N536AS

Service difficulty reports · 269

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 = 'N536AS' 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 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 737890 · Autopilot SystemSDR ASAA2015030310846Wire Harness · chafedWHILE ACCOMPLISHING TC 78472000, "ENG INLET AND FAN INSP" WIRE HARNESS FOR LPT ACCOMPLISHED, CHAFE DAMAGE FROM CONTACT WITH "C" DUCT HEAT BLANKET. ENGINE NR 1. ACFT GROUNDED. R & R NR 1 ENGINE J10 HARNESS IAW MM 73-21-06-400-802-F00 THROUGH STEP 5.F.,1, B. Mar 3, 2015 · N536AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2015030210830Valve · malfunctionedCONTROL CABIN ZONE TEMP LIGHT COMES ON DURING RECALL WITH MASTER CAUTION LIGHT. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMPERATURE CONTROLLER BITE TEST, NR 2 CONTROLLER INDICATES FLT DECK TRIM VALVE FAULT, REF MM 21-61-00-700-806-002. REPLACED FLT DECK TRIM Mar 2, 2015 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015030110819Converter · failedAPU INOPERATIVE: MAINT MGS 49-41251 START CONVERTER UNIT SHOW HIGH TEMPERATURE NO APU ROTATION SHUTDOWN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED START CONVERTOR UNIT IAW MM 49-41-61-400-801. TESTS PASSENGER ETOPS SIGNIFICANT SYSTEM GROUND VERIFICATION Mar 1, 2015 · N536AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2015021910684Sensor · intermittentNR1 ENGINE ACMS DATA SHOWS INTERMITTENT N2 VALUES FROM OIP REPORT 7. TAKEOFF AND CRUISE ACMS REPORTS SHOW NORMAL PARAMETERS. ACFT GROUNDED. REPLACED NR 1 ENGINE N2 SPEED SENSOR IAW MM 77-11-02. TESTS GOOD IAW POWER PLANT TEST REF TABLE MM 71-00-00-800-811-Feb 19, 2015 · N536AS · Boeing 737890 · Engine RPM Indicating SystemSDR ASAA2015020810587Warning Light · false activationLEFT PACK LIGHTS ILLUMINATES ON RECALL. PACK LIGHT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE CK ON PACK TEMP CONTROLLER AND PASS "GO" IAW MM 21-61-00-700-806-002. NO HISTORY 30 DAYS.Feb 8, 2015 · N536AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015020210509Warning Light · false activationON PUSHBACK RECEIVED A FMC DISAGREE LIGHT. ACFT GROUNDED. RAN CHECK LIST AND LIGHT WENT OUT.Feb 2, 2015 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014120909906Warning Light · false activationAFTER ENGINE START, DURING MASTER CAUTION RECALL THE COCKPIT ZONE TEMP LIGHT ILLUMINATED. THE LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. ACCOMPLISHED, FIM 21-62, TASK 848, NO FAULTS NOTED, NO HISTORY 30 DAYS.Dec 9, 2014 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014120609883Valve · unknownFOLLOW-UP TO NR 1 IDG FREQUENT SERVICING, ACFT GROUNDED. BAGGED NR 1 IDG, RAN FOR 10 MIN NO LEAKS NOTED. REPLACED NR 1 IDG VENT VALVE AND SERVICING FITTING IAW TSR AND AMM 24-11-00-700-804 TURN CHECK, LEAK CHECK GOOD, SERVICING GOOD, TO FULL.Dec 6, 2014 · N536AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2014101409384Warning Light · false activationAPU FAULT LIGHT ILLUMINATED DURING START. ACFT GROUNDED. INTERROGATED CPU, FOUND FAULT CODE 49-41251, START CONVERTER UNIT SHOWS HIGH TEMP. NO HISTORY LAST 90 DAYS. ACCOMPLISH TASK 49-40, TASK 812, THROUGH STEP E. 4, 2 TIMES. DID NOT GET EITHER FAULT CODE 4Oct 14, 2014 · N536AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2014092509229A/C Pack · faultedILLUMINATION OF THE FWD CABIN ZONE TEMP ON MASTER CAUTION RECALL. LIGHT EXTINGUISHES AFTER RESET OF MASTER CAUTION SYSTEM. ACFT GROUNDED. NR 2 ZONE TEMP CONTINUE LOGGED ZONE TRIM VALVE, BITE TESTED GOOD. FAULT RESET, IAW TASK 21-61-70-700-806-002.Sep 25, 2014 · N536AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014092309206Valve · failedFWD CABIN ZONE TEMP AMBER LIGHT ON OVERHEAD ILLUMINATED ON RECALL LANDING CHECK. MASTER CAUTION CLEARS ON RESET. ACFT GROUNDED. REPLACED FWD CABIN ZONE TRIM VALVE. OPS CHECKED GOOD. NO LEAKS NOTED.Sep 23, 2014 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014091809168Modulating Valve · failedAFTER START ON RECALL FWD CABIN ZONE TEMP LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. R & R FWD CABIN TRIM AIR MODULATING VALVE IAW AMM 21-61-21. OPS CK GOOD. PERFORMED BITE CK. BITE CK GOOD.Sep 18, 2014 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014091709146Warning Light · illuminatedDURING LANDING CHECKLIST AND MASTER CAUTION RECALL, FWD CABIN ZONE TEMP LIGHT ILLUMINATED. WHEN MASTER CAUTION RESET IS PUSHED, LIGHT GOES OUT. ACFT GROUNDED. NR 2 CONTROLLER LOGGED ZONE TRIM VALVE IN BIT. NO FAULTS IN PREVIOUS FLIGHT. ACCOMPLISHED ZONE TEMSep 17, 2014 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014081808883Warning Message · false activationFMC DISAGREE LIGHT ON GROUND. ACFT GROUNDED. CHECKLIST COMPLETED. FMC DISAGREE LIGHT EXTINGUISHED.Aug 18, 2014 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014080708790Warning Message · false activationMAP WARNING ANNUNCIATED ON F/O DISPLAY. ACFT GROUNDED. ACCOMPLISHED FIM TASK 34-61 NR 836. FMC OPS RESTORED. NO FAULTS LOGGED ON BOTH FMC. GROUND VERIFICATION CHECK OK. REALIGNED BOTH IRU LT AND RT FMCS. CHECKED OK.Aug 7, 2014 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014072208647Warning Message · false activationMAINTENANCE MESSAGE 49-37168 ON CURRENT STATUS PAGE. ACFT GROUNDED. VISUALLY INSPECTED APU HARNESS AND AC WIRING. DISCONNECTED AND INSPECTED P22 FCU. MEASURED RESISTANCE PINS 4 TO 5 = 110 OHMS. RECONNECTED P22 AND REACCOMPLISHED APU BITE-FAULT CLEARED.Jul 22, 2014 · N536AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2014070608466Lens · missingSMALL OVAL LIGHT OVERHEAD AISLE AT ROW 11C COVER MISSING. SMALL OVAL LIGHT OVERHEAD 17C IS CRACKED. ACFT GROUNDED. INSTALLED NEW EMERGENCY LIGHT LENS AT ROW 11C AND 17C REF MM 33-51-03, OPS NORMAL.Jul 6, 2014 · N536AS · Boeing 737890 · Emergency LightingSDR ASAA2014062808377Circuit Breaker · brokenWINDOW HEAT, OVERHEAT LIGHT ILLUMINATED RT INSIDE FORWARD WINDOW. ACFT GROUNDED. FOUND RT FWD WINDOW HEAT CIRCUIT BREAKER BROKEN. R & R CIRCUIT BREAKER, PERFORMED WINDOW HEAT CONTROL SYSTEM TEST, REF AMM 30-41-11-710-801.Jun 28, 2014 · N536AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2014060808101Satcom · malfunctionedSATCOM NOT AVAILABLE. ACFT GROUNDED. PULLED SATCOM CIRCUIT BREAKER & RESET, SAT PROMPTS APPEARED ON BOTH MCDU'S, OPS NORMAL, IAW FIM 23-15, TASK 801.Jun 8, 2014 · N536AS · Boeing 737890 · Communications SystemSDR ASAA2014060608092Sensor · failedNR 2 ENGINE ACMS DATA SHOWS INTERMITTENT N2 VALUES FROM OIP REPORT 07 DURING TAKEOFF/CRUISE. ACMS REPORTS SHOW NORMAL PARAMETERS. ACFT GROUNDED. REPLACED N2 SPEED SENSOR REF MM 77-11-02. BITE & LEAK CK OK.Jun 6, 2014 · N536AS · Boeing 737890 · Engine RPM Indicating SystemSDR ASAA2014051407813Warning Message · false activationFMC DISAGREE MESSAGE ON SCATCH PAD. ACFT GROUNDED. PERFORMED FIM 34-61, TASK 835. FMC DISAGREE MESSAGE REMOVED. TWO CIRCUIT BREAKERS OPENED, RESET FOR FIM P18-2 A6 & P6-1 D16. OPENED, RESET P6-1 D16 IAW FIM 34-61, TASK 835, OPS NORMAL. ETOPS GROUND VERIFICATMay 14, 2014 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014051207790Warning Light · false activationON APU START THE FAULT LIGHT CAME ON. RAN QRH WAITED 5 MINUTES. MADE ANOTHER ATTEMPT FAULT LIGHT CAME BACK ON. ACFT GROUNDED. ACCOMPLISHED INLET OVERHEAT SHUTDOWN FAULT PROCEDURE IAW TASK FIM 49-90, TASK 802 BY PULLING & CYCLING CIRCUIT BREAKERS. ORIGINAL FMay 12, 2014 · N536AS · Boeing 737890 · APU ControlsSDR ASAA2014051207788Sensor · failedAPU FAULT LIGHT CAME ON. WITHIN 5 MINUTES FAULT LIGHT WENT OUT. SHUTDOWN APU. ACFT GROUNDED. VERIFIED INLET TEMP SENSOR BAD, READS 300 OHMS PIN TO GROUND, IAW FIM TASK 49-60, TASK 812. REPLACED INLET TEMP SENSOR IAW AMM 49-61-31-000-801 AND 49-61-31-400-801May 12, 2014 · N536AS · Boeing 737890 · APU Indicating SystemSDR ASAA2014033107377Warning Light · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED DURING MASTER CAUTION RECALL, EXTINGUSHED WHEN RESET THE MASTER CAUTION. ACFT GROUNDED. TESTED CONTROLLER IAW MM 21-61-20, STEP F. SYSTEM OPS CHECKED GOOD. NO HISTORY IN LAST 60 DAYS.Mar 31, 2014 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014031207173Charger · faultedELECTRICAL LIGHT ILLUMINATED AFTER ENGINE START. ACFT GROUNDED. ACCOMPLISHED ELECRICAL. LIGHT MESSAGE BITE PROCEDURE, IAW AMM 24-31, TASK 801. FOUND BATTERY CHARGER INOPERATIVE. FAULT LIGHT CLEARED. ACCOMPLISHED AMM 24-31 TASK 824 BATTERY CHARGER SHOWS AMar 12, 2014 · N536AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014021606861Switch · damagedWHILE PERFORMING DUCT OVERHEAT SWITCH OPS TEST IAW NG-23EO-07569-2, FOUND OVERHEAT SWITCH DAMAGED. ACFT GROUNDED. REPLACED DUCT OVERHEAT SWITCH IAW AMM 21-61-05-400-801. OPS TESTED IAW AMM 21-61-00-700-811-002.Feb 16, 2014 · N536AS · Boeing 737890 · Overheat DetectionSDR ASAA2013121496867Start Valve · failedNR 1 START VALVE WOULD NOT OPEN, NO ROTATION, WHEN TRYING TO START THE NR 1 ENGINE. ACFT GROUNDED. FOUND NR 1 ENGINE START VALVE INOPERATIVE. REPLACED START VALVE & OPS AND LEAK CHECKED GOOD IAW AMM 80-11-03.Dec 14, 2013 · N536AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2013111396411Lamp · inoperativeEMERGENCY EXIT LIGHT UNDER L2 INOPERATIVE. ACFT GROUNDED. REPLACED LAMPS IAW AMM 33-51-04-960-801. OPS CHECKED GOOD IAW AMM 33-51-04-960-801.Nov 13, 2013 · N536AS · Boeing 737890 · Emergency LightingSDR ASAA2013111396410Controller · malfunctionedAFTER ENGINE START, ON MASTER CAUTION RECALL, CONT CABIN ZONE TEMP ANNUNCIATOR ILLUMINATED. ACFT GROUNDED. RESET NR 2 ZONE TEMP CONTROLLER IAW MM 21-60-00 AND 21-62 TASK 801.Nov 13, 2013 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013110796332Bleed Valve · no testNR 2 ENGINE PRSOV FAILED HEALTH CHECK. ACFT GROUNDED. REPLACED NR 2 ENGINE PRSOV OPS & LEAK CHECK GOOD IAW MM 36-11-04.Nov 7, 2013 · N536AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2013110696330Valve · no testNR 1 ENGINE HIGH STAGE VALVE FAILED HEALTH CHECK. ACFT GROUNDED. REPLACED NR 1 ENGINE HIGH STAGE VALVE IAW MM 36-11-06. OPS & LEAK CHECKS GOOD.Nov 6, 2013 · N536AS · Boeing 737890 · Engine Bleed Air SystemSDR ASAA2013081995846Fmc · false indicationFMC DISAGREE, ACFT GROUNDED. QRH COMPLETED, OPS NORMAL.Aug 19, 2013 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013080595738Sensor · failedRT SIDE WINDOW HEAT OVERHEAT WOULD NOT RESET AFTER COOLING. ACFT GROUNDED. WHCU SHOWS SENSOR FAULT. SWAPPED CORD WITH A NEW CORD- NO HELP. REF FIM TASK 30-41-00-810-811 SWAPPED PRIMARY SENSOR TO SPARE SENSOR TERMINAL WITHOUT REMOVING THE WINDOW, RT SIDE WHCUAug 5, 2013 · N536AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2013072295660Autothrottle Sys · malfunctionedAUTOTHROTTLES AT CRUISE CONTINUALLY DISENGAGE POSSIBLE SLIP, SPLIT IN MOVEMENT, NR 1 THROTTLE LEADS THEN TRIPS SYS OFF. ACFT GROUNDED. OPENJul 22, 2013 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013071395586Servo · inoperativeAUTOTHORTTLES DISENGAGED ON CLIMBOUT AND WILL NOT ENGAGE. ACFT GROUNDED. A/T FLT FAULT SHOWS ASM-1 RATE MONITOR FAULT. R & R ASM-1, REF 22-31-91. A/T CURRENT STATUS AND SERVO MOTOR BITE CHECKED GOOD.Jul 13, 2013 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013061595121Autothrottle Sys · inoperativeAUTOTHROTTLES WILL NOT STAY ENGAGED. ACFT GROUNDED. COULD NOT DUPLICATE, GROUND FUNCTIONAL TEST OK. A/T FAULT REVIEW LOGGED NR 1 ASM FAULT NR 22-31687 ON ONLY 1 FLT LEG OUT OF 40. ACCOMP FIM 22-32/819, A/T CURRENT STATUS CK & TORQUE CK NORMAL. ALSO ACCOMJun 15, 2013 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013042894655Circuit Breaker · noneAUTOTHROTTLE CIRCUIT BREAKER OPEN. ACFT GROUNDED. NO HISTORY OF CIRCUIT BREAKER TRIPPING LAST 30 DAYS. GVI OF CIRCUIT BREAKER PANEL, NO FAULT FOUND. A/T OPS TEST GOOD, REF AMM 22-31-00-710-801. ALL GROUND VERIFICATION TEST GOOD.Apr 28, 2013 · N536AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2013041794542Autothrottle Sys · faultyAUTOTHROTTLES WILL NOT REMAIN ENGAGED. A/T BITE SHOWS NUMEROUS ASM-2 FAULTS (22-31688 RATE MONITOR). REPLACED NR 2 AUTO THROTTLE SERVO MOTOR REF AMM TASK 22-31-91, OPS CHECKED NORMAL. ACCOMPLISHED A/T OPS TEST REF AMM 22-31-00/501 AND DFCS GP 49 LAND VERIFYApr 17, 2013 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013041194461Unknown · unknownON TAKEOFF, USED 27K BUMP FLAPS 25 BASED ON A POAT OF 29 DEG C AND PQNH OF 29.73 IN HG. PLANNED N1 WAS 102.4 AND BOX HAD 102.5. UPON SETTING N1 AFTER PRESSING TOGA, STARTED PUSHING THROTTLES FORWARD TO GET 102.4/102.5 BUT WAS GETTING 101.4 N1. CAPTAIN FIREWALLApr 11, 2013 · N536AS · Boeing 737890 · Engine Fuel and ControlSDR ASAA2013033094287Filter · malfunctionedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED DURING RECALL. EXTINGUISHES WHEN RESET IS PUSHED. PERFORMED BITE TEST ON BOTH ZONE TEMP CONTROLLERS. NR 2 ZONE TEMP CONTROLLER SHOWED FAULT FOR FLIGHT DECK TRIM VALVE. REPLACED CABIN TEMP SENSOR FILTER IAW AMM 21-6Mar 30, 2013 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013012893779Eec · faultyNR 1 ENGINE EEC BITE SHOWS SHORT TERM FAULT 73-20101. INTERNAL EEC FAULT LOGGED MULTIPLE TIMES IN LAST 10 LEGS. ACFT GROUNDED. ACCOMPLISHED T/S IAW FIM 73-21, TASK 807 - INITIAL EVALUATION CONFIRMED FAULT 73-20101 WITH NO OTHER FAULT CODES. REPLACED NR 1 ENJan 28, 2013 · N536AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2013010593610Valve · failedZONE TEMP LIGHT ON RECALL. PERFORMED PACK ZONE TEMP CONTROLLER BITE TEST ON NR 1 & 2 CONTROLLERS. NR 2 CONTROLLER FLIGHT DECK TRIM VALVE FAILED. RESET & VERIFIED TWICE. NO HISTORY FOR 90 DAYS. REF AMM 21-60-00.Jan 5, 2013 · N536AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2012122493523Warning Light · false activationFMC DISAGREE MESSAGE DISPLAYED ON GROUND. PERFORMED QRH, OPS NORMAL.Dec 24, 2012 · N536AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012121693474Autothrottle Sys · malfunctionedAUTOTHROTTLE FAILED ON TAKEOFF. WOULD NOT RE ENGAGE ON CLIMB OR CRUISE. NO CURRENT FAULTS AND LAST INFLIGHT FAULT WAS 8 FLIGHTS AGO. NO HISTORY LAST 30 DAYS. PERFORMED AUTOTHROTTLE CURRENT STATUS AND ALL INTERACTIVE TESTS IAW FIM 22-11 TASK 802, ALL OPS NODec 16, 2012 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012120593409Control Unit · faultedELEC LIGHT ILLUMINATED ON OVERHEAD ON PANEL. A/C POWER WAS REMOVED WHEN GROUND POWER WAS DISCONNECTED. VERIFIED SPCU FAULT. REPLACED SPCU. SYS TESTS GOOD REF TASK 24-34-11-700-801.Dec 5, 2012 · N536AS · Boeing 737890 · DC Generating SystemSDR ASAA2012111493302Switch · inoperativeAUTOTHROTTLE WILL NOT STAY ENGAGED. R & R NR 1 AUTOTHROTTLE SWITCH IAW AMM REF 22-31-51-000-801/22-31-51-400-801. OPS CHECKED GOOD. NO FAULTS LOGGED ON A/T INFLIGHT FAULTS, OR CURRENT FAULTS.Nov 14, 2012 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012111193285Servo · failedAUTOTHROTTLE DISCONNECTED ON TAKE OFF ROLL JUST AFTER PASSING 100 KTS. AFTER TAKE OFF, AUTOTHROTTLE WAS AGAIN ENGAGED AND WORKED FOR REMAINDER OF FLT. CURRENT STATUS TESTED GOOD AND SERVO TESTED GOOD, BUT SYS HAS PREVIOUS WRITE-UP AND THERE IS AN ASM-1 FAULTNov 11, 2012 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012110393224Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGES A FEW SECONDS AFTER ARMING THE AUTOTHROTTLE SWITCH. UNABLE TO DUPLICATE DEFECT. PERFORMED AUTOTHROTTLE OPS TEST IAW MM 22-31-00-710-801 AND AUTOTHROTTLE SYS TEST IAW MM 22-31-00-710-802. ALL TESTS PASS. ACFT IS QUALIFIED FOR CAT IIINov 3, 2012 · N536AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012101793148Indicator · activatedFOUND NR 2 ENG IDG DPI POPPED. ACFT GROUNDED. PERFORMED FIM TASK 24-11, TASK 803. COMPLETED T/C 78273000 FMC/CDU INTERROGATION. NO FAULTS LOGGED. COMPLETED T/C 78424000 IDG SCAVENGE/CHARGE FILTER INSP CHECK. NO CONTAMINATION NOTED. THIS IS DPI RESET NR 1. Oct 17, 2012 · N536AS · Boeing 737890 · AC Generator-Alternator
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