N563AS

Service difficulty reports · 561

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 = 'N563AS' 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 ASAA2016090218066Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM AT STA 328, RBL 54. ACFT GROUNDED. REMOVED CORROSION AT RBL 54, ORIGINAL THICKNESS 0.125 IAW DWG 15189-1210, REMAINING THICKNESS 0.094, REMOVED 0.031, BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-10-51-1A-1, PAR 4, FIG 105Sep 2, 2016 · N563AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016090129740Floorbeam · corrodedFWD PIT, AFT SECTION , JUST BEFORE THE A/C BAY, FLOOR SUPPORT CHANNEL HAS CORROSION AT SEVERAL SPOTS. BS 500I LBL 21 - RBL 21. GROUNDED - YES. REMOVED CORROSION FROM FLOOR SUPPORT AT 500I, LBL 21 - RBL 21 IAW ASA B737-800 SRM 51-10-02, FLOOR SUPPORT FOUND TOSep 1, 2016 · N563AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016090118101Floorbeam · corrodedSTA 294, FLOORBEAM, WL208 UPPER T-CAP HAS CORROSION AT 3 LOCATIONS BLO+1R, BL0+6L, BL012L. ACFT GROUNDED. FOUND CORROSION TO BE OUT OF LIMITS, REPAIRED REF: EA 800-53EA-17749 AND REO-G20248, REV B, DOT REMOVED.Sep 1, 2016 · N563AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016090118065Floor Support · damagedFLOOR SUPPORT AT STA 277 TO FLIGHT DECK FLOOR, BL 12L HAS SCRIBE LINE ON TOP SURFACE. ACFT GROUNDED. R & R 141A5670Y12 FLOOR SUPPORT TEE AT BS 277 LBL12 IAW SRM 51-40-02 AND DWG 141A5600, REV N. REMOVED AND REINSTALLED PULLEY BRACKETS ADJACENT TO FLOOR SUPPSep 1, 2016 · N563AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090118009Skin · crackedFOUND 2.5" CRACK ON RT HORIZONTAL LOWER SKIN AT THE REAR SPAR, STABILIZER STA 96. ACFT GROUNDED. CUTOUT DAMAGE ON LOWER SKIN IAW SRM 55-10-01-2R-11 MATERIAL ID FOR REPAIR FILLER 2024-T3 .071, PO 870187.1 AND 2024-T3, .100, PO 871757.1. FABRICATED REPAIR FILSep 1, 2016 · N563AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016090118001Seat Track · corrodedAFT CARGO COMPARTMENT CROSS TEE ATTACH POINT TO RAIL RBL 13.84 AT BS 772 HAS EVIDENCE OF CORROSION ON TOP SURFACE OF RAIL. MARKED AND STREAMER ATTACHED. ACFT GROUNDED. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02 AND CPM 20-40-00 ORIGINAL THICKNESS ISep 1, 2016 · N563AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2016090118000Shield · corrodedAFT CARGO COMPARTMENT FLOOR TRANSITION PANEL BETWEEN BS 796 AND BS 794.37 HAS EVIDENCE OF CORROSION AROUND FASTENER HOLE, MARKED. ACFT GROUNDED. REMOVED CORROSION FROM TRANSITION SHIELD ASSY AT BS 767-794 IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRSep 1, 2016 · N563AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090117999Transition Panel · corrodedAFT PIT, RT TRANSITION PANEL HAS CORROSION AT SEVERAL SPOTS, BS 727-BS 727H. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO RT TRANSITION PANEL IAW SRM 51-10-02, ORIGINAL THICKNESS .040 REMOVED .007 REMAINING THICKNESS .033" FOUND TO BE OUT OF LIMITS IAW SRSep 1, 2016 · N563AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090117953Floorbeam · corrodedFWD CARGO AFT SECTION , JUST BEFORE THE A/C BAY, FLOORBEAM HAS CORROSION AT SEVERAL SPOTS. BS 500I LBL 21 - RBL 21. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A FIG 103 DETAIL D. REMOVED AND REPLACED IAWSep 1, 2016 · N563AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016090117941Skin · crackedFOUND 1.5" CRACK ON LT HOROZONTAL LOWER SKIN AT STAB STA 138.7, 24.5" AFT OF FORWARD SPAR. GROUNDED - YES. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 55-10-01-2R-11. APPLIED TOPCOAT TO REPAIR AREA IAW AMM 51-21-Sep 1, 2016 · N563AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016090117927Floorbeam · corrodedAFT CARGO BAY FLOORBEAM TEE AT BS 772 HAS EVIDENCE OF CORROSION ON TOP AND BOTTOM SURFACE. ACFT GROUNDED. REMOVED THE CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMIITS IAW SRM 53-00-53, REPLACED IAW SRM 51-40-02 & DWG 146A7500 REV B.Sep 1, 2016 · N563AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016090117890Channel · corrodedFWD CARGO BAY RIGHT TRANSITION PANEL HAS CORROSION AT SEVERAL SPOTS. BS 500 - 500I, RBL 21. ACFT GROUNDED. REMOVED CORROSION IAW 51-10-02, FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A, FIG 103 DET D. REPAIRED IAW SRM 51-10-02, SRM 53-00-53-2R, SRM 53-30-53-0Sep 1, 2016 · N563AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016081717743Pump · failedFUEL DRIPPING FROM THE BOTTOM COWL OF NR 1 ENGINE. ACFT GROUNDED. WHILE ACCOMPLISHING ENGINE DRAINS AND VENTS INSPECTION WITH ENGINE RUNNING FUEL STARTED TO LEAK OUT FROM THE HMU ATTACHMENT TO THE FUEL PUMP AT STEADY RATE AND ALSO FROM THE FUEL PUMP PAD DRAAug 17, 2016 · N563AS · Boeing 737890 · Engine Fuel PumpSDR ASAA2016081417696Controller · malfunctionedAUTO FAIL AMBER LIGHT ILLUMINATED AND ALTN GREEN ON PREFLIGHT. ACFT GROUNDED. RESET THE CABIN PRESSURE CONTROLLER IAW AMM 21-31-TASK 801 B ITEM C. BITE PROCEDURE FOR EXISTING FAULT CLEARED.Aug 14, 2016 · N563AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2016080817644Fmc · malfunctionedDURING TAXI IN, BOTH FMC S SHOWED VTK AND FMC WAS REMOVED FROM CDU MENU. AFTER SEVERAL SECONDS ALL FUNCTIONS RETURNED TO NORMAL. ACFT GROUNDED. FMC LANDING & TAXI VTK MAP NUISANCE ERROR, IAW AMM 34-51-00. AIRCRAFT OKAY FOR CONTINUED SERVICE.Aug 8, 2016 · N563AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016080717638Control Panel · failedMCP ALTITUDE SELECTORS IS NOT WORKING PROPER AND CHANGING ALTITUDE ON ITS OWN. DIFFICULT OR IMPOSSIBLE TO MAKE SELECTIONS. ACFT GROUNDED. ACCOMPLISHED DFCS BITE TEST, NO FAULTS LOGGED. REMOVED & REPLACED DFCS MCP AS A PRECAUTION, IAW AMM 22-11-34/401. ACCOAug 7, 2016 · N563AS · Boeing 737890 · Autopilot SystemSDR ASAA2016080617614Satcom · malfunctionedSATCOM LOCKUP GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Aug 6, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016080317603Sensing Element · faultyR1 WINDOW OVERHEAT LIGHT ILLUMINATED ON APPROACH. DID NOT RESET. ACFT GROUNDED. ACCOMPLISHED BITE CHECK IAW FIM 30-41, TASK 801. FOUND WHCU RT FORWARD WINDOW SENSOR FAULT. SWITCHED ALT SENSOR IAW FIM 30-41, TASK 812.Aug 3, 2016 · N563AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2016062317144Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Jun 23, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016062117112Cdu · failedF/O`S FMC CDU HAS A PURPLE LINE ON THE RT SIDE. ACFT GROUNDED. ON INITIAL POWER UP NO PURPLE LINE WAS VISIBLE. WHEN SCREEN WAS TOUCHED, SEVERAL PURPLE LINES APPEARED AND SCREEN WAS DISTORTED. REPLACED FMC CDU, ALL OPS NORMAL, REF AMM 34-61-01.Jun 21, 2016 · N563AS · Boeing 737890 · Central DisplaySDR ASAA2016062117111Warning System · false activationTEMPORARY FMC FAILURE ON CAPTS SIDE VTK DISPLAYED FOLLOWED BY MAP FAILURE FLAGS. RETURNED TO NORMAL AFTER ABOUT 60 SECONDS, QRH REFERENCED BUT RETURNED TO NORMAL BEFORE SWITCHES WERE MOVED. ACFT GROUNDED. REF FIM 34-61, TASK 801, PERFORMED FMC BIT TEST. NOJun 21, 2016 · N563AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016061817062Unknown · malfunctionedLOST BOTH FMC, VTK FLAG BOTH SIDES, FOLLOWED BY A/T LIMIT. AFTER 30 SECONDS, LT AND RT FMC CAME BACK. ACFT GROUNDED. VERIFIED NR 1 AND NR 2 FMC RESET ON FLT LEG 1 DURING NR 1 AND NR 2 FMC BITE, REF FIM 34-61,TASK 801. NO CURRENT FAULTS ON NR 1 OR NR 2 FMC.Jun 18, 2016 · N563AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016061117007Shim · wornREF TASK CARD 78472002, FAN BLADE SHIMS WORN ON NR 2 ENGINE. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE SHIMS IAW TASK CARD 78472002.Jun 11, 2016 · N563AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016052516847Control Panel · failedMC PANEL, F/O'S COURSE DIGITAL READOUT FIRST DIGIT SHOWS SEGMENTS OF OTHER NUMBERS WHEN ON 1 & 3. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED DFCS MODE CONTROL PANEL IAW AMM 22-11-34-400-801, TEST PASSED. ALSO ACCOMPLISHED DFCS LRU REPLACEMENT TEST FOR MCP May 25, 2016 · N563AS · Boeing 737890 · Autopilot SystemSDR ASAA2016051416714Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.May 14, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016050716635Warning Light · false activationZONE TEMP FOR CONTROL CABIN ILLUMINATES WITH RECALL AND EXT WITH MASTER CAUTION RESET. CHECKED & REL IAW MEL 21-21F FLIGHT DECK PRI TEMP CONTROL INOPERATIVE. ACFT GROUNDED. PERFORMED FIM 21-62, TASK 832 AND FAULT CLEARED. GROUND FUNCTIONAL CK GOOD REF FIM May 7, 2016 · N563AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016042016477Satcom · malfunctionedHAD SATCOM LOCKOUT IN FLIGHT. PERFORMED QRH PROCEDURES. REGAINED SATCOM. ACFT GROUNDED. ACCOMPLISHED FIM 23-15, TASK 801, STEP 4B. SYSTEM CHECKS NORMAL.Apr 20, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016041316385Compensator · failedREF FQIS BITE GROUND TEST SHOWS HARD FAULT MSG 28-41208 FOR NR 2 TANK. DUE TO FAULT HISTORY, REQUIRES SYS DEFERRAL. ACFT GROUNDED. R & R COMPENSATOR UNIT, REF AMM 28-41-21-400-801. COMPENSATOR CAPACITY IS 57.8 PF. THIS CLEARS MEL 28-6B. LEAK CHECK GOOD, REApr 13, 2016 · N563AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016040916301Satcom · lockedSATCOM LOCKUP DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH, SATCOM OPS NORMAL.Apr 9, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016040516249Starter · failedNR 2 ENGINE NO ROTATION ON START. ACFT GROUNDED. R & R NR 2 ENGINE STARTER REF AMM 80-11-01. OPS GOOD. LEAK CHECKS GOOD.Apr 5, 2016 · N563AS · Boeing 737890 · Engine StarterSDR ASAA2016032516082Warning Light · false activationCONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED AFTER ENGINE START AND BLEEDS ESTABLISHED. ACFT GROUNDED. RELEASED IAW MEL 21-21F. PRIMARY FLIGHT DECK CONTROLLER INOPERATIVE. COMPLIED WITH AMM TASK 21-61-00-700-806-002. FAULT RESET AND CABIN ZONE TEMP LIGHT Mar 25, 2016 · N563AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016032316069Fmc · failedAFTER LANDING BOTH MCDU'S DISPLAYED THE MENU PAGE WITHOUT AN FMC PROMPT. FMC PROMPT LATER RETURNED WITH ALL DATA LOST. ACFT GROUNDED. FMC BITE LT & RT FAULTED LT FMC, WHILE ATTEMPTING OPS CHECK, LT FMC FAILED AGAIN. R & R LT FMC COMPUTER REF AMM 34-61-02. AMar 23, 2016 · N563AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016032016032Autoland Sys · malfunctionedREQUESTED AUTOLAND HGS APPROACH UNSUCCESSFUL, AUTOPILOT DISENGAGED AT 5 FT APPROXIMATELY. ACFT GROUNDED. ACCOMPLISHED FAULT REVIEW IAW FIM 22-11, TASK 801, GP 20, NO FAULTS LOGGED. ALSO ACCOMPLISHED DFCS LAND VERIFY TEST, GP 49, IAW AMM 22-11-00/201 AND HMar 20, 2016 · N563AS · Boeing 737890 · Autopilot SystemSDR ASAA2016031916012Indicator · failedFUELER REPORTED RIGHT HAND PANEL RIGHT HAND INDICATOR NUMBER FLASHING. GROUNDED - YES. REMOVED AND REPLACED NR 2 REFUEL QTY INDICATOR IAW AMM 28-41-61/401. FUELING INDICATION, OPS TESTED NORMAL.Mar 19, 2016 · N563AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2016031115867Satcom · lockedSATCOM LOCK-UP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS NORMAL.Mar 11, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016030315760Fmc · malfunctionedRT FMC FAILED MOMENTARILY THEN RESTORED ITSELF PRIOR TO ANY ACTION. ACFT GROUNDED. RT FMC OPS TEST OK. REF AMM 34-61-00-710-801, NO DEFICIENCIES NOTED IN FAULT HISTORY EITHER. ETOPS GROUND VERIFICATION COMPLETE.Mar 3, 2016 · N563AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016030215730Lamp · failedLEFT FWD OVERWING EXIT, EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R LT FWD OVERWING EXIT EMERGENCY LIGHT, OPS CHECK GOOD.Mar 2, 2016 · N563AS · Boeing 737890 · Emergency LightingSDR ASAA2016030215729Warning Message · illuminatedFQIS SHOW NR 2 TANK DEGRADE ATA 28-41208, REF AMM 28-41-00. ACFT GROUNDED. TRANSFERRED FUEL AND BARREL DRAINED NR 2 TANK. REMOVED LARGE QTY OF WATER VIA SUMP. RETESTED FQIS WITH NO DISCREPANCIES NOTED. NO FAULTS. GROUND TEST PASS. SYS OPS NORMAL, REF AMM Mar 2, 2016 · N563AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016022715666Satcom · malfunctionedNO SATCOM INDICATION ON MENU PAGE FOLLOWING POWER CHANGE. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURES IAW QRH. SATCOM OPS NORMAL.Feb 27, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016022315643Control Unit · failedNR 1 ENGINE WOULD NOT START. ACFT GROUNDED. NO IGNITOR WAS HEARD DURING TEST REF AMM 74-00-00-750-801-F00. R & R NR 1 ENGINE LT AND RT INGITOR BOXES, DURING OPS TEST RT IGNITOR FAILED CHANNEL B TEST. R & R NR 1 ENGINE ELECTRONIC ENGINE CONTROL REF AMM 73-2Feb 23, 2016 · N563AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2016022215626Satcom · malfunctionedON CLIMBOUT OF OGG NOTED NO, SATCOM, PROMPT IN MCDU. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURES IAW QRH. ALL OPS NORMAL.Feb 22, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016021715559Engine · malfunctionedNR 1 ENGINE WOULD NOT START, WHEN START LEVER RAISED TO IDLE FF APPROXIMATELY 1.75, BOTH FUEL SHUTOFF LIGHTS GO OUT. AFTER A FEW SECONDS THE ENGINE VALVE CLOSED ILLUMINATED, NO LIGHT OFF. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROL BITE PROCEDURE IAWFeb 17, 2016 · N563AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016021115412Sensor · dirtyCONTROLLER CABIN ZONE TEMP ON RECALL. ACFT GROUNDED. PERFORMED NR 2 PACK TEMP ZONE BITE AND FOUND TRIM AIR MOD VALVE FAULT ON FLIGHT HISTORY BUT COULD NOT DUPLICATE FAULT IN VERIFY MODE OF BITE, NUMEROUS ATTEMPTS. FOUND CONTROL CABIN TEMP SENSOR AND FILTER DFeb 11, 2016 · N563AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016020115230Satcom · lockedSATCOM LOCK UP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURES IAW QRH. SATCOM RESTORED NORMAL.Feb 1, 2016 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2016012615026Warning Message · false activationWHILE PERFORMING DFCS BITE, LIBRARY 32, FAULT CODE 22-11126 FOUND. ACFT GROUNDED. ACCOMPLISHED FIM 22-12, TASK 812, NO FAULTS. ACCOMPLISHED LANDING, VERIFY NO FAULTS. GROUND VERIFICATION SUCCESSFUL, IAW AMM 22-00-01-730-801.Jan 26, 2016 · N563AS · Boeing 737890 · Autopilot SystemSDR ASAA2016012615024Warning Message · false activationDURING MASTER CAUTION RECALL CONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED. RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMP CONT BITE TEST. FAULT RESET AND DID NOT RECUR AMM 21-61-00-700-806-002. GROUND VERIFICATION SUCCESSFUL.Jan 26, 2016 · N563AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016010914676Valve · failedON MASTER CAUTION RECALL CONTROLLER CABIN ZONE TEMP ILLUMINATES, RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. NR 2 PACK/ZONE TEMP CONT BITE INDICATES FLT DK TRIM VALVE FAULT, REF AMM 21-61-00. REPLACED FLIGHT DECK TRIM VALVE, INSTALLATION TEST NORMAL REFJan 9, 2016 · N563AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015123114597Sensor · failedR2 WINDOW OVERHEAT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. CYCLED SWITCH MULTIPLE TIMES TO ALLOW COOLING, OVERHEAT LIGHT WOULD ALWAYS COME BACK ON AFTER COOLING PERIOD WHEN R2 WINDOW HEAT SWITCH RESELECTED ON. ACFT GROUNDED. FOUND PRIMARY WINDOW HEAT SEDec 31, 2015 · N563AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2015122914543Satcom · malfunctionedNO SATCOM PROMPT ON MCDU MENU PAGE GROUNDED. FOLLOWED QRH PROCEDURE AND SAT PROMPT RETURNED.Dec 29, 2015 · N563AS · Boeing 737890 · Communications SystemSDR ASAA2015122514443Warning Message · false activationFMC DIAGREE ON GROUND. ACFT GROUNDED. CLEARED WITH QRH PROCEDURE.Dec 25, 2015 · N563AS · Boeing 737890 · Flight Management Computing Hardware System
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