V-22 EP's Exam 31 Questions with Answers 2023,100% CORRECT

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V-22 EP's Exam 31 Questions with Answers 2023 Land Immediately - CORRECT ANSWER Execute a landing WITHOUT DELAY. Continued operation of the aircraft is extremely hazardous. If over water, conduct... a controlled ditching without delay. The primary consideration is to assure the survival of occupants. Land as soon as Possible - CORRECT ANSWER Execute a landing at the nearest available site which a safe landing can be made. Land as soon as Practical - CORRECT ANSWER Extended flight is not recommended. The landing site and duration of flight is at the discretion of the pilot-in-command, but no farther than the next scheduled point of landing. M.A.P-Execute - CORRECT ANSWER 1. Maneuver Severity — Reduce 2. Airspeed — Reduce below 200 KCAS 3. PFCS — Reset 4. "M.P. — Execute" is the same procedure as "M.A.P. — Execute" except airspeed is not a factor for aircraft control or in executing a PFCS Reset. NOTE Above 200 KCAS, certain swashplate and elevator actuator faults may inhibit PFCS RESET. If a PFCS RESET cannot be reset, reduce airspeed below 200 KCAS. PFCS RESET above 200 KCAS will not produce undesirable transients. Single Engine Profile - CORRECT ANSWER Wings level, with the following configurations: CONV: Flaps-Auto, NAC-60, ASPD-90 APLN MAX CLIMB: Flaps-Auto, Nr-100%, AOA-80% EN ROUTE: Flaps-Auto, Nr-84%, ASPD-As Req. FIRE, Engine, On Ground - CORRECT ANSWER NOTE Bleed air or other hot gas leakage may trigger an engine fire warning without associated secondary indications. *1. ECLs — OFF *2. T-handle (affected engine) — ARM If fire persists: *3. DISCHARGE button — Press *4. Emergency Shutdown — Execute FIRE, Engine, In Flight - CORRECT ANSWER NOTE Bleed air or other hot gas leakage may trigger an engine fire warning without associated secondary indications. Expect affected engine to be low power. Cockpit secondary indications may include increased fuel flow and elevated MGT with low engine torque. *1. Single engine profile — Establish If fire confirmed: *2. ECL (affected engine) — OFF *3. T-handle (affected engine) — ARM If fire persists: *4. DISCHARGE button — Press If fire persists: *5. Land immediately FIRE, Wing, In Flight - CORRECT ANSWER NOTE A sustained MFD FIRE annunciation is an indication of a persistent fire. The FIRE SUPPRESSION panel indicator light(s) may or may not provide positive indication of a sustained fire. *1. TPUMP BOOST — OFF If fire persists: *2. Land immediately. FIRE, Wing, On Ground - CORRECT ANSWER *1. Emergency Shutdown — Execute ENG, Dual, NAC greater than or equal to 60° - CORRECT ANSWER WARNING Dual engine loss in CONV will result in a rapid Nr decay. If Nr decay is not arrested rapidly, autorotation is not recoverable. Simultaneously (first four) *1. TCL — Full aft *2. Nacelles — Max rate to aft stop *3. Airspeed — 120 KCAS *4. FLAPS — 0° *5. APU — EMERG RUN/ENGAGE *6. Landing gear — Down At 150 ft AGL: *7. Cyclic — Flare, level prior to impact *8. TCL — Full forward ENG, Dual, NAC < 60° - CORRECT ANSWER *1. TCL — Full aft *2. Nacelles — Max rate to downstop, then 84% Nr *3. Airspeed — 170 KCAS *4. FLAPS — AUTO *5. APU — EMERG RUN/ENGAGE *6. ELP — Intercept NOTE After configuring for glide, attempt engine restart if conditions permit. *7. Landing gear — EMERG DOWN (As required) (allow 20 seconds for extension) Extension of landing gear is recommended only if assured of landing on a prepared surface. Landing with gear extended on an unprepared surface may result in loss of aircraft control. NOTE Expect 200 to 600 fpm increase in rate of descent with landing gear extended. At approximately 400 — 200 ft AGL: *8. Mild Flare — EXECUTE, holding 8−10 nose up. Expect airspeed to decay to 120−115 KCAS on touchdown. NOTE Flaps FULL can be used on short final to slightly extend the flare. ENG, Single, Hover - CORRECT ANSWER *1. TCL — Full forward *2. Cyclic — Level attitude prior to touchdown CAUTION Aft stick control margin significantly decreases as nacelles are rotated towards 70 degrees. Consideration should be given to adjusting the nacelles aft prior to touchdown in order to achieve normal landing attitude. If a flyaway is to be attempted: *3. ENG, Single, In Flight — Execute NOTE Aircraft vertical velocity is sensitive to nacelle beep rate. During climb out, ensure beep rate is slow enough to not induce an uncommanded sink rate. ENG, Single, In Flight - CORRECT ANSWER *1. TCL — Full forward *2. Single engine profile — Establish ELEV - CORRECT ANSWER WARNING If the elevator fails trailing edge down, unrecoverable loss of longitudinal control may occur above 40 KCAS with nacelles less than 85°. *1. Cyclic — Roll toward 60 degrees AOB *2. VTOL — Convert ICDS - CORRECT ANSWER WARNING Single engine with an ICDS failure is unrecoverable below 170 to 175 KCAS. CAUTION Flapping controller is lost. Extended operations between 10° and 75° nacelle should be avoided due to heat buildup and possible elastomeric bearing failure. Transition/convert according to the following to minimize potential for damage. NAC KCAS 0 180 30 150 60 100 NOTE -The ICDS Failure warning will post in the event of a triple Nr sensor failure on one side. -Resetting PFCS may cause undesirable transient response in thrust and Nr. -Average rotor speed will increase to 104% geater than or equal to 60 deg. nacelle to preserve lateral control authority. -Interim Power must still be selected to access higher mast torque levels within the normal Interim Power envelope. -Consideration should be given to reducing gross weight and DA. *1. M.A. — Execute PRGB or TAGB - CORRECT ANSWER If secondary indications confirm impending gearbox failure: *1. Land immediately SINK - CORRECT ANSWER If VRS is suspected: *1. Nacelles — Beep forward (max rate for 2 sec/<15°) *2. Cyclic — Forward to accelerate *3. TCL — Fixed (alt permitting) CAUTION TCL power application within VRS may cause uncontrollable roll. STALL - CORRECT ANSWER *1. Maneuver Severity — Reduce to decrease angle of attack and load factor *2. TCL — Forward If unable to complete steps 1 and 2: *3. CONV — Convert, max rate *4. TCL — As required ECL NOT IN FLY - CORRECT ANSWER *1. ECLs — FLY (immediately) FCC X/Y FAIL (1/2, 1/3, 2/3) - CORRECT ANSWER WARNING Expect: — Severe difficulty controlling the aircraft in all axes. — Loss of TCRS, ECL functionality, conversion protection, SLL, primary flapping protection, and reliable stall warning. CAUTION -Overtorques are possible due to the loss of TCRS. Pilot will need to manually manage Qm. Lateral maneuvering above 109% mast torque may result in PRTR OVERTORQUE. -Backup flapping controller provides trimmed-flight flapping protection; however, in maneuvering flight the aircraft is still vulnerable to critical flapping condition. -Operations between 10° and 75° nacelle may result in destructive heat buildup in the elastomeric bearing. NOTE -Keeping the TCL softstop active may aid in reducing overtorques. Pushing through the softstop may be necessary to achieve 100% Qm. -With a FCC X/3 failure, setting flaps to 0 in APLN may improve roll control. Reset flaps to AUTO before landing. -With a FCC X/3 failure, establishing a steady-heading sideslip and keeping airspeed above 170 KCAS will help preserve some lateral authority in APLN. -The trim system will be degraded and AFCS trim backdrives are disabled. *1. M.P. — Execute FEATHERING HIGH HOT - CORRECT ANSWER CAUTION CONV operations may not clear the caution. APLN at low angle of attack or VTOL at low airspeed (<40 KCAS) is recommended. Destructive heat buildup may occur in as little as 5 minutes after caution posts if heat buildup is allowed to continue. NOTE Once the condition has been alleviated, the FEATHERING HIGH HOT condition may take several minutes to clear. *1. Maneuver Severity — Reduce FLAPPING HIGH HOT - CORRECT ANSWER CAUTION Operations between 35° and 75° nacelle may not clear the caution. Flapping is most critical near 60° nacelle, high GW, forward CG, and high DA. Destructive heat buildup may occur in as little as 1 minute after caution posts if heat buildup is allowed to continue. NOTE Once the condition has been alleviated, the FLAPPING HIGH HOT condition may take several minutes to clear. *1. Maneuver Severity — Reduce PLT NAC CONTR FAIL - CORRECT ANSWER *1. NAC CONTR switches (both sides) — Attempt to override nacelle motion *2. NAC CONTR DSBL switches — DSBL PRGB CHIPS - CORRECT ANSWER If abnormal secondary indications exist (oil pressure/temperature, noises, vibrations): *1. Land immediately PRTR VIBRATION HIGH - CORRECT ANSWER WARNING - Excessive pitch link wear can lead to catastrophic failure without initially feeling severe vibration levels. Nacelle pitching motion may provide the best indication of increasing vibration levels. - With high vibration levels, 0° nacelle may cause catastrophic failure of the nacelle downstop. *1. Maneuver Severity — Reduce If severe vibration levels are present and rotor system failure seems imminent: *2. Land immediately (ROL recommended) ROTOR LOAD HIGH - CORRECT ANSWER Indicates excessive oscillatory loads in critical rotor components. The intent of the emergency procedure is to minimize angle-of-attack and to utilize the FFR to reduce critical rotor loading conditions. NOTE Once the condition has been alleviated, the caution should clear within seconds. *1. Maneuver Severity — Reduce Emergency Shutdown - CORRECT ANSWER *1. ECLs — OFF (Simultaneously) *2. T-handles — ARM *3. ROTOR BRAKE — ON CAUTION If the reason for the emergency shutdown is due to a ICDS Fail or midwing fire or midwing accessories, do not use the ROTOR BRAKE for shutdown. *4. APU — STOP (As required) *5. BATTERY — OFF *6. Egress — As required. Cockpit or Cabin Fire In Flight - CORRECT ANSWER *1. EMERGENCY OXYGEN/Masks — ON NOTE The emergency oxygen system is designed to provide approximately 5 minutes of 100% oxygen for a crew of 4. *2. TPUMP BOOST - OFF *3. Portable fire extinguishers — Employ If fire persists: *4. Land immediately Out of Control Recovery Procedures - CORRECT ANSWER *1. Controls — Neutral *2. Pedals — Cancel yaw *3. AOA — Assess Smoke and Fume Elimination - CORRECT ANSWER NOTE The emergency oxygen system is designed to provide approximately 5 minutes of 100% oxygen. *1. EMERGENCY OXYGEN/Masks — ON Single Engine Waveoff - CORRECT ANSWER *1. TCL — Full forward *2. Single Engine profile — Establish. NOTE Aircraft vertical velocity is sensitive to nacelle beep rate. Ensure beep rate is slow enough to command an acceleration without inducing an uncommanded sink rate. [Show More]

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