N596AS

Service difficulty reports · 549

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 = 'N596AS' 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 ASAA1250897Circuit Breaker · openAUTOTHROTTLE DC 1 (P18 1 E1) CB FOUND OPEN. VERIFIED INSECTION OF C/B AND ASSOCIATED WIRING BEHIND P18 1 PANEL GOOD. RESET AT DC1 C/B REF MM 20 60 01, OPS TEST PASSED REF MM 22 31 00.Jan 4, 2012 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA11510825Apu · leakingAFTER ENGINE START WHEN TURNING ON PACKS HAD DIRTY SOCK SMELL. REF MM 05 60 00 280 801 STEP 3 FOUND OIL PRESENT IN LOAD COMPRESSOR SEAL WITNESS DRAIN. REPLACED APU REF MM 49 13 11 MM49 11 00 000 803. LEAK CHECKED AND SERVICED OIL ON NEW APU REF MM 49 11 00 4Dec 20, 2011 · N596AS · Boeing 737890 · APU Core EngineSDR ASAA11510742Unknown · malfunctionedN 2S LOW FOR START DIFFICULT TO ATTAIN 25 PERCENT. ACCOMPLISHED ENG START PROCEDURE REF MM 71 00 00 800 808F00 ALL 3 START ATTEMPTS WITHIN NORMAL PARAMETERS ON ENG 1. ACCOMPLISHED ENG START REF MM 71 00 00 800 808F00 3 START ATTEMPTS NORMAL PARAMETERS ON ENGDec 1, 2011 · N596AS · Boeing 737890 · Engine CrankingSDR ASAA11510704Engine · overspeedON CLIMBOUT LEFT ENGINE SURGED TO 100+ N1 RPM, IT WENT BACK TO 60 RPM AND BACK UP TO 100+. RETARDED ENGINE TO IDLE RAN QRC/QRH LEFT ENGINE RUNNING AT IDLE PWR. ENGINE STABILIZED AT IDLE. DIV TIME: 0:14. BITE TEST NR 1 ENG SHOWS MSG 73 20331 FMV DEMAND AND PONov 22, 2011 · N596AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA11510624Unknown · malfunctionedAFTER PUSHBACK ATTEMPTED TO START NR 2 ENGINE WITH IGNITION SWITCH IN THE L POS. HUNG START NO EGT RISE. COMPLIED WITH ABORTED ENGINE START QRL/QRH PROCEDURE. ALL CB'S WERE IN. SWITCHED THE IGNITION SWITCH TO THE R POS AND GOT A NORMAL ENGINE START ON BOTHNov 5, 2011 · N596AS · Boeing 737890 · Ignition Power SupplySDR ASAA1150581Wire Harness · failedNR 2 ENGINE TREND DATA CONTINUES TO SHOW ERRORS INDICATIVE OF EGT INDICATION SYSTEM ANOMALIES. ALL OTHER PARAMETERS ARE NORMAL. PREVIOUS MAINT S3 PROBE REPLACED. ACFT GROUNDED. REPLACED AND TESTED CJ10 HARNESS IAW MM 73-21-06. TESTS PASS. ETOPS SIGNIFICANTOct 23, 2011 · N596AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA11510516Unknown · malfunctioned"FMC DISAGREE" ON BOTH NAV DISPLAYS ON GROUND. PERFORMED QRH PROCEDURE. LIGHT RESET. OPS NORMAL.Oct 14, 2011 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510481Unknown · malfunctionedRIGHT PACK LIGHT ILLUMINATED AND RIGHT PACK TRIPPED OFF ACCOMPLISHED ABNORMAL PROCEDURES AND RESET. PACK TRIPPED AGAIN AFTER 30 SECONDS. ABOVE OCCURRED AT GATE IMMEDIATELY PRIOR TO PUSH. PERFORMED BOTH AUTO TEMP CONTROLLERS BITE TEST AND NO FAULT LOGGED ON Oct 7, 2011 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA11510462Probe · failedGE DIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA CONTINUES TO SHOW A SHIFT IN DELTA CRUISE AND TAKE OFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. PERFORMED TASK 77 21 01. FOUND T49.5 S3 PROBE FAULTY (HIGH RESISTANCE). INSTALLED NEW S3 PROBE REF 77 21 01. OPOct 5, 2011 · N596AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA1150447Unknown · faultyLEFT SIDE WINDOW OVERHEAT ILLUMINATED ON TAXI IN. CHECKED SPARE SENSOR & RESISTANCE IS WITHIN LIMIT REF MM FIM 30 41 00. REMOVED WINDOW FOR ACCESS TO SENSOR TERMINAL CONNECTOR. SWAPPED SENSOR TO ALTERNATE STUD. RE-INSTALLED WINDOW REF MM 56 12 11 CLOSED C/Oct 1, 2011 · N596AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA11510408Warning System · false activationL SIDE WINDOW "OVERHEAT" LIGHT ILLUMINATED SHORTLY BEFORE LANDING. GROUND VERIFICATION CHECK OF THE CAPT'S SLIDING WINDOW HEAT OPS CHECK NORMAL REF AMM TASK 30 41 00 710 801 (105 DEGREE F) & FIM TASK 30 41 00 810 811 (PRI SNSR 330 OHM SPARE SNSR 320 OHM). RESep 24, 2011 · N596AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA11510404Cdu · defectiveF/O'S FMC BUTTON 6R IS INTERMITTENT. REPLACED F/O'S MCDU REF MM 34 61 01 000 802 & 34 61 01 400 802. ETOPS GROUND VERIFICATION SUCCESSFUL.Sep 21, 2011 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510372Probe · defectiveNR 2 ENGINE TREND DATA CONTINUES TO SHOW ERRORS INDICATIVE OF EGT INDICATION SYSTEM ANOMALIES. ALL OTHER PARAMETERS ARE NORMAL. COCKPIT INDICATION IS STILL WITHIN RANGE. STEPS 1 & 2 OF TSR 905574 CHECKED GOOD. NO FAULTS FOUND. REPLACED CJ9 HARNESS & T49.5Sep 19, 2011 · N596AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA11510390Idg · failedIDG NR 2 NOT ILLUMINATED ON GND WITH ENGINE OFF. REPLACED NR 2 ENG IDG AS PER AMM 24 11 11 000 801 AND 24 11 11 400 801. RUN ENG NR 2. NO LEAK NOTED. PERFORMED OPERATIONAL TEST AS PER AMM 24 11 00 700 803, OPS CHECK GOOD.Sep 17, 2011 · N596AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA11510364Circuit Breaker · trippedSYS B MACH TRIM CB POPPED ON PREFLIGHT. INSPECTED AREA BEHIND P6 2 PANEL. NO DEFECTS NOTED. INSPECTED AFCS SYS B MACH TRIM DC C/B. NO DEFECTS NOTED. RESET AFCS SYS B TRIM DC C/B AMM 20 60 01. OPS CHECK GOOD REF AMM 22 11 24 740 801.Sep 13, 2011 · N596AS · Boeing 737890 · Autopilot SystemSDR ASAA11510341Indication Sys · malfunctionedELEC ON PWR DIS PANEL ILLUM. RESET OVERHEAD "ELECTRIC LIGHT FAULT" INDICATION REF FIM 24 31 00 810 801. SYS OPS CHECKS NORMAL.Aug 30, 2011 · N596AS · Boeing 737890 · DC Indicating SystemSDR ASAA11510203Unknown · malfunctionedFMC DISAGREE ILLUMINATED. PERFORMED QRH PROCEDURE OPS NORMAL.Aug 5, 2011 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510157Autothrottle Sys · malfunctionedAUTOTHROTTLES DISCONNECTED ON TAKEOFF ROLL SJC AND WOULD NOT REMAIN ENGAGED. PERFORMED FIM TASK 22 32 00 810 806 AUTOTHOTTLE AUTOMATIC DISENGAGE PROBLEM. NO FAULTS FOUND IN CURRENT STATUS. NO HISTORY 60 DAYS. OK FOR CONTINUED SERVICE.Jul 23, 2011 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA11510016Starter Gen · faultyAPU FAILS TO START. FAULT LIGHT ILLUMINATED. ACCOMPLISHED FIM TASK 49 40 TASK 806 FOUND FAULT CODE 49 41244 LOGGED. REPLACED APU STARTER GENERATOR PER M/M 49 41 21 SYSTEM, OPS CHECKS NORMAL.Jul 5, 2011 · N596AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA1159763Display · defectiveCAPT MCDU KEYPAD "CLR" BUTTON STUCK DOWN. REPLACED FMC CDU IAW B737NG AMM 34 61 01 400 802. SYSTEM CHECKS GOOD IAW B737NG AMM 34 61 01 400 802.Jun 4, 2011 · N596AS · Boeing 737890 · Central DisplaySDR ASAA1159754Detection Sys · malfunctionedFIRE PROT EXTINGUISHER LT P62 B22 AND ALT LT P62 B24 FOUND OPEN ON PREFLIGHT, ACFT GROUNDED. RESET CIRCUIT BREAKERS AND TEST GOOD PER AMM 20-60-01 AND 26-11-00.Jun 4, 2011 · N596AS · Boeing 737890 · Detection SystemSDR ASAA1159750Trim System · malfunctioned"SPEED TRIM FAIL" LIGHT ON RECALL. ACCOMPLISHED SPEED TRIM OPERATIONAL CHECK IAW AMM 22-11-00-740-801, NO DEFECTS NOTED.Jun 4, 2011 · N596AS · Boeing 737890 · Speed-Attitude Correction SystemSDR ASAA1159752Controller · malfunctionedBOTH PACK LIGHTS ILLUMINATE ON RECALL. PACK CONTROLLERS RESET IAW MM 21-51-00, OPS NORMAL.Jun 4, 2011 · N596AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA1159688Valve · failedIN CRUISE WHEN POWER COMES UP RT PACK PRESSURE 45. LT PACK PRESSURE 25 WITH POWER BACK TO ENROUTE POWER (89.0 N1) RT PACK 41, LT PACK 36 GROUNDED ACFT. REPLACED NR 1 ENG PRSOV. LEAK AND OPS CHECKED GOOD VOLTAGE AND GROUND CHECK GOOD IAW MM 36-11-04 AND 36-11May 24, 2011 · N596AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1159669Unknown · malfunctionedCLIMBOUT SEA TO FL380 FR FL230 TO FL 380 CABIN IVSI WAS CYCLING +500 TO+1000 OUT OF FL 350 IT CYCLED 500 TO +500 TIL FL380 THEN STABILIZED AT 7000 CABIN ALT. INITIAL EVAL SHOWS NO FAULTS ON DCPC OR DCPC NR 2 NO EXISTING FAULTS OR FAULTS IN HISTORY. FOLLOWED May 18, 2011 · N596AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA1159615Cdu · inoperativeTACTILE FEEDBACK LINE SELECT KEY 6R ON F/O. MCDU IS INOP. REPLACED F/O'S MCDU. MCDU OPS CHECK GOOD. GROUND VERIFICATION SATISFACTORY REF MM 34 61 01 400 802.May 5, 2011 · N596AS · Boeing 737890 · Central DisplaySDR ASAA1159405Transceiver · looseWX RADAR SPIKES ON ALL RANGES AND TILT ANGLES. FOUND RADAR TRANSCEIVER LOOSE IN RACK. RE-SECURED WEATHER RADAR TESTS GOOD.Apr 6, 2011 · N596AS · Boeing 737890 · Weather Radar SystemSDR ASAA1159368Unknown · malfunctionedMAIN AIRCRAFT BATTERY INDICATED 27VOLTS +1AMP FOR THE ENTIRE 5 HOUR FLIGHT. AUX BATT INDICATES 28VOLTS 0AMPS. ALL OTHER ELECTRIC SYSTEM INDICATIONS ARE NORMAL. CHARGER CHECK'S GOOD INDICATIONS REMAIN SAME. RE-INSTALLED ORIGINAL MAIN CHARGER. REMOVED AND RApr 2, 2011 · N596AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1159342Connector · looseAPU AIR PRESSURE FLUCTUATES W/ OR W/ OUT AIR LOAD. PERFORMED APU BITE TEST ON FMC CDU FOUND FAULT CODE 49 52194 (IGV ACTUATOR TORQUE MOTOR SHOWS OPEN CIRCUIT) AS PER FIM 49 60 TASK 801. PERFORMED FIM TASK 49 52 00 STEP F (2) GENERAL VISUAL INSPECTION OF ELECMar 24, 2011 · N596AS · Boeing 737890 · APU System WiringSDR ASAA1159273Unknown · malfunctionedEVAL AUTO LAND {OUT OF TOLERANCE LEFT OF CENTER}. DFCS GROUP 20 (FAULT REVIEW) PER FIM 22 11 00 810 801 SHOWED NO RELATED FAULTS BUT HGS FAULT HISTORY SHOWED MULTIPLE FAULTS WITH "ILS ANOMALY DET" AS CAUSE FOR LEG 6. PERFOMED DFCS GROUP 49 (LAND VERIFY) TESTMar 18, 2011 · N596AS · Boeing 737890 · Autopilot SystemSDR ASAA1159251Apu · malfunctionedON DESCENT "DIRTY SOCK" SMELL FROM AIR CONDITIONING SYSTEM. VERIFIED THAT THERE IS OIL SMELL WHEN USING LEFT AND RIGHT PACKS WITH THE APU AS THE AIR SOURCE. REMOVED AND REPLACED APU PER B737 800 AMM 49 11 00 400 803 ITEM G TO L (4) (G). RAN APU USING LEFT AMar 16, 2011 · N596AS · Boeing 737890 · APU Core EngineSDR ASAA1159164Window · malfunctionedAT 36,000 THE LEFT FWD WINDOW HEAT OVERHEAT LIGHT CAME ON. TURNED OFF THE WINDOW SWITCH LIGHT OFF. PERFORMED TASK CARD 78256003 NO DEFECTS NOTED. PERFORMED WORK ORDER 110198 COMPLIED WITH REPLACED LT #2 WINDOW PER AMM 56 12 11 000 801 & INSTALLED PER 56 12 Mar 1, 2011 · N596AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA1159060Probe · failedGE DIAGNOSTICS REPORTS AN INCREASE IN CRUISE EGT WITH A CORRESPONDING DECREASE IN EGT MARGIN ON NR 2 ENGINE ALL OTHER PARAMETERS NORMAL. FAULT CODE 77 20872 LOGGED IN NR 2 EEC FOUND S1&S4 VALUE DIFFER BY MORE THAN 200 DEG. REPLACED S4 TEMP PROBE REF MM 77 21Feb 19, 2011 · N596AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA1159056Unknown · malfunctionedAUTO THROTTLE WILL NOT ENGAGE. PERFORMED A/T CURRENT STATUS TEST, TEST PASS NO FAULTS, ALSO INTERACTIVE THROTTLE TEST PASSED NO FAULTS. GROUND VERIFICATION SUCCESSFUL.Feb 18, 2011 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA1159048Valve · failedAIR TEMPERATURE "FORWARD CAB" AND" AFT CAB NOT RESPONSIVE IN FLIGHT HAD TO CONTINUALLY INCREASE THE CONTROLS ON BOTH ALL THE WAY FULL TO MAINTAIN 21 DEG C TURNED THE CONTROLLERS TO THE OFF POSITION TRIM AIR SWITCH TO ON AS WELL AS LEFT AND RIGHT RECIRC FANS INFeb 15, 2011 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1159025Filter · dirtyWITH CABIN TEMP CONTROLLERS FULL HOT F/A'S COMPLAINING TO COLD. TEMP GAUGE SHOWS MAX TEMP OF 24 DEG AT 48DEG TAT 21 DEG. ACCOMPLISHED FIM TASK 21 61 00 810 863/864 AFT/FWD CABIN AUTO TEMPERATURE CONTROL DOES NOT OPERATE. PER STEP F1 FOUND FILTERS DIRTY. CLEFeb 12, 2011 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1158768Warning System · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL & RESETS. NR 2 CTRLR SHOWS "FLT DECK TRIM VALVE" ON BIT & PREV FLT TESTS. VERIFY TEST GO. RESET FAULT. FAULT DID NOT RETURN. NO HISTORY 60 DAYS. OPS & FUNCT CHECK CTRL CABIN TRIM VALVE GOOD. REF FIM 21Jan 12, 2011 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1158761Unknown · malfunctionedSTARTING 1 ENGINE APU GENERATOR DROPPED OFFLINE WHEN N1 RPM AT 50 PERCENT. TRIED TO START NR 2 ENGINE COULD ONLY GET 10 PERCENT N2 DUCT PRESSURE LOW. PERFORMED APU BITE CHECK FOUND FAULT CODE 49 52289. ACCOMPLISHED FIM TASK 49 54 00 810 808 STEPS F (1). CLEJan 11, 2011 · N596AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1158708Control Valve · failedWHEN RECALL IS PUSHED AND RELEASED MASTER CAUTION AIR COND ILLUMINATES AND RT PACK LIGHT ILLUMINATES EXTINGUISHES WHEN MASTER CAUTION IS PUSHED. REMOVED & REPLACED THE RIGHT TEMP CONTROL VALVE PER AMM 21 51 10.Dec 28, 2010 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1058656Sensor · failedLEFT SIDE WINDOW HOT. CORRESPONDING OVERHEAT LIGHT ILLUMINATED AFT OVERHEAD PANEL. T/S: WINDOW OHMS GOOD TAP IS CORRECT BITE SHOWS WINDOW SENSOR FAULT IN HISTORY. REMOVED WINDOW CHANGED WIRE TO SPARE SENSOR RE-INSTALLED WINDOW. OPS TEST REF 30 41 00 OPS NDec 18, 2010 · N596AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1058655Controller · faultyLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. WHILE WINDOW OVERHEAT LIGHT WAS ILLUMINATED WINDOW HEAT CONT SHOWS NO FAULTS. REMOVED & REPLACED LT SIDE WINDOW HEAT CONTROLLER REF MM 30 41 11. GROUND VERIFICATION TESTS PASSED.Dec 18, 2010 · N596AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1058654Pin · backed outLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. AFTER TURNING SWITCH OFF FOR TWO MINUTES AND BACK TO ON OVER HEAT LIGHT EXT. ON LIGHT REILLUMINATED AFTER 1 MINUTE WITH SWITCH ON. WINDOW HEAT BITE CHECK LOGGED SENSOR FAULT. NO CURRENT FAULTS. PERFORMED FIM 30Dec 18, 2010 · N596AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA1058574Unknown · malfunctionedSUSPECT RIGHT CENTER FUEL BOOST PUMP INOP. WOULD NOT PUMP 300'S IN LEVEL FLIGHT. PERFORMED CENTER TANK BOOST PUMP AUTO SHUTOFF FUNCTIONAL TEST PER AMM 28 22 00 720 805. OPS CHECK NORMAL NO DEFECTS FOUND.Dec 1, 2010 · N596AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA1058555Connector · dirtyDURING START NO START VALVE INDICATION ON NR 1 ENG. STARTER OPERATES NORMALLY. AT DP1202 PIN 5 FOUND NO GROUND PRESENT. CLEANED CONTACTS ON CONNECTORS D30434 & DP1234 AT FIREWALL. THIS RESTORED THE GROUND AT PIN 5 OF VALVE CONNECTOR. DRY MOTORED ENGINE. VNov 27, 2010 · N596AS · Boeing 737890 · Engine Starting System WiringSDR ASAA1058550Engine · malfunctionedNR 1 ENGINE LIMIT SURGE / STALL OUT OF APPROX FL220 OPERATED ENGINE AT REDUCED THRUST TO LANDING. DIVERSION TIME 27 MINUTES. LEFT EEC LOGGED ENGINE EXCEEDANCE OF 111.3 PERCENT & 106.6 PERCENT N2. ALSO LOGGED FAULT CODE 73 20331. FMU DEMAND & POSITION SIGNANov 26, 2010 · N596AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA1058525Filter · defectiveNR 1 ENG IDG OIL DPI EXTENDED. ACCOMP NR 1 ENG OIL SCAVENGE FILTER AND OIL INSPECTIONS REF MM 24 11 41. NO CONTAMINATION FOUND. RESET DPI AND REPLACED SCAVENGE FILTER AND OIL. REF MM 24 11 41. OPS CHECK NO LEAKS NOTED.Nov 19, 2010 · N596AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058314Wire Harness · misroutedWHILE ACCOMPLISHING TASK CARD 800 23EO 00095 1 STEP 16 FOUND EXISTING WIRE BUNDLE W2415 DOES NOT MATCH ROUTING PER DWG A 80023EO00095 13 FROM RTP NR 2 TO BELOW P 8 (CLAMPED IN 2413 BUNDLE LOCATION) OF P 8 TO LOWER FLOOR TRANSITION. REF L/P NR 6715232 FOR ACCOSep 28, 2010 · N596AS · Boeing 737890 · Communications System WiringSDR ASAA1058313Wire Harness · misroutedWHILE ACCOMPLISHING TASK CARD 800 23EO 00095 1 STEP 15 FOUND EXISTING WIRE BUNDLE W2413 DOES NOT MATCH ROUTING PER DWG A 80023EO00095 12 FROM RTP NR1 TO BELOW P 8. (CLAMPED IN W2415 BUNDLE LOCATION) OF P 8 TO LOWER FLOOR TRANSITION REF L/P 6715232 FOR ACCOMPLISep 28, 2010 · N596AS · Boeing 737890 · Communications System WiringSDR ASAA0852906Hydromech Unit · faultyENGINE NR 2 SHUTDOWN WHILE TAXIING IN. REPLACED HMU HIGH STAGE VALVE & HIGH STAGE REGULATOR.May 1, 2008 · N596AS · Boeing 737890 · Fuel Control/Turbine Engines
Back to N596AS