 500C+15;RBL 24;WL 156.IAW SRM 53-
- [SDR SWAA2022042190009](https://openairdocs.org/sdr/SWAA2022042190009.md): Support · cracked · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY AFT BULKHEAD SUPPORT AT STA 500D; RBL 18 TO LBL 18; WL 156. / [01] THERE IS NO SRM ALLOWABLE DAMAGE FOR FCB AFT BULKHEAD SUPPORT. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED ACTION 1;[03] REMOVED CORROSION
- [SDR SWAA2022042190012](https://openairdocs.org/sdr/SWAA2022042190012.md): Shield · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY DOOR CUTOUT FWD SHIELD FROM STA 767+3 TO STA 767+9; WL 156; RBL 25. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD ITEM: 146A8127U1 LOT: 1474614-1. LOCATED
- [SDR SWAA2022042190013](https://openairdocs.org/sdr/SWAA2022042190013.md): Shield · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY DOOR CUTOUT AFT SHIELD FROM STA 847 TO STA 867; RBL 22; WL 164. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD ITEM: 146A8127Y5 LOT: 1481640-1 PO/NUMBER: 85
- [SDR SWAA2022042190014](https://openairdocs.org/sdr/SWAA2022042190014.md): Stringer Clip · corroded · Mar 31, 2022 · N769SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRINGER CLIP AT STA 787+1; RBL 14 WL 154. / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>NO ALLOWABLE DAMAGE FOR THIS PART FOUND IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02.<BR>REMOVE
- [SDR SWAA2022042190026](https://openairdocs.org/sdr/SWAA2022042190026.md): Floor Support · corroded · Mar 31, 2022 · N769SW · Boeing 737 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR SUPPORT AT STA 727A+10; 727B+10; 727D+4; RBL 14; WL 156. / RBL 14; WL 156 FOUND TO OUT OF LIMITS WITH REMAINING OF.053' OF ORIGINAL THICKNESS.063'. IAW SRM 53-60-53-0I-2; SRM 53-00-53-1A-2 AND BAC1509-100146<BR><BR>DEPTH GAUGE USED ID
- [SDR SWAA2022042190024](https://openairdocs.org/sdr/SWAA2022042190024.md): Floor Support · corroded · Mar 31, 2022 · N769SW · Boeing 737 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR SUPPORT AT STA 767+5; LBL 2; WL 156. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS767+5; LBL 2; WL 156 IN AREA OF L=1.1'XW=.9'XD=.012' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF.051' OF ORIGINAL THICKNESS OF.063' IAW SRM
- [SDR SWAA2022042190019](https://openairdocs.org/sdr/SWAA2022042190019.md): Floor Support · corroded · Mar 31, 2022 · N769SW · Boeing 737 · Fuselage Miscellaneous Structure
  > CORROSION ON ACB FLOOR SUPPORT AT STA 767+5; RBL 2; WL 156. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS767+5; RBL 2; WL 156 IN AREA OF L=1.3'XW=.9'XD=.008' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF.055' OF ORIGINAL THICKNESS OF.063' IAW SRM
- [SDR SWAA2022042589273](https://openairdocs.org/sdr/SWAA2022042589273.md): Seat Track · corroded · Mar 29, 2022 · N769SW · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 25 BS 660+15. / [01] REMOVED CORROSION FROM SEAT TRACK WITH A MAX MATERIAL LOSS OF.037 ON THE TOP OF THE WELL. FOUND TO BE OUT OF LIMITS USING TOOL ID # ATS1225 S/N UNK CAL. DATE 07/2021 DUE 07/2022.;[02] REMOVED
- [SDR SWAA2022042589477](https://openairdocs.org/sdr/SWAA2022042589477.md): Bracket · cracked · Mar 29, 2022 · N769SW · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ON LEFT WING T/E BULB SEAL RETAINER SUPPORT AT ORSS 261; 3'BELOW FROM UPPER PANEL; 20' FWD FROM T/E.(ACCESS FROM 551GB) / [01] REMOVED L. WING T/E BULB SEAL SUPPORT PANEL AND BRACKET IAW SRM 51-40-04 AND AMM 20-50-01 AND LOCATED AND DRILLED NEW BRACKET I
- [SDR SWAA2022042189280](https://openairdocs.org/sdr/SWAA2022042189280.md): Support Angle · cracked · Mar 29, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS691 RBL1. / [01] REMOVED DAMAGED BRACKET AT BS 691 RBL1 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS691 RBL1 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM 51-
- [SDR SWAA2022042189281](https://openairdocs.org/sdr/SWAA2022042189281.md): Support Angle · cracked · Mar 29, 2022 · N769SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS692 RBL24. / [01] REMOVED DAMAGED BRACKET AT BS692 RBL 24 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS692 RBL24 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM
- [SDR SWAA2022042189270](https://openairdocs.org/sdr/SWAA2022042189270.md): Seat Track · corroded · Mar 29, 2022 · N769SW · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 BS 480+6; BS 500+7; BS 500A+7; BS 500A+18; BS 500C+9. / [01] SEAT TRACK TO BE WORKED ON CARD #TTG8Q00BKCK4;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED CORRECITVE ACTION 1 AND 2;[04] AMT ACTION IS COMPLETE
- [SDR SWAA2022042588891](https://openairdocs.org/sdr/SWAA2022042588891.md): Barrier · cracked · Mar 28, 2022 · N769SW · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK IN LEFT HAND VAPOR BARRIER AT B.S. 663; L.B.L. 8; W.L. 150. / [38] INSTALLED L/H VAPOR BARRIER BS 663 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV-B AND 111A1001 REV-B AND 111A7000 REV-A. REQ OK TO INSTALL STEPS 4; 12 AND 13;[39] OK TO INSTALL EXHAUST PNL
- [SDR SWAA2021091315452](https://openairdocs.org/sdr/SWAA2021091315452.md): Sensor · malfunctioned · Sep 8, 2021 · N769SW · Boeing 7377H4 · Leading Edge Slat Position Indicating System
  > AFTER T/O FLAPS RETRACTED NORMALLY; PASSING 6000 AMBER LIGHT FLAP TRANSIT LT ILLUMINATE AND. #4 FLAP INDICATOR ILLUMINATED AMBER ON OVERHEAD PANEL. AIRSPEED WAS 250 AND HIT 25O DURING TROUBLESHOOTING; THEN DECREASED TO 210. LIGHTS CAME AND WENT W/FLAPS. UP. N
- [SDR SWAA2021060779234](https://openairdocs.org/sdr/SWAA2021060779234.md): Lens · missing · Jun 2, 2021 · N769SW · Boeing 7377H4 · Emergency Lighting
  > RIGHT OVERWING EMER EXIT LIGHT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED COVER IAW AMM 33-51-01; INSPECTED
- [SDR SWAA2021060779229](https://openairdocs.org/sdr/SWAA2021060779229.md): Lens · missing · Jun 2, 2021 · N769SW · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR; LOWER EMER. EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED LENS COVER IAW AMM 33-51-01; INSPECTED
- [SDR SWAA2021060779228](https://openairdocs.org/sdr/SWAA2021060779228.md): Lens · missing · Jun 2, 2021 · N769SW · Boeing 7377H4 · Emergency Lighting
  > FWD SERVICE DOOR; LOWER EMER. EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-01
- [SDR SWAA2021060779227](https://openairdocs.org/sdr/SWAA2021060779227.md): Sign · missing · Jun 2, 2021 · N769SW · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EMER EXIT LIGHT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED SIGN IAW AMM 33-51-01; INSPECTED
- [SDR SWAA2021050546784](https://openairdocs.org/sdr/SWAA2021050546784.md): Seal · cracked · Feb 4, 2021 · N769SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > RH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL CRACKED / R&R'D RH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2021050546783](https://openairdocs.org/sdr/SWAA2021050546783.md): Seal · cracked · Feb 4, 2021 · N769SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL CRACKED. / R&R LH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER MM REF 53-31-31

Next page: https://openairdocs.org/deregistered/N769SW-2024-10-30/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 = 'N769SW' AND deregistration_id = 'N769SW-2024-10-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N769SW-2024-10-30/reports

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