N360WA
Service difficulty reports · 170
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR TSAA2026031900003Window · crackedL1 WINDOW CRACKED IMMEDIATELY AFTER TAKEOFFSDR TSAA2026031700003Window · crackedFLT 55. CAPTAIN'S WINDOW L1 CRACKED.SDR TSAA2026022800002Not Reported · crackedCRACK FOUND 3 INCH FWD OF BS 727E ALONG STR 22RSDR TSAA2026030270001Skin · crackedWHILE 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 EXISTSDR TSAA202510020001Skin · crackedPOST 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 24SDR NACA2025050700002Frame · damagedDEFECTED HOLES (4EA) FOUND ON STA 400 FRAME REPAIR.SDR NACA2025041700005Stringer Clip · crackedA 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 NACA2025041700004Stringer Clip · crackedA 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 NACA2025041700003Stringer Clip · crackedA 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 NACA2025041000002Stringer Clip · crackedUPPER 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 NACA2025041000001Failsafe · crackedA 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 04/28SDR NACA2025040900004Stringer Clip · damagedSTRINGER 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 NACA2025040900005Stringer Clip · crackedUPPER 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 NACA2025040900003Stringer Clip · crackedUPPER 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 NACA2025040900002Skin · corrodedDURING 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 THSDR NACA2025040900001Skin · corrodedDURING 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 THSDR NACA2025040800008Skin · debondedRH 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 (R1SDR NACA2025040800007Skin · chafedCORROSION 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 BESDR NACA2025040800006Skin · corrodedCORROSION 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 UPPERSDR NACA2025040800005Skin · corrodedCORROSION 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.4SDR NACA2025040800004Skin · chafedLEFT 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 1SDR NACA2025040800003Skin · chafedCORROSION 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 REPSDR NACA2025040700006Structure · damagedPERFORMED 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 NACA2025040700008Angle · corrodedCORROSION 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 & DWSDR NACA2025040700007Pressure Web · crackedMAIN 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 NACA202504070006Floorbeam · crackedFLOOR BEAM CRACK AROUND FASTENER ON STA294.5 RBL 51, APPROXIMATE SIZE: 0.375" NEAR FWD SERVICE DOOR CUTOUT FWD LOW CORNER.SDR NACA2025040700005Door · corrodedLH 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 NACA2025040700004Door · corrodedRH 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 NACA2025040700003Skin · corrodedCORROSION 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 NACA2025040700002Skin · corrodedCORROSION 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 NACA2025040700001Skin · chafedCORROSION 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 FSDR NACA2025040500004Skin · gougedGOUGE 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 NACA2025040100005Skin · crackedSURFACE 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 NACA2025040400001Skin · chafedRH 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 NACA2025040300004Skin · chafedCHAFING 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 4SDR NACA2025040300003Skin · chafedCHAFING 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 4SDR NACA2025040300002Beam · corrodedCORROSION 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 NACA2025040200001Skin · bulgedRH 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 NACA2025040100013Plug · damagedREMOVE AND REINSTALL PASSENGER CABIN WINDOW PLUG PER AEIR-817-MM 56-21-11 PAGE 401 SERVICEABLE PARTS TAG ATTACHED ON NRC CA1624-082SDR NACA2025040100014Plug · corrodedPASSENGER 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 NACA202540100013Plug · corrodedPASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 847+11" S-11L+1", AREA: L 2.239", W 0.339".SDR NACA2025040100012Plug · corrodedPASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 727E+5" S-11L+10", AREA: L 0.680", W 2.420".SDR NACA2025040100011Plug · corrodedPASSENGER 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 SCRESDR NACA2025040100010Plug · corrodedPASSENGER 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 NACA2025040100009Plug · corrodedPASSENGER 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 NACA2025040100008Plug · corrodedPASSENGER CABIN WINDOW PLUG GOT CORROSION, STA 559+10" S-11R+15", AREA: L 3.50", W 0.432".SDR NACA2025040100007Plug · corrodedPASSENGER 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 2SDR NACA2025040100006Plug · corrodedPASSENGER 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 NACA2025040100004Skin · bulgedBULGE 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 NACA2025040100003Skin · bulgedBULGE 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
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