JASC 2210

Service difficulty reports · 4,016

Reports filed under 2210 · Autopilot System, 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 jasc_code = '2210'
  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 SWAA2015041638589Control Panel · malfunctionedDECLARED EMER, MCP LOCKUP. 20,000 FEET IN DESCENT AUTOPILOT DISENGAGED & ALL MODES FROZEN. NO TIME TO ATTEMPT MCP RESET BEFORE APPROACH & LANDING. RESET MODE CONTROL PANEL IAW MM.Apr 13, 2015 · N630WN · Boeing 7373H4SDR SIMA20150408002Actuator · failedUNCOMMANDED RUDDER MOVEMENT WITH NO INDICATION ON EICAS. RUDDER LIMIT APPEARED ON FLIGHT CONTROL PAGE. RUDDER PEDALS DID NOT MOVE WITH RUDDER MOVEMENT & RUDDER INDICATION WAS NOT MOVING EITHER. RTF DECLARED EMER. TRANSFERRED TO NRWC 512-ORD-01953. R & R LApr 8, 2015 · N512AE · Cndair CL6002C10SDR ASAA2015032511117Control Panel · malfunctionedMCP DIGITS DO NOT DISPLAY, EVEN WITH "LIGHTS TEST" SELECTED. ACFT GROUNDED. CYCLED CB'S FOR MCP, P18-1, D5, MCP, DC1 AND P6-2, C3, MCP DC2 AND DIGITS DISPLAYED. PERFORMED MCP INSTALLATION TEST IAW MM 22-11-34. ALL TESTS PASSED. NO HISTORY 30 DAYS. GROUND VMar 25, 2015 · N402AS · Boeing 737990ERSDR ASAA2015032511116Control Panel · malfunctionedCAPTAIN'S COURSE SELECTOR ON MCP IS BLANK. COURSE INFORMATION IS STILL SHOWING ON NAV DISPLAY. ACFT GROUNDED. COULD NOT DUPLICATE PROBLEM. EXITING CREW FROM LAST FLIGHT VERBALIZED MCP CAPT COURSE WINDOW NORMAL. OPS, NO BLANKING. NO HISTORY LAST 30 DAYS. Mar 25, 2015 · N570AS · Boeing 737890SDR ASAA2015032411103Autopilot Sys · malfunctionedAFTER 4TH DISCONNECT AUTOPILOT A SELECTED APPROXIMATELY 3.5 HRS INTO FLIGHT AT FL 360 AUTO PILOT B DISCONNECTED NO INDICATION OF CAUSE FOR FIRST DISCONNECT LATER IN FLIGHT AUTO PILOT B DISCONNECTED 2 MORE TIMES AT 3RD DISCONNECT A VERY BRIEF SPEED LIMIT OR SPEMar 24, 2015 · N517AS · Boeing 737890SDR ASAA2015031710992Actuator · faultedAUTOPILOT B CHANNEL INOPERATIVE, AILERON SURFACE TEST FAILED 60.31. ACFT GROUNDED. WHILE PERFORMING TC 7822200, FMS FUNCTION CHECK. SURFACE TEST FAILED FOR AILERON 60.31 CHANNEL B. FAULTS 22-11340 AND 22-11146 WERE LOGGED. ALL OTHER LIBRARY GROUP TESTS PASMar 17, 2015 · N512AS · Boeing 737890SDR ASAA2015031710991Autoland Sys · malfunctionedAUTOLAND NOT SUCCESSFUL, 40' LT OF CENTERLINE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE PROCEDURE FIM 22-11, TASK 801. NO FAULTS LOGGED CURRENT STATUS AND PREVIOUS 15 LEGS. PERFORMED LANDING, VERIFY TEST IAW MM 22-11-00. ALL TESTS PASS.Mar 17, 2015 · N596AS · Boeing 737890SDR ASAA2015031610981Control Panel · faultedIN CRUISE AT FL 37.0 AUTOPILOT DISENGAGED IN A TURN RE-ENGAGED WITH NO FURTHER ACTION. ACFT GROUNDED. FLT FAULT REVIEW SHOWS "MCP DATA INVALID ", B CHANNEL HAS HISTORY BOTH A & B CHANNELS. REPLACED MCP, REF MM 22-11-34. PERFORMED BITE GPS NR 32, 49 LAND VERIMar 16, 2015 · N569AS · Boeing 737490SDR ASAA2015031410944Autopilot Sys · unknownAUTOPILOT B DISENGAGED TWICE IN CRUISE FLIGHT WITHOUT ANY PILOT INPUT. ACFT GROUNDED. ACCOMPLISHED DFCS BITE NR 49 LAND VERIFY TEST. PASSED GROUND VERIFICATION SUCCESSFUL.Mar 14, 2015 · N569AS · Boeing 737490SDR FDEA201503130917Computer · malfunctionedDURING CLIMB OUT AT 16K FEET, ENGAGED AP 1 & RECEIVED STAB OUT OF TRIM LEVEL 2. RAN QRH & LEVEL 2 DID NOT GO AWAY. TRIM SEEMED TO BE MOVING ON AP1, BUT LEVEL 2 WAS STILL THERE, ON AP 2 THE AUTOPILOT WOULD DISENGAGE. AFTER LANDING LEVEL 1 SEL LSAS RIB OFF Mar 13, 2015 · N604FE · Doug MD11FSDR ASAA2015031110920Autopilot Sys · malfunctionedAFTER APPROXIMATELY 2 HRS AT CRUISE, AUTOPILOT CMD A DISENGAGED ON ITS OWN WITH NO INADVERTENT PILOT ACTION. ACFT BEGAN AA GENTLE 200'-300' CLIMB THAT WAS ARRESTED IN 20. ACFT HAND FLOWN BACK TO ASSIGNED ALTITUDE, RETRIMMED VERY SLIGHTLY, NOSE DOWN. A/P ENGAMar 11, 2015 · N569AS · Boeing 737490SDR AALA20150309003Transmitter · faultedAUTOPILOT DISENGAGED ON APPROACH. AN EMERGENCY WAS NOT DECLARED, LANDED UNEVENTFULLY. REMOVED AND REPLACED LEFT ENGINE PRESSURE RATIO TRANSMITTER PER AMM 77-11-02.Mar 8, 2015 · N9401W · Doug DC983SDR ANCF2015030802Yaw Damper · faultedAFTER ENG 1 START ECAM AUTO FLT YAW DAMPER 1 FAULT. COMPUTER RESET WAS PERFORMED UNSUCCESSFUL. IAW AMM 22-91-00-710-001-A AFS GND SCAN WAS PERFORMED UNSUCCESSFUL. IAW MEL 22-63-01-1 CAT C, THIS ITEM WAS DEFERRED TO DMI 495. IAW AMM 27- 60-00-040-001 THE YAMar 8, 2015 · N266CT · Airbus A319112SDR ASAA2015030610876Transmitter · failedON CLIMBOUT NEITHER AUTOPILOT A OR B WOULD STAY ENGAGED. AFTER SEVERAL SECONDS OF BEING ENGAGED THE AUTOPILOT WOULD DISENGAGE WITH AN ABRUPT TURN TO THE RIGHT. ACFT GROUNDED. FOUND BAD AILERON POSITION SENSOR. REPLACED SAME REF MM 22-11-29-000-801 & -400-8Mar 6, 2015 · N536AS · Boeing 737890SDR ASAA2015030610875Transmitter · failedWHILE ACCOMPLISHING, TC 78222000 GROUND FUNCTIONAL TEST 60.31 FAILS WITH MAINTENANCE MESSAGE 22-11159, SPOILER POSITION 9. ACFT GROUNDED. FOUND NR 9 SPOILER POSITION SENSOR OUT OF ADJUSTMENT AT NEUTRAL. ADJUSTED NR 9 SPOILER POSITION SENSOR REF AMM 22-11-27Mar 6, 2015 · N568AS · Boeing 737890SDR ASAA2015030310839Control Panel · malfunctionedON DESCENT IAS/MACH BUG FROZE AS WELL AS MODE CONTROL PANEL READOUT. CYCLING FLIGHT DIRECTORS DIDN'T WORK NOR DID SWITCHING TO APU GENERATOR. AFTER LANDING, IAS/MACH RETURNED TO NORMAL OPS. GROUNDED - YES. PERFORMED BITE LIBRARY TEST OF DFCS,(A1/A2) LIBRARY TEMar 3, 2015 · N532AS · Boeing 737890SDR ASAA2015022810797Transmitter · failedMCP SPEED FROZEN WHEN SPEED WINDOW IS OPEN. ACFT GROUNDED. NR 9 SPOILER POSITION SENSOR "A" & "B" CHANNELS SPREAD BETWEEN VALUES TOO WIDE. REPLACED NR 9 SPOILER POSITION SENSOR, ADJUSTED, AND TESTED. TESTS PASS. REF AMM 22-11-27-400-801, 22-11-27-820-801 & Feb 28, 2015 · N532AS · Boeing 737890SDR SWAA2015052539958Control Panel · malfunctionedAIR TURN BACK, MODE CONTROL PANEL ALTITUDE LOCKED SHOWING 50000' FEET. R & R MODE CONTROL PANEL IAW MM.Feb 22, 2015 · N559WN · Boeing 73773VSDR ASAA2015022010716Autoland Sys · failedAUTOLAND FAIL. ACFT TOUCHED DOWN APPROXIMATELY 35' LT OF CENTERLINE. ACFT GROUNDED. TEST IAW FIM 22-11, TASK 825, LAND VERIFY TEST PASSES REF AMM TASK 22-11-00-700--801. NO FAULTS. NO PREVIOUS HISTORY LAST 30 DAYS.Feb 20, 2015 · N461AS · Boeing 737990ERSDR ASAA2015022010715Autoland Sys · malfunctionedON GLIDE SLOPE CAPTURE, "A" AUTOPILOT NOSED OVER AT APPROXIMATELY 5-6 DEGREES IAW SECOND, LEVEL AT 3000 FT 4 DEGREES NOSE UP TO 1 DEGREE NOSE DOWN IN A SECOND, TO CAPTURE GLIDE SLOPE. GLIDE SLOPE CAPTURE WAS AT 1 DOT LOW. NOSE OVER BEGAN TO DIVERGE FROM GS TFeb 20, 2015 · N592AS · Boeing 737890SDR RU3A20140219008Selector · malfunctionedPILOT MODE SELECTOR PANEL & AUTO PILOT CONTROL PANEL STARTED FLASHING. PF FELT WHAT WAS BELIEVED TO BE AN UNCOMMANDED ENGAGING & DISENGAGING, BUMP OF THE YAW DAMPER IN THE RUDDER PEDALS. REPLACED MODE SELECTOR & AP MODE CONTROLLER.Feb 19, 2015 · N73 · Beech 300BEECHSDR CA150217001Fmc · failed(CAN) EN-ROUTE IN CRUISE, CREW EXPERIENCED A SIMULTANEOUS FMGC FAILURE. A RESET WAS SUCCESSFULLY CARRIED OUT. MTC CONTROL WAS ADVISED. REPLACED FMGC NR 2 IAW AMM 22-83-34PB401. CAT III LAND TEST CARRIED OUT, CHECKED SERVICEABLE.Feb 16, 2015 · Airbus A319114SDR CA150216003Computer · failed(CAN) AFTER TAKEOFF AT 300 AGL, WHEN AUTO PILOT WAS SELECTED ON, FLIGHT DIRECTOR COMMANDED A 30 DEGREE LEFT TURN IGNORING THE FMS SID. MTC CONTROL ADVISED. INBOUND FLIGHT DECK EFFECTS SHOWED NO FAULTS RELATED TO AUTOPILOT. PERFORMED AFDS SYS TEST, PASSED NOFeb 16, 2015 · Boeing 777333ERSDR CA150224026Computer · failed(CAN) UN-COMMANDED HARD RIGHT ROLL WITH AUTOPILOT ON. CAPTAIN OVERCAME THE ROLL BY FORCING THE CONTROL TO THE LEFT. AUTOPILOT DID NOT DISCONNECT. ACFT THEN ROLLED TO THE LEFT UN-COMMANDED. CAPTAIN FORCED THE CONTROL TO THE RIGHT TO CENTER THE ACFT. AP REMFeb 11, 2015 · Cndair CL6002B19SDR AALA20150211006Control Panel · faultyAIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, THE AUTOPILOT PUSH TO RESET LIGHT ILLUMINATED & FIRST OFFICER’S FLIGHT DIRECTOR DISAPPEARED & ALL MODE CONTROL PANEL DISPLAYS WENT BLANK. R & R MODE CONTROFeb 11, 2015 · N941AN · Boeing 737823SDR ASAA2015020310533Autopilot Sys · malfunctioned"B" AUTOPILOT VERTICAL SPEED FUNCTION STICKS AND WILL NOT ADJUST CLIMB RATE EITHER UP OR DOWN. "A" AUTOPILOT WORKS GOOD "B" AUTOPILOT WORKS IN OTHER MODES OF CLIMB AND DESCENT. ACFT GROUNDED. PLANNING RECOMMENDED MCP PART CHANGE PRECAUTIONARY. REPLACED MCP IFeb 3, 2015 · N589AS · Boeing 737890SDR ASAA2015013010482Autopilot Sys · inoperativeUNABLE TO ENGAGE B AUTOPILOT. A AUTOPILOT FUNCTIONS PROPERLY. ACFT GROUNDED. OPENJan 30, 2015 · N558AS · Boeing 737890SDR ASAA2015013010484Circuit Breaker · trippedF/O'S COURSE WINDOW IS BLANK. ACFT GROUNDED. FOUND MCP 1 CIRCUIT BREAKER OUT ON P18-1 AND YAW DAMP 1 DC CIRCUIT BREAKER OUT. ACCOMPLISHED CIRCUIT BREAKER RESET PROCEDURE REF 20-61-00. NO DEFECTS NOTED. MCP TEST NORMAL REF. 22-11-34. ACFT REMAINS CAT IIIA AJan 30, 2015 · N469AS · Boeing 737990ERSDR ASAA2015012910483Circuit Breaker · trippedAFCS SYS A WARNING LIGHT, BAT, CIRCUIT BREAKER TRIPPED IN FLIGHT. ACFT GROUNDED. FFR SHOWS NO FAULTS LAST LEG. CHICKED BEHIND P18-1 PANEL FOR CONTAMINATION OR DEFECTS, NONE NOTED. RESET CIRCUIT BREAKER IAW MM 20-60-01. ACCOMPLISHED LAND VERIFY, DFCS OPS NORMJan 29, 2015 · N537AS · Boeing 737890SDR ASAA2015012810462Autopilot Sys · malfunctionedAUTOPILOT WAS ENGAGED. SELECTED B FOR AUTOLAND, A AUTOPILOT THEN DISCONNECTED. RENGAGED A AUTOPILOT AND BOTH SHOWED ENGAGED BUT SINGLE CHANNEL ONLY. DISCONNECTED AND LANDED NORMALLY. ACFT GROUNDED. CURRENT STATUS DOES NOT SHOW ANY FAULTS. FLIGHT HISTORY DOEJan 28, 2015 · N564AS · Boeing 737890SDR ASAA2015012610440Warning System · false activationACFT WAS ALIGNED WITH THE LT EDGE OF THE RUNWAY DURING AUTOLAND AT APPROXIMATELY 100 FT. RECEIVED APPROACH WARNING AT 50 FT. ACFT GROUNDED. TROUBLESHOT IAW FIM REF 22-11, TASK 825. PERFORMED LAND VERIFY TEST IAW AMM TASK 22-11-00-700-801. TEST PASSED NO FAJan 26, 2015 · N419AS · Boeing 737990ERSDR UIEA2015012600011Autopilot Sys · disconnectedENCOUNTERED MOUNTAIN WAVE & AIRSPEED INDICATED. ACCOMPANIED BY SIREN. AUTOPILOT DISCONNECTED & ACFT RETURNED TO NORMAL PARAMETERS. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-03, ALL FOUND TO BE NORMAL, NO DEFECTS NOTED.Jan 26, 2015 · N718BA · Boeing 7474H6SDR ASAA2015012510413Control Panel · failedF/O COURSE DISPLAY ON MCP IS BLANK. COURSE DOES DISPLAY ON F/O ND APP MODE ON EFIS SELECT SWITCH, KNOB. ACFT GROUNDED. R & R DFCS MCP IAW AMM 22-11-34, OPS NORMAL. PERFORMED DFCS LRU INTERFACE TEST FOR MCP AMM 22-11-34, LAND VERIFY TEST IAW AMM 22-11-00, ANJan 25, 2015 · N569AS · Boeing 737490SDR RU3A20140123004Control Cable · frayedAILERON AUTOPILOT SERVO CABLE FRAYED FROM CONTACT WITH GUARD POST. REPOSITIONED CAPSTAN GUARD POSTS TO ALLOW FOR CLEAR MOVEMENT OF CABLE.Jan 23, 2015 · N73 · Beech 300BEECHSDR CA150126001Cable · broken(CAN) DURING CRUISE FLIGHT, AILERON TRIM LWD EICAS CAUTION POSTED INTERMITTENTLY AND AUTOPILOT CONTROL WAS REPORTED UNRELIABLE ON LEFT TURNS. PILOT DISENGAGED AUTO PILOT TO HAND FLY THE AIRCRAFT AND CONTINUED TO HAVE FULL CONTROL (MINOR AILERON INPUTS ARE REQUJan 20, 2015 · Bombdr BD7001A10SDR ASAA2015012010321Autopilot Sys · malfunctionedAUTOPILOT NR 2 WOULD NOT ENGAGE AFTER ABANDONING APPROACH DUE TO ACFT ON RUNWAY-IT WAS WORKING FINE UNTIL CIRCLING BACK FOR NEXT APPROACH. ACFT GROUNDED. FFR LOGGED A/P DISC SW INV & MAIN ELECTRICAL TRIM. COULD NOT DUPLICATE MALFUNCTION. BITE GROUP NR 20 NJan 20, 2015 · N583AS · Boeing 737890SDR ASAA2015011910294Sensor · out of limitsWHILE ACCOMPLISHING ELEVATOR RIGGING TEST, FOUND ELEVATOR POSITION SENSOR VALUES OUT OF LIMITS. ACFT GROUNDED. ADJUSTED ELEVATOR POSITION SENSOR, REF MM 22-11-30-820-801. ADDITIONAL LWMP TESTS REQUIRED. ELEV POS SENSOR STILL FAILS ELECTRICAL RIGGING TEST. Jan 19, 2015 · N568AS · Boeing 737890SDR ASAA2015011310258Autoland Sys · malfunctionedLOW WEATHER/AUTOLAND HOUSING PERFORMANCE NOTED BELOW. ACFT TOUCHED DOWN LEFT OF CENTER LINE. RT MAIN ON RWY CENTERLINE. ACFT GROUNDED. ACCOMPLISHED FIM 22-11 TASK 825. OPS TEST GOOD. DFCS FAULT REVIEW & HGS FAULT REVIEW. SHOWS NO FAULTS. NO HISTORY LAST Jan 13, 2015 · N467AS · Boeing 737990ERSDR ASAA2015010910190Warning Light · false activationCAPTAIN'S PFD HAS AN AMBER "FD" INDICATION. ALSO, THE MCP CAPT SIDE F/D ON SWITCH/LIGHT WILL NOT INDICATE ON WHEN SELECTED FIRST. ALSO, AUTOPILOT A WILL NOT ENGAGE. ACFT GROUNDED. DUE TO FAULTY GATE POWER FCC-A FAULTED. TRANSFERRED TO APU POWER. FCC-A RETUJan 9, 2015 · N413AS · Boeing 737990ERSDR ASAA2015010810187Autoland Sys · malfunctionedAUTOLAND UNSATISFACTORY, AIRCRAFT DRIFTED TO THE RT AT APPROXIMATELY 100' FOLLOWED BY APPROACH WARNING. ACFT GROUNDED. FLIGHT FAULT REVIEW SHOWS NO FAULTS LOGGED. ACCOMPLISHED LAND VERIFY IAW FIM TASK 22-11, TASK 825. NO FAULTS. NO HISTORY LAST 10 DAYS. Jan 8, 2015 · N407AS · Boeing 737990ERSDR ASAA2015010410143Autoland Sys · malfunctionedPRACTICE AUTOLAND COMPLETED. ACFT TOUCHED DOWN OUTSIDE 35 FT CENTERLINE LIMIT SO DEEMED NOT SUCCESSFUL. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825, NO FAULTS AND LAND VERIFY NR 49 BITE TEST GOOD.Jan 4, 2015 · N419AS · Boeing 737990ERSDR ASAA2014122710065Control Panel · failedCONTROL PANEL INOPERATIVE. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL IAW AND CHECKED OK REF 22-11-34-400-801. LRU INTERFACE TEST 22-11-34-50, BITE GROUP NR 32. LAND VERIFY 22-11-00-201 BITE GROUP NR 49. HGS SENSOR TEST REF 34-36-00.Dec 27, 2014 · N471AS · Boeing 737990ERSDR ASAA2014121709989Warning Light · illuminatedAFCS UNTLK 2 ON P6-2 PANEL CIRCUIT BREAKER INOPERATIVE. ACFT GROUNDED. REF SWPM 20-00-10, NO DEFECTS NOTED, FLT CREW CHANGE, AFCS INTLK 2 CB CLOSED. ACCOMPLISHED LWMP SYS TABLE CFCS TESTS, LAND VERIFY, GROUP BITE 49, REF MM 22-11-00/201, AND HGS SYS TEST, REDec 17, 2014 · N462AS · Boeing 737990ERSDR CA141217016Actuator · failed(CAN) CREW REPORTED UNCOMMANDED YAW OSCILLATIONS IN FLIGHT, QRH PROCEDURES FOLLOWED AND WAY DAMPERS DISENGAGED BUT OSCULLATIONS CONTINUED. ADJUSTING RUDDER TRIM TENDED TO INCREASE OSCILLATIONS. THE ACFT LANDED WITHOUT EVENT. MAINT. REPLACED THE FCP, BOTH YAW Dec 15, 2014 · Cndair CL6002C10SDR ASAA2014121509959Circuit Breaker · trippedCIRCUIT BREAKERS ON P6-2 ROW B, NR 2 AND 3 TRIPPED. ACFT GROUNDED. RESET CIRCUIT BREAKER`S AFCS SYS B MACH TRIM DC AND FCC DC IAW AMM 20-60-01. PERFROMED FCC B INSTALLATION TEST IAW AMM 22-11-33-400-801. ALL TEST PASSED.Dec 15, 2014 · N590AS · Boeing 737890SDR CA141224006Cable · worn(CAN) DURING THE FIVE YEAR SCHEDULED FLIGHT CONTROL CABLE CHANGE, THE ELEVATOR CABLE IN THE FORWARD NOSE WAS FOUND TO BE INTERFERING ON THE STEC AUTOPILOT PULLEY CLUSTER. IT WAS HELD IN THIS INCORRECT POSITION BY A SCREW ON THE PULLEY GUARD CLUSTER. THE ELEVATDec 14, 2014 · Dhav DHC6300SDR ASAA2014121409945Computer · failedCAPTAIN`S FLIGHT DIRECTOR LIGHT ON AUTOPILOT PANEL INOPERATIVE, FD, FLAG ON CAPT ADI. CB P-18 D-1, WARN LIGHT (BAT), POPPED. ACFT GROUNDED. REPLACED FCC A COMPUTER, COMPUTER DEAD, REF MM 22-11-33-400-801. SOFTWARE CHECK GOOD IAW SAME IAW MM 20-60-01 CIRCUDec 14, 2014 · N589AS · Boeing 737890SDR CA141210004Control Panel · failed(CAN) ACFT DID AN IN-FLIGHT TURNBACK DUE TO FLT ALT WINDOW STUCK AT 5000 FT. MAINTENANCE TROUBLESHOT AND FOUND THE MODE CONTROL PANEL TO BE AT FAULT. MCP WAS REPLACED AND SYSTEM TESTED SERVICEABLE, WORK DONE IN ACCORDANCE WITH MM 22-11-34Dec 9, 2014 · Boeing 737*SDR ASAA2014120809897Warning Message · false activationSTAB OUT OF TRIM LIGHT ILLUMINATED, CONDITION WERE LEVEL FLAP 5 AUTO PILOT A ENGAGED. RAN CHECKLIST, AFTER A/P DISCONNECTED LIGHT EXTINGUISHED AND DIDN'T ILLUMINATE AGAIN. TRIM OPERATED NORMALLY. ACFT GROUNDED. ACCOMPLISHED STABILIZER MOTOR TEST IAW AMM REF Dec 8, 2014 · N506AS · Boeing 737890SDR R61A201412071221Autopilot Sys · malfunctionedCREW REPORTED THAT THE AUTO PILOT DISENGAGED AND SHORTLY AFTER RECEIVED SLAT FAIL, SHAKER ANTICIPATED, AP FAIL, AOA LIMIT FAIL AND SPOILER FAIL MESSAGES. CREW RAN QRH, CONTACTED MAINTENANCE CONTROL AND ELECTED TO CONTINUE. ABOUT 100 MILES FROM DESTINATION, CRDec 7, 2014 · N119HQ · Emb ERJ170200LR
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