Boeing 757-2Q8

Service difficulty reports · 2,798

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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 aircraft_model_key = '7572Q8'
  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 AALA20060742Cap · missingDFW - EMERGENCY LIGHTS AT AFT LAVATORY RIGHT HAND SIDE AND SEATS 7D, 24D, 25C, AND ROW 1AB AND ROW 6AB MISSING END CAPS. REPLACED END CAPS FOR EMERGENCY LIGHTS AT AFT LAVATORY RIGHT HAND SIDE AND SEATS 7D, 24D, 25C, AND ROW 1AB AND ROW 6AB. SYSTEM GROUND CHESep 26, 2006 · N702TW · Boeing 7572Q8 · Emergency LightingSDR AALA20060741Lens · damagedDFW - EMERGENCY PATH LIGHTS AT FIRST CLASS AND SEAT 24D LENS DAMAGED. REPLACED LENS FOR EMERGENCY PATH LIGHTS AT FIRST CLASS AND SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.Sep 26, 2006 · N702TW · Boeing 7572Q8 · Emergency LightingSDR XXUA200609030Indicator · inoperativeCAPT AIRSPEED INDICATOR SPEED POINTER SHOWED ZERO AT 80 KNOTS. ACCOMPLISHED HIGH SPEED ENERGY STOP IAW MM CHAP. 5-51-14 WITH NO FINDINGS AND ISSUED A DEFERRAL IAW MEL 34-13-1 AND DEPARTED. REPLACED CAPT AIRSPEED INDICATOR IAW 34-13-02, OPS CHECKS NORMAL. MEL Sep 19, 2006 · N401JS · Boeing 7572Q8 · Airspeed/Mach IndicatorSDR 200609030Indicator · malfunctionedCAPT'S AIRSPEED INDICATOR SPEED POINTER SHOWED ZERO AT 80 KNOTS. ACCOMPLISHED HIGH SPEED ENERGY STOP AS PER MM CHAP 5-51-14 WITH NO FINDINGS AND ISSUED A DEFERRAL PER MEL 34-13-1 AND DEPARTED. REPLACED CAPT'S AIRSPEED INDICATOR IAW 34-13-02, OPS CHECKS NORMASep 19, 2006 · N401JS · Boeing 7572Q8 · High Speed WarningSDR 200609029Charger · inoperativeDURING DAILY CHECK FOUND EMERGENCY LIGHTS INOP AT OVERHEAD BINS AT SEATS 1B AND 2B. REPLACED CHARGER AND BATTERY ASSY M731 AT L1 AISLE OVERHEAD PER MM 33-51-07, OPS CHECKS OK.Sep 17, 2006 · N401JS · Boeing 7572Q8 · Emergency LightingSDR AALA20060700Cap · missingDFW - EMERGENCY ESCAPE PATH LIGHTING IN CABIN AT M10765 MISSING FORWARD END CAP. REPLACED FORWARD END CAP AT M10765 FOR EMERGENCY ESCAPE PATH LIGHTING IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.Sep 15, 2006 · N710TW · Boeing 7572Q8 · Emergency LightingSDR 200609027Bottle · lowDURING DAILY CHECK FOUND L4 DOOR SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L4 DOOR SLIDE IAW MM 25-66-01, CHECKS OK.Sep 9, 2006 · N401JS · Boeing 7572Q8 · Escape SlideSDR AALA20060624Light · inoperativeSEA - EMERGENCY LIGHT ABOVE ROW 28ABC INOPERATIVE. RELAMPED EMERGENCY LIGHT ABOVE ROW 28ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 27, 2006 · N706TW · Boeing 7572Q8 · Emergency LightingSDR ASM200608020Actuator · leakingDURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT RUDDER ACTUATOR. RUDDER ACTUATOR WAS REPLACED IAW MM 27-21-20, TESTED CORRECT.Aug 27, 2006 · N805AM · Boeing 7572Q8 · Rudder ActuatorSDR AALA20060511Light · inoperativeDFW - EMERGENCY LIGHT STRIP ON FLOOR BETWEEN SEATS 1AB AND 2AB INOPERATIVE. REPLACED LIGHT STRIP ON FLOOR BETWEEN SEATS 1AB AND 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 1, 2006 · N709TW · Boeing 7572Q8 · Emergency LightingSDR ASMF200607017Pdu · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH THE LT FLAP/SLAT SYSTEM DID NOT OPERATE HYDRAULICALLY IN NORMAL MODE PROCEEDING TO THE ALTERNATE MODE AND FLAPS DISAGREE MESSAGE APPEARED IN EICAS. FIM 27-51-00 PROCEDURE AND BITE 27-7 WERE PERFORMED TO FSEU SHOWING PDU/TJul 23, 2006 · N805AM · Boeing 7572Q8 · Trailing Edge Flap Control SystemSDR ASMF200607008Slide · incorrectAIRCRAFT RETURNED TO PLATFORM, RT DOOR NR 1 SLIDE WAS NOT ARMED CORRECTLY. SLIDE WAS ARMED IAW MM 25-66-01 AND DOOR WAS VERIFIED BY CONDITION, BEING ALL CORRECT.Jul 10, 2006 · N803AM · Boeing 7572Q8 · Escape SlideSDR AALA20060449Idg · inoperativeRIGHT ENGINE DRIVE ILLUMINATED ON CLIMB-OUT. APU FLAMED OUT TWICE AFTER INFLIGHT START. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR AND P2 SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 10, 2006 · N709TW · Boeing 7572Q8 · Alternator-Generator DriveSDR 2006FA0000728Hose · misinstalledNR 1 ENGINE HYDRAULIC PUMP SUCTION/SUPPLY DISCONNECT. DURING THE REPLACEMENT OF NR 1, ENGINE EDP DUE TO NO OFFLOAD, IT NOTED THAT THE SUPPLY DISCONNECT WAS FITTED WITH THE PUMP UNION AT THE WRONG END OF THE DISCONNECT, AND ON REMOVAL IT WAS NOTED THAT THE INTJul 3, 2006 · N719BC · Boeing 7572Q8 · Hydraulic System, MainSDR XXUA0607001Skin · canningFUSELAGE SKIN BS 1620-1640, STRINGER 29L & 29R WITH OIL CANNING.Jul 2, 2006 · N403JS · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR ASMF200606017Engine · failedAIRCRAFT RETURNED TO PLATFORM, (L ENG REV CONT) AND (L ENG PRI CONT) MESSAGES WERE SHOWN IN EICAS. FIM 78-34-00, FIGURE 112 PROCEDURE WAS PERFORMED AND LT ENGINE EXCEDENCIES PAGE WAS VERIFIED SHOWING P PDIU/EEC S PDIU/ S354-29, S354-4 CODES. MESSAGES WERE ERASJun 28, 2006 · N803AM · Boeing 7572Q8 · Engine Exhaust SystemSDR AALA20060394Manifold · leakingMSY - INFLIGHT MCO DFW SHUT DOWN NUMBER ONE ENGINE DUE TO OIL QUANTITY LOSS. LANDED MSY WITHOUT INCIDENT. FLIGHT DATA RECORDER DOWNLOADED. REPLACED LEFT HAND ENGINE BREATHER DECOILER MANIFOLD ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.Jun 20, 2006 · N710TW · Boeing 7572Q8 · Turbine Engine Oil SystemSDR ASMF200606008Engine · leakingON ARRIVAL, CAPTAIN REPORTED AIRCRAFT FLEW WITH REDUCED THRUST 1.5 HRS DUE TO LOW OIL QUANTITY INDICATION (3QTS) IN LT ENG. MX DETECTED AN OIL LEAK THRU OIL PRESSURE TRANSMITTER AND CORRECTED THE LEAK. SERVICED ENG 12 QTS, RAN ENG. NO DISCREPANCIES REPORTEJun 12, 2006 · N803AM · Boeing 7572Q8 · Turbine Engine Oil SystemSDR CNMA20060014Slide · low pressureR1 DOOR SLIDE/RAFT PRESSURE GUAGE OUT OF GREEN BAND. REMOVED AND REPLACED R1 EVACUATION SLIDE/RAFT IAW MM 25-66 OPS CHECK GOOD. VENDOR FINDINGS: FOUND BAD VALVE OVERHAULED UNIT.Jun 10, 2006 · N459AX · Boeing 7572Q8 · Escape SlideSDR AALA20060342Engine · making metalDFW - EXPERIENCED LEFT HAND ENGINE OVERHEAT AND PARTIAL POWER FAILURE AT OR NEAR 132 KNOTS. MAXIMUM EXHAUST GAS TEMPERATURE 815. SHUTDOWN LEFT HAND ENGINE PER QRH. NO FIRE INDICATION. LANDED DFW WITHOUT INCIDENT. FOUND METAL IN TAIL PIPE. REPLACED LEFT HMay 27, 2006 · N706TW · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200604009Slide · unwanted deployAT PLATFORM, GROUND PERSONNEL DEPLOYED THE R1 DOOR RAFT-SLIDE. DURING REVIEW, IT WAS DETECTED THE BAR IN ARMED POSITION. THE RAFT-SLIDE AND POWER RESERVOIR WERE REPLACED IAW MM 25-66-01 AND 52-11-33, TESTED CORRECT.Apr 16, 2006 · N806AM · Boeing 7572Q8 · Escape SlideSDR ASMF200604008Wheel · damagedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING SPOILERS LIGHT AND EICAS MESSAGE WERE SHOWN. BITE TO SPOILERS MODULE WAS PERFORMED CONTINUING THE FAILURE, REPORT WAS DEFERRED IAW MEL 27-63-1. DURING CHECK WAS DETECTED FOD IN THE LEFT WHEEL OApr 16, 2006 · N803AM · Boeing 7572Q8 · Nose/Tail Landing GearSDR ASMF200601008Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF OIL LOW PRESSURE AND HIGH EGT INDICATIONS DURING THE LEFT ENGINE STARTING. AT PLATFORM, THE TECHNICAL PERSONNEL PERFORMED AN ENGINE STARTING TEST IAW MM 71-00-04, ALL CORRECT. DURING OVERNIGHT SERVICE, THE LEFTJan 14, 2006 · N806AM · Boeing 7572Q8 · Engine Oil QuantitySDR ASMF200601006O-Ring · leakingDURING OVERNIGHT CHECK, THE RIGHT ENGINE WAS REPLACED FOR MAINTENANCE CONVENIENCE AND DURING TESTS WAS DETECTED FUEL LEAK AT FLOW TRANSMITTER. THE TRANSMITTER O-RING WAS REPLACED AND TESTED IAW MM 71-00-02, ALL CORRECT.Jan 12, 2006 · N804AM · Boeing 7572Q8 · Engine Fuel DistributionSDR ASMF200601004Idg · failedDURING TRANSIT CHECK, CAPTAIN REPORTED THAT APU OIL LIGHT TURNED ON. THE APU REPORT WAS DEFERRED IAW MEL 49-11-1 CAT C AND AIRCRAFT WAS DISPATCHED. LATER, AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CRUISE THE L GEN DRIVE EICAS MESSAGE WAS SHOWN AJan 10, 2006 · N803AM · Boeing 7572Q8 · Alternator-Generator DriveSDR ASMF200512015Iru · failedDURING TRANSIT CHECK, THE LT RDMI SHOWED HDG AND VOR FLAGS. THE SENSORS WERE CHECKED IN FMC SHOWING THAT THE THREE INERTIAL UNITS WERE CORRECT; THE LT AND CENTRAL IRS ALIGN PROCEDURE WAS PERFORMED AND THE RMIS WERE INTERCHANGED, BUT FAILURE CONTINUED. THE RT ADec 16, 2005 · N805AM · Boeing 7572Q8 · Inertial Guidance SystemSDR AALA20050815Battery Pack · dischargedLGA - EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACE BATTERY PACK AND REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 12, 2005 · N704X · Boeing 7572Q8 · Emergency LightingSDR ASMF200512004Engine · flamed outAC PERFORMED AN UNSCHEDULED LANDING, FWD AND AFT FUEL PUMP LIGHTS TURNED ON AND RT ENGINE FLAMED OUT ON FLIGHT AND DURING LANDING THE TIRES POSITION 4 AND 8 WAS FLATTED. THE TIRES POSITION 3, 4, 7 AND 8 WERE REPLACED IAW MM 32-45-01 PAGE 401. DURING MAINTENANCNov 28, 2005 · N806AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200512003Engine · noneAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE LT ENGINE WAS SHUTOFF WITH 420 OF EGT. DURING MAINTENANCE REVISION, THE LT ENGINE PARAMETERS WAS VERIFIED FINDING WITHIN LIMITS IAW MM 71-00-00. THE LT ENGINE WAS STARTED AND THE OPERATIONAL TEST WAS PERFORMED INov 28, 2005 · N806AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200511009Starter · damagedDURING LT ENGINE STARTING, THE PNEUMATIC STARTER FAILED. DURING MAINTENANCE REVISION WAS DETECTED THE PNEUMATIC STARTER WITH DAMAGE, SO IT WAS REPLACED IAW MM 80-11-01 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT.Nov 23, 2005 · N805AM · Boeing 7572Q8 · Engine StarterSDR AALA20050767Battery Pack · inoperativeDFW - FORWARD ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD ESCAPE PATH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 20, 2005 · N707TW · Boeing 7572Q8 · Emergency LightingSDR AALA20050739Fan · inoperativeSTL INFLIGHT T1727/11NOV - FLIGHT ATTENDANTS AND PASSENGERS REPORTED STRONG AND DISTINCT ODOR OF BURNING ELECTRICAL OR INSULATION IN THE CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL Nov 11, 2005 · N709TW · Boeing 7572Q8 · Air Distribution FanSDR ASMF200511003Pressure Switch · failedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF EICAS MESSAGE -L ENG FUEL FILT- WAS SHOWN. THE FUEL PUMP FILTER AND DEFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 73-11-02 AND MM 73-34-014 RESPECTIVELY, TESTED CORRECT.Nov 4, 2005 · N806AM · Boeing 7572Q8 · Engine Fuel/Oil CoolerSDR AALA20050709Guide Vane · leakingDFW INFLIGHT T450/28OCT - AFTER TAKEOFF, RIGHT ENGINE OIL TEMPERATURE INDICATED 184 DEGREES FOLLOWED BY HEAVY SMOKE IN COCKPIT AND CABIN. SOURCE CLEARED WHILE ON APPROACH AND OIL TEMPERATURE RETURNED TO NORMAL. FOUND OIL LEAKING FROM VARIABLE GUIDE VANES ON Oct 28, 2005 · N704X · Boeing 7572Q8 · Engine Air Intake SystemSDR ASMF200510011Start Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START, THE STARTER VALVE LIGHT TURNED ON AND EICAS MESSAGES, L ENG STARTED. DISPLAYED WITH START SELECTOR IN GND, ENGINE FAILED TO ROTATE. THE BREAKERS WERE RESEATED AND THE LEFT ENGINE WASOct 16, 2005 · N804AM · Boeing 7572Q8 · Engine Start Valves/ControlsSDR AALA20050676A/C Pack · smokeMCO - INFLIGHT SHORTLY AFTER TAKEOFF HAD A STRONG OIL SMELL WITH VERY LITE SMOKE IN THE CABIN. SHUT OFF THE RIGHT PACK AND THE SMELL CLEARED. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.Oct 13, 2005 · N704X · Boeing 7572Q8 · Cabin Cooling SystemSDR ASMF200510003Blade · damagedDURING TRANSIT CHECK, DETECTED A BLADE DAMAGED, LT ENGINE LPC 1ST STAGE. THE BLADE WAS OUT OF LIMITS WITH A DAMAGE OF 4 X 0.750 AT LEADING EDGE. DURING OVERNIGHT CHECK, THE TWO BLADES SET OF LPC 1 ST STAGE WAS REPLACED IAW MM 72-31-02, VIBRATION TEST NR 8 WAOct 3, 2005 · N804AM · Boeing 7572Q8 · Turbine Engine Compressor SectionSDR ASMF200510002Idg · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXING. THE LT GENERATOR SHUTDOWN AND EICAS MESSAGES (RUDDER PCU, R ELEV PCU, L ELEV PCU, EQPT CLG TEST) WERE SHOWN. THE LT IDG REPORT WAS DEFERRED AND MAINTENANCE PROCEDURE WAS PERFORMED IAW MEL 24-00-1. THE LT IDG WAS ROct 3, 2005 · N804AM · Boeing 7572Q8 · Alternator-Generator DriveSDR ASMF200509013Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES START, APU SHUT DOWN, FAULT LIGHT TURNED ON AND EICAS MESSAGE APU FAULT WAS DISPLAYED. THE FIM 49-11-00 PROCEDURES WAS PERFORMED. THE ENGINES START WAS PERFORMED WITH GROUND EQUIPMENT, ALL CORRSep 22, 2005 · N804AM · Boeing 7572Q8 · APU Core EngineSDR ASMF200509006Eec · failedCAPTAIN REPORTED RT ENGINE EGT INDICATION WITH OSCILLATIONS OF 100 GRADES IN EICAS. THE RT EEC EBG AND THERMOCOUPLE HARNESS JUNCTION BOX WERE REPLACED IAW MM 73-21-04 AND 77-51-12, RT ENGINE WAS TESTED IAW MM 71-00-01, ALL CORRECT.Sep 13, 2005 · N806AM · Boeing 7572Q8 · Fuel Controlling SystemSDR ASMF200509001Acm · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK, THE AIR CONDITION PACKAGE FAILED WITH EICAS MESSAGES OF RIGHT ENGINE PURGE VALVE DID NOT OPERATE. REPORT WAS DEFERRED IAW MEL 36-11-1.Sep 1, 2005 · N804AM · Boeing 7572Q8 · Cabin Cooling SystemSDR AALA20050483Pan · corrodedMCI - CORROSION FOUND AROUND FORWARD LAVATORY DUMP CHUTE BETWEEN FORWARD LAVATORY SERVICE PAN AND UPPER PAN IN AREA 12 INCHES BY 12 INCHES. REPLACED FORWARD LAVATORY SERVICE PANEL UPPER PAN.Jul 27, 2005 · N702TW · Boeing 7572Q8 · Waste Disposal SystemSDR ASMF200507016Elevator · out of rigCAPTAIN REPORTED THAT THE MESSAGE -ELEV ASYM- WAS SHOWN IN EICAS. THE FIM 27-09-00 FIG. 106 PROCEDURE WAS PERFORMED AND DURING CONTROLS TESTS REPEATED THE MESSAGE. DURING ELEVATOR SURFACE INSPECTION WAS DETECTED ASYMMETRY IN ELEVATORS. AIRCRAFT WAS SENT TO THEJul 21, 2005 · N804AM · Boeing 7572Q8 · Elevator Control SystemSDR AALA20050450Light · inoperativeDFW FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT AT SEAT 1AB INOPERATIVE. REPLACED FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT ASSEMBLY AT SEAT 1AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)Jul 19, 2005 · N707TW · Boeing 7572Q8 · Emergency LightingSDR ASMF200507013Window · openAIRCRAFT REJECTED TAKEOFF AT 90 KTS AS A CONSEQUENCE OF LT WINDSHIELD OPENED WITHOUT APPARENT REASON. WINDSHIELD ADJUSTMENT CHECKED IAW MM56-11-01, TESTED CORRECT. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT.Jul 17, 2005 · N806AM · Boeing 7572Q8 · Flight Compartment WindowsSDR AALA20050438Monitor · odorELECTRICAL FUMES IN CABIN DURING FLIGHT. DIVERTED TO MOB. FIRE DEPARTMENT REPORTS VIDEO SCREEN BETWEEN ROWS 9 AND 10 LT SIDE AS SOURCE. INSPECTED AND NO DAMAGE TO CONNECTORS NOTED. REPLACED MONITOR AND RESET CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL Jul 12, 2005 · N712TW · Boeing 7572Q8 · Entertainment SystemSDR ASMF200506021Starter · failedACFT RETURNED TO PLATFORM. DURING RT ENGINE STARTING, N2 INDICATION REACHED 23 PERCENT AND WENT TO ZERO. PNEUMATIC STARTER AND PNEUMATIC STARTER VALVE REPLACED IAW MM 80-11-01 / -02, TESTED CORRECT.Jun 19, 2005 · N804AM · Boeing 7572Q8 · Engine StarterSDR ASMF200506013Idg · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING THE LEFT ENGINE STARTED, THE N2 REACHED 30 PERCENT AND IT DID NOT INCREASE. THE LEFT ENGINE WAS STARTED AGAIN OPENING THE STARTER VALVE MANUALLY AND IT STARTED TO SLOW, APPEARING THE L DRIVE AND L GEN OJun 10, 2005 · N805AM · Boeing 7572Q8 · Alternator-Generator DriveSDR ASMF200506003Idg · failedAIRCRAFT RETURNED, LT GENERATOR FAILURE, APU DID NOT START AT 35 000 FT, 24 22 25 EICAS MESSAGES, 01 GEN OFF DISPLAYED AND 01 AS BUSS OFF REMAINED ILLUMINATED. QRH ABNORMAL PROCEDURE WAS PERFORMED, PAGE 09-03, RETURNING. DURING TEST WAS DETECTED LOW QUANTITY OJun 2, 2005 · N805AM · Boeing 7572Q8 · APU ControlsSDR ASMF200505027Engine · failedCAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITCH WAS SHUT OFF AND THE ACCELERATOR WAS HELD BUT LIGHT CONTINUED. ENGINE WAS SHUT DOWN. AT PLATFORMay 24, 2005 · N805AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)
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