# Service difficulty reports: N570WN

A list on [N570WN](https://openairdocs.org/aircraft/N570WN.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 4 · 179 reports

- [SDR SWAA2026061109905](https://openairdocs.org/sdr/SWAA2026061109905.md): Slide · out of adjust · Jun 7, 2026 · N570WN · Boeing 7377CT · Escape Slide
  > FWD ENTRY DOOR SLIDE OUT OF CASE. REINSTALLED EMERGENCY SLIDE ON CASE FOR L1 ENTRY DOOR IAW MT- 725-61-06 PERFORMED L-1 DOOR OPS CHECK. OPS CHKD GOOD. ACFT OK FOR SERVICE.
- [SDR SWAA2026051803121](https://openairdocs.org/sdr/SWAA2026051803121.md): Skin · pulled · May 15, 2026 · N570WN · Boeing 7377CT · Wing, Plate/Skin
  > RIGHT WING LOWER PANEL (651GB) HAS 5 RIVETS PULLED THROUGH AT FWD O/B WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE ASSY IAW SRM 51-40-02 AND REINSTALLED WING PANEL 651GB IAW AMM 57-05-03
- [SDR SWAA2025042325101](https://openairdocs.org/sdr/SWAA2025042325101.md): Light · inoperative · Apr 15, 2025 · N570WN · Boeing 7377CT · Emergency Lighting
  > LEFT HAND OVERWING EMERGENCY EXIT LIGHT ON AFT SIDE INOP <[01]. REMOVED LEFT OVERWING EMERGENCY EXIT SIGN LIGHT ASSEMBLY IAW AMM 33-51-01-960-802; FOUND BROKEN WIRE OF CONNECTOR D12396. REPAIRED WIRE OF CONNECTOR D12396 IAW WDM 33-51-21; SWPM 20-30-12 AND PE
- [SDR SWAA2025042324389](https://openairdocs.org/sdr/SWAA2025042324389.md): Seat · loose · Apr 13, 2025 · N570WN · Boeing 7377CT · Passenger Compartment Equipment
  > SEAT AT ROW 11ABC I/B REAR FOOT WILL NOT TIGHTEN <[01]. REMOVED AND REPLACED THE REAR I/B SEAT FOOT IAW SOPM 20-50-01. INSTALLED SEAT AND TORQUED IAW AMM 25-22-00-400-802. ATS3239; DUE 03/2026; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABL
- [SDR SWAA2025042323602](https://openairdocs.org/sdr/SWAA2025042323602.md): Scuff Plate · cracked · Apr 10, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO FWD CORNER SCUFF PLATE CRACKED <[01]. REPAIRED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. SCUFF PLATE IS TO BE INSTALLED ON CUSTOMER CARD TTG8Q00ZL13U; [02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2025042321761](https://openairdocs.org/sdr/SWAA2025042321761.md): Skin · cracked · Apr 4, 2025 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > CRACK NOTED ON RH HORIZONTAL STABILIZER LOWER SKIN AT STA 193.90 RIB; 17.5' FROM FWD EDGE; L: 0.75' MARKED <[01]. EDITED 13 TO PARTIAL; [02] PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER SKIN AT STA 193.90 RIB; 17.5' FROM FWD EDGE IAW SRM 51-40-02-0G-0 A
- [SDR SWAA2025042321205](https://openairdocs.org/sdr/SWAA2025042321205.md): Scuff Plate · cracked · Apr 2, 2025 · N570WN · Boeing 7377CT · Cargo Compartments
  > FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED <[01]. UPON FURTHER INVESTIGATION; SCUFF PLATE WAS DAMAGED BEYOND REPAIR. RECEIVED NEW FCB FWD CORNER SCUFF PLATE FROM STORES. LOCATED AND DRILLED IAW BOEING DWG 143A8331 REV-C AND SRM 51-40-05.; [02] VER
- [SDR SWAA2025042320972](https://openairdocs.org/sdr/SWAA2025042320972.md): Floor Panel · delaminated · Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Floor Panel
  > PASS CABIN FLOOR 241AF DELAMINATED IN SEVERAL AREAS <[01]. FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]; [02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025042321200](https://openairdocs.org/sdr/SWAA2025042321200.md): Scuff Plate · cracked · Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT; AFT CORNER SCUFF PLATE IS CRACKED. <[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975 EQUIPMENT USED; WELDING MACHINE ID# E10583 CAL DUE DATE 01/2
- [SDR SWAA2025042321202](https://openairdocs.org/sdr/SWAA2025042321202.md): Structure · corroded · Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION ON CREASE BEAM INNER CHORD UPPER SURFACE; STA 687-727; RBL65 WL208. <[01] REMOVED AND REPLACED INNER CREASE BEAM CHORD BS 675-732 RBL 65 WL 208 P/N 144A5910U10 LOT 1601385-1 I.A.W SRM 51-40-02-0G-0 AND DWG 144A5900; [02] REMOVED AND REPLACED INNER CR
- [SDR SWAA2025042321203](https://openairdocs.org/sdr/SWAA2025042321203.md): Panel · cracked · Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACKED PANEL BREAK BS 540 BL0-LBL25; WL208 <[01]. INSTALLED NEW PANEL BREAK BS 540 BL0-LBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025042321204](https://openairdocs.org/sdr/SWAA2025042321204.md): Panel · cracked · Apr 2, 2025 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACKED PANEL BREAK BS 540 BL0-RBL25; WL208 <[01]. REMOVED AND REPLACED PANEL BREAK BS 540 BL0-RBL25; WL208 PER SRM 51-40-02; 51-40-05 AND DWG 143A0060 REV A.; [02] VERIFIED ACTION 1. JOB COMPLETE.
- [SDR SWAA2025042320085](https://openairdocs.org/sdr/SWAA2025042320085.md): Pressure Deck · cracked · Mar 31, 2025 · N570WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACKED HORIZONTAL PRESSURE DECK ABOVE MLG WHEEL WELL BS664 RBL41 WL203. <[01] REMOVED FASTENERS COMMON TO REPAIR AREA AND CUT AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202. INSTALLED REPAIR PARTS AND APPLIED CIC PER SRM 53-
- [SDR SWAA2025033119511](https://openairdocs.org/sdr/SWAA2025033119511.md): Cover · detached · Mar 29, 2025 · N570WN · Boeing 7377CT · Emergency Exits
  > FO OVERWING EXIT HANDLE COVER FELL OFF<[01] INSTALLED PER SIP
- [SDR SWAA2025033119092](https://openairdocs.org/sdr/SWAA2025033119092.md): Seat · inoperative · Mar 28, 2025 · N570WN · Boeing 7377CT · Passenger Compartment Equipment
  > CABIN SEAT RECLINE IN EMERGENCY EXIT ROW NEEDS TO BE INOP AT 11D<[01] LOCKED OUT HYDRAULIC AT SEAT 11D IAW AMM 25-22-00.
- [SDR SWAA2024112570197](https://openairdocs.org/sdr/SWAA2024112570197.md): Tray · out of adjust · Nov 21, 2024 · N570WN · Boeing 7377CT · Passenger Compartment Equipment
  > TRAY TABLE DOES NOT SLIDE FREELY ON SEATBACK 11F EMERGENCY EXIT ROW.<[01] R&R TRAY TABLE ON SEATBACK 11F EMERGENCY EXIT ROW PER CMM 25-21-42
- [SDR SWAA2024102451434](https://openairdocs.org/sdr/SWAA2024102451434.md): Light · detached · Oct 21, 2024 · N570WN · Boeing 7377CT · Emergency Lighting
  > LOWER EXIT SIGN COVER FELL OFF FWD ENTRY DOOR.<[01] R&R?D FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSAY. PER AMM 33-51-01.
- [SDR SWAA2024012343553](https://openairdocs.org/sdr/SWAA2024012343553.md): Hmu · faulted · Jan 22, 2024 · N570WN · Boeing 7377CT · Engine (Turbine/Turboprop)
  > TOD AT 380; NR 1 ENG EXPERIENCED VIBRATION/SHUTTER W/ROLLBACK. ENGINE RECOVERED; THEN ANOTHER SHUDDER; THEN ROLLBACK SHUTDOWN ENGINE AND CONTINUED TO DEN. NO EGT LIMITS EXCEEDED. ON LANDING; BOTH (CONTD) (CONTD FROM ABOVE) ENGINE CONTROL LIGHTS ILLUMINATED<[01
- [SDR SWAA2023053150042](https://openairdocs.org/sdr/SWAA2023053150042.md): Light · inoperative · May 19, 2023 · N570WN · Boeing 7377CT · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED L2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.
- [SDR SWAA2023053148972](https://openairdocs.org/sdr/SWAA2023053148972.md): Battery Pack · inoperative · May 16, 2023 · N570WN · Boeing 7377CT · Emergency Lighting
  > SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED BATTERY PACKS AT POS. M2335; M1668; M1669; M1674; M1675; M1672; AND M1673 AS PER REFERENCE AMM 33-51-06-960-805. PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST; AS PER REFEREN
- [SDR SWAA2023053142260](https://openairdocs.org/sdr/SWAA2023053142260.md): Support · corroded · Apr 27, 2023 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION****AFT CARGO COMPARTMENT R/H FLOOR SUPPORT STA 787 TO 767 RBL 23' LOWER SURFACE CORROSION AT NUT PLATES.<[01] PART #146A8127-12 IS OUT OF LIMITS PER REF SRM 53-60-15-1A-1. WILL BE REPLACED FROM STA 767-807; FOR WORK ACCOMPLISHED REFERENCE TASK CARD #
- [SDR SWAA2023053142259](https://openairdocs.org/sdr/SWAA2023053142259.md): Support · corroded · Apr 27, 2023 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION****AFT CARGO COMPARTMENT R/H FLOOR SUPPORT STA 807 - 780 RBL 23' LOWER SURFACE CORROSION AT NUT PLATES.<[01] PART #146A8127-12 IS OUT OF LIMITS PER REF SRM 53-60-15-1A-1. WILL BE REPLACED FROM STA 767-807; FOR WORK ACCOMPLISHED REFERENCE TASK CARD #T
- [SDR SWAA2023053142261](https://openairdocs.org/sdr/SWAA2023053142261.md): Channel · corroded · Apr 27, 2023 · N570WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION** AFT CARGO COMPARTMENT R/H 'Z' CHANNEL FRON STA 807 TO 767 HAS SEVERAL POINT OF CORROSION<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT SHIELD AT STA 767-807 RBL 21 PER REF SRM 51-40-02-0G-0;[02] INSTALLED NEW AFT CARGO COMPARTMENT SHIELD AT STA 7
- [SDR SWAA2023053142055](https://openairdocs.org/sdr/SWAA2023053142055.md): Winglet · delaminated · Apr 26, 2023 · N570WN · Boeing 7377CT · Wing Main, Frame Structure
  > RH WINGLET AFT (CARBON FIBER) SPAR;SIGNS OF DELAMINATION AND LOOSE FIBERS AT MOST UPPER TOOLING HOLES.<[01] DAMAGE FOUND AT RH WINGLET UPPER SKIN INTERNAL AREA OUTSIDE OF AAR MIAMI REPAIR CAPABILITIES; WINGLET TO BE REPLACED. INSTALL ACCOMPLISHED ON ROUTINE C
- [SDR SWAA2023053142056](https://openairdocs.org/sdr/SWAA2023053142056.md): Winglet · delaminated · Apr 26, 2023 · N570WN · Boeing 7377CT · Wing Main, Frame Structure
  > LH WINGLET AFT (CARBON FIBER) SPAR;SIGNS OF DELAMINATION AND LOOSE FIBERS AT MOST UPPER TOOLING HOLES.<[01] DAMAGE FOUND AT LH WINGLET UPPER SKIN INTERNAL AREA OUTSIDE OF AAR MIAMI REPAIR CAPABILITIES; WINGLET TO BE REPLACED. INSTALL ACCOMPLISHED ON ROUTINE C
- [SDR SWAA2023053146362](https://openairdocs.org/sdr/SWAA2023053146362.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > R/H OVERWING FAIRING ACCESS PANEL # 195CR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REMOVED PANEL 195CL FOR ACCESS REF B-737-700 SRM 51-40-02-0G-0
- [SDR SWAA2023053146000](https://openairdocs.org/sdr/SWAA2023053146000.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > R/H OVERWING FAIRING ACCESS PANEL # 195BR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED PANEL #195BR PER B737 SRM 51-70-06-2R-9 PARA 4.E. MATERIALS USED RESIN P/O#2008859; CLOTH P/O#1690463;[02] VERIFIED ALL STEPS
- [SDR SWAA2023053146361](https://openairdocs.org/sdr/SWAA2023053146361.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > R/H UNDERWING FAIRING ACCESS PANEL # 192AR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] APPLIED REPAIRED AT FAIRING # 192AR PER B737 SRM 51-70-04-2R-0 MATERIAL USED RESIN EY 3804 PO#2008859 AND FIBERGLASS PO# 1690463 AND DRILLED HOLES REF B-737-700 SRM 51-4
- [SDR SWAA2023053146363](https://openairdocs.org/sdr/SWAA2023053146363.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > L/H LOWER AFT FAIRING ACCESS PANEL # 194DL HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED ACCESS PANEL # 194DL AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED; RESIN PO# 1800550 AND CLOTH PO# 1738579.;[02] VERIFIED ALL STEPS
- [SDR SWAA2023053146364](https://openairdocs.org/sdr/SWAA2023053146364.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > LOWER FWD CENTER WHEEL WELL ACCESS PANEL # 193B HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] APPLIED A PERMANENT REPAIR ON DAMAGE FASTENER HOLES AS MARKED ON LOWER CENTER WHEEL ACCESS PANEL #193B AS PER B737 SRM 51-70-04-2R-9. MATERIALS USED PO#1776837; PO#
- [SDR SWAA2023053146366](https://openairdocs.org/sdr/SWAA2023053146366.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > RIGHT WING-TO-BODY FAIRING ACCESS PANEL # 194AR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED DAMAGE AREAS AT R/W TO BODY FAIRING ACCESS PANEL #194AR AS PER SRM 51-70-04-2R-9. MATERIAL USED BMS9-3-120TYD CL7 PO#1690463 PLUS EY 3804 A/B PO#2008859.;[
- [SDR SWAA2023053147152](https://openairdocs.org/sdr/SWAA2023053147152.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > LOWER FUSELAGE AFT FAIRING CENTER ACCESS PANEL # 194E HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REMOVED DAMAGED AND PREPARED AREA FOR REPAIR AS MARKED ON ACCESS PANEL #194 E AS PER B737 SRM 51-70-04-2R-9<BR>APPLIED REPAIR IN DAMAGED AREA AT ACCESS PANEL
- [SDR SWAA2023053147153](https://openairdocs.org/sdr/SWAA2023053147153.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > R/H UPPER AFT FAIRING ACCESS PANEL # 19FR HAS SEVERAL FASTENER HOLES BULGING/CRACKED PANEL # 194FR<[01] REMOVED AND PREPARED DAMAGED AREA FOR REPAIR ON ACCESS PANEL #194FR AS PER; B737 SRM 51-70-04-2R-9<BR>APPLIED REPAIR IN DAMAGED AREA AT ACCESS PANEL #194 FR
- [SDR SWAA2023053147364](https://openairdocs.org/sdr/SWAA2023053147364.md): Panel · cracked · Apr 26, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > R/H LOWER AFT I/B FAIRING ACCESS PANEL # 194CR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED DAMAGE HOLES AT R/H LOWER AFT I/B FAIRING ACCESS PANEL #194CR AS PER SRM 51-70-04-2R-9. MATERIAL USED EY3804 PO# 1800550 PLUS BMS9-3-7781 PO#1738579;[02] VE
- [SDR SWAA2023053146360](https://openairdocs.org/sdr/SWAA2023053146360.md): Panel · bulged · Apr 25, 2023 · N570WN · Boeing 7377CT · Wing, Plate/Skin
  > LEFT WING LOWER MID SPAN T/E ACCESS PANEL # 561BB HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] REPAIRED ACCESS PANEL #561BB AS PER B737 SRM 51-70-04-2R-9. MATERIAL USED CAB PO# 1776837 AND RESIN PO# 1800550 AND CLOTH PO#1738579.;[02] VERIFIED PANEL #561BB
- [SDR SWAA2023053141641](https://openairdocs.org/sdr/SWAA2023053141641.md): Support Beam · worn · Apr 25, 2023 · N570WN · Boeing 7377CT · Wing Main, Frame Structure
  > LEFT WING DEFLECTOR PANEL UPPER SUPPORT BEAM WORN<
- [SDR SWAA2023053146359](https://openairdocs.org/sdr/SWAA2023053146359.md): Panel · cracked · Apr 25, 2023 · N570WN · Boeing 7377CT · Aerodynamic Fairings
  > RIGHT FUSELAGE ACCESS PANEL # 193CR HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] PAINT;[02] APPLIED REPAIR IN DAMAGE AREA ON RIGHT FUSELAGE ACCESS PANEL # 193CR.; AS PER B737 SRM 51-70-06-2R-9 MATERIAL USED PO.1473815 AND PO.1800550;[03] VERIFIED ALL STEPS
- [SDR SWAA2023053131070](https://openairdocs.org/sdr/SWAA2023053131070.md): Stiffener · cracked · Apr 24, 2023 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > LH HORIZONTAL STABILIZER RIN #4 CRACKED AT #3 STIFFENER<[01] ALL INSPECTION STEPS COMPLETED.;[02] ALL RII INSPECTION COMPLETED.;[03] SUMMARY=CUT AND REMOVED THE DAMAGED FROM THE VERTICAL STIFFENER #3 OF THE RIB AS PER REF B/737 SRM 55-10-09-2R-4 REPAIR 4. REMO
- [SDR SWAA2023053130673](https://openairdocs.org/sdr/SWAA2023053130673.md): Skin · corroded · Apr 23, 2023 · N570WN · Boeing 7377CT · Cargo/Baggage Doors
  > CORROSION- AFT CARGO DOOR INTERNAL SKIN LOWER SURFACE 14 INCHES FROM THE LWR FWD. CORNER<[01] PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS AT AFT CARGO DOOR INTERNAL SKIN LOWER SURFACE 14' FROM LOWER FWD. CORNER; IAW NDTM PART 6; 51-0
- [SDR SWAA2023053130355](https://openairdocs.org/sdr/SWAA2023053130355.md): Door · out of adjust · Apr 21, 2023 · N570WN · Boeing 7377CT · Passenger/Crew Doors
  > FWD ENTRY DOOR NEED ADJUSTMENT<[01] ACCOMPLISHED FWD ENTRY DOOR ADJUSTMENT AND TEST PER B737 AMM 52-11-00-820-801-NG;[02] VERIFIED ADJUSTMENT
- [SDR SWAA2023053129863](https://openairdocs.org/sdr/SWAA2023053129863.md): Floor Panel · delaminated · Apr 20, 2023 · N570WN · Boeing 7377CT · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241EF FWD CORNERS CRUSHED/DELAMINATED AT I/B EDGE<[01] APPLIED REPAIR IN DAMAGED AREA AT FLOOR PANEL 241EF AS PER B737 SRM 53-00-50-2R-4; MATERIAL USED PO# 2013314;[02] VERIFIED APPLIED REPAIR IN DAMAGED AREA AT FLOOR PANEL 241EF AS PER
- [SDR SWAA2023053129866](https://openairdocs.org/sdr/SWAA2023053129866.md): Floor Panel · cracked · Apr 20, 2023 · N570WN · Boeing 7377CT · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242AF HAS MULTIPLE DENTS AND POSSIBLE CRACK UPPER SKIN<[01] APPLIED REPAIR IN DAMAGED AREA AT FLOOR PANEL 242 AF AS PER B737 SRM 53-00-50-2R-1; MATERIAL USED PO# 1738579; PO# 1799598;[02] VERIFIED APPLIED REPAIR IN DAMAGED AREA AT FLOOR
- [SDR SWAA2023052529861](https://openairdocs.org/sdr/SWAA2023052529861.md): Floor Panel · cracked · Apr 20, 2023 · N570WN · Boeing 7377CT · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232RF CRACKED/PUNCTURED ON LOWER SKIN<[01] REPAIRED DAMAGED AREA ON MAIN CABIN FLOOR PANEL 232RF. REF B737 SRM 53-00-50-2R-1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#:1694548 AND RESIN EPOCAST50A PO#: 1799598.
- [SDR SWAA2022120277549](https://openairdocs.org/sdr/SWAA2022120277549.md): Light · peeling · Dec 2, 2022 · N570WN · Boeing 7377CT · Emergency Lighting
  > FORWARD RIGHT PHOTO LUMINESCENT STRIP PEELING AT FWD MOST END. SECURED FWD RT PHOTO LUMINESCENT STRIP AT FWD MOST END IAW SIP.
- [SDR SWAA2022120277559](https://openairdocs.org/sdr/SWAA2022120277559.md): Seal · cracked · Dec 2, 2022 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL FWD UPPER SLIDER SEAL IAW MM 53-31-31-400-802-NG.
- [SDR SWAA2022120277561](https://openairdocs.org/sdr/SWAA2022120277561.md): Seal · cracked · Dec 2, 2022 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDER SEAL CRACKED. REPLACED R/H STAB SLIDING FORWARD LOWER SEAL PER MM 53-31-31.
- [SDR SWAA2022120277562](https://openairdocs.org/sdr/SWAA2022120277562.md): Seal · cracked · Dec 2, 2022 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED UPPER FRONT SPAR SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2022120277564](https://openairdocs.org/sdr/SWAA2022120277564.md): Seal · cracked · Dec 2, 2022 · N570WN · Boeing 7377CT · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER SEAL DAMAGED & CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FWD LOWER SLIDER SEAL IAW AMM 53-31-31-400-803-NG.
- [SDR SWAA2022120277563](https://openairdocs.org/sdr/SWAA2022120277563.md): Attach Bracket · broken · Dec 2, 2022 · N570WN · Boeing 7377CT · Fuselage Main, Attach Fittings
  > FWD KEEL PANEL 192BR AFT ATTACH BRACKETS BROKEN THIS NON ROUTINE IS FOR PANEL 192E NOT 192BR. / [01] REMOVED AND REPLACED 2 EA AFT ATTACH BRACKETS AT FWD KEEL PANEL 192BR.;[02] WORK ACCOMPLISHED PER SRM 51-40-02.;[03] C/W
- [SDR SWAA2022050301093](https://openairdocs.org/sdr/SWAA2022050301093.md): Unknown · cracked · Apr 30, 2022 · N570WN · Boeing 737 · Fuselage Main, Plate/Skin
  > RT O/W EXIT UPPER SILL SHIELD ASSY LEXAN CRACKED AT ALL 4 FASTENER LOCATIONS / [01] FAULT RESOLVED ON OTHER FAULT. REF TTG8Q00C70LW AND<BR>EA. 22-153-01298

Next page: https://openairdocs.org/aircraft/N570WN/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 = 'N570WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N570WN/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.