N558AS

Service difficulty reports · 535

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 = 'N558AS' 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 ASAA1057775Unknown · malfunctionedAFT CARGO FIRE LIGHT DOES NOT ILLUMINATE DURING TEST. AFT CARGO PIT FIRE DETECTION TEST NORM. PERFORMED TEST NUMEROUS TIMES. REF FIM 26 16 TASK 806, NO HISTORY 90 DAYS, GROUND FUNCTIONAL TESTS PASS.Apr 29, 2010 · N558AS · Boeing 737890 · Fire DetectionSDR ASAA1057571Oil Cooler · leakingDURING APU SERVICING APU APPEARS TO HAVE A OIL LEAK AFT AREA. FOUND APU OIL COOLER SATURATED WITH OIL. REMOVED AND REPLACED APU OIL COOLER OPS / LEAK CHECK GOOD REF AMM 49 91 41. PART EFFECTIVITY VERIFIED BY SEAMC. SEAMC NOTIFIED.Mar 22, 2010 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA1057553Valve · malfunctionedWHEN RECALL IS PUSHED ZONE TEMP LIGHT FOR CONTROL CABIN ILLUMINATES. FOLLOWED QRH TRIP RESET PUSHED LIGHT REMAINS ON. MASTER CAUTION RESET IS PUSHED LIGHT GOES OUT. FAULT CODE 216 212 00. VERIFIED NR 2 ZONE TEMP CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT.Mar 18, 2010 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057385Controller · malfunctionedCONT CAB/ZONE TEMP LIGHT ILLUMINATED. NR 2 ZONE/TEMP CONTROLLER LOGGED FLIGHT DECK TRIM VALVE FAULT. RESET FAULT ON NR 2 ZONE/TEMP CONTROLLER. GROUND VERIFICATION TEST PASSED REF MM 21 61 00.Feb 15, 2010 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057375Unknown · malfunctionedDURING 30 DAY EVAL AUTOLAND WAS UNUSUALLY FAR TO THE LEFT OF CENTERLINE, ABOUT HALF WAY BETWEEN CENTERLINE AND RUNWAY EDGE. SLIGHT TAILWIND (040/6) AND GROUND CONTROLLER VERIFIED PROTECTED AREA WAS CLEAR. AUTOTHROTTLES SEEMED TO LAG TO IDLE AND A/C "HUNTED" Feb 14, 2010 · N558AS · Boeing 737890 · Autopilot SystemSDR ASAA1057367Actuator · faultyRIGHT PACK LIGHT ILLUMINATED ON RECALL AFTER ENGINE START. REPLACED RT RAM AIR ACTUATOR. ALL SYS OPS NORMAL. REF MM 21 51 21.Feb 10, 2010 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057326Linkage · wornRIGHT RAM AIR DEFLECTOR DOOR IS OUT OF RIG. ON DEFERRAL.Feb 5, 2010 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057283Fire Detector · no testDURING PREFLIGHT AFT CARGO FIRE LIGHT DID NOT ILLUMINATE DURING TEST. CYCLED LIGHTS TEST SWITCH. CARGO FIRE OP CHECK NORMAL.Jan 24, 2010 · N558AS · Boeing 737890 · Fire DetectionSDR ASAA1057227Transceiver · faultyBOTH C/A AND F/O RADAR DISPLAYS "SPIKES" OR "SPIKING" INTERMITTENTLY ACROSS THE SCREEN IN ALL MODES OF OPERATION. PULLED & TAGGED WX R/T C/B. REMOVED AND REPLACED RD WX RADAR R/T PER 34 43 41 ROTABLE COMPONENT VERIFIED BY SEAMC. UNTAGGED & RESET C/B. SYS OJan 12, 2010 · N558AS · Boeing 737890 · Weather Radar SystemSDR ASAA0957167Idg · failedNR 1 IDG DRIVE LIGHT IN NOT ILLUMINATED WITH ENGINE SHUTDOWN. GROUNDED YES. REMOVED AND REPLACED NR 1 ENGINE IDG IN REF 24-11-11 PB 401. OPS CHECK NORMAL.Dec 24, 2009 · N558AS · Boeing 737890 · AC Generation SystemSDR ASAA0957144Igniter · failedNR 1 ENGINE WOULD NOT LIGHT OFF WITH THE RIGHT IGNITION SELECTED. STARTED OK WITH IGNITION ON LEFT. REPLACED NR 1 ENGINE RIGHT IGNITER PLUG REF MM 74 21 02, OPS CHECK GOOD.Dec 8, 2009 · N558AS · Boeing 737890 · Spark Plug/IgniterSDR ASAA0957128Display · malfunctionedRT MCDU LOCKED UP. VERIFIED DISCREPANCY, ALSO FOUND SEVERAL BUTTONS INOP REF FIM 34 61 TASK 802. REPLACED F/O MCDU REF MM 34 61 01.Dec 2, 2009 · N558AS · Boeing 737890 · Central DisplaySDR ASAA0957126Fmc · malfunctionedRIGHT FMC FROZE ON LEGS PAGE. VERIFIED RIGHT FMC FAILURE RESET RIGHT FMC AND TESTS NORMAL PER FIM 34 61 TASK 807. GROUND VERIFICATION OF SYSTEM OPERATION NORMAL.Dec 2, 2009 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0956867Warning System · malfunctionedWHILE TAXIING TO RUNWAY IN OGG OBSERVED "FMC DISAGREE" ON BOTH NAV DISPLAYS. ACCOMPLISHED APPROPRIATE QRH CHECKLIST WHICH RE-ESTABLISHED DUAL FMC OPS.Oct 26, 2009 · N558AS · Boeing 737890 · Central WarningSDR ASAA0956645Monitor · failedGE DIAGNOSTICS REPORTS NR 1 ENGINE NR 4 BEARING LEVEL 2 MESSAGE EXISTS AFTER LAST DATA ERASURE. REMOVED AND REPLACED AVM REF 77 31 03 TO STEP 5 (B)(1). ACCOMPLISHED REMAINING STEPS PER MM 73 31 03 AND 77 31 00 970 805 F00. S/N AC43765 PUT ON SOS. VERIFIED Sep 17, 2009 · N558AS · Boeing 737890 · Engine Ignition Analyzer SystemSDR ASAA0956625Warning System · malfunctionedWHILE PERFORMING T/C 08031001 FOUND NR 4 BRG MSG IN AVM: E1 LEVEL 2 NR 1 ENGINE. C/W TASK CARD 78472040 FOUND NO MATERIAL IN SCREENS. PER INSTRUCTION ACCOMPLISHED AVM FAULT HISTORY ERASE REF TASK 77 31 00 970 803 F00. CURRENT BITE AND FAULT HISTORY SHOWS NOSep 13, 2009 · N558AS · Boeing 737890 · Engine Ignition Analyzer SystemSDR ASAA0956578Control Valve · faultyLEFT PACK LIGHT ILLUMINATED AFTER RECALL RESET WITH MASTER CAUTION LIGHT EXTINGUISHED. ACCOMP PACK/ZONE TEMP CONT BITE CHECK RECORDED TCV FAULT LT PACK. REMOVED & REPLACED LT PACK TCV LEAK & OPS NORMAL REF M/M 21 51 10. ALL FAULTS CLEARED BITE CHECK GOOD RESep 8, 2009 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0956412Drive Unit · malfunctionedWX RADAR HAS INCREASING FREQUENCY OF SPIKING +/ 30' OF CENTERLINE. SUBSEQUENT SPIKING NOW ALL QUADRANTS. UNABLE TO DUPLICATE. DUE TO HISTORY OF WXR RADAR ANT SPOKING PROBLEMS REPLACED WXR RADAR ANT DRIVE REF MM 34 43 11. OPS NORMAL REF MM 34 43 00.Aug 17, 2009 · N558AS · Boeing 737890 · Weather Radar SystemSDR ASAA0956377O-Ring · pinchedNR 1 ENG OIL CAP O-RING IS SWOLLEN & PINCHED UNDER CAP. REMOVED AND REPLACED NR 1 ENG OIL FILLER CAP O-RING PER MM 79 11 01 300 801 F00.Aug 5, 2009 · N558AS · Boeing 737890 · Engine Oil Storage (Airframe Furnished)SDR ASAA0956354Sense Line · blownPRESSURIZATION DUCT SPLIT IN FLIGHT CLIMBING THROUGH 2000 FT L25 R45. AT FL 350 L28 R44. AT FL 370 L28 R42. ACCOMP PNEUMATIC SYS T/S REF M/M 36 00 00 101 NR 1 ENG. FOUND THE CONT PRESS SENSE LINE FOR THE PRSOV/450 STAT BLOWN OUT. REPLACED CONT PRESS SENSEAug 1, 2009 · N558AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0956192Warning System · false activationAIR COND AND PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL AFTER ENGINE START. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST REF AMM 21 51 00 700 803, NO FAULTS NOTED. OPS CHECK GOOD.Jul 11, 2009 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0956187Smoke Detector · faultyAFT CARGO FIRE DETECTION WILL NOT TEST "DETECTOR FAULT" LIGHT ILLUMINATES. FOUND SMOKE DETECTOR POSITION B2 AT AFT CARGO PIT FAULTY. REMOVED AND REPLACED DETECTOR B2 REF MM 26 16 01 000 801. PERFORMED OPS TEST REF MM 26 16 00 710 801. SYS CHECKS NORMAL. OJul 8, 2009 · N558AS · Boeing 737890 · Smoke DetectionSDR ASAA0956003Fire Loop · dirtyDURING CARGO FIRE TEST AFT LIGHT WASN’T ILLUMINATED. GROUNDED YES. FOUND LOOP B2 FAULTED. CLEANED WITH AIR ALL B LOOPS. PLACED SELECTOR TO BOTH AND TESTED CARGO SMOKE DETECTION OPS TEST PASS REF MM 26 16 01 100 801 AND 26 16 00 710 801.Jun 20, 2009 · N558AS · Boeing 737890 · Fire DetectionSDR ASAA0955970Contact · dirtyON INITIAL CARGO FIRE TEST AFT ARM LIGHT FAILED TO ILLUMINATE AND DETECTOR FAULT ILLUMINATED. WHILE ISOLATING LOOPS SUBSEQUENT TESTS OK. REMOVED AFT ARM LIGHT AND CLEANED CONTACTS RESET C/B AND PERFORMED GOOD FUNCTIONAL CHECK IAW AMM 26 16 00 710 801.Jun 18, 2009 · N558AS · Boeing 737890 · Fire DetectionSDR ASAA0955798Transceiver · inoperativeSFO ARINC REPORTS HF NR 1 TRANSMITS NORMALLY BUT ONLY RECEIVES GARBLED NOISE (1 X 1). HF NR 2 TRANSMIT & RECEIVE NORMAL. SNAG NR 23107048. CONFIRMED NR 1 HF TRANSCEIVER INOP. INSTALLED SERVICEABLE HF TRANSCEIVER IN NR 1 POSITION. PART NUMBER VERIFIED WITH May 29, 2009 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA0955544Filter · dirtyTEMP CONTROL OF MAIN CABIN VERY ERRATIC. LARGE TEMP SWINGS + 15 DEGREES WITH SLIGHTEST MOVEMENT OF CONTROL KNOBS (SUPPLY DUCT READING). WITH POSITIONED TRIM AIR SWITCH TO OFF ABLE TO KEEP TEMP SWINGS REASONABLE BOTH MAIN CABIN KNOBS POSITIONED IN THE TWO O'CMay 8, 2009 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0955559Engine · malfunctionedECM DATA SHOWS LOWER THAN NORMAL EGT MARGIN ON THE NR 1 ENGINE. GROUNDED YES. ACCOMPLISHED MM 72 00 00 100 803 F00 CLEAN THE ENGINE GAS PATH WITH PURE WATER.May 7, 2009 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0955558Engine · malfunctionedECM DATA SHOWS LOWER THAN NORMAL EGT MARGIN ON THE NR 2 ENGINE. GROUNDED YES. CLEANED NR 2 ENG GAS PATH WITH PURE WATER REF AMM72 00 100 803 F00.May 7, 2009 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0955327Paint · erodedFAN BLADE LUBE T/C 78472002 FOUND NR 2 ENGINE FRONT SPINNER CONE PAINT ERODED PAST 20 PERCENT. INSTALLED NEW FRONT SPINNER CONE IN REF WITH T/C 78472002.Apr 25, 2009 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954895Shim · damagedNR 1 ENG REF T/C 78472002 FOUND BLADE SHIMS MISSING MORE THAN 25 PERCENT OF MOLYDAG COATING REF MM 72-21-02-200-801-F00. SHIMS NIS SEA DEFERRED FOR 250 CYCLES IAW MM 72-21-02-200-801 SEAMC NOTIFIED.Mar 23, 2009 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954894Paint · missingREF T/C 78472002 STEP 6 NR 1 ENGINE FRONT SPINNER CONE IS MISSING MORE THAN 20 PERCENT OF WHITE ANTI EROSION PAINT. REPLACED FRONT SPINNER CONE IAW T/C 78472002.Mar 23, 2009 · N558AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954699Computer · malfunctionedAFTER ENG START W/ENG GENERATORS ON THE BUSSES FLT CONTROL MASTER CAUTION LIGHT ILLUMINATED ON RECALL. SPD TRIM FAIL AND MACH TRIM FAIL LIGHTS ILLUMINATED ON OVERHEAD FD FLAG ILLUMINATED ON CAPTAIN'S EADI. AFCS SYS A WARN LIGHT (BAT) C/B POPPED ON P18 PANEL.Mar 10, 2009 · N558AS · Boeing 737890 · Flight ControllerSDR ASAA0954496Unknown · malfunctionedCONT CABIN ZONE TEMP LIGHT ON RECALL. NR 2 TEMP CONTROLLER LOGGED "FLIGHT DECK TRIM VALVE" LAST LEG WITH NO PRIOR HISTORY. CLEARED FAULT REF MM 21 61 00, CABIN TEMP CONTROL OPS NORMAL.Feb 24, 2009 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0954484Fire Detector · failedAT CRUISE WITH APU RUNNING APU DET INOP LIGHT ILLUMINATED. PERFORMED FIM 26 10 00 810 801. FOUND APU TAILPIPE DETECTOR M1925 TO BE AT FAULT. FAULT CONFIRMED. REMOVED AND REPLACED M1925 PER MM 26 15 01 400 802. VERIFIED PART NUMBER SEAMC. OPS TESTED PER MFeb 20, 2009 · N558AS · Boeing 737890 · Fire DetectionSDR ASAA0854040Engine · oil consumptionSEAMC REPORTS NR 1 ENGINE EXCEEDED ETOPS OIL CONSUMPTION RATE NR 1 ENGINE CURRENT CONSUMPTION AT .0.71 QUARTS PER HOUR. ACFT GROUNDED. RAN NR 1 ENGINE AT IDLE FOR APPROX. 5 MINUTES. NO LEAKS DETECTED. ACFT RELEASED FOR ETOPS SERVICE. NR 1 ENGINE WITHIN OIDec 13, 2008 · N558AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853820Fmc · malfunctionedFMC DISAGREE DISPLAYED ON TAXI IN CUN FOLLOWED QRH PROCEDURES DUAL FMC RESTORED. PERFORMED FIM TASK 34 61TASK 835 PER STEP D2 FAULT WAS INTERMITTENT W/NO OTHER OCCURRENCES LAST 30 DAYS. OK FOR CONTINUED SERVICE.Nov 19, 2008 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853792Controller · malfunctionedPRESSURIZATION CONTROLLER FAILED HAD AUTO FAIL AND ALTN LIGHTS CPC NR 2 LOGGED CODE 101 AND 006. FIM 21 31 TASKS 803 AND 804 NEED TO BE ACCOMPLISHED. NO FAULTS LOGGED ON CPC NR 1. CONFIRMED AUTO FAIL FLIGHT ILLUMINATED IN AUTO POSITION. PERFORMED FIM TASK 2Nov 16, 2008 · N558AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0853766Control Unit · malfunctionedTHE L SIDE WINDOW 'OVERHEAT' LIGHT ILLUMINATED AND PER CHECK LIST WOULD NOT RESET (380 53SAT NORMAL WARM TO TOUCH). FOUND C/B C392 POPPED. PERFORMED FIM TASK 30 41 00 810 806. REPLACED CIRCUIT BREAKER C392 REF WDM 30 41 12. VERIFIED LEFT SIDE WINDOW HEAT ONov 14, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853730Window · overheated45 MINUTES INTO FLIGHT AT FL 35 000. LT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. QRH PROCEDURES WERE ACCOMPLISHED AND LIGHT REMAINS ON WHEN SWITCH WAS TURNED BACK ON. GROUNDED YES. R&R THE LT SLIDING WINDOW PER MM 56 12 11. OPS CHECKS OK. REMOVED C/N 6608314Nov 8, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853753Control Unit · faultyLEFT SIDE WINDOW HEAT "OVERHEAT" LIGHT ILLUMINATED IN CRUISE AT FL 400. FOLLOWED AND TURNED OFF FOR 5 MIN. TURNED BACK ON STILL ILLUMINATED. SWITCHED BACK OFF. SHOOK LT SLIDING WINDOW COIL CORD. UNABLE TO DUPLICATE. DUE TO HISTORY REMOVED LT WINDOW HEAT Nov 7, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853752Circuit Breaker · trippedWINDOW HEAT "LEFT SIDE" OVERHEAT LIGHT ON. FOUND P6 12 "B7" C/B "LT SIDE WINDOW HEAT" OPEN RESET SAME PER SP CHAPTER 20 61 00. TESTED WINDOW HEAT ELEMENT FILM RESISTANCE AND SENSOR VALUES FOR CORRECT VALUES, NO FAULTS NOTED. COMPLETED FIM TASK AFTER C/B RESNov 5, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853751Controller · malfunctionedWINDOW HEAT LEFT SIDE OVERHEAT LIGHT ON. INFO CAME ON AT 30 MIN AFTER T/O, ALT 37000 (TAT 31C). FOLLOWED QRH SWITCH OFF. RESET LEFT SIDE WINDOW HEAT POWER C/B PER MM 20 60 01. ACCOMPLISHED FIM 30 41 00 810 801. NO FAULTS NOTED. GROUND VERIFICATION SUCCESNov 5, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853658O-Ring · deformedNR 1 ENG OIL TANK CAP O-RING IS DEFORMED. REMOVED & REPLACED O-RING SEAL REF MM 79 11 01 300 801 F00.Oct 21, 2008 · N558AS · Boeing 737890 · Engine Oil Storage (Airframe Furnished)SDR ASAA0853660Idg · leakingFOLLOW UP TO FREQUENT NR 2 IDG SERVICING WITH REPORT OF OIL STREAKS. ACCOMPLISH IDG STATIC LEAK CHECK REF AMM 24 11 00 700 801. ACCOMP TSR NO LEAKS FOUND DURING IDLE RUN. REMOVED & REPLACED NR 2 ENG IDG REF MM 24 11 11 LEAK & OPS NORMAL REF MM 24 11 00. P/Oct 21, 2008 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853559Radar · malfunctionedTHE RADAR HAS INTERMITMENT SPOKES OF GREEN AND YELLOW ALONG WITH NORMAL WX RETURNS. UNABLE TO CONFIRM FAULT. WXR SYSTEM TEST GOOD REF MM 34 43 00. FLT CREW CHECK WXR OPS NORMAL. VERIFICATION FLT SATISFACTORY.Oct 6, 2008 · N558AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853557Control Unit · failedLEFT SIDE WINDOW OVERHEAT (C/B POPPED). INSPECTED C/B C392AND RESET IAW MM 20 60 01. PERFORMED FIM 30 41 00 810 814 FOUND 7 BUSS POWER FAULTS. PERFORMED FIM 30 41 00 810 816. SENSOR AT 326 OHMS NML MM 30 41 00 HEAT FILM AT 71 0 OHMS NML 30 41 21. REPLACED Sep 30, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853536Warning System · activatedWINDOW HEAT OVERHEAT LIGHT ILLUMINATED (LEFT SIDE) AFTER REAPPLYING POWER IAW THE QRH PROCEDURE THE OVERHEAT LIGHT CAME ON AGAIN. THE OUTSIDE STATED AIR TEMP WAS 60C, CONFIRMED LEFT SIDE WINDOW HEAT OVERHEAT ONE WITH WINDOW HEAT C/B POPPED. RESET WINDOW HEATSep 29, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853531Idg · malfunctionedNR 1 ENG IDG DELTA P POPPED. RESEARCH IN ARCTIC SHOWS THIS IS THE 3RD EXTENTION ON THIS IDG ACCOMPLISHED MM 24 11 41 200 801, REMOVED & REPLACED IDG OIL FILTERS. NO DEBRIS FOUND. REMOVED AND REPLACED NR 1 ENGINE IDG. REF MM 24 11 11. NR 1 ENGINE IDG OPS LSep 25, 2008 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853519Controller · malfunctionedAUTO FAIL LIGHT ILLUMINATED PRESSURIZATION PANEL. DUPLICATED FAULT BOTH PRESSURIZATION CONTROLLERS SHOWED CONTROL PANEL FAULT. RESET & CLEARED FAULTS ON BOTH AUTO PRESS CONTROLLERS AND ACCOMPLISHED FIM 21 31 00 810 801, OPS CHECK NORMAL.Sep 20, 2008 · N558AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0853480Idg · malfunctionedNUMBER 2 GENERATOR ANNUNCIATION AT GATE. REPLACED IDG.Sep 9, 2008 · N558AS · Boeing 737890 · AC Generator-Alternator
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