N530AS

Service difficulty reports · 357

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 = 'N530AS' 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 ASAA2017122723013Fcu · faultedFURTHER EVALUATION OF APU COLD SOAKED START WITH FAULT IAW ENGINEERING REQUEST, PERFORMED APU BITE IAW AMM 49-61-00. ONE FAULT FOUND. STARTS OLD FAULT 49-31016 OVERTEMP SHUTDOWN. ACFT GROUNDED. PERFORMED FIM 49-30, TASK 803, STEP B 1-3. LOOKED FOR BLOCKADec 27, 2017 · N530AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2017122523059Indication Sys · out of tolerancePERFORMED TASK CARD 78273000, NR 2 ENGINE HAS FAULT 77-20862; THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE, ECONOMIC FAULT. ACFT GROUNDED. REPLACED EGT TEMP PROBE T495S3 FOR #2 ENGINE REF B737-800 AMM 77-21-01. PERFORMED EEC TEST REF AMM 73-21-00-700-Dec 25, 2017 · N530AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2017121122909Connector · looseREF T/C 78273000 # 2 ENG MAINT FAULT 77-20862 (THE BOTTOM LEFT EGT SIGNAL IS OUT OF RANGE) - ECONOMIC FAULT. GROUNDED - YES. PERFORMED AN INPUT MONITORING CHECK OF THE #2 ENGINE T49.5 PROBES PER B737-800 FIM 77-21 TASKS 803 AND 805. FOUND S3 BLANK, WITH AN Dec 11, 2017 · N530AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2017120822860Indicator · false indicationAFTER SHUTDOWN, RED BOX ON #2 ENGINE EGT GAUGE. GROUNDED - YES. PERFORMED AN INPUT MONITORING CHECK OF THE #2 ENGINE T49.5 PROBES PER B737-800 FIM 77-21 TASKS 803 AND 805. FOUND S3 BLANK, WITH AN ASSOCIATED FAULT 77-20862 ON LEGS 3 AND 4. PERFORMED A T49.5 PRODec 8, 2017 · N530AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2017120822843Connector · dirtyGE DIAGNOSTICS REPORTS #2 ENGINE TREND DATA SHOWS A SUDDEN DELTA EGT INCREASE AND EGT HDM DECREASE. EGT INDICATION ERRORS ARE SUSPECT. GROUNDED - YES. ACCOMPLISHED T/C 78273000. #2 ENGINE SHOWS MAINT MSG. 77-20862 "THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OFDec 8, 2017 · N530AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017113022755Wire Harness · failedWHILE PERFORMING T/C 78273000 FOUND MAINT MSG NBR 77-20862 FOR NO#2 ENGINE. THIS IS AN ECONOMIC FAULT (THE BOTTOM LEFT EGT IS OUT OF RANGE, CT495S3). GROUNDED - YES. ACCOMPLISHED T/C 78273000. #2 ENGINE SHOWS MAINT MSG 77-20862 "THE BOTTOM LEFT EGT SIGNAL (T49Nov 30, 2017 · N530AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2017111722617Indicator · failedFUELER FOUND CENTER GAGE INDICATOR INOP. GROUNDED - YES. REMOVED AND REPLACED CENTER REFUELING INDICATOR, OPS NML REF AMM 28-41-61-400-801. THIS CLEARS MEL 28-12B.Nov 17, 2017 · N530AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2017111622608Circuit Breaker · trippedNR 2 ENGINE HPSOV CONTROLLER AND HPSOV INDICATOR CIRCUIT BREAKERS FOUND TRIPPED DURING PRE-FLIGHT. ACFT GROUNDED. INSPECTED THE NR 2 ENGINE HPSOV CONTROLLER AND HPSOV INDICATOR CIRCUIT BREAKERS ON P6-3 E3, E4. NO DEFECTS NOTED, RESET THE CIRCUIT BREAKERS IAWNov 16, 2017 · N530AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2017111222526Warning System · false activationAFTER APU START "MAINT" BLUE LIGHT ILLUMINATED. GROUNDED - YES. SHUTDOWN APU. ACCOMPLISHED APU BITE CHECK PER FIM 49-60 TASK 801. FAULT READ LOW OIL QUANTITY. VISUALLY CONFIRMED AT APU OIL SIGHT GAUGE THAT OIL LEVEL IS FULL. PERFORMED APU BITE CHECK AGAIN - OINov 12, 2017 · N530AS · Boeing 737890 · APU Indicating SystemSDR ASAA2017101392183Probe · dirtyFAULT CODE 77-20862 THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE ECONOMIC DEFERRED PER T/C 78273000. GROUNDED - YES. DEFERRED CODE PLT, ECONOMIC FAULT 500 FLT HRS, DEFERRED PER T/C 78273000. FOUND T49.5 S3 SIGNAL TEMP HAD ALL DASHES WHEN LOOKING AT CONOct 9, 2017 · N530AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2017100722159Sensor · dirtyGE DIAGNOSTICS REPORTED THE NR 2 ENGINE TREND DATA SHOWS A SUDDEN DELTA EGT INCREASE AND EGT HDM DECREASE. EGT INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. ACCOMPLISHED EGT CLEANING IAW AMM 77-21-00-140-801. BEFORE TEMPS: S1/44.39, S2/19.19, S3/18.56, S4/43Oct 7, 2017 · N530AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017100722135Unknown · unknownDURING TAXI IN, THE CAPTAIN`S SIDE FMC FAILED WITH VTK ON DISPLAY. RAN THE QRH, PG 11.3 AND CONFIRMED THAT THE LEFT FMC FAILED. ACFT GROUNDED. OPS CHECKED THE CAPTAIN`S FMC SYSTEM, CHECKED GOOD IAW AMM 34-61-00.Oct 7, 2017 · N530AS · Boeing 737890 · Navigation SystemSDR ASAA2017092822065Warning Light · noneZONE TEMP CONTROL CABIN ILLUMINATED ON MASTER RECALL. LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62 TASK 842. NO FAULTS. PACK OPS NORMAL IAW AMM. 21-00-00.Sep 28, 2017 · N530AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017092722058Idg · leakingWHILE ACCOMPLISHING TSR818719, FOUND THE NR 1 IDG LEAKING OIL FROM CONNECTOR PLUG DP1205 FLANGE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE IDG ASSEMBLY IAW AMM 24-11-11. OPS CHECKED NORMAL IAW AMM 24-11-00-700. OK FOR SERVICE.Sep 27, 2017 · N530AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2017090821864Coupler · failedUNABLE TO RECEIVE RECEPTION VOLUME OR SIDE TONE ON HF 1 ON ANY FREQUENCY. HF 2 WORKS NORMALLY. ACFT GROUNDED. R & R THE NR 1 & 2 HF COUPLER IAW AMM 23-11-61-000-801, & AMM 23-11-61-400-801. OPS CHECKED OK.Sep 8, 2017 · N530AS · Boeing 737890 · Communications System WiringSDR ASAA2017090121790Connector · damagedLEFT TRANSFER BUSS OFF LIGHT ILLUMINATED AND NR 1 ENGINE DRIVEN GENERATOR DROPPED OFF BUSS. COMPLIED WITH QRH PROCEDURE AND COMPLETED FLIGHT WITH APU POWERING LEFT BUSSES. ACFT GROUNDED. PERFORMED FIM 24-21, TASK 818. FOUND OPEN BETWEEN PINS 6-7, AND 7-1 ONSep 1, 2017 · N530AS · Boeing 737890 · Electrical Power System WiringSDR ASAA2017082621722Fmc · inoperativeFIRST OFFICER`S FMC P/RST LIGHT DOES NOT CLEAR WHEN CLEARED FROM LEFT OR RIGHT MCDU KEYPAD. ACFT GROUNDED. REMOVED & REPLACED THE NR 1 FMC IAW AMM 34-61-02. OPS CHECKED NORMALAug 26, 2017 · N530AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017081221614Sliding Window · failedRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. RAN QRH PROCEDURE, LIGHT ILLUMINATED AGAIN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 SLIDING WINDOW IAW AMM 56-12-11/401. WINDOW OPS CHECKED AND LEAKS CHECKED GOOD IAW WDM 30-41-11, MOVED TERMINAL TO TAB 2 Aug 12, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017081221616Warning Light · false activationRT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURES, LIGHT EXTINGUISHED, DID NOT COME BACK ON.Aug 12, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017081221613Warning Light · false activationRIGHT SIDE WINDOW OVERHEAT LIGHT. EXTINGUISHED AFTER PERFORMING QRH PROCEDURE. ACFT GROUNDED. OPS CHECKED THE RT WINDOW HEAT, NORMAL IAW AMM 30-41-00-710-801.Aug 12, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017081121615Warning Light · false activationRIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. LIGHT EXTINGUISHED.Aug 11, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017080921588Controller · failedRIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED, ON LIGHT EXTINGUISHED ON SHORT FINAL. LIGHT EXTINGUISHED AND ON LIGHT RETURNED DURING TAXI IN. ACFT GROUNDED IAW AMM 30-41-11/401. REMOVED WHCU M320. REMOVED WHCU M322 AND INSTALLED IT ON M320 POSITION FOR THAug 9, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017080721569Warning Message · false activationR2 WINDOW OVERHEAT ILLUMINATED IN FLIGHT. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. R2 WINDOW HEAT OPS RESTORED TO NORMAL.Aug 7, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017080621553Hf Comm · malfunctionedDURING PREFLIGHT, THE HF 2 SELECTED BOTH ACTIVE AND STANDBY FREQUENCIES SHOWING FAILED WITH NO SIDE TONE OVER SPEAKER. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 803. HF 2 BITE TESTED OK, IAW FIM 23-11, TASK 801. INTERMITTENT FAULT IAW FIM. GROUND VERIFICATION Aug 6, 2017 · N530AS · Boeing 737890 · HF Communications SystemSDR ASAA2017080621551Transceiver · failedHF 2 RADIO DISPLAYS FAIL ON BOTH ACTIVE & STANDBY FREQUENCY WITHOUT SIDE TONE TRANSMISSION. ACFT GROUNDED. PERFORMED A BITE CHECK IAW FIM 23-11-801, NO FAULTS. REMOVED AND REPLACED NR 2 HF TRANSCEIVER IAW AMM 23-11-21-000-801 AND 23-11-21-400-801. NO FURTHERAug 6, 2017 · N530AS · Boeing 737890 · HF Communications SystemSDR ASAA2017080521545Probe · no testNR 2 ENGINE MAX POWER ASSURANCE EGT INDICATION IS HIGH AT 65% N1. INDICATION ERROR IS SUSPECTED: S1 = 535, S2 = 558, S3 = 697, S4 = 545. ACFT GROUNDED. INITIAL EVAL UPON RETURN TO HANGAR: T495 = 126.91, S1-113.05, S2-88.53, S3-195.05, S4-109.14. ACCOMPLISHEAug 5, 2017 · N530AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017073121505Warning Light · false activationCAPT REPORTS F/O'S SLIDING WINDOW OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH AND F/O'S SLIDING WINDOW HEAT FUNCTIONED NORMALLY AFTER THAT. ACFT GROUNDED. PREFORMED GROUND TEST OF RT SLIDING WINDOW HEAT SYSTEM IAW AMM 30-41-00-701-801. GROUND TESTED OK.Jul 31, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017072521466Window · malfunctionedAT FL 370, THE RIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. RAN QRH, TURNED SWITCH OFF FOR 3 MINUTES. TURNED SWITCH BACK AFTER APPROX 6 MINUTES OVERHEAT LIGHT CAME BACK ON. TURNED SWITCH OFF FOR THE REMAINDER OF THE FLIGHT. ACFT GROUNDED. PRESSURIZED AIRCJul 25, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017070721311Warning Light · false activationAFTER PUSH BACK DURING MASTER CAUTION RECALL THE MACH TRIM FAIL LIGHT ILLUNINATED AND TURNS OFF WHEN MASTER CAUTION SYSTEM RESET. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 801, MT FAIL LIGHT ON WHEN MASTER CAUTION SWITCH IS PUSHED. CHECKED GOOD. OPS NORMAL. Jul 7, 2017 · N530AS · Boeing 737890 · Autopilot SystemSDR ASAA2017062321175Warning Light · malfunctionedRIGHT SIDE WINDOW OVERHEAT LIGHT REMAINED EXTINGUISHED AFTER RUNNING QRH. ACFT GROUNDED. ACCOMPLISHED R2 WINDOW HEAT SYSTEM OPERATIONAL TEST IAW AMM 30-41-00-710-801, TESTED PASSES. REF TSR818563 FOR CORRECTIVE ACTION: WHCU BITE LOGGED 4 WINDOW SENSOR FAULTSJun 23, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017062221176Warning Light · false activationRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. QRH PROCEDURE COMPLETED, LIGHT EXTINGUISHED. ACFT GROUNDED. TURNED ON WINDOW HEAT ALL GREEN ON LIGHTS ILLUMINATED IAW AMM 30-41-41-860-007.Jun 22, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017061621109Control Unit · failedRIGHT SIDE WINDOW OVERHEAT ILLUMINATED. RAN QRH. DID NOT ILLUMINATE AGAIN. OVERHEAT OCCURRED DURING CLIMBOUT AROUND 18000 FT, TEMPERATURE ON THE GROUND WAS 34DEG C AT AIRPORT. ACFT GROUNDED. REMOVED AND REPLACED THE RT WINDOW HEAT CONTROL UNIT IAW AMM 30-41-Jun 16, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017061421078Actuator · malfunctionedRIGHT A/C PACK LIGHT ILLUMINATED DURING DESCENT, RECALL RT PACK LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. REPLACED THE NR 2 RAM AIR INLET ACTUATOR IAW AMM 21-51-21. OPS CHECKED GOOD. REPLACED THR NR 2 RAM AIR CONTROL TEMP SENSOR IAW AMM Jun 14, 2017 · N530AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017061221041Wire Harness · malfunctionedRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED DURING CLIMB THROUGH 19,000 FT. WINDOW HEAT RESET AFTER 5 MINUTES COOLING. ACFT GROUNDED. INSPECTED RT SIDE SLIDE WINDOW HEATER RESISTANCE AND FOUND WITHIN LIMITS AND THE PAT IS SET AT THE CORRECT POSITION IAW WDJun 12, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017060821011Indicator · failedCENTER FUEL REFUELING QUANTITY INDICATOR IS BLANK. FLT DECK READS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED REFUELING CENTER TANK INDICATOR, OPS NORMAL IAW AMM 28-41-61-400-801.Jun 8, 2017 · N530AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017060821003Warning Light · false activationRIGHT A/C PACK LIGHT ILLUMINATED ON MASTER CAUTION PRE FLIGHT CHECK. ACFT GROUNDED. PACK-ZONE TEMPERATURE CONTROLLER BITE TEST DONE ON THE RT AND LT SIDE IAW AMM 21-61-00-700-806-002. BITE TESTED GOOD.Jun 8, 2017 · N530AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017060821002Warning Light · false activationON RECALL PRIOR TO DESCENT, RIGHT PACK LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. RIGHT PACK LIGHT EXTINGUISHED.Jun 8, 2017 · N530AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017060620982Warning Message · false indicationHF 2 RADIO FREQUENCY SHOWS FAILED. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 801, COMMS SYSTEM BITE PROCEDURE. NO FAULTS NOTED. OPS NORMAL.Jun 6, 2017 · N530AS · Boeing 737890 · HF Communications SystemSDR ASAA2017060420959Sliding Window · failedAT 10,000 FEET DURING DESCENT, RECEIVED AN R2 WINDOW OVERHEAT LIGHT. RAN CHECKLIST, LIGHT WENT OUT. ACFT GROUNDED. WINDOW HEAT SYSTEM TEST COMPLETED IAW AMM 30-41-00-710-801, TESTED GOOD. WHCU BITE COMPLETED IAW FIM 30-41, TASK 801. BITE HISTORY SHOWS WINJun 4, 2017 · N530AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA2017060420945Indicator · malfunctionedFUELER REPORTED THE CENTER TANK REFUEL QUANTITY INDICATOR IS BLANK. ACFT GROUNDED. PERFORMED RESET OF 2 CIRCUIT BREAKERS FOR CENTER TANK REFUEL QUANTITY INDICATOR. CENTER TANK INDICATOR POWERED ON. PERFORMED OPS TEST OF REFUEL QUANTITY PANEL. OPS TESTED GOODJun 4, 2017 · N530AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017060220946Control Unit · failedRIGHT SIDE WINDOW R2 OVERHEAT DURING DESCENT. QRH RESET NOT SUCCESSFUL. ACFT GROUNDED. REMOVED AND REPLACED R2 WINDOW HEAT CONTROL UNIT IAW AMM 30-41-11. TESTED GOOD.Jun 2, 2017 · N530AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017052520899Exciter · faultedAPU FAULT LIGHT ON START. FOLLOWED QRH PROCEDURES. STILL HAD FAULT LIGHT. ACFT GROUNDED. ON APU START UP, FOUND FAULT 49-41180, IGNITION UNIT CIRCUIT SHOWS HIGH CURRENT. IAW FIM 49-40 TASK 804, REPLACED EXCITER UNIT IAW AMM 49-41-31. TO ADDRESS PREVIOUS FAULMay 25, 2017 · N530AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2017052120844Hf Comm · lockedNR 1 HF INOP. GROUNDED - YES. PERFORMED BITE CHECK, REF AMM 23-11 TASK 801. PERFORMED BITE OF BOTH HF TRANSCEIVERS. FOUND NR 1 LOCKED. CYCLED POWER TO NR 1 SYSTEM. PERFORMED OPERATIONAL SYSTEM TEST, SYSTEM OPS CHECK NORMAL ON GROUND. GROUND VERIFICATION CHECKSMay 21, 2017 · N530AS · Boeing 737890 · HF Communications SystemSDR ASAA2017052020838Warning Light · false activationNR 2 PACK LIGHT ON, RECALL, EXTINGUISHES AFTER RESET. ACFT GROUNDED. RT PACK TEMP CONTROL INOPERATIVE. PERFORMED PACK, ZONE TEMP CONTROL BITE TEST IAW AMM 21-61-00-700-806-002. RAM AIR ACTUATOR WAS FAULTED ON PREVIOUS LEG. PERFORMED FIM 21-53 TASK 804, May 20, 2017 · N530AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017050720699Seal · damagedNR 1 ENGINE CHIP DETECTOR INDICATION. ACFT GROUNDED. ACCOMPLISHED AMM 79-00-00-200-804-F00 H. (7)(L)(2)(B). FOUND DAMAGE TO AIR/OIL SEAL. ENGINE REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 1 ENGINE.May 7, 2017 · N530AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2017042920569Connector · looseAPU INOP, NO ROTATION WITH FAULT LIGHT ON. GROUNDED - YES. APU BITE SHOWS NUMEROUS "NO FLAME SHUTDOWN" MSG 49-41011 AND "FCU RESOLVER CIRCUIT SHOWS BAD" MSG 49-31175. CONFIRMED FAULT, APU NO ROTATION INOP FOLLOWED BY FAULT LIGHT. ACCOMPLISHED FIM 49-32 TASK 80Apr 29, 2017 · N530AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2017042720555Warning Light · illuminatedSTAB OUT OF TRIM LIGHT ON IN DESCENT FL 330 DISENGAGED AP AND HAND FLEW. ACFT GROUNDED. PERFORMED FIM 22-11 TASK 801 DFCS BITE PROCEDURE FAULT HISTORY SORTED BY FLIGHT DECK EFFECT FOUND FAULT CODE 22-11177 PRIMARY STAB TRIM ELEC ACTUATOR. PERFORMED LR TEST FOApr 27, 2017 · N530AS · Boeing 737890 · Autopilot SystemSDR ASAA2017042620536Warning Light · false activationDURING DESCENT, PRESSED RECALL AND RECEIVED A RIGHT PACK LIGHT ILLUMINATION. IAW LIST PRESSED MASTER CAUTION, LIGHT EXTINGUISHED CONTINUED TO DESTINATION. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE IAW AMM 21-51-00-700-803. NR 2 CONTROLLER SApr 26, 2017 · N530AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017041120483Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN HAS CRACK INDICATION INBD OF RIB STA 147.90. ACFT GROUNDED. REMOVED THE DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, FIG 204, REPAIR 11.Apr 11, 2017 · N530AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016122019110Warning Message · false activationSINGLE PDC OPERATION MESSAGE. APPROXIMATELY 5 MINUTES LATER RIGHT NAVIGATION DISPLAY LOST NAVIGATION DISPLAY OR NAVIGATION COURSE MAGENTA LINE. FOLLOWED QRH, FMC BOTH ON 1. ALL DATA RESTORED TO NORMAL. ACFT GROUNDED. PERFORMED BOTH FMC BITES IAW FIM TASKDec 20, 2016 · N530AS · Boeing 737890 · Flight Management Computing Hardware System
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