N537AS
Service difficulty reports · 285
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 = 'N537AS' 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 = 'N537AS' 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 ASAA2026050866053Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 143A5810-533 IS DELAMINATED. GROUNDED - YES. FABRICATED NEW MAIN CABIN FLOOR PANEL 143A5810-533 IAW ASA B737-800 SRM 53-00-50-2R-0 AND AIPC 53-21-51-58B.SDR ASAA2026050866052Floor Panel · damagedMAIN CABIN FLOOR PANEL 147A5810-123 HAS MISSING INSERTS. GROUNDED - YES. ACCOMPLISHED PERMAMENT REPAIR OF TWO (2) EA MISSING DAMAGED INSERTS IAW ASA B737-800 SRM 53-00-50-2R-0 AND AIPC 53-21-51-56.SDR ASAA2026050666273Web · corrodedAFT CARGO DOOR THRESHOLD HAS CORROSION ON UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION, EVALUATED REMAINIG THICKNESS, ORIGINAL THICKNESS .050, REMOVED .007, REMAING THICKNESS .043 FOUND TO BE OUT OF LIMITS, REMOVED AFT CARGO WEB, LOCATED AND DRILLED NEW WSDR ASAA2025082260347Lens · detachedFORWARD EXIT LIGHT PLACARD FELL OFF. GROUNDED - YES. REMOVED AND REPLACED FWD EXIT LIGHT ASSEMBLY BY L1 DOOR. AS REQ'D, OPS CHECK NORMAL. REF AMM 33-51-01.SDR ASAA2025081860220Sign · detachedEXIT LABELED SIGN FELL OFF BELOW OUTBOARD FORWARD FLIGHT ATTENDANT SEAT. GROUNDED - YES. RE-INSTALLED EXIT SIGN OK FOR SERVICED PER AMM 33-51-01SDR ASAA2025081860197Cover · missingEXIT LIGHT COVER BY R2 DOOR MISSING. GROUNDED - YES. INSTALLED R2 DOOR EXIT LIGHT COVER. REF AMM 33-51-01. OPS CHECK OF EMER LIGHT GOOD.SDR ASAA2025052358222Lens · missingEXIT SIGN PLACARD ADJACENT TO R2 DOOR IS MISSING. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR EXIT SIGN LIGHT ASSEMBLY REF AMM 33-51-01-960-802. OPS CHECK GOOD. SEAMC TOMMY NOTIFIED.SDR ASAA2025051557994Skin · corrodedBUBBLING PAINT AT STR 23L STA 727G+17. GROUNDED - YES. REPAIRED SKIN AT LAP SPLICE STR 23L STA 727G-727J IAW ALASKA EA # 800-53EA-28682 REV 00 CAT B INSPECTION REQUIREMENTS MUST BE ISSUED PRIOR TO THRESHOLD OF 50,000 TOTAL FLIGHT CYCLESW= 2" O= .080 R= .071 L=SDR ASAA2025050357996Skin · corrodedBUBBLING PAINT AT STR 23L STA 727I+2. GROUNDED - YES. REPAIRED SKIN AT LAP SPLICE STR 23L STA 727G-727J IAW ALASKA EA# 800-53EA-28682 REV 00. CAT B REPAIR INSPECTION REQUIREMENTS MUST BE ISSUED PRIOR TO THRESHOLD OF 50,000 TOTAL FLIGHT CYCLESW= 2" O= .080" R= SDR ASAA2023111346162Lens · brokenEXIT SIGN IN ROW 16 (ABC) HAS BROKEN OFF. GROUNDED - YES. FOUND EXIT INDICATOR BODY TABS BROKENREPLACED EXIT INDICATOR ASSY ON ROW 16ABC REF AMM 33-51-02.OPS CHECK GOOD.SDR ASAA2023103145955Unknown · unknownFUEL CROSS FEED STUCK OPEN FOR SEVERAL MINUTES IN CRUISE. CIRCUIT BREAKER NOT TRIPPED. RECYCELED SEVERAL TIMES AND EVENTUALLY CLOSED. GROUNDED - YES. PERFORMED CROSSFEED VALVE OPERATIONAL TEST REF AMM 28-22-21. OPS NORMAL WITH NO DEFECTS NOTED. NO PREVIOUS HISSDR ASAA2023101445638Control Module · faultyALL LAV TOILETS DO NOT FLUSH. GROUNDED - YES. DIVERSION -- FOUND VACUUM WASTE CONT C/B ON P91 PANEL POPPED, TROUBLESHOOT PER WDM TASK 38-32-13-3. REMOVED & REPLACED LOGIC CONTROL SENSOR MODULE PER AMM 38-33-03, OPS CHECK GOOD.SDR ASAA2023101345655Control Panel · faultyFO RADAR DISPLAY SHOWS GROUND CLUTTER IN ALL MPDES. "GC" BUTTON DOES NOT CHANGE DISPLAY. GROUNDED - YES. (RESOLVED ON W/O: 1971907 TASKCARD: N/R-00002 ) REMOVED AND REPLACED THE WRCP. OPS CHECK GOOD. THIS REMOVES MEL 34-15J. PLACARD REMOVED. SEAMC NOTIFIED.SDR ASAA2023100945529Unknown · unknownFIRST OFFICERS RADAR DISPLAY ONLY MANUAL INFORMATION WITH RADAR IN AUTO AND MANUAL MODE. GROUNDED - YES. RESET BREAKERS, OPS CKED NORMAL AND NO 30 DAY HISTORY NOTED A/C OK FOR SVC REF AMM 34-43-00.SDR ASAA2023100445464Unknown · unknownENGINE #2 ECONOMIC FAULTMSG #77-20862 THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023080844503Unknown · unknownFIRST OFFICERS WEATHER RADAR RETURNS SIGNIFICANTLY DIFFERENT THAN CAPTAINS WHEN SET TO AUTO, WX/T. IN MANUAL RETURNS ON CAPTAINS AND FOS SCREENS SIMILAR. GROUNDED - YES. COULD NOT DUPLICATE MALFUNCTION.NO FAULTS IN CDS.VERIFIED BOTH RADAR & TERR BUSSES SWITCH SDR ASAA2023072444214Unknown · unknownPERFORMANCE DATA WILL NOT FULLY LOAD. GROUNDED - YES. ACCOMPLISHED FIM 22-11 TASK 831. NO FAULTS FOUND ON ADIRU, FMC OR FQIS. RELOADED SOFTWARE ON LH FMC. OPS, ND, OPC, ADDB, LDDB AND NAV DATA. REF AMM 34-61-00. J. ROBERTS 38885.FOUND LDDB, OPC SOFTWARE DEFAULSDR ASAA2023072144161Unknown · unknownDURING AUTOLAND/HGS APPROACH WE RECEIVED AN NO AIII & APRCH WARN ANNUN CAUTION IN HUD AT 50 FT. IT SEEMED TO BE ENTERING FLARE MODE FOR A/C NORMALLY THOUGH A/P WAS DISCONNECTED AND LANDED A/C MANUALLY. PROTECTED AREA WAS CLEAR. ONE A/C LANDED BEFORE US BUT WASSDR ASAA2023071143993Unknown · unknownENG #2 THE START SWITCH SIGNAL AND ARINC BUS DATA DISAGREE. MSG NBR:73-30312. SHORT TERM FAULT. GROUNDED - YES. (RESOLVED ON W/O: 1959933 TASKCARD: N/R-00003 ) PERFORMED FIM 73-24 TASK 813, ALL TESTS PASS. NO FAULT MESSEGES NOTED AT THIS TIME FOR #2 ENGINE PRISDR ASAA2023070943931Unknown · unknownLEFT #2 WINDOW "OVERHEAT" LIGHT ILLUMINATED. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023061143521Unknown · unknownON DESCENT THRU 12,000' CAPT LEFT SIDE WINDOW OVHT LIGHT ILL PERF QRH AND LIGHT CAME BACK ON. GROUNDED - YES. PERF BT CK B737-800 FIM 30-41 TASK 801 NO ACTIVE FAULTS BT TEST GOOD INTERMITTENT FAULT.SDR ASAA2023060343439Unknown · unknownLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED ON APPROACH INTO KDCA. GROUNDED - YES. RAN QRH 3.6. OVERHEAT LIGHT EXTINGUISHED AND STAYED EXTINGUISHED.SDR ASAA2023052543399Power Supply · failedEMERGENCY LIGHT SYSTEM BATTERY PACK (M1673) FAILED CAPACITY CHECK. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT POWER SUPPLY (M1673) IAW B737NG AMM 33-51-06-960-806.OPS CHECK GOOD.SDR ASAA2023052543398Power Supply · failedEMERGENCY LIGHT SYSTEM BATTERY PACK (M2816) FAILED CAPACITY CHECK. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT POWER SUPPLY (M2816) IAW B737-800 AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2023051243277Insert · damagedMID CABIN FLOOR BOARD P/N 144A5810-124 INSERT MISSING DAMAGE. GROUNDED - YES. REPAIRED MID CABIN FLOOR BOARD P/N 144A5810-124 INSERT MISSING DAMAGE IAW ASA B737-800 RM 53-00-50-0I-1 & 53-00-50-2R-2 REP 2 *SDR ASAA2023050543276Intercostal · corrodedMAIN CABIN FLOOR INTERCOSTAL STA 947-967 LBL 50 HAS CORROSION AROUND ANCHOR PLATE. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .200" REMAINING THICKNESS .165" REMOVED .035" OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. RECEIVED, LOCATED AND DRILLED TOSDR ASAA2023050243275Pan · corrodedL-2 DOOR HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED CORRODED HANDLE PAN & INSTALLED NEW HANDLE PAN 147A6137U3 IAW BAC DWG 147A0116 & B737-800 SRM 51-40-02.SDR ASAA2023050243179Floor Panel · damagedR/H OUTBD FLOOR PANEL AT ABOUT STA 860, PANEL P/N 146A5810-464 HAS DAMAGED SCREW HOLE. GROUNDED - YES. REPAIRED DAMAGE SCREW HOLE ON PANEL 146A5810-464 IAW B737-800 SRM 53-00-50-2R-4, 53-00-50-2R-0.SDR ASAA2023043043274Intercostal · corrodedSIDE WEB AT R2 DOOR FORWARD CORRODED STATION 945. GROUNDED - YES. REMOVED CORROSION FROM INTERCOSTAL WEB. ORIGINAL THICKNESS 0.150, REMAIINING THICKNESS 0.110, REMOVED 0.040. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A. REMOVED DAMAGED INTERCOSTAL IAW B737-800 SDR ASAA2023043043273Floorbeam · corrodedGALLEY MOUNT FITTING @ STATION 947 LEFT SIDE CORRODED. GROUNDED - YES. REMOVED CORROSION ON FLOOR BEAM UNDER GALLEY MOUNT. ORIGINAL THICKNESS 0.180 IAW B737-800 SRM 53-70-51-0I-1. REMAINING THICKNESS 0.100, REMOVED 0.080. OUT OF LIMITS IAW B737-800 SRM 53-70-5SDR ASAA2023042943280Angle · corrodedFWD PIT, RH AFT BULKHEAD ANGLE HAS CORROSION ON BOTTOM SIDE. GROUNDED - YES. EVALUATED FWD PIT R/H AFT BULKHEAD ANGLE; MINIMUM THICKNESS: .056, REMOVED: .026, REMAINING .045 & IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-01. REMOVED, LOCATED & DRILLED, SDR ASAA2023042943272Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 727A-727F+14. GROUNDED - YES. REPAIRED THE AFT PIT, L/H TRANSITION PANEL FROM STA 727-727F+14 USING MAT BAC1496-377 PER B737-800 SRM 53-00-53-2R-5. EVALUATED AFT PIT TRANSITION PANEL STA 727A-727F+14. ORIG THICKNSDR ASAA2023042943271Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 758-808. GROUNDED - YES. EVALUATED AFT CARGO L/H TRANSITION PANEL FROM FR STA 758 TO FR STA 808. ORIGINAL MATERIAL THKS .040 PER BAC PROFILE DWG 1496-377 REMOVED .040, REMAINING .000 FOUND TO BE OUT OF LIMITS PERSDR ASAA2023042943270Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 727H+14-757. GROUNDED - YES. EVALUATED AFT CARGO L/H TRANSITION PANEL FROM FR STA 727H +14 TO FR STA 757 ORIGINAL MATERIAL THKS .040 PER BAC PROFILE DWG 1496-377 REMOVED .005 REMAINING .035 FOUND TO BE OUT OF LIMSDR ASAA2023042943269Transition Panel · corrodedAFT PIT, RH TRANSITION PANEL IS CORRODED AT STA 727G-767. GROUNDED - YES. REPAIRED THE AFT PIT R/H TRANSITION PANEL FROM STA 727F+10-767 USING MAT BAC 1496-377 PER B737-800 SRM 53-00-53-2R-5. EVALUATED AFT PIT TRANSITION PANEL STA 727G-767. ORIG THICKNESS .040SDR ASAA2023042943266Transition Panel · corrodedAFT PIT, RH TRANSITION PANEL IS CORRODED AT STA 727A-727C+10. GROUNDED - YES. REPAIRED THE AFT PIT, R/H TRANSITION PANEL FROM STA 727-727D+10 USING MAT BAC 1496-377 PER B737-800 SRM 53-00-53-2R-5.EVALUATED THE CORROSION ON THE R/H TRANSITION PANELSTA 727A-727CSDR ASAA2023042843279Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL AT STA 500E+11-500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+11-500I PER B737-800 SRM 53-00-53-1A-2.2.D. 100% MATERIAL LOSS AND IS FOUND TO BE OUT OF LIMITS PER B737-800 SSDR ASAA2023042843278Transition Panel · corrodedFWD PIT L/H TRANSITION PANEL AT STA 500H-500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500H-500I PER B737-800 SRM 53-00-533-1A-2.2.D. ORIG THICKNESS IS .040" PER B737-800 SRM 53-30-53-0I-2 TABLE 2. REMOVEDSDR ASAA2023042843265Shield · corrodedFWD PIT, AFT SHIELD IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT AFT SHIELD PER B737-800 SRM 53-30-15-1A-1 2.A. 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-30-15-1A-1 REMOVED SHIELD PER B737-800 SRM 51-40-02. RECEIVED NEW SSDR ASAA2023040942786Panel · faultyTHE HF/ UPPER HALF OF THE #1 HF/ SAT XFER SWITCH LIGHT IS DARK. IT DOES HOWEVER ILLUMINATE DURING LIGHTS TEST. HF RADIO #1 APPERA TO BE WORKING NORMALLY. GROUNDED - YES. REMOVED AND REPLACED HF/ SAT PANEL REF B737-800 AMM 23-15-00. OPS CHECK GOOD.SDR ASAA2023040242920Battery Pack · inoperativeTHE AISLE EMERGENCY LIGHT AT FWD CABIN IS INOP. GROUNDED - YES. REMOVE AND REPLACE BATTERY PACK FOR EMERGENCY CEILING LIGHT AT LH-FWDMAIN CABIN IAW B737 AMM 33-51-06-960-805 OP/CHECK GOOD.SDR ASAA2023040242682Battery · inoperativeBOTH EMERGENCY LIGHTS ON L/H SIDE ARE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY OVERWING LIGHTS AT L/H MAIN CABIN IAW B737-800 AMM 33-51-06-960-805.SDR ASAA2023031942434Lens · missingEXIT SIGN MISSING AFT RT GALLEY. GROUNDED - YES. REPLACED EXIT SIGN COVER IN AFT RH GALLEY NEXT TO R2 DOOR REF. B737-800 AMM 33-51-01.SDR ASAA2023031742397Unknown · unknownCONT CABIN ZONE TEMP LITE ON RECALL- RESET WITH MASTER CAUTION. GROUNDED - YES. T/S IAW B737-800 FIM 21-62 TASK 801 - PASS. PACK CONTROLLER HISTORY SHOWED FLT DECK TRIM AIR FAULT ON PACK #2 CONTROLLER. OPS / IND NML - TEST PASS.SDR ASAA2023031442370Unknown · unknownEXIT SIGN COVER HAS COME OFF IN AFT GALLEY BY A/C RT TRASH BIN. GROUNDED - YES. RE-SECURED EXIT SIGN LIGHT LENS PER B737-800 AMM 33-51-01. NO DEFECTS NOTED.SDR ASAA2023031242306Light · detachedR-2 DOOR EXIT SIGN FELL OFF. GROUNDED - YES. REPLACED EXIT SIGN AT R-2 DOOR WITH SERVICEABLE UNIT. OK FOR SERVICE.SDR ASAA2023030142142None · none#1 ENGINE FRONT SPINNER HAS EXCESSIVE PAINT MISSING REF ASA T/C 78472010. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FRONT SPINNER CONE REF ASA T/C 78472010.SDR ASAA2023030142141Blade · none#1 FAN BLADE FAILED INSPECTION DUE TO SHIM WEAR REF ASA T/C 78472010. GROUNDED - YES. REMOVED AND REPLACED BOTH #1 & #13 FAN BLADES REF ASA T/C 78472010.SDR ASAA2023022642115Actuator · faultedON RECALL LEFT PACK LIGHT ILLUMINATES. CLEARS WHEN RESET. GROUNDED - YES. BITE SHOWS LEFT RAM ACT FAULT. REMOVED AND REPLACED THE L/H RAM AIR INLET ACTUATOR. REF B737-800 AMM 21-51-21. OPS CHECK NORMAL.SDR ASAA2023021441977Controller · faultyL PACK LIGHT ILLUMINATES ON RECALL, EXTINGUISHES W/ MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST REF B737-800 AMM 21-61-00-700-806-802 FOUND RAM AIR ACT FAULT ON #1 CONTROLLERS, CLEARS AFTER RESET. PERFORMED BITE PER B737
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