N360WA
Service difficulty reports · 171
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 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 PSDR NACA2025040100002Skin · corrodedCORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.135 , STR-9. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003SDR NACA2025040100001Fuel Tank · corrodedSURFACE CORROSION ON LH SIDE CENTER WING TANK LOWER SKIN BETWEEN STRINGERS S9C BETWEEN LBL40.875+5" AND LBL40.875+8. PERFORMED PERMANENT REPAIR PER NAC EO 737-57-0053 CAT B REPAIR.SDR NACA2025022800000Structure · corrodedCORROSION FOUND ON RH HORIZONTAL STAB AT STA 98. REPAIRED PER EO 737-55-0017SDR NACA2025020200002Keelbeam · corrodedWHILE PERFORMING N360WA SERVICE CHECK, CORROSION WAS FOUND ON THE KEEL BEAM LOWER CHORD AT BS 540, LBBL 6.50. FOLLOWING CORROSION REMOVAL, IT WAS DETERMINED THAT THE BLENDOUT EXCEEDED THE 737-300 BOEING SRM 53-60-12 ALLOWABLE LIMITS. AAC ENGINEERING CONTACTEDSDR NACA2024041600001Skin · crackedFOUND CRACK INDICATION BELOW STRINGER 2R @ BS 400 + 1/38. FOUND INTERNAL NICK ON SKIN. REPAIRED NICK @ BS400 + 1 3/8 STR 2R PER NAC EO 737-53-0341-01 AEI EO 233-49SDR NACA2024031200001Unknown · crackedMECHANIC FOUND CRACK DURING SERVICE CHECK AT BS 727E, STR 22L APPROX 2 1/8" LONG. CRACK CONFIRMED BY EDDY CURRENT, COMPLETED REPAIR OF CRACK FOUND ON BS 727E STR 22L IAW SRM 52-31-00 REPAIR 31 & NAC PROJECT WORKSHEET ON 3/20/2024 & WITH REF TO EO 737-53-0339.SDR NACA202401300001Seal · fodAUTOFAIL LIGHT WITH CABIN ALT WARNING ACCOMPANIED BY HISSING NOISE FROM CAPT SIDE WINDOW, COULD NOT PRESSURIZE. PERFORMED OPS TEST OF PRESSURIZATION CONTROLLER IAW AMM 21-31-00 OPS CHECK OK. CHECKED AND CLEANED CAPT'S SLIDING WINDOW SEAL. NO DEFECTS NOTED.SDR NACA20230720002Unknown · unknown#2 ENGINE.- DURING ACCOMPLISHMENT OF AD 200-16-51 WAS FOUND RH 5TH STAGE ENGINE BLEED VALVE CORRODED AND STUCKED P/N 3202222-1 AND S/N 2243. "REMOVED AND REPLACED RH 5TH STAGE ENG BLEED AIR CHECK VALVE IAW B737 AMM 36-11-35 PAG 401-408. PERFORMED LEAK CHECK IASDR NACA202307200001Unknown · unknownRH WING.- INBD T/E MID FLAP UPPER SKIN SHOW CORROSION. REMOVED AND REPLACED MID FLAP ASSY AT INBD T/E FLAP ON RH WING IAW B737 AMM 27-51-04, PAGE 401-415. PERFORMED OPS CHECK AND ADJUSTMENT TEST IAW B737 AMM 27-51-04, PAGE 415-423, VERIFIED SATISFACTORY.SDR NACA2023072003Unknown · unknownAFT CARGO COMPT.- SECTION 46 S-27L SPLICE WITH CORROSION STA 907.0. PERFORMED MAJOR REPAIR CATEGORY "A" ON AFT CARGO CAOMPARTMENT SECTION 45 STA 907.0, S-27L. REMOVED CORRODED SPLICE IAW B737 SRM 51-40-02 PAG 4, FABRICATED SPLICE FROM AL 7075 "0" 0.063 IAW B73SDR NACA2023072001Unknown · unknownLH WING.- OUTBD AFT FLAP LWR PART WITH CORROSION POINT STA WBL 351.0. REMOVED DAMAGED AREA OUTBD AFT FLAP LWR PART STA WBL 351.0 ON LH WING IAW B737 SRM 51-70-10 REV 130. FABRICATED FILLER AND DOUBLER OF CLAD 2024 T3-0.016 IAW SRM 57-53-02, REV 130 APPLIED PRISDR NACA202307201003Unknown · unknownLH WING.- WING SKIN UPPER SURFACE CORRODED AT FORWARD SPAR WS 235.00. EFFECTED OEM FASTENER REMOVED AND NEW FASTENER INSTALLED IAW SRM 57-20-01 ALLOWABLE DAMAGE 4 TABLE II AND IAW BOEING REPAIR MESSAGE: NAC- NAC -23-0022-08B , DATED 13, APRIL 2023 RESTORED AERSDR NACA202307201002Unknown · unknownRH WING.- WING SKIN UPPER SURFACE CORRODED AT FORWARD SPAR WS 495.00. CORROSION DAMAGE REMOVED AT WING STATION 494.00 AT REAR SPAR R/H IAW BOEING REPAIR MESSAGE NAC-NAC 23-0022-08B, DATED 13, APRIL 2023, NOMINAL MATERIAL THICKNESS WAS 0.145 MAXIMUM MATERIAL RESDR NACA2023072010001Unknown · unknownRH WING.- WING SKIN UPPER SURFACE CORRODED AT REAR SPAR WS 495.00. CORROSION DAMAGE REMOVED FROM UPPER SURFACE WING STATION 495.00 AT FRONT SPAR R/H IAW BOEING REPAIR MESSAGE : NAC- NAC 23-0022-08B, DATED 13, APRIL 2023, NOMINAL MATERIAL THICKNESS WAS 0.150 MASDR NACA2023010700001Skin · crackedFOUND CRACK AT LOCATION LAP 142 BS 807 BETWEEN 807 +2 AND 807 +4. REF PROJECT WORKSHEET AND NR TASK CARD 0004, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-01SDR NACA2022092400001Frame · damagedFOUND 3/8 INCH HOLE IN BS 520L FRAME BETWEEN STR 16 AND 17 ON THE RADIUS. REPAIRED 520L FRAME PER EO# 19321, REFERENCE PROJECT WORKSHEET.SDR NACA2022020400001Not Reported · not reportedCRACK INDICATIONS AT BS 360+11 @ STRINGER 19R - 11/16 AND 1 3/4 INCHES. BS 727E +12 AND STR 23R - 2 5/16 INCHES. B727D+15 AND STR 23 R - 3 3/4 INCHES. REPAIR PERFORMED IAW SRM 53-00-01 REPAIR 31.SDR NACA2021F00057Warning Light · illuminatedON GEAR RETRACTION THE HYDRAULIC SYSTEM A, ENGINE LOW PRESSURE LIGHT CAME ONSDR NACA2021032900001Isolation Valve · leakingDISCREPANCY: HYDRAULIC SYSTEM A, LOSS ALL FLUID ON CLIMB OUT THROUGH 14,000FT. RAN QRH, NORMAL LANDING. CORRECTIVE ACTION: REMOVED AND REPLACED SYSTEM A ELEVATOR ISOLATION VALVE IAW AMM 27-31-84, LEAK AND OPT CHECKED GOOD.SDR NACA2021F00056Hydraulic System · leakingHYDRAULIC SYSTEM - A, LOSS ALL FLUID ON CLIMB OUT THROUGH 14,000 FT. REF THE QRH, NORMAL LANDING.SDR NACA2021FA0000090Hydraulic System · leakingHYDRAULIC SYSTEM - A, LOSS ALL FLUID ON CLIMB OUT THROUGH 14,000 FT. REF THE QRH, NORMAL LANDING.SDR NACA2021032200004Skin · crackedDISCREPANCY: 1.25 INCH CRACK AT BS907+7.25 INCHES, STR25R. CORRECTIVE ACTION: INSTALLED REPAIR PER SRM 53-00-01, REPAIR 31 DETAIL XXVIII.SDR NACA2021032200003Skin · crackedDISCREPANCY: 1 7/8 INCH CRACK AT BS927 + 6 3/4 INCHES, STR25R. CORRECTIVE ACTION: INSTALLED REPAIR PER SRM 53-00-01 REPAIR 31 DETAIL XIX.SDR NACA202008170016Skin · crackedDISCREPANCY: ON WALK AROUND FOUND 2.5" CRACK LOCATED BS727D + 2.5 TO BS727D + 5, BELOW STR23R. CORRECTIVE ACTION: REPAIRED IAW SRM 53-00-01 DETAIL VII PAGE 234.SDR NACA2020070600010Beam · corrodedLEFT HORIZONTAL STAB HAS CORROSION ON UPPER TRAILING EDGE BEAM AT STAB STA 258.28 AND 239.9. STA 258.28 CLEAN, TREATED AND PRIMED AREA, WITHIN LIMITS PER SRM 51-10-2. STAB STA 239.9 INSTALLED REPAIR PER ENGINEERING REPAIR ORDER FOR INSTALL OF FASTENER DEVIATSDR NACA2020070600009Spar Cap · corrodedRIGHT HORIZONTAL STAB REAR SPAR UPPER CHORD HAS CORROSION. COMPLIED WITH DRAWING NR 5510D2824.SDR NACA2020070600008Spar Cap · corrodedLT HORIZONTAL STAB REAR SPAR UPPER CHORD HAS CORROSION. COMPLIED WITH DRAWING 5510D2824.SDR NACA2019082100139Intercostal · damagedCRACK AND DAMAGED HOLE ON INTERCOSTAL "L" ANGLE STA 291-270 STR 11-12R. CRACK AND DAMAGED HOLE ON INTERCOSTAL "L" ANGLE STA 291-270 STR 11-12R REPLACED "L" ANGLE WITH MADE REPAIR PART IAW SRM REV 120 SEC 51-30-01 AND REFER TO SRM REV 120, 53-10-15 PAGE 4 AND 5SDR NACA2019082100138Stringer · damagedSTA 312 STR 6R HAS EXTRA HOLES AND HOLE DAMAGE AT EXISTING FASTENERS. INSTALLED NEW STR AT STA 312 STR 6R IAW SRM REV 120 CH 51-40-02 PARA 4 AND PARA 7 AND DOCUMENT #65-45800 REV F.SDR NACA2019082100135Beam · crackedBS180 LBL5.7 WL178 CRACKED VERTICAL BEAM. STA 180 LBL 5-7 WL 178 CRACKED VERTICAL BEAM REPLACED WITH NEW PART IAW DWG 65C38473 REV -.SDR NACA2019082100134Beam · crackedBS180 RBL5.7 WL183 CRACKED VERTICAL BEAM. STA 180 RBL 5.7 WL 183 CRACKED VERTICAL BEAM REPAIRED IAW SERVICE BULLETIN 737-53A1225 REV 1 APRIL 15,2005.SDR NACA2019082100133Shear Tie · corrodedBS807 AND BS767 ABOVE S20L SHEAR TIES CORRODED. STA 807 AND 767 ABOVE STR 20L SHEAR TIES REPLACED WITH MADE REPAIR PART IAW DWG 65-46549 REV H AND INSTALLED IAW SRM REV 120 51-40-02; AND DWG 65-46551 REV D.SDR NACA2019082100132Bulkhead · crackedBS1016 AT S6L AFT PRESSURE BULKHEAD WEB CRACKED. STA 1016 @ STR 6L AFT PRESSURE BULKHEAD REPAIRED IAW SRM 53-80-08 REPAIR 7, FIG 201 REV 120.SDR NACA2019082100131Bulkhead · crackedBS1040 AFT PRESSURE BULKHEAD HAS 3 CRACKED WEBS. STA 1016 AFT PRESSURE BULKHEAD 3 CRACKED WEBS REPAIRED. IAW SR #3-4470-728395. 5 CRACKED STIFFENERS FOUND WHILE ACCOMPLISHING GORE WEB REPAIR REPLACED IAW SR# 4- 4501377456. SEE ATTACHED MTC 114S FOR DETAILS. RSDR NACA2019082100130Frame · crackedCRACK FOUND WHILE CARRYING OUT AD 2017-13-13 @ STA 344 BELT FRAME WEB 1 INCH HOLE BETWEEN STR 23L & 24L. CRACKED FRAME AT STN 344 BETWEEN STR23L AND 24L: REPLACED COMPLETE FRAME AT STA 344 STR 22L TO 28L IAW DWG 65- 45815 REV H AND SRM REV120 51-40-02 AND SR SDR NACA2019082100129Skin · crackedBS304 S7R R1 DOORWAY SKIN CORNER CUTOUT CRACKED. STA 304 STR 7R RI DOORWAY SKIN CORNER CUTOUT CRACK REPAIRED IAW SR# 4-4490828110.SDR NACA2019082100128Doubler · crackedBS303.9 S16L DOOR STOP FITTING CUT OUT REINFORCEMENT DOUBLER CRACKED. STA 303.9 STR 16L DOOR STOP FITTING CUT OUT REINFORCEMENT DOUBLER REPAIRED IAW SB 737-53A1197 PART 3 FIG 3,4 DATED AUG 25, 2006.SDR NACA2019082100127Shear Web · crackedRIGHT HAND BS294 - BS312 RBL53 AT S17R CRACKED SHEAR WEB. CREASE BEAM WEB AT R1 SILL. RT STA 294 - 312 RBL 53 AT STR 17 SHEAR WEB REPLACED WITH MADE REPAIR PART IAW SRM REV 119 CH 53-10-15 AND CH 51-30-01.SDR NACA2019082100126Shear Tie · corrodedRIGHT HAND BS344 S27R AND S26R CORROSION FOUND ON FRAME SHEAR TIE. RT STA AT 344 STR 27R AND 26R CORRRODED SHEAR TIE. REPLACED WITH MADE REPAIR PART IAW SRM REV 119 CH 53-00-07 REPAIR 8.SDR NACA2019082100125Frame · corrodedBS360 - BS351 BETWEEN LBL1- RBL3 CORROSION FOUND ON FRAME WEB. STA 360-351 BTW LBL 1-RBL 3 CORROSION ON FRAME WEB REPAIRED IAW SRM 53-00-07 REV 119. REPAIR 3 FIGURE 201.SDR NACA2019082100124Shear Tie · corrodedLEFT HAND BS344 - BS351 BETWEEN S27L - S26L CORROSION FOUND ON FRAME SHEAR TIE AND SKIN DOUBLER. LT STA 344 STR 27L CORRODED SHEAR TIE REPLACED WITH MADE REPAIR PART IAW DWG 65-45885 REV D VIEW BS AND SRM REV 119 CH 57-40-02.SDR NACA2019082100123Stringer Splice · crackedBS360 S15L STRINGER SPLICE IS CRACKED. STA 360 STR 15L STRINGER SPLICE REPLACED WITH NEW STRINGER SPLICE IAW SRM REV 120 51-40-02 AND DWG 65-17685 REV E.SDR NACA2019082100122Stringer Clip · crackedBS351 S15L CLIP IS CRACKED. STA 351 STR 15L SLIP REPLACED WITH MADE PART IAW DWG #65- 45817 REV BE. PART INSTALLED IAW SRM 51-40-02 REV 120, DWG #65-45817 REV F.SDR NACA2019082100121Beltframe · corrodedBS847 BELTFRAME CORRODED AT S25-27L [RT]. STA 847 CARGO DOOR OPENING FRAME AT STR 17R-27R REPLACED WITH NEW FRAME IAW DRAWING 65-47960 REV K AND SRM REV 120 51-40-02.SDR NACA2019082100120Intercostal · crackedBS294.5-303 S7L INTERCOSTAL CRACKED @ TWO LOCATIONS. STA 294.5-303 STR 7L INTERCOSTAL REPLACED WITH NEW PARTS IAW SR# 4-4491026014. SEE FAA FORM 8100-9 ID 201906040114-0003 FOR APPROVAL.SDR NACA2019082100118Stringer · corrodedBS967 TO BS987, S25L AFT PIT CORRODED STRINGER. FS 967 TO 987 STR 25L AFT PIT STRINGER REPLACED WITH MADE REPAIR PARTS IAW SRM REV 120 53-00-03 FIG 201 REPAIR 1.SDR NACA2019082100117Stringer · corrodedBS817, BS867, BS897 [STRINGER] S20L IN AFT PIT CORRODED. FS 817, 867 & 897 STR 20L IN AFT PIT REPLACED WITH NEW PART AND INSTALLED IAW SRM REV 120 53-00-03.SDR NACA2019082100116Stringer · crackedBS500C S2L HAS SUSPECTED CRACK AND TOOLING MARKS ON STRINGER. STA 500C STR 2L REPAIRED IAW R23553.1-053-014-001 REV IR.SDR NACA2019082100115Keelbeam · corrodedBS520 S28R CORROSION FOUND ON KEEL BEAM ON VERTICAL FLANGE. REPAIRED IAW SRM SECTION 53-60-12 REPAIR 3 DETAIL II REV 119. CORRODED KEEL BEAM SECTION REPLACED WITH MADE REPAIR PARTS IAW SRM SECTION 53-60-12 REPAIR 3 REV 119.
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