# Service difficulty reports: N360WA

A list on [N360WA](https://openairdocs.org/aircraft/N360WA.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 · 170 reports

- [SDR TSAA2026031900003](https://openairdocs.org/sdr/TSAA2026031900003.md): Window · cracked · Mar 19, 2026 · N360WA · Boeing 737301 · Flight Compartment Windows
  > L1 WINDOW CRACKED IMMEDIATELY AFTER TAKEOFF
- [SDR TSAA2026031700003](https://openairdocs.org/sdr/TSAA2026031700003.md): Window · cracked · Mar 17, 2026 · N360WA · Boeing 737301 · Flight Compartment Windows
  > FLT 55. CAPTAIN'S WINDOW L1 CRACKED.
- [SDR TSAA2026022800002](https://openairdocs.org/sdr/TSAA2026022800002.md): Not Reported · cracked · Feb 28, 2026 · N360WA · Boeing 737301 · Fuselage Structure (General)
  > CRACK FOUND 3 INCH FWD OF BS 727E ALONG STR 22R
- [SDR TSAA2026030270001](https://openairdocs.org/sdr/TSAA2026030270001.md): Skin · cracked · Feb 27, 2026 · N360WA · Boeing 737300 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING SERVICE CHECK, CRACK WAS FOUND. CRACK IS APPROXIMATELY 1 5/8 INCHES LONG, 7 ¼ INCHES AFT OF STA 727D (727D +7 ¼), 12 INCHES FWD OF STA 727E (727E -12), 7 ½ BELOW S-20R, 3 ¾ INCHES AFT OF THE WING-TO-BODY FAIRING, 10 ¾ INCHES ABOVE THE EXIST
- [SDR TSAA202510020001](https://openairdocs.org/sdr/TSAA202510020001.md): Skin · cracked · Sep 8, 2025 · N360WA · Boeing 737301 · Fuselage Main, Plate/Skin
  > POST FLIGHT CHECK FOUND CRACK IN FUSELAGE AFT OF THE AFT CARGO DOOR. CRACK MEASURES AT 2 1/8 WIDE AFT OF BS 868 ALONG STR 24
- [SDR NACA2025050700002](https://openairdocs.org/sdr/NACA2025050700002.md): Frame · damaged · May 7, 2025 · N360WA · Boeing 737301 · Fuselage Main, Frame
  > DEFECTED HOLES (4EA) FOUND ON STA 400 FRAME REPAIR.
- [SDR NACA2025041700005](https://openairdocs.org/sdr/NACA2025041700005.md): Stringer Clip · cracked · Apr 17, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > A STRINGER TIE CLIP CRACK WAS FOUND AT STA 616, S-5R & S-5L. STRINGER TIE CLIP REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025041700004](https://openairdocs.org/sdr/NACA2025041700004.md): Stringer Clip · cracked · Apr 17, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > A STRINGER TIE CLIP CRACK WAS FOUND AT STA 747, S-4R. STRINGER TIE CLIP REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025041700003](https://openairdocs.org/sdr/NACA2025041700003.md): Stringer Clip · cracked · Apr 17, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > A STRINGER TIE CLIP CRACK WAS FOUND AT STA 727B, S-3L, 727C, S-6R 727D, S-4R STA 727D, S-5R, STA 727E, S-5L. STRINGER TIE CLIPS REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025041000002](https://openairdocs.org/sdr/NACA2025041000002.md): Stringer Clip · cracked · Apr 10, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE STRINGER CLIP CRACK, STA907, 4R & 8L. STRINGER TIE CLIP REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025041000001](https://openairdocs.org/sdr/NACA2025041000001.md): Failsafe · cracked · Apr 10, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > A CRACK WAS FOUND AT FAIL-SAFE CHORD S-15R OF RIGHT SIDE(AT UPPER FASTENER LOCATION, LENGTH 5MM). PERFORMED REPAIR AT FAIL-STAFE CHORD STA 380, S-15R. 1. TRIM OFF DAMAGED AREA 2. MADE REPAIR PARTS AND INSTALLED I.A.W. EO 737-53-0379, REF FAA 8110-3 DTD 04/28
- [SDR NACA2025040900004](https://openairdocs.org/sdr/NACA2025040900004.md): Stringer Clip · damaged · Apr 9, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > STRINGER TIE CLIP (STA 847-4L SYMBOL "D") REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025040900005](https://openairdocs.org/sdr/NACA2025040900005.md): Stringer Clip · cracked · Apr 9, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE STRINGER CLIP CRACK, STA827, 4L. STRINGER TIE CLIP (STA 827-4L SYMBOL "D") REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025040900003](https://openairdocs.org/sdr/NACA2025040900003.md): Stringer Clip · cracked · Apr 9, 2025 · N360WA · Boeing 737301 · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE STRINGER CLIP CRACK, STA887, 4R. STRINGER TIE CLIP (STA 827-4L SYMBOL "D") REPLACED. PER EO 737-53-0251-01 SB 737-53-1268 APPENDIX A PAGE 288-289 & TABLE 35 PAGE 318-319. B737-300 SRM 51-40-02 PARA 4.
- [SDR NACA2025040900002](https://openairdocs.org/sdr/NACA2025040900002.md): Skin · corroded · Apr 9, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > DURING NRC: CA1624-309 CORRECTION,AFT ANGLE REMOVE FOUND CORROSION AT RH WING UPPER SKIN UPPER SURFACE WS.258 STR-13. REMOVED CORROSION LEVEL 2 AT RH WING UPPER SKIN ANGLE WWS.258 BETWEEN STR-11 -STR-12. FROM PN 65C27356-22, AFTER CORROSION REMOVED, ANGLE TH
- [SDR NACA2025040900001](https://openairdocs.org/sdr/NACA2025040900001.md): Skin · corroded · Apr 9, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > DURING NRC: CA1624-309 CORRECTION,AFT ANGLE REMOVE FOUND CORROSION AT RH WING UPPER SKIN UPPER SURFACE WS.259 STR-13. REMOVED CORROSION LEVEL 2 AT RH WING UPPER SKIN ANGLE WWS.259 BETWEEN STR-11 -STR-12. FROM PN 65C27356-22, AFTER CORROSION REMOVED, ANGLE TH
- [SDR NACA2025040800008](https://openairdocs.org/sdr/NACA2025040800008.md): Skin · debonded · Apr 8, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > RH WING OUTBOARD AFT FLAP LOWER SKIN DISBOND BETWEEN WBL.270~WBL.280. PERFORMED CATEGORY A METAL BOND REPAIR WITH 250 F CURE MATERIAL AT RH WING OUTBOARD AFT FLAP LOWER SKIN BETWEEN WBL 270-WBL 280 IAW B737-300 SRM 57-53-02 REPAIR 2 & SRM 51-70-10 REPAIR 4 (R1
- [SDR NACA2025040800007](https://openairdocs.org/sdr/NACA2025040800007.md): Skin · chafed · Apr 8, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER SURFACE BETWEEN WS.399 AND WS.401, REAR SPAR AREA. CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER SURFACE BETWEEN WS.390 AND WS.392, REAR SPAR AREA. CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER SURFACE BE
- [SDR NACA2025040800006](https://openairdocs.org/sdr/NACA2025040800006.md): Skin · corroded · Apr 8, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER SURFACE BETWEEN WS.372 AND WS.374, BETWEEN S-11 AND S-12 AREA. CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER SURFACE BETWEEN WS.409.5 AND WS.412, S-13 AREA. CORROSION WAS FOUND AT LH WING UPPER SKIN UPPER
- [SDR NACA2025040800005](https://openairdocs.org/sdr/NACA2025040800005.md): Skin · corroded · Apr 8, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LT WING UPPER SKIN UPPER SURFACE BETWEEN WS.364 AND WS.367, LEADING EDGE SKIN AREA. WS.371 AND WS.374, LEADING EDGE SKIN AREA. WS.422 AND WS.424, LEADING EDGE SKIN AREA. WS.428 AND WS.430, LEADING EDGE SKIN AREA. WS 456 AND WS.4
- [SDR NACA2025040800004](https://openairdocs.org/sdr/NACA2025040800004.md): Skin · chafed · Apr 8, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > LEFT WING UPPER SKIN UPPER SURFACE BETWEEN WS.260 AND WS.208.5, 363, AND WS.366, WS.376 AND WS.380, WS 417 AND WS.418.5, WS.427 AND WS.428.5, WS.433 AND WS.434.5, FRONT SPAR AREA. REMOVED CORROSION LEVEL AT LH WING UPPER SKIN SURFACE SRM 51-10-02 PARA 1
- [SDR NACA2025040800003](https://openairdocs.org/sdr/NACA2025040800003.md): Skin · chafed · Apr 8, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.135, STR-7, WS.136, STR-6, WS.137, STR-4, WS.140, STR-4, WS.147, STR-7. CORROSION FOUND AT RH WING UPPER SKIN ANGLE WS.143 BETWEEN STR-9~ STR-10. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REP
- [SDR NACA2025040700006](https://openairdocs.org/sdr/NACA2025040700006.md): Structure · damaged · Apr 7, 2025 · N360WA · Boeing 737301 · Fuselage Structure (General)
  > PERFORMED REPAIR AT STA 294.5 RBL51. TRIMED OUT DAMAGED AREA. MADE REPAIR PARTS AND INSTALLED. PER B737-300 SRM 53-10-51 REPAIR 5 FIG 201.
- [SDR NACA2025040700008](https://openairdocs.org/sdr/NACA2025040700008.md): Angle · corroded · Apr 7, 2025 · N360WA · Boeing 737301 · Wing Main, Frame Structure
  > CORROSION FOUND AT RH WING UPPER SKIN ANGLE WS.259 BETWEEN STR 11-12. REMOVED CORROSION LEVEL 2 AT RH WING UPPER SKIN ANGLE WWS.259 BETWEEN STR-11 -STR-12. FROM PN 65C27356-22, AFTER CORROSION REMOVED, ANGLE THROUGH REPLACED ANGLE PER SRM 51-40-02 PARA 4 & DW
- [SDR NACA2025040700007](https://openairdocs.org/sdr/NACA2025040700007.md): Pressure Web · cracked · Apr 7, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > MAIN WHEEL WELL PRESSURE WEB CRACK STA663.75+3" LBL24.5+8" APPROXIMATE SIZE L0.375. PERFORMED REPAIR AT STA 663.75+3, LBL 245.5+8 IAW SRM 53-60-51 REPAIR 4.
- [SDR NACA202504070006](https://openairdocs.org/sdr/NACA202504070006.md): Floorbeam · cracked · Apr 7, 2025 · N360WA · Boeing 737301 · Fuselage Main, Floor Beam
  > FLOOR BEAM CRACK AROUND FASTENER ON STA294.5 RBL 51, APPROXIMATE SIZE: 0.375" NEAR FWD SERVICE DOOR CUTOUT FWD LOW CORNER.
- [SDR NACA2025040700005](https://openairdocs.org/sdr/NACA2025040700005.md): Door · corroded · Apr 7, 2025 · N360WA · Boeing 737301 · Emergency Exits
  > LH OVERWING EMERGENCY EXIT HATCH CORROSION AROUND LOW PORTION. REPLACED NEW SEAL ANGLE - BOTTOM IAW B737-300 SRM 51-40-02 PARA 4 PAGE 2 AND DWG NO. 50-7978 SH 2.
- [SDR NACA2025040700004](https://openairdocs.org/sdr/NACA2025040700004.md): Door · corroded · Apr 7, 2025 · N360WA · Boeing 737301 · Emergency Exits
  > RH OVERWING EMERGENCY EXIT HATCH CORROSION AROUND LOW PORTION. REPLACED NEW SEAL ANGLE - BOTTOM IAW B737-300 SRM 51-40-02 PARA 4 PAGE 2 AND DWG NO. 50-7978 SH 2.
- [SDR NACA2025040700003](https://openairdocs.org/sdr/NACA2025040700003.md): Skin · corroded · Apr 7, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.565 BETWEEN STR-11~ STR-12. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003.
- [SDR NACA2025040700002](https://openairdocs.org/sdr/NACA2025040700002.md): Skin · corroded · Apr 7, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.583 BETWEEN STR-11~ FRONT SPAR. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003.
- [SDR NACA2025040700001](https://openairdocs.org/sdr/NACA2025040700001.md): Skin · chafed · Apr 7, 2025 · N360WA · Boeing 737301 · Wing, Plate/Skin
  > CORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.252, FRONT SPAR. WS.261, FRONT SPAR. CORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.266, SKIN FWD EDGE. CORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.268, SKIN FWD EDGE. CORROSION F
- [SDR NACA2025040500004](https://openairdocs.org/sdr/NACA2025040500004.md): Skin · gouged · Apr 5, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > GOUGE WAS FOUND AT LH WIN O/B FORE FLAP NOSE LOWER SKIN, WBL 412.11. MADE REPAIR PARTS. INSTALL REPAIR PARTS AT LH WIN O/B FORE FLAP NOSE LOWER SKIN PER: 737-300 SRM 57-53-01 REPAIR 1. (R136)"
- [SDR NACA2025040100005](https://openairdocs.org/sdr/NACA2025040100005.md): Skin · cracked · Apr 5, 2025 · N360WA · Boeing 737301 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE LH SIDE WATER SERVICE PANEL 1501L EXTERNAL SURFACE. REPLACED LH SIDE WATER SERVICE PANEL PER AMM 52-48-00 PAGE 1 REV 101.
- [SDR NACA2025040400001](https://openairdocs.org/sdr/NACA2025040400001.md): Skin · chafed · Apr 4, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > RH WING INBOARD FORE FLAP SKIN WORN AT WBL.73. REMOVED THE DAMAGED DOUBLER AT RH WING INBOARD FORE FLAP SKIN AT WBL.73. PERFORMED CATEGORY A METAL BONDING WITH250 F CURE MATERIAL. IAW B737-300 SRM 57-53-02 REPAIR 1 & SRM 51-70-10 REPAIR 4 (REV136).
- [SDR NACA2025040300004](https://openairdocs.org/sdr/NACA2025040300004.md): Skin · chafed · Apr 3, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > CHAFING WAS FOUND AT LH WING O/B MID FLAP LOWER SKIN, WBL 272.6, L:2.1 INCH, W:0.4 INCH. PERFORMED PERMANENT METAL BOND REPAIR WITH 250 F CURE MATERIAL AT LH WING O/B MID FLAP LOWER SKIN, WBL 272.6 IAW B737-300 SRM 57-53-01 REPAIR 6 & SRM 51-70-10 REPAIR 4
- [SDR NACA2025040300003](https://openairdocs.org/sdr/NACA2025040300003.md): Skin · chafed · Apr 3, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > CHAFING WAS FOUND AT LH WING O/B MID FLAP LOWER SKIN, WBL 258.6, L:2.1 INCH, W:0.5 INCH. PERFORMED PERMANENT METAL BOND REPAIR WITH 250 F CURE MATERIAL AT LH WING O/B MID FLAP LOWER SKIN, WBL 258.6 IAW B737-300 SRM 57-53-01 REPAIR 6 & SRM 51-70-10 REPAIR 4
- [SDR NACA2025040300002](https://openairdocs.org/sdr/NACA2025040300002.md): Beam · corroded · Apr 3, 2025 · N360WA · Boeing 737301 · Horizontal Stabilizer Structure
  > CORROSION AT RH HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE AT STAB STA 223. CORROSION REMOVED & CONDITION CHECK. THE BLEND-OUT DEPTH IS 0.048 ' INCH. WERE OVER LIMIT. MADE REPAIR DOUBLER TO INSTALL WITH REPAIR WASHER & SEALANT PER B737-300 SRM
- [SDR NACA2025040200001](https://openairdocs.org/sdr/NACA2025040200001.md): Skin · bulged · Apr 2, 2025 · N360WA · Boeing 737301 · Leading Edge Devices
  > RH WING INBOARD AFT FLAP LOWER NOSE SKIN SKIN BULGE AT WBL.115. CORROSION REMOVED SKIN THROUGH. REPLACED NOSESKIN ASSY AT RH WING I/B AFT FLAP WBL 115 PER B737-300 SRM 51-40-02 PAGE 2-3 (R136) & DWG 65-46434.
- [SDR NACA2025040100013](https://openairdocs.org/sdr/NACA2025040100013.md): Plug · damaged · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > REMOVE AND REINSTALL PASSENGER CABIN WINDOW PLUG PER AEIR-817-MM 56-21-11 PAGE 401 SERVICEABLE PARTS TAG ATTACHED ON NRC CA1624-082
- [SDR NACA2025040100014](https://openairdocs.org/sdr/NACA2025040100014.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 847+5" S-11L+9", AREA: L0.383", W 1.825". REPLACED PASSENGER CABIN WONDOW PLUG PER AEI R-817-MM 56-21-11 PAGE 401.
- [SDR NACA202540100013](https://openairdocs.org/sdr/NACA202540100013.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 847+11" S-11L+1", AREA: L 2.239", W 0.339".
- [SDR NACA2025040100012](https://openairdocs.org/sdr/NACA2025040100012.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 727E+5" S-11L+10", AREA: L 0.680", W 2.420".
- [SDR NACA2025040100011](https://openairdocs.org/sdr/NACA2025040100011.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 887+10" S-11R+15", AREA: L 1.310", W 0.921". REPLACED PASSENGER CABIN WINDOW PLUG PER AEI R-817-MM 56-21-11 PAGE 401. REPLACED PASSENGER CABIN WINDOW PLUG PER AEI R-817-MM 56-21-11 PAGE 401 AND CABIN WINDOW SCRE
- [SDR NACA2025040100010](https://openairdocs.org/sdr/NACA2025040100010.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 559+4" S-11R+7", AREA: L 0.460", W 1.023". REPLACED PASSENGER CABIN WINDOW PLUG PER AEI R-817-MM 56-21-11 PAGE 401.
- [SDR NACA2025040100009](https://openairdocs.org/sdr/NACA2025040100009.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 559+4" S-11R+7", AREA: L 0.460", W 1.023". REPLACED PASSENGER CABIN WINDOW PLUG PER AEI R-817-MM 56-21-11 PAGE 401.
- [SDR NACA2025040100008](https://openairdocs.org/sdr/NACA2025040100008.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 559+10" S-11R+15", AREA: L 3.50", W 0.432".
- [SDR NACA2025040100007](https://openairdocs.org/sdr/NACA2025040100007.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 559+16" S-11R+11", AREA: L 1.081", W 9.0". CORROSION LEVEL 2 AT PASSENGER CABIN WINDOW PLUG STA559+16", S-11R+11", AREA: L1.081", W9.0" CORROSION REMOVED AND FOUND DAMAGE AREA OVER LIMIT PER CMM 56-21-51 REPAIR 2
- [SDR NACA2025040100006](https://openairdocs.org/sdr/NACA2025040100006.md): Plug · corroded · Apr 1, 2025 · N360WA · Boeing 737301 · Fuselage Main, Structure
  > PASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 360+8" S-11R+15", AREA: L1.130", W0.516". REPLACED PASSENGER CABIN WINDOW PLUG PER AEI R-817 MM 56-21-11 PAGE 401.
- [SDR NACA2025040100004](https://openairdocs.org/sdr/NACA2025040100004.md): Skin · bulged · Apr 1, 2025 · N360WA · Boeing 737301 · Leading Edge Devices
  > BULGE WAS FOUND AT LH WING I/B AFT FLAP NOSE LOWER SKIN, BETWEEN WBL 136 AND WBL 140. SHIM REPLACED, REMOVED AND INSTALLED LEADING EDGE SKIN AT LH WING I/B AFT FLAP, BETWEEN WBL 136 AND WBL 140. PER AIR ASIA NRC: CA1624-102 FOR SHIM FABRICATION.
- [SDR NACA2025040100003](https://openairdocs.org/sdr/NACA2025040100003.md): Skin · bulged · Apr 1, 2025 · N360WA · Boeing 737301 · Trailing Edge Flaps
  > BULGE WAS FOUND AT LH WING I/B AFT FLAP NOSE LOWER SKIN, BETWEEN WBL 149 AND WBL 151. SHIM REPLACED, REMOVED AND INSTALLED LEADING EDGE SKIN AT LH WING I/B AFT FLAP, BETWEEN WBL 149 AND WBL 151. PER AIR ASIA W.P.S. CODE LM 65-46434-506, SRM 51-40-02 PARA 4 P

Next page: https://openairdocs.org/aircraft/N360WA/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 = 'N360WA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N360WA/reports

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