N585AS
Service difficulty reports · 564
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 = 'N585AS' 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 = 'N585AS' 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 ASAA2019072030183Battery Pack · dischargedEMERGENCY LIGHTS INOP THROUGHOUT CABIN. GROUNDED - YES. REMOVED AND REPLACED LT FWD EMERGENCY POWER SUPPLY ASSY BATTERY PACK M1675 IAW AMM 33-51-06 OP CHECK GOOD ALL EMERGENCY LIGHTS OPERATIONAL.SDR ASAA2019071130130Baffle · crackedFORWARD CARGO COMPARTMENT AT STR 25R BETWEEN STA 500F AND 500G BAFFLE CRACKED. GROUNDED - YES. REMOVED & REPLACED CRACKED BAFFLE IN FWD CARGO COMPARTMENT BETWEEN BS 500F & 500G PER BAC DWG 143A7505 & EA 80-53EA-21874 REV 00.SDR ASAA2019070530065Stringer Clip · crackedFORWARD CARGO COMPARTMENT RIGHT SIDE STRINGER CLIP ON AFT SIDE OF STRINGER S-25R AT FRAME 500D IS CRACKED. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD CARGO RIGHT SIDE STR 25R AFT FACE OF THE FRAME 500-D IAW SRM 51-40-02. LOCATED, DRILLED, AND INSTALLED NEW CLSDR ASAA2019070530019Stringer Clip · crackedFORWARD CARGO COMPARTMENT RIGHT SIDE STRINGER CLIP ON AFT SIDE OF STRINGER S-25R AT FRAME 500D IS CRACKED. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD CARGO RIGHT SIDE STR 25R AFT FACE OF THE FRAME 500-D IAW B737-800 SRM 51-40-02. LOCATED, DRILLED, AND INSTALLSDR ASAA2019070330103Channel · corrodedFWD PIT RT ZEE CHANNEL IS CORRODED @ BS500I GROUNDED - YES. REMOVED CORROSION ON ZEE CHANNEL AT BS 500 I ORIG. MATL 0.040, MATL REMAINING 0.030, REMOVED 0.010 AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-2A-2 FIG. 103, REMOVED AND REPLACED ZEE CHANNEL FROM SDR ASAA2019070330067Channel · corrodedFWD PIT LT ZEE CHANNEL IS CORRODED @ BS500I. GROUNDED - YES. REMOVED AND INSTALLED NEW ZEE CHANNEL AND SPLICE PLATE STA BS5001 IAW SRM 53-00-53. REMOVED CORR. FROM ZEE CHANNEL ORIG. THICKNESS .040 IAW SRM 53-530-53 MAT. LOSSED .010 REMAINING THICKNESS.030 FOUNSDR ASAA2019070230066Intercostal · crackedFWD WET AREA FLOOR SUPPORT INTERCOSTAL AT STA 328-344 LBL 50 ISCRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT STA 328-344 LBL SOPW BAC DWG 141A5400REV. - AND SRM 51-40-02.SDR ASAA2019063030017Attach Angle · crackedFWD PIT LEFT SIDE ATTACH CLIP ANGLE CRACK AT BS 500H STR25L AFT SIDE OF FRAME. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT LEFT SIDE BS 500H STR 25L IAW SRM 51-40-02. LOCATED AND DRILLED NEW DIP PART #143A7502V155 AND INSTALLED AS PER DWG 143A7505 REV A.SDR ASAA2019063030012Attach Angle · crackedFWD PIT LEFT SIDE ATTACH CLIP ANGLE CRACK AT BS 500H STR25L FWD SIDE OF FRAME. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT LEFT SIDE BS 500H STR 25L IAW SRM 51-40-02. LOCATED AND DRILLED NEW DIP PART # 143A7502V15A AND INSTALLED AS PER DWG 143A7505 REV A.SDR ASAA2019063030011Attach Angle · crackedFWD PIT LEFT SIDE ATTACH CLIP ANGLE CRACK AT BS 500F STR25L FWD SIDE OF FRAME. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT LEFT SIDE BS 500F STR25L IAW SRM 51-40-02. LOCATED AND DRILLED NEW CLIP PART #143A7502V15A AND INSTALLED AS PER DWG 143A7505 REV A.SDR ASAA2019063030010Attach Angle · crackedFWD PIT RIGHT SIDE ATTACH CLIP ANGLE CRACK AT BS 500A STR25R AS MARK. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT RIGHT SIDE BS 500A STR25R IAW SRM 51-40-02. LOCATED AND DRILLED NEW CLIP PART #143A75020154 AND INSTALLED AS PER DWG #143A7505 REV A.SDR ASAA2019063030009Attach Angle · crackedFWD PIT RIGHT SIDE ATTACH CLIP ANGLE CRACK AT BS 500H STR25R FWD OF FRAME AS MARK. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT RIGHT SIDE AT BS 500H STR 25R. FWD OF FRAME IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW CLIP PART #143A7502V158 AS PER DSDR ASAA2019063030008Attach Angle · crackedFWD PIT RIGHT SIDE ATTACH CLIP ANGLE CRACK AT BS 500H STR25R AFT SIDE OF FRAME AS MARK. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT RIGHT SIDE AT BS500H STR25R AFT SIDE OF FRAME IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW CLIP PART #143A7502V154 ASDR ASAA2019063029997Angle · crackedFWD PIT RIGHT SIDE ATTACH CLIP ANGLE CRACK AT BS 500D STR 25R AS MARK. GROUNDED - YES. REMOVED CRACKED CLIP ANGLE AT FWD PIT RIGHT SIDE AT BS500D STR25R IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW CLIP PART# 143A7502U158 AS PER DWG 143A7505 REV A.SDR ASAA2019063029994Angle · crackedFWD PIT LEFT SIDE CLIP ANGLE HAS SIGN OF CRACK AT FWD SIDE OF FRAME BS500G STR25L. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT LEFT SIDE BS 500G STR 25L IAW SRM 51-40-02. LOCATED AND DRILLED NEW CLIP PART #143A7502V159 AND INSTALLED AS PER DWG 143A7505 REVSDR ASAA2019063029993Angle · crackedFWD PIT RIGHT SIDE CLIP ANGLE HAS SIGN OF CRACK AT BS500G STR25R AS MARK. GROUNDED - YES. REMOVED DAMAGED CLIP AT FWD PIT RIGHT SIDE AT BS 500G STR 25R IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW CLIP PART #143A7502V158 AS PER DWG #143A7505 REV A.SDR ASAA2019062929920Angle · crackedMAIN CABIN SECTION 43 INTERCOSTAL UPPER ANGLE AT STA. 380 TO STA 400 RBL 10 IS CRACKED GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN 1 EA 43 INTERCOSTAL UPPER ANGLE AT FS 380 TO FS 400 RBL 10 IAW DWG 143A5400 REV AND SRM 51-40-02.SDR ASAA2019062930069Structure · corrodedMAIN CABIN INNER CHORD AT STA. 717 RBL 60 HAS CORROSION. GROUNDED - YES. CORRODED INNER CHORD AT FS 717 RBL 60 EXEEDED SERVICIABLE LIMITS IAW SRM 53-40-13, REMOVED DAMAGED INNER CHORD IAW SRM 51-40-02 RECIEVED NEW PART P/N: 144A5910-4, LOCATED, DRILLED AND INSSDR ASAA2019062929933Angle · crackedMAIN CABIN SECTION 43 INTERCOSTAL UPPER ANGLE AT STA. 380 TO STA. 400 BL 0 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN SEC 43 INTERCOSTAL UPPER ANGLE AT FR 380 TOFS 400 AT BL 0 IAW DWG 143A5400 REV - AND SRM 51-40-02.SDR ASAA2019062929927Angle · crackedMAIN CABIN SECTION 43 INTERCOSTAL UPPER ANGLE AT STA. 380 TO STA. 400 LBL 10 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN SEC 43 INERCOSTAL UPPER ANGLE AT FS 380 TO FS 400 LBL 10 IAW BAC DWG 143A5400 REV A AND SRM 51-40-02.SDR ASAA2019062929926Panel · crackedMAIN CABIN SECTION 43 PANEL BREAK AT STA. 540 BL 0 TO RBL 24 IS GOUGED. GROUNDED - YES. REMOVED AND REPLACED GOUGED PANEL BREAK AT MAIN CABIN STA. 540, BL 0 TO RBL 24 IAW SRM 51-40-02 AND BAC DWG 143A0060 REV "-".SDR ASAA2019062929919Panel · crackedMAIN CABIN SECTION 43 PANEL BREAK AT STA. 540 BL 0 TO LBL 24 IS CRACKED GROUNDED - YES. REMOVED AND REPLACED PNL BREAK AT FS 540 BL 0 TO LBL 24 IAW BAC DWG 143A0060 REV.SDR ASAA2019062329827Converter · failedAPU GEN FAILED DURING PUSHBACK. GROUNDED - YES. REMOVED AND REPLACED APU STARTER GENERATOR IAW AMM 49-41-21. COMPLIED WITH FIM 24-21 TASK 820. FOUND BAD START CONVERTER UNIT. REMOVED AND REPLACED START CONVERTER UNIT AND OPS CHECK GOOD IAW AMM 49-41-61 APU BISDR ASAA2019061089639Fire Loop · malfunctionedENG #2 LOOP A TEST INOP. GROUNDED - YES. PERFORMED M279 BITE REF 26-10 TASK 801. NO FAULTS LOGGED FOUND. ACCOMPLISHED ENGINE - WIRING HARNESS/FIRE DETECTOR - FAULT ISOLATION 26-10 TASK 805. ALL READINGS FOUND WITHIN LIMITS. DUE TO LONG HISTORY OF #2 ENG A LOOPSDR ASAA2019060399540Converter · inoperativeFAULT LIGHT ILLUMINATED ON APU START. GROUNDED - YES. ACCOMPLISHED START CONVERTER UNIT SHOWS START SYSTEM INOP-FAULT ISOLATION. VERIFIED MAINT HISTORY MESSAGE 49-41250 REF B737-800 FIM 49-40 TASK 811. REMOVED AND REPLACED APU START CONVERTER UNIT REF B737-800SDR ASAA2019060399537Handle · no testNR 2 FIRE HANDLE DOES NOT TEST DOES NOT ILLUMINATE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019052429478Unknown · malfunctioned#2 ENG FIRE HANDLE WILL NOT TEST IN NORMAL, "A", OR "B". GROUNDED - YES. ACCOMPLISHED FIM 26-10 TASK 801 NO FAULTS FOUND. FIRE TEST FROM FLIGHT DECK. TEST OK. REF AMM 26-10-00.SDR ASAA2019050129218Terminal · dirtyNR 2 ENGINE FIRE DETECTOR TEST FAIL. TESTS IN A OR B BUT NOT "NORMAL.". GROUNDED - YES. REF FIM 26-10 TASK 801 PERFORMED FIRE DETECTION BITE TEST IN E/E, BITE TEST PASSED, REF FIM 26-10 TASK 810, CLEARED NR 2 ENG FIRE DETECTION LOOP TERMINALS. PERFORMED ENG/APSDR ASAA2019041658996Control Panel · degradedDFCS MODE CONTROL PANEL VERTICAL SPEED WINDOW LCD DEGRADED AND LAST TWO DIGITS HARD TO READ. GROUNDED - YES. REMOVED AND REPLACED DFCS MCP PER B737-800 AMM 22-11-34-000-801/AMM 22-11-34-400-801. PERFORMED DFCS GROUP #32 (MCP LRU REPLACEMENT) TEST PER AMM 22-11SDR ASAA2019040588889Floor Support · crackedINTERCOSTAL STA 312 TO 328 LBL45 IS CRACKED AT FASTENER HOLE. GROUNDED - YES. REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INSTERCOSTAL IAW B737 800 SRM 51 40 02 0G 0.SDR ASAA2019040588886Floorbeam · corrodedFLOOR BEAM STA 986 HAS MULTIPLE SPOTS OF CORR ACROSS LENGTH OF BEAM. GROUNDED - YES. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR OF STA 986 FLOOR BEAM UPPER CAP IAW B737 800 SRM 53 70 51 2R 4 W 2 O .150 R .118 L 6 D .032.SDR ASAA2019040588885Floor Support · corrodedFLOOR SUPPORT STA 947 TO 967 LBL16 HAS CORR. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT IAW B737 800 SRM 51 40 02 0G 0 W 2 O .080 R .062 L 2 D .018.SDR ASAA2019040328872Channel · corrodedL2 MOPSILL HAS CORR. GROUNDED - YES. REMOVED AND REPLACED L2 MOPSILL IAW B737 800 SRM 51 40 02 0G 0 W 2 O .080 R .061 L 6 D .019.SDR ASAA2019040388864Floor Support · corrodedFLOOR SUPPORT STA 947 TO 967 RBL 16 HAS CORR. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT IAW B737 800 SRM 5 40 02 0G 0 W 1 O .080 R .067 L 2 D. 013.SDR ASAA2019031728630Warning System · false indicationBOTH PACK CONTROL LIGHTS ILLUMINATE ON RECALL AND CLEAR ON RESET. GROUNDED - YES. C/W AMM 21-61-00, PACK/ZONE TEMP CONTROLLER BITE TEST IS GOOD, THIS CLEARS MEL 21-32B, NO FURTHER DEFECTS NOTED. HISTORY SHOWS "RAM AIR SENSOR" FAULT PREVIOUS FLIGHT.SDR ASAA2019031128583Fire Loop · out of positionENGINE NR 2 FIRE WARNING WILL NOT TEST. GROUNDED - YES. NR 2 FIRE TEST LOOP A SELECTED, SHOWS OVHTLIGHT. GVI NR 2 FAN COWL DET FOUND LOOP TOUCHING. CLEARED LOOP NO DEFECTS NOTED. FIRE TEST OKAY. REF AMM 26-10-00-710-801, FIRE CONTROL BITE TEST REF FIM 26-10 TASDR ASAA2019031128576Receiver · malfunctionedNR 2 HF FAIL. GROUNDED - YES. REBOOTED HF 2 RCVR, OPS NORMAL REF FIM 23-11 TASK 801.SDR ASAA2019022538300Control Valve · failedON MASTER CAUTION RECALL, CONT CAB ZONE TEMP LIGHT ILLUMINATES. EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. REMOVED & REPLACED TCV V143 B737-800 AMM 21-61-21 OPS CHECK NORMAL.SDR ASAA2019022028277Autothrottle Sys · disconnectedAUTO THROTTLE DISCONNECTED SEVERAL TIMES ON DESCENT WITH THROTTLES AT IDLE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019021628198Servo Motor · faultedAUTO-THROTTLE DISCONNECTED DURING DESCENT WHILE IN "VNAV" "PATH" WITH "ARM" ANNUNCIATED AND IN "LVL CHG" WITH "ARM" ANNUNCIATED. GROUNDED - YES. AUTOTHROTTLE BITE PER FIM 22-31 TASK 801 SHOWED SEVERAL INSTANCES OF FAULT 22-31518 "ASM-1 MOTOR PWR" LOGGED FOR LASDR ASAA2019021428199Autothrottle Sys · malfunctionedAUTOTHROTTLE TRIPPED OFF TWICE DURING DESCENT. GROUNDED - YES. ACCOMPLISHED AUTOTHROTTLE SYSTEM- OPERATIONAL TEST REF AMM 22-31-00-710-801. ALL TESTS PASSED. ACCOMPLISHED AUTOTHROTTLE SYSTEM- SYSTEM TEST REF AMM 22-31-00-710-802. ALL TESTS PASSED. GROUND VERIFSDR ASAA2019020828144Computer · failedAUTOTHROTTLES DISENGAGED TWICE DURING DESCENT WHILE THRUST LEVERS WERE AT IDLE. GROUNDED - YES. PERFORMED REVIEW OF A/T INFLIGHT FAULTS. AGAIN "ASM- 1 MOTOR PWR FAILED". MSG 22-31518. REF PREVIOUS HISTORY ASM-1 ALREADY CHANGED. T/S PER FIM 22-31 TASK 805. PERFSDR ASAA2019020428032Servo Motor · faultyAUTOTHROTTLE SWITCH WILL NOT ENGAGE. GROUNDED - YES. A/T BITE REF FIM 22-31-00-810-801. NO CURRENT FAULTS, HISTORY SHOWS LEG 07, AND LEG 10 WITH 30 ASM-1 FAULTS. MESSAGES: 22-315011 22-31687. REMOVED AND REPLACED ASM-1. ALL REQUIRED TESTS PASSED. REF AMM 22-31SDR ASAA2019010927725Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. LIGHT EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PACK/ ZONE TEMP CONT BITE TEST, NO FAULTS FOUND REF AMM 21-61-00-700-806-002 OPS CHECK GOOD. THIS CLEARS MEL 21-21G.SDR ASAA2019010727707Unknown · malfunctionedDURING AFTER START CHECKLIST ON RECALL AMBER AIR COND ILLUMINATED WITH OVERHEAD ZONE TEMP. LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. FLIGHT DECK PRIMARY TEMP CONTROL INOP. NR 2 PACK ZONE TEMP CONT SHOWS FLT DECK TRIM VALVE ON PREVIOUS FLT, SDR ASAA2019010727692Warning System · false activationAFTER PUSH AUTO FAIL LIGHT ILLUMINATED. RAN MEL 21-14C. LIGHT EXTINGUISHED. PER NOTE IN MEL. GROUNDED - YES. RESET PER FIM 21-31 TASK 827. BITE TESTS NML AFTER RESET PER FIM 21-31 TASK 801. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2018121127312Valve · failed#2 COWL VALVE OPEN LIGHT ILLUMINATED AND REMAINS BRIGHT BLUE WHEN TURNED ON AS WELL AS IAI LIGHT TURNS AMBER ALTERNATE DEACTIVATION PROCEDURES PER CHAPTER 5 TABLE 3 ITEMS 3&5. GROUNDED - YES. REMOVED & REPLACED # 2 ENG COWL TAI VALVE REF B737-800 AMM 30-21-11 SDR ASAA2018120312766Sensor · dirtyCONT CAB "ZONE TEMP" LIGHT ILLUMINATED ON RECALL. EXTINGUISHES ON RECALL. EXTINGUISHES WITH RESET. GROUNDED - YES. SYSTEM HAD A CONTROL CABIN SENSOR FAULT. CLEANED CONTROL CABIN SENSOR T485, SYSTEM OPS CHECKS GOOD IAW B737-800 AMM 21-61-00-700-806-002.SDR ASAA2018113027182Keyboard · defectiveFO FMC "EXEC" BUTTON REQUIRES HEAVY PRESSURE TO MAKE CONTACT WITH THE SENSOR UNDERNEATH. GROUNDED - YES. REMOVED AND REPLACED FMCS KEYBOARD F/O SIDE IAW AMM 34-61-01. OPS TEST NORMAL.SDR ASAA2018102926637Warning System · false activation"VTK" ON F/O'S PFD DISPLAYED INTERMITTENTLY. GROUNDED - YES. PERFORMED RT FMC BITE PER FIM 34-61 TASK 801 NO FAULTS FOUND. PERFORMED FIM 34-61 TASK 807. NO FAULTS FOUND.
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