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 ASAA2017061021008Transceiver · failedABOUT 30 MINUTES FROM TOP OF DESCENT, THE NR 1 COMMS BECAME GARBLED AND BARELY READABLE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 HF TRANSCEIVER IAW AMM 23-11-21. OPS CHECKED GOOD. NR 1 COMMS NO LONGER GARBLED AND BARELY READABLE.Jun 10, 2017 · N560AS · Boeing 737890 · HF Communications SystemSDR ASAA2017060220944Transceiver · failedDURING CLIMB, HF 2 RADIO DISPLAYED FAIL IN BOTH ACTIVE AND STANDBY DISPLAYS. ACFT GROUNDED. PERFORMED BITE TEST. NO FAULTS FOUND AND FAIL LIGHTS EXTINGUISHED. REMOVED AND REPLACED THE NR 2 HF TRANSCEIVER IAW AMM 23-11-21-400-801. OPS CHECKED GOOD. NO HISTOJun 2, 2017 · N560AS · Boeing 737890 · HF Communications SystemSDR ASAA2017042220496Unknown · malfunctionedIN STABLE CRUISE FLIGHT WITH BOTH PACK ON AND TRIM AIR ON TEMP OUTPUT OF PACKS SHOULD BE IDENTICAL. IN THIS AIRPLANE, THE LEFT PACK TEMP OUTPUT VARIES EVERY 25 SECONDS FROM 5 DEG TO 15 DEG, THE RIGHT PACK IS STABLE AT 11DEG REF SYS HANDBOOK SEC 2.020 PG 2 "BALApr 22, 2017 · N560AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017040320346Coupler · failedNR 2 HF INOPERATIVE, WILL NOT TRANSMIT. ACFT GROUNDED. NO SIDE TONE OR KEY INTERLOCK LED WHEN TRANSMITTING FROM NR 2 HF TRANSCEIVER. REPLACED THE NR 2 HF COUPLER. INSTALLATION TEST FOR THE COUPLER PASSED IAW AMM 23-11-61/401.Apr 3, 2017 · N560AS · Boeing 737890 · HF Communications SystemSDR ASAA2017032920296Fmc · intermittentEXITING THE RUNWAY BOTH FMCS DISAPPEARED WITH AMBER LIGHT FOR ABOUT 15 SECONDS. ACFT GROUNDED. FMC DOES NOT OPERATE IAW FIM 34-61, TASK 836. BOTH FMC RESTORED TO NORMAL. INTERMITTENT FAULT.Mar 29, 2017 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017021219784Warning Light · false activationAFTER ENGINE START, ESTABLISHED ENGINE BLEEDS, THE AUTOFAIL ALT GREEN LIGHT ILLUMINATED AS WELL WHEN MASTER RECALL IS PUSHED AIR COND ILLUMINATED, CONTROL CABIN ZONE TEMP LIGHT. GOES OUT. ACFT GROUNDED. CONFIRMED CONTROL CABIN ZONE TEMP ANNUNCIATOR ILLUMINATFeb 12, 2017 · N560AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017020419659Control Panel · failedMCP ALTITUDE SELECTOR READOUT HAS DIGITAL NUMERIC BLEED THROUGH. ACFT GROUNDED. REMOVED AND REPLACED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. ALT DEACT REVERSED. TESTS GOOD. PERFORMED DFCS LRU REPLACEMENT TEST FOR MCP TEST GROUP 32 IAW AMM 22-11-34, LAND VFeb 4, 2017 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2017020419667Module · failedON FINAL, SELECTING TAXI LIGHT TO ON FUEL VALVE OPEN LIGHT ILLUMINATED THEN EXTINGUISHED. SELECTING FIXED LANDING LIGHT FROM PULSE, VALVE OPEN LIGHT ILLUMINATED. ON SHUT DOWN AT GATE, SELECTING FUEL PUMP OFF VALVE LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. INSPEFeb 4, 2017 · N560AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2017010819273Servo Motor · failedAUTOTHROTTLES INOPERATIVE, NOT ARMING. ACFT GROUNDED. VERIFIED FAULT IS STILL ACTIVE THROUGH A/T BITE. REPLACED THE NR 1 AUTOTHROTTLE SERVO MOTOR IAW AMM 22-31-91-020-801. OPS CHECKED GOOD.Jan 8, 2017 · N560AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2017010719262Fmc · inoperativeLEFT FMC FAILED DURING CRUISE. ACCOMPLISHED QRH UNABLE TO RESTORE LT FMC. ACFT GROUNDED. VERIFIED FAULT. OPEN & CLOSED THE CIRCUIT BREAKER FOR LT FMC. LT FMC RETURNED TO NORMAL IAW FIM 34-61 TASK 836. OPS TEST PASSED IAW AMM 34-61-00-710801.Jan 7, 2017 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017010519257Probe · no testDURING ACCOMPLISHMENT OF NG-28FCD-18088-1, FQIS NR 1 TANK AND COMP UNITS TESTING, FOUND TU'S F4 AND F6 OUT OF LIMITS. ACFT GROUNDED. REMOVED AND REPLACED TANK 1 F4 AND F6 TANK UNIT PROBES IAW AMM 28-41-21-400-801. ACCOMPLISHED FQIS SYSTEM TEST IAW AMM 28-41Jan 5, 2017 · N560AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017010419243Probe · no testDURING ACCOMPLISHMENT OF NG-28FCD-18090-1, FQIS NR 2 TANK AND COMP UNITS TESTING FOUND TU F1,F2,F3, F8 AND F10 OUT OF LIMITS. ACFT GROUNDED. REMOVED TANK UNIT PROBES F1,F2, F3, F8, AND F10 IAW AMM 28-41-21-400-801. ACCOMPLISHED FQIS SYSTEM TEST IAW AMM 28-4Jan 4, 2017 · N560AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017010319238Satcom · malfunctionedNR 1 AND 2 SATCOM WOULD NOT CONNECT WITH APPROPRIATE HF/SAT TRANSFER SWITCH SELECTED TO SAT. BLUE SQUARE SAT ANNUNCIATOR ILLUMINATED, AUDIO SELECT PANEL SELECTED TO APPROPRIATE SAT. SATCOM SHOWED CYCLING BUT NEVER CONNECTED DISPLAYS, NO NUMBER AT BOTTOM OF SJan 3, 2017 · N560AS · Boeing 737890 · Communications SystemSDR ASAA2017010319239Probe · malfunctionedWITH ALL SIX FUEL PUMPS ON, FUEL GAUGES DISPLAYED AMBER IMBALANCE ANNUNCIATION AND INDICATED 71000 LB IMBALANCE WITH THE RIGHT WING TANK (AMBER) LOWER THAN LEFT. FMC ALSO INDICATED SIGNIFICANTLY OVER BURN AT NEXT WAYPOINT. FAN FUEL IMBALANCE CHECKLIST WHICHJan 3, 2017 · N560AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016122819178Autothrottle Sys · malfunctionedAUTOTHROTTLE SWITCH WILL ONLY ENGAGE FOR 3-5 SEC THEN TURNS OFF. AUTO THROTTLE WILL NOT ENGAGE. ACFT GROUNDED. A/T LOGGED 22-31675 T/O SET LOW. ACCOMPLISHED FIM 22-31 TASK 817, FOUND FAULT TO BE INTERMITTENT. CURRENT STATUS TEST PASSED.Dec 28, 2016 · N560AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016121519071Connector · corrodedON TAXI LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED FOR 30 SECS. ENGINE WAS AT IDLE POWER. GROUNDED - YES. ACCOMPLISHED FIM 73-05 TASK 801 FOUND MAINT MESSAGE 73-31071. NR 1 ENG FUEL DIFFERENTIAL PRESSURE SWITCH CONNECTOR RUSTY. INSTALLED SERVICEABLE FUEL FILTERDec 15, 2016 · N560AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2016120818981Autopilot Sys · malfunctionedAUTOPILOT B DISENGAGED AT FL 360 TWO TIMES. AUTOPILOT A, WORKED FINE. ACFT GROUNDED. PERFORMED CURRENT STATUS CHECK, NO FAULTS. PERFORMED LAND VERIFY BITE GROUP 49, ALL TESTS PASSED. ACFT REMAINS CAT IIIA AUTOLAND & HGS.Dec 8, 2016 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2016112318822Fmc · malfunctionedVTK ON CAPTS NAV DISPLAY. BOTH FMC PROMPTS NOT AVAILABLE ANOMALY CLEAR ITSELF PRIOR TO QRH. GROUNDED - YES. ACCOMPLISHED FIM 34-61 TASK 836, BOTH FMC'S RECOVERED NORMALLY. ONLY FMC-L HAD AN INFLIGHT FAULT. CK'S GOOD FOR SERVICE.Nov 23, 2016 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016111918740Not Reported · failedTECH SERVICES REQUEST CHECK NR 1 FUEL TANK, TANK UNIT AND COMPENSATOR VALUES. GROUNDED, YES. ACCOMPLISHED TSR 818103 ALL STEPS AND T/C 78528000 FUEL ENTRY PERMIT. REMOVED AND REPLACED NR 1 FUEL TANK F15, F1, F2, AND F3 REF AMM 28-41-21. OPS TEST PASSED WITH NONov 19, 2016 · N560AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016111118620Circuit Breaker · trippedAPU POWER WILL NOT CONNECT TO AIRPLANE. APU GEN CONT UNIT CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. ACCOMPLISHED GVI OF CIRCUIT BREAKER AND ASSOCIATE ACCESSIBLE WIRING, NO DEFECTS NOTE. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01-860-801. ACCOMPLISHED FIM 24-21Nov 11, 2016 · N560AS · Boeing 737890 · Electrical Power System WiringSDR ASAA2016110918629Fmc · malfunctionedLEFT FMC FAILURE AT CRUISE VTK LNAV & VNAV DISENGAGED. QRH FOLLOWED & FMC RESTORED. CONTINUED & DIDN'T HAPPEN AGAIN. ACFT GROUNDED. CYCLED POWER AT FMC. VERIFIED OPS RESTORED FOR BOTH FMC'S IAW FIM 34-61 TASK 836.Nov 9, 2016 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016101318344Sensor · faultedAPU FAULT LIGHT ON AFTER APU START ATTEMPT. ACFT GROUNDED. VERIFIED DISCREPANCY. FOUND FAULT 49-61223 LOGGED. ACCOMOPLISHED FIM 49-60 TASK 812. FOUND INLET SENSOR INOPERATIVE IAW AMM 49-61-31. R & R THE INLET SENSOR. PERFORMED APU BITE 49-60 TASK 801. FAULTOct 13, 2016 · N560AS · Boeing 737890 · APU ControlsSDR ASAA2016081617720Warning Light · false activationPRESSURIZATION AUTO FAIL LIGHT ILLUMINATES ON LANDING. ACFT GROUNDED. SELECTED MANUAL FOR 10 SECONDS AND BACK TO AUTO. AUTO FAIL LIGHT WENT OUT. NR 2 CONTROLLER FFR SHOWED OFV LRU FAIL FAULT. CURRENT BITE TEST OF SYSTEM. 1 & 2 PRESSURE CONTROLLERS TEST & RESAug 16, 2016 · N560AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2016072117597Floorbeam · corrodedFLOORBEAM AT BS 986.5 BL31R HAS CORROSION UPPER SURFACE. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-70-51. PERFORMED DVI IAW SRM 53-70-51. ACCOMPLISHED HFEC IAW NDT MANUAL 51-00-00, PROC .236 PT 6 NO CRACK INDICATIONS. FABRICATED REPAIR PARTS, SPOT FACEDJul 21, 2016 · N560AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016072017494Support Angle · crackedFWD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500H, STRINGER 25L. ACFT GROUNDED. REMOVED & REPLACED THE SUPPORT ANGLE IAW DWG 143A7505 REV A & B, AND SRM 51-40-02.Jul 20, 2016 · N560AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016072017493Support Angle · crackedFWD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500G, STRINGER 25L. ACFT GROUNDED. REMOVED & REPLACED THE INTERCOSTAL SUPPORT ANGLE IAW DWG 143A7505 REV A, & SRM 51-40-02.Jul 20, 2016 · N560AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016072017492Support Angle · crackedFWD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT 500G, STRINGER 25R. ACFT GROUNDED. REMOVED & REPLACED THE INTERCOSTAL SUPPORT ANGLE IAW DWG 143A7505 REV A, B, AND SRM 51-40-02.Jul 20, 2016 · N560AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016072017491Support Angle · crackedFWD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT 500H, STRINGER 25R. ACFT GROUNDED. REMOVED & REPLACED THE INTERCOSTAL SUPPORT ANGLE IAW DWG 143A7505 REV A, B, & SRM 51-40-02.Jul 20, 2016 · N560AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016071817544Floor Panel · corrodedAFT CARGO FLOOR PANEL 140BF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG EDGES. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610 REV E, & PL 453A2610-32 REV D.Jul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817539Floor Panel · corrodedPARTS RACK, FORWARD CARGO FLOOR PANEL 120DF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG EDGES. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 120DF IAW DWG 453A1610-20, REV C AND SRM 53-30-58-0I, TABLE 2. ALODINE TREATED IAW DWG 453A1610-20, REV C AND SRM 51-20Jul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817530Floor Panel · corrodedPARTS RACK AFT CARGO FLOOR PANEL 140DF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG EDGES. ACFT GROUNDED. MATERIAL ID FOR FLOOR PANEL 140DF IS 2024-T3-071 IAW DWG 453A2610, REV K, PO 871290.2, FABRICATED, LOCATED AND DRILLED NEW FLOOR PANEL 140DF IAW DWG 453AJul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817529Floor Panel · corrodedPARTS RACK, FWD CARGO FLOOR PANEL 120CF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG EDGES. ACFT GROUNDED. MATERIAL ID FOR FLOOR PANEL 120CF IS 2024-T3, .071 IAW DWG 453A1610, REV PO 871290.2. FABRICATED, LOCATED AND DRILLED IAW DWG 453A1610, REV C, ALODINEDJul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817517Floor Panel · corrodedAFT CARGO FLOOR PANEL 140AF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG EDGES. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED IAW DWG 453A2610, REV C, ALODINED IAW SRM 51-20-01, PRIMED IAW SOPM 20-41-02, INSTALLATION ACCOMPLISHED ON W/O TASK CARD.Jul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817490Floor Panel · corrodedAFT CARGO FLOOR PANEL 140EF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG THE EDGES. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED A NEW FLOOR PANEL IAW DWG 453A2610, REV C.Jul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071817489Floor Panel · corrodedFWD CARGO FLOOR PANEL 120BF HAS SEVERAL LONG GOUGES, AND CORROSION ALONG THE EDGES. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610 REV E, ALODINED IAW SRM 51-20-01, PRIMED IAW 20-44-02.Jul 18, 2016 · N560AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016071717574Stop Fitting · gougedMAIN CABIN FORWARD ENTRY DOOR, AFT SIDE, LOWER STOP PIN GOUGED. ACFT GROUNDED. REMOVED AND REPLACED THE STOP FITTING IAW DWG 141A6101 REV-, PERFORMED DOOR ADJUSTMENT CHECKS IAW AMM 52-11-00-820-801.Jul 17, 2016 · N560AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2016071017330Knob · dirtyTHE GAIN AND TILT KNOBS ON THE RADAR CONTROL PANEL FOR THE CAPTAIN'S SIDE ARE JAMMED TOGETHER AND DO NOT FUNCTION PROPERLY. ACFT GROUNDED. GAIN AND TILT KNOBS STUCK TOGETHER DUE TO GRIME AND DIRT. CLEANED KNOBS AND CHECKED SYSTEM IAW AMM 34-43-00, GROUND FJul 10, 2016 · N560AS · Boeing 737890 · Weather Radar SystemSDR ASAA2016063017234Regulator · failedOBSERVED DUCT PRESSURE (RT ENGINE LESS THAN 18PSI THRU 50% N1) WHILE PERFORMING BLEED AIR CROSSOVER TEST. LEFT ENGINE OK. ACFT GROUNDED. HIGH STAGE REGULATOR FAILED BLEED AIR HEALTH CHECK T/C NG-36WC-0001. REPLACED HIGH STAGE REGULATOR IAW AMM 36-11-07. OPS CJun 30, 2016 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2016062917205Valve · failedWHILE ACCOMPLISHING ENGINE BLEED AIR CROSSOVER TEST FOUND HIGH DUCT PRESSURE ON THE NR 1 ENGINE. 20% =20 PSI, 30% = 30 PSI, 40% = 30 PSI, 50% = 32 PSI, 60% = 45 PSI, 70% = 65 PSI, 80% = 52 PSI REF. TSR 817767 NGS DEGRADED BLUE LIGHT ON/. ACFT GROUNDED. ACCOMPLJun 29, 2016 · N560AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2016062817197Shim · wornNR 2 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R 24 SHIMS, REF TASK CARD 78472002.Jun 28, 2016 · N560AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2016062717184Unknown · malfunctionedA/T WOULD NOT ENGAGE ON TAKEOFF AND FLIGHT, CLIMB, CRUISE, DESCENT. ACFT GROUNDED. PERFORMED A/T SERVO TEST, REF AMM 22-31-00. INITIALLY THROTTLE 1 FAILED TEST. CYCLED A/T DC-1 C/B. PERFORMED A/T SERVO TEST AGAIN AND A/T SYS OPS TEST MULTIPLE TIMES, REF AMMJun 27, 2016 · N560AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016062017097Servo · failedAUTOTHROTTLES WILL NOT STAY ENGAGED, TRIED ON TAKEOFF AND AGAIN DURING CLIMB. ACFT GROUNDED. R & R ASM-1 IAW AMM 22-31-91, OPS NORMAL. PERFORMED A/T SYSTEM, OPS TEST IAW AMM 22-31-00, OPS NORMAL. ETOPS GROUND VERIFICATION SUCCESSFUL.Jun 20, 2016 · N560AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016061117009Shim · wornNR 1 ENGINE REQUIRES NEW FAN BLADE SHIM 24 EA. ACFT GROUNDED. R & R NR 1 ENGINE FAN BLADE SHIMS IAW T/C 78472002.Jun 11, 2016 · N560AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016061117005Fmc · malfunctionedON LANDING ROLLOUT, SINGLE FMC OPS APPEARED WITH MAP & VTK FLAG ON F/O PFD. ACFT GROUNDED. POWERED DOWN ACFT, AFTER SEVERAL MINUTES POWERED UP ACFT, MAP & VTK FLAGS ON F/O'S PFD DID NOT REAPPEAR. ACCOMPLISHED FIM TASK 34-61-801, FMC SYS BITE, NO FAULTS NOTEJun 11, 2016 · N560AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016060816993Bulb · failedOUTPUT TEMP OF RT & LT PACKS ARE NOT THE SAME IN CRUISE FLIGHT. RIGHT PACK IS STABLE 22C. LEFT PACK VARIES FROM 0-10C IN A SLOW CYCLE. TRIM AIR ON. ACFT GROUNDED. R & R LT PACK TEMP BULB T488 IAW WDM 21-61-51. LEFT PACK TEMP INDICATION NORMAL.Jun 8, 2016 · N560AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016060416953Module · failedAFTER DEPARTURE ON CLIMBOUT THE ENGINE NR 2 OVERHEAT LIGHT CAME ON, FOLLOWED QRH PROCEDURES. AFTER BRINGING THROTTLE TO IDLE, LIGHT WENT OUT, RETURNED TO PSP. ACFT GROUNDED. REPLACED ALL 4 NR 2 ENGINE FIRE DETECTORS AND M279 MODULE, REF AMM 26-11-01, NO HELPJun 4, 2016 · N560AS · Boeing 737890 · Detection SystemSDR ASAA2016060416939Fire Warning · false activationWHEN STARTING ENGINE NR 2 WITH NR 2 LOOP B ON MEL, LOOP A SELECTED. THE ENGINE 2 OVERHEAT LIGHT ILUMINATED ON START AND EXTINGUISHED WHEN ENGINE WAS SHUTDOWN. ACFT GROUNDED. OPENED ENGINE NR 2 FAN COWLS & CHECKED LOOPS FOR OBVIOUS DEFECTS. NO DEFECTS NOTED. Jun 4, 2016 · N560AS · Boeing 737890 · Fire DetectionSDR ASAA2016060316937Wire Harness · damagedENGINE NR 2 OVERHEAT LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. ACFT GROUNDED. FIRE DETECTION UNIT BITE TEST. R & R MULTIPLE DETECTORS, M279 MODULE, AND WIRING HARNESS FOR WORK ACCOMPLISHED. OPS CHECK GOOD, NO DEFECTS NOTED.Jun 3, 2016 · N560AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2016052816867Autopilot Sys · malfunctionedJUST AFTER TOC A/P A DISCONNECTED. CAPTAIN HAPPENED TO OBSERVE A BRIEF FLICKER OF THE SOURCE OFF LIGHT ILLUMINATED FOR GENERATOR 2. MASTER CAUTION DID NOT ILLUMINATE. RECALL WAS CLEAR. RE-ENGAGED A/P A AND CONTINUED WITH OUT INCIDENT. ACFT GROUNDED. ACCOMPLISMay 28, 2016 · N560AS · Boeing 737890 · Autopilot SystemSDR ASAA2016052116803Warning Message · false activationZONE TEMP FOR CONT CAB ILLUMINATES ON RECALL AND EXTINGUISHES ON RESET. ACFT GROUNDED. PERFORMED PACK CONTROLLER BITE TEST, REF FIM 21-62, TASK 801. RAN LT PACK, FAULT INTERMITTENT, NO ZONE TEMP LIGHT. BITE TEST PASSED, NO HISTORY 60 DAYS.May 21, 2016 · N560AS · Boeing 737890 · Cabin Temperature Control System
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