MH-65E Flight Crew Operations
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Questions and Answers

What is the purpose of the Engine Fire Warning and Extinguisher Controls?

  • To signal an engine fire and allow for extinguishing it (correct)
  • To engage the main rotor system
  • To manage fuel usage effectively
  • To monitor engine performance metrics

Which component is responsible for the lubrication of the main gearbox?

  • Primary Hydraulic System
  • Main Gearbox Lubrication System (correct)
  • Main Rotor Blade
  • Tail Rotor System

What is the primary purpose of this publication regarding the MH-65E flight crews?

  • To reduce the weight of the aircraft
  • To provide information on flight plan manipulation and safety (correct)
  • To offer guidelines for maintenance procedures
  • To detail the specifications of the flight director system

What does the Fuel Quantity Indicator display?

<p>Amount of fuel remaining in the tanks (B)</p> Signup and view all the answers

Which modes are mentioned as part of the flight director's interactions?

<p>Hover and Transition modes (A)</p> Signup and view all the answers

What is indicated by the Main Gear Box Indications and Warning Messages?

<p>Issues related to the main gearbox (D)</p> Signup and view all the answers

What does the Training Switch enable in the engine?

<p>One engine inoperative training mode (C)</p> Signup and view all the answers

What is one of the benefits of the automated interactions in the MH-65E FD and FMS?

<p>Reduces pilot workload during approach profiles (A)</p> Signup and view all the answers

What is the responsibility of commanding officers regarding this supplement?

<p>Ensure the information reaches all affected personnel (D)</p> Signup and view all the answers

Which system is responsible for the control and indicators of the landing gear?

<p>Landing Gear Hydraulic System (B)</p> Signup and view all the answers

What are the Main Rotor Blade responsible for?

<p>Generating lift during flight (B)</p> Signup and view all the answers

What does the warning in the document emphasize?

<p>Export laws are strictly enforced and violators face penalties (A)</p> Signup and view all the answers

Where is the Fuel Cell Location indicated?

<p>In the Fuel Management Panel (A)</p> Signup and view all the answers

Which statement is about the destruction of classified documents?

<p>Follow procedures specified in DoD guidelines for destruction (A)</p> Signup and view all the answers

Where should unclassified, limited documents be destroyed?

<p>By any method that prevents disclosure of contents (B)</p> Signup and view all the answers

What is not described as part of the MH-65E flight crews' operation?

<p>Performing manual flight maneuvers exclusively (C)</p> Signup and view all the answers

What component is primarily identified for radar display features?

<p>Radar Test Pattern (A)</p> Signup and view all the answers

Which component would likely be responsible for data and voice privacy?

<p>Data and Voice Privacy-200 Control Head (B)</p> Signup and view all the answers

Which display component is used for showing radar status on the primary flight display?

<p>Radar Status Displayed on Primary Flight Display (B)</p> Signup and view all the answers

Which subsystem is associated with the Electro-Optical Infrared Sensor System?

<p>Electro-Optical Infrared Sensor System Subsystems (C)</p> Signup and view all the answers

What feature enhances the clarity of rain on radar displays?

<p>Rain Echo Attenuation Compensation Technique Mode (B)</p> Signup and view all the answers

Which unit is designed for control of display indicators?

<p>Display Unit Controls and Indicators (B)</p> Signup and view all the answers

What is the primary intent of the automation discussed?

<p>To reduce pilot workload in specific flight scenarios (B)</p> Signup and view all the answers

Which component would be directly linked with mission data recording?

<p>Mission Data Recorder (C)</p> Signup and view all the answers

Which option refers to controls for a joystick unit?

<p>Joystick Control Unit (A)</p> Signup and view all the answers

At what speed does the climb rate become limited to +/- 225 FPM?

<p>Below 40 KIAS (C)</p> Signup and view all the answers

What occurs if the course for the next leg differs from the hover heading?

<p>A turn will occur almost immediately (C)</p> Signup and view all the answers

To prevent an automated transition from THOV or HOV, what must be done first?

<p>Deselect the THOV or HOV lateral modes (D)</p> Signup and view all the answers

How can the active LND, HOV, STP, or APR leg be removed from the flight plan?

<p>By executing a direct-to a future leg or deleting the leg (A)</p> Signup and view all the answers

What will engage and capture the current aircraft altitude and speed when certain conditions are met?

<p>BALT/RALT and ASPD/GSPD (A)</p> Signup and view all the answers

What is the effect of selecting a source other than ACP (i.e. VOR/ILS or TCN)?

<p>It sequences the flight plan by pilot manipulation (A)</p> Signup and view all the answers

What happens when the flight plan changes from MANUAL back to AUTO?

<p>The system engages automated transitions to new legs (C)</p> Signup and view all the answers

What is one of the diagrams included in the material?

<p>Cockpit Instruments and Controls Diagram (D)</p> Signup and view all the answers

Which table is mentioned in the list of tables?

<p>Table 1-A-1 (A)</p> Signup and view all the answers

What section contains the Coast Guard Rescue Swimmer Deployment hand signals?

<p>FO-11 (D)</p> Signup and view all the answers

Which electrical system is detailed in the content?

<p>Direct Current Electrical System (B)</p> Signup and view all the answers

What is covered under the general arrangement diagrams?

<p>General Arrangement Diagram Right (A)</p> Signup and view all the answers

Which of the following is NOT a type of diagram mentioned?

<p>Turbulence Simulation Diagram (C)</p> Signup and view all the answers

What is the primary purpose of the Coast Guard Boat Crew Hand Signals indicated?

<p>To communicate effectively during operations (D)</p> Signup and view all the answers

Which section indicates the alternating current electrical system?

<p>FO-8 (A)</p> Signup and view all the answers

What is the primary purpose of the Liquid Crystal Display (KY-100) Annunciators?

<p>To indicate system warnings and statuses (D)</p> Signup and view all the answers

Which function does the Data and Voice Privacy-200 Value Pushbutton serve?

<p>To enable or disable data and voice privacy (D)</p> Signup and view all the answers

What does the Target Alert Depth and Range Characteristics specify?

<p>The parameters for alerting on nearby targets (C)</p> Signup and view all the answers

In relation to video integrated processor levels, what do the Display Levels indicate?

<p>Operational statuses of system functions (C)</p> Signup and view all the answers

Which of the following is NOT a feature of the TCAS Modes?

<p>Navigation performance readings (C)</p> Signup and view all the answers

What does the Joystick Control Unit primarily manage?

<p>Aircraft maneuverability and control inputs (D)</p> Signup and view all the answers

Which statement about ESS MFD Only Modes is true?

<p>They enable visual representation of system metrics. (C)</p> Signup and view all the answers

What is the role of the Tactical and Beacon Scan Status?

<p>To assess and display situational awareness (A)</p> Signup and view all the answers

Flashcards

Automated Features in MH-65E

The MH-65E flight director (FD) and civil flight manager systems (FMS) have automated features designed to reduce the workload of pilots during various approach profiles.

Purpose of MH-65E FD and FMS

The MH-65E Flight Director (FD) and Civil Flight Manager Systems (FMS) contain automated interactions designed to make flight operations easier and safer.

Flight Director (FD)

A flight director (FD) is a cockpit instrument that provides guidance to pilots during flight

Flight Plan (FPLN)

A flight plan (FPLN) is a pre-determined route or plan of flight.

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Transition to Hover (THOV) Lateral Mode

A transition to hover (THOV) lateral mode is a flight director (FD) mode designed to guide the aircraft smoothly into a hovering position.

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Hover (HOV) Mode

A hover (HOV) mode is a flight director (FD) mode that helps maintain a stable hovering position once the aircraft has reached it.

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Purpose of the Document

The intent of the document is to inform MH-65E flight crews about the safe use of Flight Director (FD) modes during flight plan (FPLN) manipulation.

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Flight Plan and Flight Director Interaction

Flight plans (FPLN) can be manipulated while using Flight Director (FD) modes like Transition to Hover (THOV), Hover (HOV), and FPLN.

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Liquid Crystal Display (LCD)

A type of display technology that uses liquid crystals to produce images.

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Data and Voice Privacy Control Head

A control unit used for privacy settings in data and voice communication systems.

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Data Storage Unit

A device designed for storing large amounts of data.

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Radar Display Features

Visual features on a radar display showing information like range, altitude, and weather.

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Controller

A device responsible for controlling and managing the functions of a system.

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Rain Echo Attenuation Compensation Technique

A technique used to compensate for signal loss caused by rain.

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Radar Test Pattern

A pattern used for testing and calibrating radar systems.

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Radar Status Display

A display showing the status of the radar system in the cockpit.

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FO-1. General Arrangement Diagram Left

A diagram that shows the arrangement of parts on the left side of the helicopter, such as the engine, transmission, rotor system, and landing gear.

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One Engine Inoperative Training Mode Display

A display that shows the status of the training mode, specifically indicating if one engine is inoperative.

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Training Switch

A switch that enables pilots to practice operating with simulated engine malfunctions.

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FO-2. General Arrangement Diagram Right

A diagram that shows the arrangement of parts on the right side of the helicopter, such as the engine, transmission, rotor system, and landing gear.

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FO-3. Cockpit Arrangement Diagram

A diagram that shows the layout of the cockpit, including instruments, controls, and crew seating.

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Engine Ratings

The power levels at which engines can operate, indicated by specific limits.

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Hover Increased Power Search and Rescue Mission Usage Flag Symbology

A visual representation of special conditions indicating an increased power demand during a search and rescue mission.

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FO-4. Cockpit Instruments and Controls

A diagram that shows the location, function, and connectivity of all the instruments and controls in the cockpit.

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FO-6. Fuel Supply System

A diagram that shows the flow of fuel from the tanks to the engine.

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Engine Fire Warning and Extinguisher Controls

A system that detects an engine fire and allows for its suppression through specific controls.

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Main Rotor Head

The core component of a helicopter's main rotor system, responsible for rotating the blades.

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FO-7. Direct Current Electrical System

A diagram that shows the electrical system that uses direct current, such as the battery and the generator.

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FO-8. Alternating Current Electrical System

A diagram that shows the electrical system that uses alternating current, such as the alternator and the electrical bus.

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Main Rotor Blade

A rotating part of the helicopter, responsible for generating lift and contributing to propulsion.

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Tail Rotor System

A system located at the tail of the helicopter, responsible for controlling yaw (rotation around a vertical axis) and stabilizing the aircraft.

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FO-9. Automatic Flight Control System Block Diagram

A diagram that shows the components and connections of the automatic flight control system, which helps maintain stability and control of the helicopter.

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Automated Transition

This automation is designed to reduce pilot workload during missed approaches or flight plan changes, ensuring the helicopter transitions to the new leg smoothly.

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Limited Climb Rate (below 40 KIAS)

The maximum climb rate in the automated transition is limited to +/- 225 FPM when the helicopter's speed is below 40 KIAS.

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Limited Climb Rate (above 40 KIAS)

For speeds above 40 KIAS, the climb rate is controlled by the CDU FD SELECT VSPEED setting.

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Automated Turn

When the new leg's course is different from the hover heading, the helicopter will initiate a turn almost immediately, potentially even at low speed without considering wind conditions.

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Automatic Altitude and Speed Capture

If a different source (VOR/ILS or TCN) is chosen for the flight plan, the helicopter will automatically capture its current altitude and speed.

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Preventing Automated Transition from THOV or HOV

To prevent an automated transition from THOV or HOV mode, the lateral modes need to be deselected before editing the flight plan.

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Exiting THOV or HOV

By selecting another mode (HAUG, RALT, BALT) or deselecting all modes, the helicopter will exit THOV or HOV.

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Removing Active Leg

After exiting THOV or HOV, the active leg can be removed by using direct-to, deleting it, or changing the sequencing mode from MANUAL to AUTO .

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Annunciators

Visual cues on a display that inform the pilot of important system status, warnings, or malfunctions.

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200 Value Pushbutton

A button on the control panel that allows pilots to securely transmit or receive data and voice communications.

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Primus 700 Functions Table

A table that lists all the different functions available in the Primus 700 system.

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Display Levels and VIP Levels

Different display levels on the instruments are linked to the corresponding levels within the Video Integrated Processor (VIP)

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Electronic Centralized Aircraft Monitoring System (EICAS)

A system that provides warnings and alerts to pilots based on information from various aircraft systems.

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Joystick

The flight control handle that pilots use to manipulate the aircraft's direction.

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Tracker Mode

A mode that allows pilots to track and identify aircraft targets, displaying information about them on the display.

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