N529AS

Service difficulty reports · 344

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 = 'N529AS' 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 ASAA2015041511447Floor Support · crackedMAIN CABIN FLOORBEAM INTERCOSTAL STA 344 TO 360 LBL 12 IS CRACKED AT AFT FASTENER HOLE. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02, REF BAC DWG 141A5400, REV B, REMOVED DOT.Apr 15, 2015 · N529AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015041411443Skin · cracked1" CRACK INDICATION AT STABILIZER STA 184 2" AFT OF FRONT SPAR ON RT HORIZONTAL STABILIZER LOWER SKIN, MARKED IN RED. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLAISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, FIG 204, REPAIR 11 IS A CATEGORY B REPAIR, INSPECTION Apr 14, 2015 · N529AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015041411442Floorbeam · crackedMAIN CABIN FLOORBOARD SUPPORT CHANNEL CRACKED AT STA 540, LBL 2.0. ACFT GROUNDED. REMOVED MAIN CABIN FLOORBOARD SUPPORT CHANNEL AT STA 540, LBL 2.0 IAW SRM 51-40-02, LOCATED AND DRILLED NEW FLOOR SUPPORT CHANNEL IAW SRM 51-40-05, INSTALLED NEW FLOORBOARD SUPApr 14, 2015 · N529AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015041311432Floor Support · crackedMAIN CABIN FLOOR INTERCOSTAL HAS APPROX 1.2500" CRACK AT FASTENER HOLE IN UPPER FLANGE BS 344-360 BL 0. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-052, REF BAC DWG 1415400, REV B, REMOVED DOT.Apr 13, 2015 · N529AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015041111472Floor Panel · gougedPER CUSTOMER REP NED: FABRICATE NEW AFT CARGO COMPARTMENT FLOOR PANEL 140EF DUE TO SEVERAL DEEP GOUGES. GROUNDED - YES. FABRICATED NEW FLOOR PANEL 140EF AFT CARGO PIT IAW BAC DWG 453A2610 ALODINED AND PRIMED AIW B737-800 SRM 51-20-01.Apr 11, 2015 · N529AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2015040911291Fmc · malfunctionedTEMPORARY LOSS OF RT FMC APPROXIMATELY 4 + 25 MINUTES INTO FLIGHT. RESTORED TO NORMAL OPERATION WITHIN 2 MINUTES. ACFT GROUNDED. ACP FIM TASK 34-61-801. NO FAULTS LOGGED. GROUND VERIFICATION CK GOOD. REF AMM 34-61-00-710-801. NO PREVIOUS HISTORY IN 30 DAYSApr 9, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015040511248Shim · worn24 EA SHIMS WORN & MISSING COATING, NR 2 ENGINE. ACFT GROUNDED. R & R 24 EA SHIMS IN REF TASK CARD 78472002, NR 2 ENGINE.Apr 5, 2015 · N529AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015033111192Unknown · unknownWITH LIGHTS TEST SWITCH IN DIM, EXEC, CALL AND MSG LIGHTS ON CA MCDU FLASHED DIM TO BRIGHT APPROXIMATELY 60 CPS. OK IN BRIGHT. ACFT GROUNDED. UNABLE TO DUP/VERIFY DISCREPANCY. UPON ACFT POWER UP, REF MM 34-61-00, TEST OF THE ANNUNCIATORS OPS NORMAL W/ DIMMar 31, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015031710994Sign · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN AT RT FORWARD OVERWING EXIT IS BROKEN AND LENS IS MISSING. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED EXIT LOCATOR LIGHT ASSY AT RT FORWARD OVERWING EXIT IAW MM 33-51-01-960-802. OPS NORMAL.Mar 17, 2015 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2015022310753Keyboard · malfunctioned"OFST" LIGHT ON CAPTAIN'S FMC WILL NOT DIM WHEN COCKPIT LIGHTS ARE SELECTED DIM. ACFT GROUNDED. REPLACED THE MCDU KEYBOARD WITH NEW ONE. ACCOMP CDU LAMP TEST AND KEY TEST, BOTH PASS REF MM 34-61-01-400-801.Feb 23, 2015 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015011110225Power Supply · failedLIGHTS FROM SEATS ROWS 17-24 , L1 DOOR, AND FWD GALLEY CENTER LIGHTS FAILED TO STAY ILLUMINATED FOR 15 MINUTES. ACFT GROUNDED. R & R EMERGENCY POWER SUPPLIES REF WDM 33-51-22 AND 33-51-21. EMERGENCY LIGHTS OPS TEST NORMAL.Jan 11, 2015 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2014122710080Windshield · failedWINDOW HEAT "R" SIDE OVERHEATED TWICE. WOULD NOT RESET. ACFT GROUNDED. BITE TEST SHOWS SENSOR FAULT,IMMEDIATE, SWAPPED TO A/T SENSOR, TEST CABLE, DELAYED OVERHEAT W/SENSOR FAULT. HEATER RESISTANCE, D10572, PINS 3 & 4 = 59 OHMS, H15. CONFIRMED RT SLIDER WINDDec 27, 2014 · N529AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2014121209926Fmc · malfunctionedCAPTAIN`S FMC OFST ANNUNICATOR DOES NOT DIM WHEN LIGHTS SELECTOR SWITCH SELECTED TO DIM ALL SIDE BAR ANNUNNICATORS ARE BRIGHT. ACFT GROUNDED. TESTED CAPTAIN`S FMC OFST ANNUNCIATOR UNABLE TO DUPLICATE DEFECT AT THIS TIME, NO HISTORY IN LAST 60 DAYS.Dec 12, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014121009912Hf Comm · malfunctionedHF NR 1 RADIO IS INOPERATIVE. ACFT GROUNDED. PERFORMED HF COMM TEST IAW MM 23-11-00 730-801. SYSTEM OP CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.Dec 10, 2014 · N529AS · Boeing 737890 · HF Communications SystemSDR ASAA2014113009796Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL AND EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED AMM TASK 21-61-00-700-806-002. PACK/ZONE TEMP CONTROL BITE. NO FAULTS, NO HISTORY PAST 30 DAYS.Nov 30, 2014 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014102709517Light · inoperativeR1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R THE LIGHT IAW AMM 33-51-04-960. OPS CHECKED GOOD.Oct 27, 2014 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2014102309477Warning Message · false activationFMC DISAGREE, ACFT GROUNDED. REBOOTED IAW QRH.Oct 23, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014101309373Power Supply · inoperativeEMERGENCY AISLE LIGHTS AT ROWS 8 ABC AND 11 ABC INOPERATIVE. ACFT GROUNDED. REPLACED POWER SUPPLY AND BATTERY PACK, REF MM33-51-06 AND AREA LIGHT, AISLE LIGHT, ASSY AT ROW 8 ABC REF. MM33-51-03. TESTED- OPS. NORMAL.Oct 13, 2014 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2014091509134Charger · inoperativeDURING LANDING, ELECTRIC LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. CONFIRMED ELECTRIC LIGHT ON ON OVHD PANEL. FOUND BATTERY CHARGER FAULT WHILE PERFORMING TEST. PERFORMED FIM 24-31, TASK 824. NO FAULTS NOTED AT THIS TIME.Sep 15, 2014 · N529AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014081308837Cover · dislodgedSEAT 17F EMERGENCY EXIT PLASTIC COVER FELL OFF. ACFT GROUNDED. FOUND BASE OF LIGHT ASSY BAD, REMOVED AND INSTALLED SERVICEABLE ASSY. OPS GOOD. OK FOR CONTINUED SERVICE.Aug 13, 2014 · N529AS · Boeing 737890 · Emergency LightingSDR ASAA2014080808784Circuit Breaker · malfunctionedDURING FLIGHT, CIRCUIT BREAKER FOR BATTERY STBY SWITCH, POS INDICATION, RT 28 VOLT DC AT B5, IS OUT. ACFT GROUNDED. RESET BATTERY, STBY, SWITCH POS IND CIRCUIT BREAKER IAW AMM 20-60-01. CIRCUIT BREAKER RESET PROCESS. PERFORMED SPCU INSTALLATION TEST IAW AMM 2Aug 8, 2014 · N529AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014062208310Satcom · malfunctionedAFTER TRANSFERRING FROM EXTERNAL TO APU ELECTRICAL POWER NO SATCOM PROMPT. ACFT GROUNDED. SATCOM LOCKED UP PROCDURE ACCOMPLISHED ON GROUND-SATCOM PROMPT RETURNED.Jun 22, 2014 · N529AS · Boeing 737890 · Communications SystemSDR ASAA2014060408039Shim · wornNR 1 ENGINE FAN BLADE SHIMS MOLYDAG COATING WORN. ACFT GROUNDED. R & R FAN BLADE SHIMS ON NR 1 ENGINE REF T/C 78472002.Jun 4, 2014 · N529AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2014052209322Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SURFACE HAS TWO CRACKS VERIFIED BOTH CRACKS HFEC 51 PART 6, APPROXIMATELY ONE INCH AND SECOND CRACK APPROXIMATELY .5. ACFT GROUNDED. REPAIRED THE CRACKS IAW SRM 55-10-01-2R-11.May 22, 2014 · N529AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014043007656Blade · crackedDURING FAN BLADE LUBE ON NR 2 ENGINE, FOUND NR 18 PLATFORM CRACKED ON LATERAL SURFACE. ACFT GROUNDED. REPLACED NR 18, PLATFORM AND NR 6, OPPOSITE, POSITION PLATFORM IAW T/C 78472002. ACCOMPLISHED ENGINE NR 2 VIBRATION SURVEY IAW MM 71-00-00.Apr 30, 2014 · N529AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2014042807625Fireshield · crackedNR 2 ENG AFT FLANGE, FIRE SHIELD, HAS CRACKS AT BOLT HOLES. ACFT GROUNDED. REPLACED AFT FLANGE ASSY IAW AMM 72-56-400-801, STEP 3 A-E AND F (2) THRU G.Apr 28, 2014 · N529AS · Boeing 737890 · Nacelle/Pylon, Main FrameSDR ASAA2014042407573Satcom · malfunctionedAFTER PUSHBACK SATCOM LOCKED UP ON GROUND, ACFT GROUNDED. RAN CHECKLIST REGAINED SATCOM FUNCTION IAW FIM TASK 23-15-00-23-801, NO FURTHER ACTION REQUIRED.Apr 24, 2014 · N529AS · Boeing 737890 · Communications SystemSDR ASAA2014040907499Radar · malfunctionedRADAR SHOWS FALSE RETURN AT 10 & 2 O'CLOCK. ACFT GROUNDED. COULD NOT DUPLICATE. NO HISTORY 90 DAYS. ACCOMPLISHED WEATHER RADAR SYS - SYS TESTED IAW MM 34-43-00-730-802-001, TEST PASSED. OK FOR SERVICE. ETOPS SIGNIFICANT SYS GROUND VERIFICATION SUCCESSFULApr 9, 2014 · N529AS · Boeing 737890 · Weather Radar SystemSDR ASAA2014040807476Satcom · malfunctionedNO SATCOM PROMPT ON MCDU AFTER ENGINE START. ACFT GROUNDED. QRH PROCEDURE FOLLOWED TO SUCCESSFULLY RESET SATCOM.Apr 8, 2014 · N529AS · Boeing 737890 · Communications SystemSDR ASAA2014031807247Eec · failedNR 1 ENGINE ALTERNATE POWER CHANNEL B CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. INSPECTED AND RESET CIRCUIT BREAKER WITH NO DEFECTS NOTED. PERFORMED NR 1 ENGINE START AND CIRCUIT BREAKER TRIPPED AGAIN. R & R NR 1 ENGINE EEC IAW AMM 73-21-60-00-801-F00 AND 73-2Mar 18, 2014 · N529AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014031807240Satcom · malfunctionedMISSING SATCOM SELECT ON MCDU MENU. ACFT GROUNDED. PERFORMED QRH PROCEDURE, OPS NORMAL.Mar 18, 2014 · N529AS · Boeing 737890 · Communications SystemSDR ASAA2014031007128Warning Light · false activationBOTH PACK LIGHTS ILLUMINATED ON RECALL LANDING CHECK. LIGHTS EXTINGUISH ON RESET OF MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED FIM 21-62, TASK 801. NO FAULTS NOTED ON EITHER TEMP CONTROLLER. NO HISTORY LAST 30 DAYS. RAN BOTH PACKS. NO FAULT WHILE ADJUSMar 10, 2014 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014030707109Valve · failedNR 2 ENGINE ANTI-ICE VALVE COWL VALVE OPEN SHOWS DISAGREEMENT. POSITION IN OPEN OR COWL. TAI SHOWS ON PANEL. ACFT GROUNDED. DIVERSION TIME: 52 MINUTES. R & R NR 2 ENG COWL TAI VALVE IAW AMM 30-21-11-400-801. OPS CHECK NORMAL IAW SAME.Mar 7, 2014 · N529AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2014030407051Nozzle · malfunctionedAPU CT5ATP EGT DATA SHOWS EGT IS TRENDING TOWARDS ESTABLISHED THRESHOLD. ACFT GROUNDED. REMOVED ALL APU FUEL NOZZLES, REF AMM 49-31-14-000-801. INITIATED INSTALLATION OF ALL APU FUEL NOZZLES IAW AMM 49-31-14-400-801. STEP 3A-3F(G), APU REQUIRES INSTALLTION Mar 4, 2014 · N529AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2014020506786Apu · unknownAPU INLET TEMPERATURE SENSOR, T2, HAS SUDDEN INCREASE IN CT5ATP. ACFT GROUNDED,Feb 5, 2014 · N529AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2014011912407A/C Pack · faultedDURING LANDING, MASTER CAUTION LIGHT ILLUMINATED FOR A RT PACK, EXTINGUISHED WITH RESET. ACFT GROUNDED. IAW FIM 21-62, TASK 801, SHOWS INTERMITTENT RT RAM ACTUATOR FAULT. VERIFICATION TEST OK. FAULT RESET, RT PACK LIGHT REMAINS EXTINGUISHED ON RECALL.Jan 19, 2014 · N529AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014011712409Fmc · faultedCAPTAIN`S FMC CDU DIM MODE FOR ACARS AND OTHER ALERTS INOPERATIVE. ACFT GROUNDED. PERFORMED TEST OF CAPTAIN`S MCDU IAW MM 34-6101-400-802 PARA D.(2) MCDU TESTS NORMAL. BRIGHTNESS AND DIM FUNCTIONS TEST NORMAL FOR BOTH DISPLAY AND KEY PAD. HAD DISPATCH SEND MEJan 17, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014011412392Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL DURING LANDING CHECK. ACFT GROUNDED. PERFORMED FIM 21-62-842. TESTS OK. CABIN ZONE TEMP LIGHT STAYS OUT. NO HISTORY 90 DAYS. GROUND VERIFICATION TESTS OK.Jan 14, 2014 · N529AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014011212381Computer · failedRIGHT FMC FAILED, QRH PROCEDURE FOLLOWED WITH SINGLE FMC. ACFT GROUNDED. VERIFIED FAULT. CYCLED C/B FOR RT MFC & 10 MIN RT FMC BITE, INOPERATIVE WILL SHOW ON FMC CDU. REPLACED RT FMC WITH SERVICEABLE ONE. ACCOMPLISHED FMC SOFTWARE CROSSLOAD. AFTER CROSSLOAJan 12, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014011112369Fmc · malfunctionedSINGLE OPERATION DISPLAYED ON SCRATCH PAD. RAN QRH. FIRST TIME RESET. SECOND TIME IT WOULD NOT RESET CONTINUED ON SINGLE FMC OPERATION. ACFT GROUNDED. RT FMC INOPERATIVE IAW CREW. TROUBLESHOT RT FMC REF FIM 34-61, TASK 836. SYSTEM RESET & IS CONSIDERED INJan 11, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014010612331Warning Message · false activationFMC DISAGREE ANNUNCIATION AFTER ENGINE START. ACFT GROUNDED. NORMAL OPS RESTORED AFTER CHECKLIST PROCEDURE.Jan 6, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014010512327Fmc · failedMAP AND VTK FLAGGED ON CAPTAIN`S ND. BOTH CDUS DISPLAYED NO INFORMATION. SWITCHED FMC TO BOTH ON RT BUT DUAL FMC OPS WAS NOT RESTORED. ACFT GROUNDED. REPLACED RT FMC REF AMM 34-61-02. OPS CHECK GOOD. SUCCESSFUL ETOPS GROUND VERIFICATION.Jan 5, 2014 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013122412226Filter · cloggedAPU OIL LUBE FILTER HAS CLOGGED INDICATION. ACFT GROUNDED. R & R APU OIL LUBE FILTER IAW AMM 49-91-13-600-801.Dec 24, 2013 · N529AS · Boeing 737890 · APU Oil SystemSDR ASAA2013122312231Fcu · leakingAPU OIL CONSUMPTION RATE CALCULATED AT .29 QPH THIS IS AN UNSATISFACTORY CONSUMPTION RANGE IAW AMM 49-11-00-710-802. ACFT GROUNDED. WITH APU RUNNING FOR 10 MINUTES, FOUND OIL LEAK, APPROX 20 DROPS IAW MINUTE AT THE WITNESS PORT, COMING FROM THE FUEL CONTROL/Dec 23, 2013 · N529AS · Boeing 737890 · APU Oil SystemSDR ASAA2013121296870Computer · failedCAPTAIN`S NAV DISPLAY SHOWED VTK AND MAP. BOTH CDUS DISPLAYED MENU PAGE WITHOUT FMC. RAN FMC FAIL CHECKLIST AND COMPLETED WITH FMC SOURCE ON RT. FMC -LT ON POS SHIFT PAGE IS BLANK. ACFT GROUNDED. REMOVED DISCREPANT LT FMC COMPUTER IAW AMM 34-61-02. INSTALLDec 12, 2013 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013120596640Idg · failedNR 1 SOURCE OFF LIGHT ILLUMINATED, NR 1 GEN DRIVE LIGHT ALSO ILLUMINATED. ACFT GROUNDED. PERFORMED BPCU BITE PROCEDURE 24-41, TASK 801. NO FAULTS FOUND. PERFORMED NR 1 ENG GCU BITE PROCEDURE 24-21, TASK 801. NO FAULTS FOUND. ALL SYSTEMS ARE GREEN. INSPECTEDec 5, 2013 · N529AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2013120496605Generator · failedMAINTENANCE LIGHT ILLUMINATED DURING START. APU PROVIDED POWER BUT THEN DISCONNECTED. APU POWER COULD NOT BE BROUGHT BACK ON LINE. ACFT GROUNDED. R & R & TESTED THE APU SGU IAW 49-41-21/401 & EA 737-49EA-11734. GROUND VERIFICATION OF FAULT RESOLUTION FOUNDec 4, 2013 · N529AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2013120396594Cdu · failedCAPT MCDU MESSAGE AND CALL LIGHTS FLICKERED BRIGHT, DIM WITH LIGHTS SWITCH IN DIM THEN STAYED BRIGHT FOR REMAINDER OF FLIGHT. ACFT GROUNDED. REPLACED CAPTAIN`S FMC CDU AND OPS NORMAL REF MM 34-61-01. GROUND VERIFICATION SUCCESSFUL.Dec 3, 2013 · N529AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013111496417Valve · failedNR 2 ENGINE TAIL LIGHT AMBER WHEN ENGINE ANTI-ICE PUT ON AROUND 10000FT ON DESCENT, TURNED GREEN AROUND 2500FT AGL AND STAYED GREEN REST OF FLIGHT. ACFT GROUNDED. REPLACED NR 2 ENGINE TAIL COWL VALVE IAW AMM 30-21-11. ETOPS GROUND VERIFICATION TEST NORMAL IANov 14, 2013 · N529AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2013103196269Display · failedCAPTAIN`S MCDU EXEC LIGHT WILL NOT DIM WHEN LIGHTS DIM SWITCHED PLACED TO DIM AND EXECUTE FUNCTION REQUIRED. INTERMITTENTLY FLASHES BETWEEN DIM AND BRIGHT. ACFT GROUNDED. REPLACED MCDU 34-61-01-400-802. VERIFIED S/W CONFIG REF 34-61-00-750-802.Oct 31, 2013 · N529AS · Boeing 737890 · Flight Management Computing Hardware System
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