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.

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.Jul 20, 2019 · N585AS · Boeing 737890 · Emergency LightingSDR 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.Jul 11, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 CLJul 5, 2019 · N585AS · Boeing 737890 · Fuselage Main, Attach FittingsSDR 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 INSTALLJul 5, 2019 · N585AS · Boeing 737890 · Fuselage Main, Attach FittingsSDR 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 Jul 3, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 FOUNJul 3, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jul 2, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 DJun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 AJun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 REVJun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 30, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 INSJun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 "-".Jun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Jun 29, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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 BIJun 23, 2019 · N585AS · Boeing 737890 · APU System WiringSDR 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 LOOPJun 8, 2019 · N585AS · Boeing 737890 · Fire DetectionSDR 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 B737-800May 29, 2019 · N585AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2019060399537Handle · no testNR 2 FIRE HANDLE DOES NOT TEST DOES NOT ILLUMINATE. GROUNDED - YES. ON DEFERRAL.May 29, 2019 · N585AS · Boeing 737890 · Detection SystemSDR 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.May 24, 2019 · N585AS · Boeing 737890 · Fire DetectionSDR 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/APMay 1, 2019 · N585AS · Boeing 737890 · Fire DetectionSDR 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 22-11Apr 15, 2019 · N585AS · Boeing 737890 · Autopilot SystemSDR 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.Mar 28, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Mar 28, 2019 · N585AS · Boeing 737890 · Fuselage Main, Floor BeamSDR 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.Mar 28, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Mar 28, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Mar 28, 2019 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR 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.Mar 17, 2019 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR 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 TAMar 11, 2019 · N585AS · Boeing 737890 · Fire DetectionSDR ASAA2019031128576Receiver · malfunctionedNR 2 HF FAIL. GROUNDED - YES. REBOOTED HF 2 RCVR, OPS NORMAL REF FIM 23-11 TASK 801.Mar 11, 2019 · N585AS · Boeing 737890 · HF Communications SystemSDR 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.Feb 23, 2019 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2019022028277Autothrottle Sys · disconnectedAUTO THROTTLE DISCONNECTED SEVERAL TIMES ON DESCENT WITH THROTTLES AT IDLE. GROUNDED - YES. ON DEFERRAL.Feb 20, 2019 · N585AS · Boeing 737890 · Auto Throttle SystemSDR 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 LAFeb 16, 2019 · N585AS · Boeing 737890 · Auto Throttle SystemSDR 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 VERIFFeb 14, 2019 · N585AS · Boeing 737890 · Auto Throttle SystemSDR 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. PERFFeb 8, 2019 · N585AS · Boeing 737890 · Autopilot ComputerSDR 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 22-31Feb 4, 2019 · N585AS · Boeing 737890 · Auto Throttle SystemSDR 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.Jan 9, 2019 · N585AS · Boeing 737890 · Cabin Temperature IndicatorSDR 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, Jan 7, 2019 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR 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.Jan 7, 2019 · N585AS · Boeing 737890 · Cabin Pressure Control SystemSDR 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 Dec 10, 2018 · N585AS · Boeing 737890 · Nacelle/Pylon StructureSDR 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.Dec 1, 2018 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR 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.Nov 30, 2018 · N585AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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.Oct 27, 2018 · N585AS · Boeing 737890 · Flight Management Computing Hardware System
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