# Service difficulty reports: N727SW, cancelled Sep 18, 2024

A list on [N727SW, cancelled Sep 18, 2024](https://openairdocs.org/deregistered/N727SW-2024-09-18.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 · 300 reports

- [SDR SWAA2022081240436](https://openairdocs.org/sdr/SWAA2022081240436.md): Door Actuator · faulty · Aug 10, 2022 · N727SW · Boeing 7377H4 · Nose/Tail Landing Gear
  > 'DURING GEAR RETRACTION ON TAKEOFF; WE HEARD A 'BUMP'. AS WE ACCELERATED ABOVE 210 K/AS WE NOTICED CONSIDERABLE MORE NOISE THAN NORMAL FROM THE NOSE GEAR AREA. WE STAYED BELOW 250 K/AS AND RETURNED FO / [01] INSPECTED INSTALLATION OF LH NOSE GEAR DOOR UPPER PU
- [SDR SWAA2022072733523](https://openairdocs.org/sdr/SWAA2022072733523.md): Slide · loose · Jul 24, 2022 · N727SW · Boeing 7377H4 · Escape Slide
  > AFT ENTRY SLIDE FELL OUT OF BOX / [01] REPACKED L2 DOOR SLIDE IAW AMM 25-66-01.
- [SDR SWAA2022062320535](https://openairdocs.org/sdr/SWAA2022062320535.md): Slide · out of position · Jun 19, 2022 · N727SW · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR ESCAPE SLIDE COMING OUT BOTTOM OF DOOR. / [01] RE-POSITIONED AFT SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01.
- [SDR SWAA2022042900429](https://openairdocs.org/sdr/SWAA2022042900429.md): Fitting · cracked · Apr 28, 2022 · N727SW · Boeing 737 · Landing Gear Doors
  > LEFT MLG CENTER GEAR DOOR AFT LOWER DOOR FITTING ON GEAR DOOR CRACKED. / [01] REMOVED AND REPLACED LEFT MLG CENTER GEAR DOOR AFT LOWER DOOR FITTING REF AMM 32-13-21.
- [SDR SWAA2022013164595](https://openairdocs.org/sdr/SWAA2022013164595.md): Panel · elongated · Jan 27, 2022 · N727SW · Boeing 7377H4 · Aerodynamic Fairings
  > 193D PANEL HAS MULTIPLE ELONGATED HOLES; / [01] REPLACED PANEL 193D PER AMM 53-51-21. <BR><BR>TSR#202200680
- [SDR SWAA2022013164594](https://openairdocs.org/sdr/SWAA2022013164594.md): Panel · elongated · Jan 27, 2022 · N727SW · Boeing 7377H4 · Aerodynamic Fairings
  > 194E PANEL HAS MULTIPLE ELONGATED HOLES.; / [01] REMOVED AND REPLACED PANEL 194E REF AMM 52-51-11
- [SDR SWAA2022011159799](https://openairdocs.org/sdr/SWAA2022011159799.md): Lens · delaminated · Jan 8, 2022 · N727SW · Boeing 737 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION: OVERHEAD BIN EMERGENCY EXIT LIGHT AT 4 ABC HAS FRACTURED AND SEPARATING LENS. / [01] REPLACED LENS AT 4ABC OPS CK GOOD REF AMM 33-51-03; [02] C/W
- [SDR SWAA2022011159794](https://openairdocs.org/sdr/SWAA2022011159794.md): Lens · detached · Jan 8, 2022 · N727SW · Boeing 737 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHT AT 6 DEF DETACHED FROM OVERHEAD BIN. / [01] REPLACED LENS REF AMM 33-51-03; [02] C/W
- [SDR SWAA2021052775721](https://openairdocs.org/sdr/SWAA2021052775721.md): Slide · out of position · May 23, 2021 · N727SW · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT. RE-POSITIONED AND SECURED SLIDE REF AMM 25-66-01
- [SDR SWAA2021031554132](https://openairdocs.org/sdr/SWAA2021031554132.md): Cover · missing · Mar 10, 2021 · N727SW · Boeing 7377H4 · Emergency Lighting
  > ROW 6DEF EMERGENCY LIGHT COVER MISSING. LIGHT WORKS NORMALLY / CLOSING DMA 0154430 INSTALLED LENS COVER @ ROW 6DEF EMERGENCY LIGHT AS PER AMM 33-51-03. CL# 71277
- [SDR SWAA2021020144741](https://openairdocs.org/sdr/SWAA2021020144741.md): Battery Pack · failed · Jan 26, 2021 · N727SW · Boeing 7377H4 · Emergency Lighting
  > BATTERY PACKS FAILED CAPACITY TEST AT FOLLOWING POSITIONS; FRONT LEFT; ROW 16 LEFT; LEFT OVERWING; RIGHT OVERWING; AFT LEFT; AND AFT RIGHT. REMOVED AND REPLACED PER AMM.33-51-06.
- [SDR SWAA2020111229518](https://openairdocs.org/sdr/SWAA2020111229518.md): Lamp · inoperative · Nov 11, 2020 · N727SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE THE FORWARD ENTRY DOOR THRESHOLD PORTION HAS LIGHTS OUT. REPLACED LAMPS FOR EMERGENCY LIGHT AT THE FWD ENTRY DOOR THRESHOLD AND PERFORMED GOOD TEST, PER AMM 33-51-01-960-801.
- [SDR SWAA2020111628888](https://openairdocs.org/sdr/SWAA2020111628888.md): Battery Pack · no test · Nov 7, 2020 · N727SW · Boeing 7377H4 · Emergency Lighting
  > DURING EMERGENCY LIGHTING TEST L1067, L730,ND L1065 ARE INOPERABLE AT STA 429. REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1674, PER AMM 33-51-06-960-805.
- [SDR SWAA2020111627310](https://openairdocs.org/sdr/SWAA2020111627310.md): Crease Beam · corroded · Nov 1, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION, ON CREASE BEAM INNER CORD BS 639 LBL 55 WL 208. REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD BS 532-675 LBL 55 WL 208, IAW BOEING DWGS 144A5910, 144A5901, 143A5240 AND SRM 51-40-02-0G-0 BS 639 LBL 55 WL 208 CREASE BEAM INNER CHORD CORROSION WA
- [SDR SWAA2020111625593](https://openairdocs.org/sdr/SWAA2020111625593.md): Skin · corroded · Oct 22, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION, EXTERNAL FUSELAGE SKIN NUTPLATE HOLES AT ADF ANTENNAE LOCATION BS 678-702 STR 1-2RT. REPAIRED DAMAGE ON EXTERNAL FUSELAGE SKIN NUTPLATE HOLES AT ADF ANTENNA LOCATIONS BS 678-702 STR 1-2RT, PER ER 20-03489 REV IR AND EA 20-153-02201 REV IR.
- [SDR SWAA2021021124964](https://openairdocs.org/sdr/SWAA2021021124964.md): Support Plate · corroded · Oct 21, 2020 · N727SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / EVALUATED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT. REMOVED 0.015'; FROM ORIG.040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2
- [SDR SWAA2021021124963](https://openairdocs.org/sdr/SWAA2021021124963.md): Support Plate · corroded · Oct 21, 2020 · N727SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT; BS727-847; REMOVED.015' FROM ORIG.040'; FOUND TO BE OUT OF LIMITS; LOCATED;
- [SDR SWAA2020111629266](https://openairdocs.org/sdr/SWAA2020111629266.md): Skin · dented · Oct 21, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BS 907 +10; 2' BELOW STR 18L. DENT MEASURES L=2.6' W=2' Y=.024 W/Y=83 IS WITHIN LIMITS, PER SRM 53-00-01-1A-1 & EA 20-153-02206 REV IR & ER 20-03499 REV IR. APPLIED DAMAGE IDENTIFICATION, AS PER MPM 52.03.01.02 & PER EA 20-153-02206 RE
- [SDR SWAA2020111629048](https://openairdocs.org/sdr/SWAA2020111629048.md): Skin · dented · Oct 21, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BS 927+3, COMMON TO STR 18L. DENT ON FUSELAGE SKIN BS 927+3, COMMON TO STR 18L WAS FOUND TO BE OUT OF LIMITS, DUE TO LOCATION AT STRINGER 18L. REPAIRED PER ATS ER 20-03499 REV IR AND EA 20-153-02206 REV IR.
- [SDR SWAA2020111624846](https://openairdocs.org/sdr/SWAA2020111624846.md): Attach Angle · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 693 LBL 1 WL 204-207, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 693 LBL 1 WL 204-207, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV B DWG 273A9110 REV A.
- [SDR SWAA2020111624845](https://openairdocs.org/sdr/SWAA2020111624845.md): Attach Angle · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 LBL 24 WL 204, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 LBL 24 WL 204, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV A 273A9110 REV A.
- [SDR SWAA2020111624844](https://openairdocs.org/sdr/SWAA2020111624844.md): Attach Angle · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 24 WL 204, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 24 WL 204, IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV A DWG 111A6000 REV A.
- [SDR SWAA2020111624843](https://openairdocs.org/sdr/SWAA2020111624843.md): Attach Angle · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 1 WL 207, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 1 WL 207, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV B DWG 273A9110 REV A.
- [SDR SWAA2020111624841](https://openairdocs.org/sdr/SWAA2020111624841.md): Crease Beam · corroded · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION, ON CREASEBEAM WEB ATTACH ANGLE STA 664 RBL 67 WL 208 UPPER SURFACE, MARKED. REMOVED CORROSION ON CREASEBEAM WEB ATTACH ANGLE STA 664 RBL 67 WL 208 UPPER SURFACE. MAX MATERIAL REMOVED FROM.056' 7075T6 LOT NR 1331117-2. REMOVED OLD AND LOCATED & D
- [SDR SWAA2020111624723](https://openairdocs.org/sdr/SWAA2020111624723.md): Stringer · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK COMMON TO END OF STR 23L IN SNAKE PIT BS 536 WL 163. STRINGER WAS REPAIRED, PER ATS ER 20-03457 REV IR AND SWA EA 20-153-02126 REV IR.
- [SDR SWAA2020111624726](https://openairdocs.org/sdr/SWAA2020111624726.md): Stringer · corroded · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION COMMON TO END OF STR 27L IN SNAKE PIT BS 536 WL 150. CORROSION COMMON TO END OF STR 27L BS 536 WL 150 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION BS 500D+11'-BS 536 STR 27L. REPAIRED SECTION, PER SRM 53-00-03-2R-1 SRM
- [SDR SWAA2020111624725](https://openairdocs.org/sdr/SWAA2020111624725.md): Stringer · corroded · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION COMMON TO END OF STR 26L IN SNAKE PIT BS 536 WL 152. CORROSION COMMON TO END OF STR 26L BS 536 WL152 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION BS 500D+11'-BS 536 STR 26L. REPAIRED SECTION, PER SRM 53-00-03-2R-1 SRM 5
- [SDR SWAA2020111624724](https://openairdocs.org/sdr/SWAA2020111624724.md): Stringer · cracked · Oct 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK COMMON TO END OF STR 26R IN SNAKE PIT BS 536 WL 152. REMOVED DAMAGE AND REPAIRED STR 26R IN SNAKE PIT BS 536 WL 152, IAW SRM 53-00-03-2R-1.
- [SDR SWAA2021081324604](https://openairdocs.org/sdr/SWAA2021081324604.md): Plate · missing · Oct 19, 2020 · N727SW · Boeing 7377H4 · Cargo/Baggage Doors
  > STRIKER PLATES ON BOOMERANG ANGLE LOCATED ON R/H AC BAY DOOR #192CR ARE MISSING OR DAMAGED / REMOVED AND REPLACED BOOMERANG ANGLE ON R/H AC BAY DOOR IAW AIPC 52-48-11-03 AND SOPM 20-50-01.
- [SDR SWAA2021080924608](https://openairdocs.org/sdr/SWAA2021080924608.md): Door · corroded · Oct 19, 2020 · N727SW · Boeing 7377H4 · Fluid Service Doors
  > EXTERIOR LAV SERVICE DOOR HAS CORROSION ON THE INTERNAL SIDE OF DOOR AROUND THE BONDING JUMPER STUD / FOUND CORROSION ON INTERNAL SIDE OF THE EXTERIOR LAV SERVICE DOOR TO BE OUT OF LIMITS; ORIGINAL THICKNESS 0.100; REMOVED 0.040 MATERIAL PER SRM 52-40-01-0I-4;
- [SDR SWAA2021082624439](https://openairdocs.org/sdr/SWAA2021082624439.md): Angle · cracked · Oct 18, 2020 · N727SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE TRANSVERSE WEB ABOVE #2 PYLON FAIRING AFT TIP THE O/B ATTACH ANGLE CRACKED / REMOVED AND REPLACED R/W T/E TRANSVERSE WEB O/B ATTACH ANGLE (CLIP) ABOVE #2 PYLON FAIRING AFT TIP IAW SRM 51-40-02-0G-0 PARA 4; AIPC 57-42-51-02; AND BAC DRA
- [SDR SWAA2020111624252](https://openairdocs.org/sdr/SWAA2020111624252.md): Pressure Deck · cracked · Oct 18, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Structure
  > DURING COMPLETION OF CCN 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK CRACKED ON LEFT SIDE AT BS 663 WL 201 LBL 30 AND 32. ALSO AT BS 673 WL201 LBL 30 AND 38, AREAS MARKED. REMOVED DAMAGE PART OF THE HORIZONTAL PRESSURE DECK BS 663-674 LBL 30-LBL 60 WL 201 A
- [SDR SWAA2020111624251](https://openairdocs.org/sdr/SWAA2020111624251.md): Stiffener · cracked · Oct 18, 2020 · N727SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) HAS CRACK AT 4TH STIFFENER. REPAIRED LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 AT STAB STA 120.30 4TH STIFFENER, IAW SRM 55-10-09-2R-5. 59796C 20 OCT '20.
- [SDR SWAA2020111629163](https://openairdocs.org/sdr/SWAA2020111629163.md): Pressure Deck · dented · Oct 16, 2020 · N727SW · Boeing 7377H4 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. REPAIRED FLIGHT DECK FLOOR DAMAGE AT BS 255 RBL 4-LBL 14 WL 207.54, PER ER 20-03451 REV IR AND EA NR 20-153-02181 REV IR.
- [SDR SWAA2020111624172](https://openairdocs.org/sdr/SWAA2020111624172.md): Stiffener · cracked · Oct 16, 2020 · N727SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 (STAB STA 120.30) STIFFENER 2 IS CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) 2ND STIFFENER AT LOWER END, IAW SRM 55-10-09-2R-5.
- [SDR SWAA2020111624173](https://openairdocs.org/sdr/SWAA2020111624173.md): Stiffener · cracked · Oct 16, 2020 · N727SW · Boeing 7377H4 · Horizontal Stabilizer Structure
  > LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 (STAB STA 120.30) STIFFENER 3 IS CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 AT STAB STA 120.30 3RD STIFFENER, IAW SRM 55-10-09-2R-5 59796C 20 OCT '20.
- [SDR SWAA2020111224159](https://openairdocs.org/sdr/SWAA2020111224159.md): Handle · loose · Oct 16, 2020 · N727SW · Boeing 7377H4 · Emergency Equipment
  > FWD ENTRY DOOR ASSIST HANDLES ARE LOOSE. TIGHTENED FED ASSIST HANDLE, PER SOPM 20-50-01.
- [SDR SWAA2020101422218](https://openairdocs.org/sdr/SWAA2020101422218.md): Slide · loose · Oct 11, 2020 · N727SW · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE LOOSE IN COVER / ADJUSTED FWD SERVICE DOOR SLIDE PER S.I.P.
- [SDR SWAA2020101422217](https://openairdocs.org/sdr/SWAA2020101422217.md): Light · unsecure · Oct 11, 2020 · N727SW · Boeing 7377H4 · Emergency Lighting
  > EXIT FLOOR LIGHT STRIPS LOOSE NEW FORWARD ENTRY DOOR / SECURED EXIT FLOOR LIGHT STRIP PER S.I.P.
- [SDR SWAA2020100821722](https://openairdocs.org/sdr/SWAA2020100821722.md): Slide · out of adjust · Oct 7, 2020 · N727SW · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE PARTIALLY DEPLOYED. AFT SLIDE NOTE DEPLOYED, PARTIALLY FELL OUT OF CONTAINER. REINSTALLED SLIDE, PER MT 725-61-06. A/C OK FOR SERVICE STS LINE MX Q6TR841X.
- [SDR SWAA2021080532950](https://openairdocs.org/sdr/SWAA2021080532950.md): Floor Panel · cracked · Mar 20, 2020 · N727SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT AFT FLOOR PANEL CRACKED / REMOVED & REPLACED FWD CARGO COMPARTMENT AFT FLOOR PANEL PER AMM 25-52-1
- [SDR SWAA2022032373869](https://openairdocs.org/sdr/SWAA2022032373869.md): Support · elongated · Oct 22, 2019 · N727SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > REF LP: 1213458 LOWER AFT FAIRING FOR RH WHEEL WELL CUT OUT (PN: 149A7603-120) HAS SEVERAL ATTACHING HOLES THAT ARE ELONGATED / 'REFERENCE DMA 0156733' REMOVED AND REPLACED WHEEL WELL FAIRING SUPPORT PER SRM 51-40-02 CL #27301
- [SDR SWAA2019071934997](https://openairdocs.org/sdr/SWAA2019071934997.md): Handle · loose · Jul 17, 2019 · N727SW · Boeing 7377H4 · Emergency Exits
  > RT WING OVER WING EMERGENCY EXIT HANDLE MOLDING LOOSE. SECURED HANDLE REF MM.
- [SDR SWAA2022031173891](https://openairdocs.org/sdr/SWAA2022031173891.md): Panel · elongated · Jul 16, 2019 · N727SW · Boeing 7377H4 · Aerodynamic Fairings
  > 193 B PANEL HOLES FOR SCREWS ARE ENLARGED / R&R 193B PANEL PER BOEING DOCUMENT NUMBER 149A7652-13 PL AND EO 14108 SA-M 326: A1073171
- [SDR SWAA2019071834950](https://openairdocs.org/sdr/SWAA2019071834950.md): Bracket · loose · Jul 15, 2019 · N727SW · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR SLIDE GIRT BAR ATTACHMENT HANGING LOOSE. TIGHTEN GIRT BAR BRACKETS PER MT.
- [SDR SWAA2022031074102](https://openairdocs.org/sdr/SWAA2022031074102.md): Spoiler · debonded · May 30, 2019 · N727SW · Boeing 7377H4 · Spoilers
  > DURING COMPLETION OF CCN: EA 1-A57-15168 FOUND #7 SPOILER TO BE DISBONDED AT 4 EA LOCATIONS. 1 = 14' FROM O/B EDGE AND 10' FROM L/E. 2 = 9' FROM L/E AND 29.5' FROM O/B EDGE. 3 = 5' FROM T/E AND 20' FROM I/B EDGE. 4 = 8' FROM L/E AND 19' FROM I/B EDGE. / REMOVE
- [SDR SWAA2019060333309](https://openairdocs.org/sdr/SWAA2019060333309.md): Skin · debonded · May 30, 2019 · N727SW · Boeing 7377H4 · Spoilers
  > R/H WING #12 SPOILER DEBONDED AT 14.5" FROM INBOARD EDGE AND 9" FROM LEADING EDGE. / R&R #12 OUTBOARD GROUND SPOILER PER AMM.
- [SDR SWAA2019060333308](https://openairdocs.org/sdr/SWAA2019060333308.md): Skin · debonded · May 30, 2019 · N727SW · Boeing 7377H4 · Spoilers
  > R/H WING #10 SPOILER DEBONDED AT 12" FROM OUTBOARD EDGE AND 9" FROM LEADING EDGE. / R&R #10 SPOILER PANEL IAW AMM.
- [SDR SWAA2019060333307](https://openairdocs.org/sdr/SWAA2019060333307.md): Skin · debonded · May 30, 2019 · N727SW · Boeing 7377H4 · Spoilers
  > R/H WING #9 SPOILER DEBONDED AT 3" FROM OUTBOARD EDGE AND 10" FROM TAILING EDGE. / R&R #9 SPOILER PANEL IAW MM.
- [SDR SWAA2019060333306](https://openairdocs.org/sdr/SWAA2019060333306.md): Skin · debonded · May 30, 2019 · N727SW · Boeing 7377H4 · Spoilers
  > L/H WING #6 SPOILER DEBONDED. R&R #6 INBOARD GROUND SPOILER PER AMM.

Next page: https://openairdocs.org/deregistered/N727SW-2024-09-18/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 = 'N727SW' AND deregistration_id = 'N727SW-2024-09-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N727SW-2024-09-18/reports

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