N560AS

Service difficulty reports · 562

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 = 'N560AS' 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 ASAA2022012937451Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED JUST INBD OF STAB STA 157.10 (MARKED AND VERIFIED BY HFEC). GROUNDED - YES. REPAIRED L/H HORIZONSTAL STAB LOWER SKIN INBOARD OF STA 157.10 IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11, REPAIR IS A CATEGORY B REPAIR AND RJan 29, 2022 · N560AS · Boeing 737890 · Horizontal Stabilizer StructureSDR ASAA2022010737093Unknown · unknownTRANSITORY L FMC FAILURE FOR APPROXIMATELY 3 MIN. GROUNDED - YES. REF B737-800 FIM 34-61 TASK 801 FOUND WATCHDOG TIMER FAULT ON LEG 1 BOTH L AND R FMC LOGGED FAULT. PER FIM FAULT WAS INTERMITTENT FMC OPS TEST OK.Jan 7, 2022 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2022010537080Fmc · faultedFMC DISAGREE ON PREFLT. GROUNDED - YES. FOLLOWED QRH. CORRECTED ITSELF.Jan 5, 2022 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2022010337068Modulating Valve · noisyCONT CAB ZONE TEMP ON RECALL. GROUNDED - YES. ACCOMPLISHED PACK TEMP CONTROLLER BITE REF B737-800 FIM 21-62 TASK 801. TEST PASSED BUT THE CONT CAB TRIM AIR MODULATING VALVE WAS MAKING A LOUD WHINING NOISE. BECAUSE OF THE HISTORY AND THE NOISE, CHANGED OUT THE Jan 3, 2022 · N560AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2022010137040Unknown · unknownON TAKEOFF FO DID NOT HAVE FLIGHT DIRECTOR GUIDANCE. MCP NOT PROVIDING GUIDANCE TO FO SIDE AND N1 SETTING. ALTITUDE ALERTER INDICATING ONLY 50,000 FT AND CONTINUOUS ALTITUDE ALERTING HORN. RAN MODE CONTROL PANEL LOCKUP QRH AND AFTER RESETTING CB'S ACFS MCP DC Jan 1, 2022 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021122136987Unknown · unknownDURING T/C 7827300 ON #1 ENGINE FOUND FAULT CODE 73-20311, THE START SIGNAL AND ARINC BUS DATA DISAGREE, SHORT TIME FAULT, DEFERRED PER T/C 7827300. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE ELECTRONIC CONTROL UNIT, REF B737-800 AMM 73-21-60. OPERATIONAL Dec 21, 2021 · N560AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2021121736931Unknown · unknownB AUTOPILOT DISENGAGED AT CRUISE. "B" WOULD NOT REENGAGE. GROUNDED - YES. PERFORMED REQUIRED TESTS IAW B737-800 AMM 22-11-00. OPS CHECK NORMAL.Dec 17, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021120236791Unknown · unknownFIRST OFFICERS FLIGHT DIRECTOR FAIL DURING CRUISE FLIGHT. THIS ALSO RESULTED IN AUTO PILOT DISENGAGEMENT. THE FIRST OFFICIER'S FLIGHT DIRECTOR CAME BACK ON AFTER APPROXIMATELY 25 MINS. GROUNDED - YES. PERFORMED LAND VERIFY TEST REF B737-800 AMM 22-11-00/201FOUDec 2, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021112436741Blade · damagedBLADE #22 ON #1 ENGINE HAS DAMAGE IN CRITICAL AREA J. GROUNDED - YES. REMOVED DAMAGE FAN BLADES #22 AND OPPOSITE FAN BLADE PAIR #10 REF B737-800 AMM 72-21-02-000-802-F00. ACCOMPLISHED CFM BLAMAP V 3.0 BLADES MAPPING. NY 38359 11/25/2021. INSTALLED NEW SERVICEANov 24, 2021 · N560AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2021112436740Blade · bent#1 ENG FAN BLADE #12 HAS BENT TIP. GROUNDED - YES. REMOVED DAMAGE FAN BLADES #12 AND OPPOSIT FAN BLADE PAIR #24 REF. AMM 72-21-02-000-802-F00. ACCOMPLISHED CFM BLAMAP V 3.0 BLADES MAPPING. NY 38359 11/25/2021. INSTALLED NEW SERVICEABLE PAIR OF FAN BLADES ON #1Nov 24, 2021 · N560AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2021111336602Unknown · unknownFMC DISAGREE GROUNDED - YES. ACOOMPLISHED FMC RESET PROCEDURE PER QRH. RESTORED NORMAL.Nov 13, 2021 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2021110336514Control Panel · inoperativeMCP CONTROL PANEL LIGHTS VERY DIM. GROUNDED - YES. VERIFIED DEFECT ALL MODE SELECT ON MCP ARE STUCK IN DIM POSITION RLS OPS NML. REMOVED AND REPLACED MCP REF B737-800 AMM 22-11-34, LRU REPLACEMENT TEST PASSED. REF L/P 60199146 FOR DOWNGRADE.Nov 3, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021102936446Control Panel · inoperativeAT CRUISE FL390 W/ A/P B ENGAGED A/P DISCONNECT AND BOTH F/D'S TURNED OFF W/ NO WARNING. NO FAILURE FLAGS APPEARED. AFTER 30 SECS A/P A AND CAPT F/D RESPONDED. F/D ON FO SIDE WILL NOT RESPOND. FLIGHT CONTINUED ON CAPT F/D AND A/P B. AT LOC/GS INTERCEPT FO'S F/Oct 29, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021102836426Transceiver · failedAFTER LDG TURNED WX TO TEST PWS FAIL, WXR FAIL, TERR FAIL. GROUNDED - YES. REPLACED WEATHER RADAR R/T REF. B737-800 AMM 34-43-41-400-801. OPS CHECK NORMAL REF. AMM 34-43-00-710-802-001.Oct 28, 2021 · N560AS · Boeing 737890 · Independent Position Determining SystemSDR ASAA2021102636412Unknown · unknownAT FINAL APPROACH FIX WITH AP 'A' ENGAGED IN APP MODE, AIRPLANE SUDDENLY PITCHED DOWN TO 1,000 FPM. AT TIME OF UPSET AP WAS IN GS AND LOC CAP, AUTO-PILOT DISENGAGED ON ITS OWN. AIRPLANE FLOWN MANUALLY FOR REMAINDER OF FLIGHT. THERE WAS NO DISTORTION OF ILS SIGOct 26, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021101336286Fire Loop · inoperativeENGINE #1 A LOOP FIRE INOP. GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 805 FOUND NO ACTIVE FAULTS AND OVERHEAT TEST OPS NORMAL. ALL ENG 1 LOOPS MEASURE WITHIN LIMITS. FOUND BROKEN STUD ON UPPER FAN LOOP A DECTECTOR. REPLACED UPPER FAN LOOP REF B737-800 Oct 13, 2021 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2021101136260Eec · faulty#2 ENGINE FMC CDU SHOWS FAULT CODE 73-21272. ALT. VOLTAGE TO EEC OUT OF RANGE. GROUNDED - YES. REMOVED AND REPLACED STATOR ALTERNATOR HOUSING REF: B737-800 AMM 73-21-08. PERFORMED ENGINE RUN EEC BITE CHECK, NO FAULTS FOUND. REF: AMM 71-00-00.Oct 11, 2021 · N560AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2021100736230Actuator · faultyAPU FAULT LIGHT ILLUMINATED DURING APU START. GROUNDED - YES. PERFORMED APU SHUTOFF VALVE OPERATIONAL TEST FOUND VALVE TO BE FAULTING REF B737-800 AMM 28-25-02-710-801. REQUIRES REPLACEMENT. REMOVED AND REPLACED APU FUEL SHUTOFF VALVE ACTR AS REQUIRED REF AMM Oct 7, 2021 · N560AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2021100636212Coupler · inoperativeAFTER TAKEOFF, WHILE CONDUCTING HF RADIO CHECK, UNABLE TO TRANSMIT ON EITHER HF RADIO. AUDIO COMES IN NORMALLY. BUT HF TRANSMITTER DOESNT SEEM TO ACTIVATE. GROUNDED - YES. REMOVED AND REPLACED #1 HF ANTENNA COUPLER. REMOVED AND REPLACED #2 HF COUPLER PER B737-Oct 6, 2021 · N560AS · Boeing 737890 · HF Communications SystemSDR ASAA2021092336072Terminal · damaged#1 ENG OVERHEAT TEST FAILED. GROUNDED - YES. REF B737-800 FIM 26-10 TASK 801 FOUND ENG 1 UPPER FAN DETECTOR FAULT. REF FIM 26-10 TASK 805 FOUND TERMINAL AT M1760 ENGINE CORE RIGHT FIRE DETECTOR ASSEMBLY. REPLACED WIRE HARNESS MW0325 REF B737-800 WDM ASA D280A1Sep 23, 2021 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2021091235953Control Module · no test#1 A LOOP INOP. DOES NOT TEST. GROUNDED - YES. REPLACED CONNECTOR D30252 PER B737 SWPM 20-63-00 .REMOVED AND REPLACED CONNECTOR D39927 PER SWPM 20-60-06, ENGINE APU FIRE CONTROL MODULE FAULTS UPPER FAN A LOOP. REMOVED AND REPLACED UPPER FAN LOOP REF B737-800 ASep 12, 2021 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2021082335830Wire Harness · inoperativeDURING FIRE TEST , ENGINE # 1 HANDLE DID NOT ILLUMINATE. TEST IS ACCEPTABLE WHEN LOOP B IS SELECTED. GROUNDED - YES. ACCOMPLISHED ALTERNATE DEACTIVATION PER CHAPTER 5 TABLE 3 ITEM 7 FOR #1 ENGINE. REMOVED M279 MODULE RESISTANCE AT D1002 PINS 25 TO 24 IS 2.1 OHAug 23, 2021 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2021081635756Wire Harness · no testNO 1 ENGINE FIRE TEST DOES NOT ILLUMINATE LIGHT ON A LOOP. GROUNDED - YES. VERIFIED DISCREP. M279 MODULE SHOWS RIGHT CORE FAULT. REF. B737-800 MM 26-10-01, AND B737-800 WDM 26-11-11 PG 1 SHT 1, REMOVED M279 MODULE, AND LOOP A PIN 25 TO GND READS 1.318K OHMS. SAug 16, 2021 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2021081335697Switch · inoperativeAUTOTHROTTLE WOULD NOT DISCONNECT WHEN THE #1 THRUST REVERSER LEVER DISCONNECT SWITCH IS PUSHED (NORMAL DISCONNECT USING #2). GROUNDED - YES. REMOVED AND REPLACED #1 THRUST LEVER A/T DISCONNECT SWITCH REF B737-800 AMM 22-31-51/401. 1 C/B OPENED, TAGGED, AND REAug 13, 2021 · N560AS · Boeing 737890 · Engine Thrust ReverserSDR ASAA2021080835678Wire Harness · no testENGINE #1 LOOP A ENG OVERHEAT WILL NOT TEST. GROUNDED - YES. FOLLOWED B737-800 FIM 26-10 TASK 805 FOR ENGINE- WIRING HARNESS/FIRE DETECTOR. FOUND INCONSISTENT READING BETWEEN CONNECTOR DP1501 AND DP1552. REMOVED AND REPLACED FAN FIRE DETECTION HARNESS REF B737Aug 8, 2021 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2021080835666Anti-Ice Valve · failedWHILE CHECKING C/BS FOUND P18-3 (A-1) OPEN WING ANTI ICE VALVE. GROUNDED - YES. OPEN P18-3 INSP NO DEFECTS CLOSED P18-3 ACCESSED L WING ANTI ICE VALVE DISCONNECTED CLOSED C/B TESTED R WING TEST PASS RECONNECTED L WING VALVE TEST FAILED REF B737-800 AMM 20-60-0Aug 8, 2021 · N560AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2021080235607Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL. HGS OK. PRIOR TO AND DURING FLARE AIRCRAFT DRIFTED LEFT OF COURSE SIGNIFICANTLY AND AUTOPILOT HAD TO BE DISCONNECTED PRIOR TO TOUCHDOWN. ILS CRITICAL AREA WAS CLEAR. GROUNDED - YES. ACCOMPLISHED DFCS BITE PER B737-800 FIM 22-11 TASK 801 Aug 2, 2021 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2021073135587Fire Loop · faulted#1 ENGINE OVHT/DET "A" LOOP "FAULT" LIGHT ILLUMINATES. GROUNDED - YES. DUE TO HISTORY AND PREVIOUS PART REPLACEMENTS, REMOVED AND REPLACED ALL 4 #1 ENGINE FIRE DETECTION ASSEMBLIES REF B737-800 AMM 26-11-01. OP CHECK GOOD REF AMM 26-11-00. ETOPS GROUND VERIFICJul 31, 2021 · N560AS · Boeing 737890 · Smoke DetectionSDR ASAA2021072035498Unknown · faulted#1 ENGINE FIRE SWITCH NOT LIGHTING UP CORRECTLY DURING OVERHEAT/FIRE TEST. GROUNDED - YES. PERFORMED ALTERNATE DEACTIVATION REF CHAP 5 TABLE 3 ITEM 7. COULD NOT DUPLICATE DEFECT, OVERHEAT/FIRE TEST OPERATES NORMALLY. TESTED ALL 4 A LOOP DETECTORS, ALL 4 DETECTJul 20, 2021 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2021071735422Terminal · dirty#1 ENGINE "A" FIRE LOOP INOP. GROUNDED - YES. INSPECTED AND FOUND CORE RIGHT LOWER DETECTOR FAULT ACTIVE ON M279 MODULE. ACCESSED MM1760 AND PERFORMED B737-800 FIM 26-10 TASK 810. RESISTANCE WERE WITHIN LIMITS. CLEANED DETECTOR TERMINAL AND CHECKED LUGS. REINSJul 17, 2021 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2021060635041Fmc · faultedFMC DISAGREE DURING TAXI. GROUNDED - YES. COMPLETED QRH - FMC DISAGREE NO LONGER DISPLAYED.Jun 6, 2021 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2021060134997Anti-Ice Valve · inoperativeON PREFLIGHT, FOUND WING ICE R VALVE OPEN LIGHT BRIGHT BLUE WITH SWITCH IN OFF POSITION. GROUNDED - YES. REMOVED & REPLACED R/H WING ANTI ICE VALVE IAW B737-800 AMM 30-11-11. OPS CHECK & LEAK CHECK GOOD.Jun 1, 2021 · N560AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2021053034971Fmc · false indicationFMC DISAGREE ON PUSHBACK. GROUNDED - YES. PERFORMED 11.2 PROCEDURES. SYSTEM OK.May 30, 2021 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2021050734781Terminal · broken#1 ENG OVERHEAT DETECTOR "A" INOP, FAULT LT ILLUMINATED. GROUNDED - YES. REMOVED ENGINE & APU FIRE DETECTION CONTROL MODUEL (M279). RESISTANCE CKS FOR A-LOOP PINS 24 & 25 D1002 SHOWS 70 OHMS. DURING SHAKE DOWN OF A-LOOP HARNESS, TERMINAL BROKE FROM UPPER FAN DMay 7, 2021 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2021050534759Eec · faultyUPON LANDING "ENGINE CONTROL" LIGHT ILLUMINATED. GROUNDED - YES. #2 OK (#1 EEC BITE SHOWS MSG 73-11281) "B" CHANNEL WILL NOT PWR. RAN #1 ENG REF. B737-800 MM TASK 71-00-00-700-808-F00 - FAULT STILL ACTIVE AFTER RUN. REF B737-800 FIM TASK 73-28-TASK 805 #1 EEC May 5, 2021 · N560AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2021042834689Wire · brokenDURING T/S OF FIRE DETECTION , FOUND DETECTOR #4 WIRE BROKEN ON MW0326. GROUNDED - YES. REMOVED AND REPLACED CORE FIRE DETECTION HARNESS MW0326, REF B737-800 AMM 26-11-02. GROUND VERIFICATION TESTS OK FOR #1 ENGINE LOOP "B".Apr 28, 2021 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2021042534688Fire Loop · false activation#1 ENG OVHT DET "A" LOOP WILL NOT TEST. GROUNDED - YES. #1 ENGINE BITE OF CONTROL MODULE DONE WITH NO FAULTS FOUND REF B737-800 FIM 26-10 TASK 801. ENG FIRE DETECTION OPERATIONAL TEST GOOD FOR A AND B LOOPS. #1 ENGINE OPENED WITH ALT DE-ACTIVATION AND ALL FIRApr 25, 2021 · N560AS · Boeing 737890 · Detection SystemSDR ASAA2021040934547Bulb · burned outFWD OVERWING EXIT EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED FWD OVERWING EXIT EMERGENCY LIGHT BULB REF B737-800 AMM 33-51-04. OPS CHECK GOOD.Apr 9, 2021 · N560AS · Boeing 737890 · Emergency LightingSDR ASAA2021040334493Warning Light · intermittentTHE ELEC LIGHT ON THE OVERHEAD PANEL IS ILLUMINATED. GROUNDED - YES. PERFORMED BITE CHECK B737-800 FIM 24-31 TASK 801 CLEARED FAULT OF AUX BAT CHARGER ALL OPS CHECK NORMAL.Apr 3, 2021 · N560AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2021032434400Satcom · malfunctionedWHEN MAKING SATCOM CALLS WE COULD HEAR THE CALL RECEPIENT BUT THEY COULD NOT HEAR US. TRIED SATCOM 1 AND 2 AND ALL AIRCRAFT MICS. GROUNDED - YES. ACCOMPLISHED OPS CHECKS REF B737-800 AMM 23-15-00-730-801. NO FAULTS FOUND.Mar 24, 2021 · N560AS · Boeing 737890 · Communications SystemSDR ASAA2021021834153Fmc · malfunctionedRIGHT FMC FAILED THEN RECOVERED THEN FAILED AGAIN LOT OF SWITCHING BETWEEN LEFT AND RIGHT. GROUNDED - YES. FMC 1 LOGGED PGM FAULT RT FMC LOGGED RESYNC. LT & RT FMC SYSTEMS OPS CHK NORMAL PER B737-800 AMM 34-61-00-710-801.Feb 18, 2021 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2021012633948Eec · inoperativeENGINE 2 EEC CHANNEL B DATA NOT AVAILABLE MESSAGE IN FMC EEC BITE MENU. GROUNDED-YES. FOUND ENGINE 2 EEC CHANNEL B INOPERABLE. EEC INTERNAL FAULT 73-10102. REMOVED AND REPLACED NR 2 EEC, PER B737-800 AMM 73-21-60/401 AND OPERATIONS CHECKED, PER AMM 73-21-0Jan 26, 2021 · N560AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2021011333877Lamp · inoperativeR1 EMERGENCY EXIT LIGHT INOPERABLE (EXTERIOR). GROUNDED-YES. RELAMPED OPERATIONS GOOD.Jan 13, 2021 · N560AS · Boeing 737890 · Emergency LightingSDR ASAA2020121733720Probe · out of limitsTECH SERVICES REQUEST DUE TO RECENT FUEL IMBALANCE ISSUE. ACCOMPLISH FUEL QUANTITY INDICATING SYSTEM TEST, PER B737-800 AMM 28-41-00-730-801. GROUNDED-YES. ACCOMPLISHED STEP NR 2 OF THIS TSR. RT TANK CAPACITANCE VALUE IS 398.3PF, REF B737-800 AMM 28-41-00-Dec 17, 2020 · N560AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2020121633719Indication Sys · false indicationFUEL IMBALANCE INDICATION CAME ON 1 HOUR FROM LANDING. THE FUEL IMBALANCE CHECKLIST WAS RUN. THERE WERE NO ABNORMAL ENGINE INDICATIONS, NO SUSPECTED FUEL LEAK AND NO FUEL LOSS. THE WINGS WERE LEVEL AND THE AIRPLANE WAS IN TRIM. GROUNDED-YES. PERFORMED FQIDec 16, 2020 · N560AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2020121233670Autothrottle Sys · disconnectedAUTO THROTTLES DISCONNECTED WHEN TOGA PUSHED. GROUNDED-YES. ACCOMPLISHED B737-800 FIM 23-21 TASK 801. CURRENT STATUS PASSES. NO INFLIGHT FAULTS. ACCOMPLISHED LAND VERIFY TEST, REF B737-800 AMM 22-11-00-700-801. ALL TESTS PASS.Dec 12, 2020 · N560AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2020111333553Coupler · inoperativeAFTER TAKEOFF WHILE USING HF1-WE FOUND XMIT FUNCTION ON THAT RADIO DID NOT WORK, WHILE STILL ABLE TO XMIT ON HF2. DF NOTE-BEEP HEARD DURING FREQ CHANGE ON HF1 STILL OCCURRED WHILE PRESSING XMIT ALL BUTTONS, BUT BEEP LASTED AT LEAST 8-10 SECONDS, MUCH LONGER TNov 13, 2020 · N560AS · Boeing 737890 · Communications System WiringSDR ASAA2020111233554Transceiver · inoperativeNR 1 HF RADIO TUNING TONE INITIATES AT RANDOM TIMES MAKING RADIO UNUSABLE FOR COMMUNICATION. GROUNDED-YES. REMOVED AND REPLACED HF TRANSCEIVER, IAW B737-800 AMM 23-11-210. OPERATIONS CHECK NORMAL, OK FOR SERVICE. NOTIFIED SEAMC LESTER.Nov 12, 2020 · N560AS · Boeing 737890 · HF Communications SystemSDR ASAA2020102433403A/C Pack · inoperativeRELEASED PER MEL 21-32B L HAND PACK PRIMARY TEMP CONTROL INOPERABLE. GROUNDED-YES. LEFT PZTC BITE SHOWED PREVIOUS FLIGHT FAULT FOR "THIS PACK TCV". ACCOMPLISHED T/S, PER B737-800 FIM 21-62 TASK 830-INITIAL EVALUATION (VERIFY TEST) DID NOT CONFIRM FAULT-TESOct 24, 2020 · N560AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2020100733300Display · malfunctionedFIRST OFFICER NAV DISPLAY "MAP" AMBER INDICATION, WOULD NOT CLEAR. GROUNDED-YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836. RIGHT FMC RESTORED.Oct 7, 2020 · N560AS · Boeing 737890 · Flight Management Computing Hardware System
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