Workbook 4

What is the primary purpose of the fire/overheat protection systems in an aircraft?. To extinguish fires automatically. To provide indication to the flight crew when a fire or overheat condition exists. To cool down overheated components.

Which of the following areas are typically equipped with automatically operated fire detection and extinguishing systems?. Engines and Cargo Compartment. Lavatory. Wheel Well and APU.

Which system is manually operated for fire detection and extinguishing?. Lavatory. Engine system. Flight compartment windows.

Which system is protected by fire/overheat detection but not necessarily extinguishing systems, and is manually operated?. APU system. Cargo system. Wheel well system.

How many fire extinguisher bottles protect the cargo compartment?. 1 bottle. 2 bottles. 3 bottles.

Which fire control panel is used to manage the fire extinguishing system for the cargo compartment?. Panel 8 fire control panel. Panel 8 cargo fire control panel. Panel 40 apu fire control panel.

How many fire extinguisher bottles protect each engine?. 1 bottle per engine. 2 bottles. 3 bottles per engine.

Which panel is used to operate the fire extinguishing system for the APU?. Panel 8 fire control panel. Panel 8 cargo fire control panel. Panel 8 apu remote control panel and Panel 40 apu fire control panel.

Besides the APU remote control panels, from where else can the APU fire extinguisher bottle be discharged?. Pilot's overhead panel. Nose landing gear. Main landing gear.

What are the three main air sources for the pneumatic system of an aircraft?. APU, Landing Gear, and Brakes. Engines, External Ground Power Unit, and APU. Cabin Pressurization, Engines, and Wing Anti-Ice.

How many ground air connectors are typically installed in the Ground Air Supply System?. 1 connector. 2 connectors. 3 connectors.

Which of the following are considered Primary Flight Controls?. Slats and Flaps. Ailerons, Rudder, Elevator and spoiler. Spoilers and Stabilizer Trim.

Which of the following are considered Secondary Flight Controls?. Ailerons and Elevators. Leading edge Slat, Trailing edge Flap, and Stabilizer trim. Rudder and Spoilers.

How many Ailerons are installed on the aircraft, and how are they distributed?. 2 Ailerons, 1 on each wing. 4 Ailerons, 1 inboard and 1 outboard per wing. 6 Ailerons, 3 on each wing.

How many Elevators are installed, and how are they distributed?. 2 Elevators, 1 on each side of the horizontal stabilizer. 4 Elevators, 1 inboard and 1 outboard per side. 6 Elevators, 3 on each side.

How many Spoiler panels are on each wing, and how are they numbered?. 2 panels per wing, numbered 1-2. 4 panels per wing, numbered 1-4. 6 panels per wing, 2 inboard and 4 outboard, numbered from left to right.

How many Flaps are installed on each wing?. 2 Flaps per wing. 4 Flaps per wing (4 inboard and 1 outboard on each wing). 5 Flaps per wing.

How many Slats are installed on each wing?. 6 Slats per wing (5 outboard and 1 inboard on each wing). 12 Slats per wing. 5 Slats per wing.

What is the primary function of the Horizontal Stabilizer Trim?. To control pitch during rapid maneuvers. To provide a quick response to pilot inputs. To make long-term changes in the airplane's attitude.

How many actuators move the rudder, and what powers them?. Two actuators powered by one hydraulic system. Three actuators, each powered by a separate hydraulic system. Four actuators powered by the electrical system.

How many wheels and brakes are mounted on the Main Landing Gear (MLG)?. 4 wheels and 4 brakes per gear. 6 wheels and 6 brakes per gear. 8 wheels and 8 brakes per gear (4 wheels and 4 brakes on a dual axle truck per gear).

What is the maximum nose wheel steering angle when using the tiller?. 7.5 degrees. 60 degrees. 65 degrees.

What is the maximum nose wheel steering angle when using the rudder pedals?. 7.5 degrees. 15 degrees. 30 degrees.

What is the purpose of the tail skid on the Boeing 767-300?. To improve aerodynamic stability. To protect the aft fuselage area in case of a tail strike during takeoff or landing. To provide an additional braking system.

Which areas are protected by the aircraft's Ice Protection System?. Fuselage and Engines. Wing leading edge slats, Engine nose cowls, and Pitot static probes. Landing gear doors and Flaps.

Which of the following probes are protected by the Ice Protection System?. Cabin Altimeter Probes. Pitot static probes and Angle of attack probes (AOA). OAT (Outside Air Temperature) probes.

Which probes, related to engine performance, are protected by the Ice Protection System?. EGT (Exhaust Gas Temperature) probes. Engine Probes Pt2/Tt2 and Engine Mach Probes. Oil Temperature probes.

Which of these components are protected by the Ice Protection System?. Main landing gear wheels. Flight compartment windows and Water and waste lines. Aileron control surfaces.

What is the function of the Windshield Wiper system?. To defrost the windshields. To assist in moisture removal from the windshields, improving forward visibility. To clean the windshields of dirt and debris.

Which of the following is NOT protected by the Ice Protection System?. Wing leading edge slats. Engine nose cowls. Cargo compartment liners.

For manual fire detection and extinguishing, which area is typically NOT listed?. Engine system. APU system. Lavatory.

How many fire extinguisher bottles protect the APU system?. 1 bottle. 2 bottles. The number varies depending on the aircraft model.

Which of these is a primary flight control surface?. Trailing edge flap. Aileron. Leading edge slat.

The purpose of the Horizontal Stabilizer Trim is to: Quickly change the aircraft's attitude during flight. Provide fine-tuning for long-term attitude adjustments. Act as a primary pitch control surface.

How many wheels are on the Main Landing Gear (MLG) in total?. 4. 6. 8.

The tail skid on the Boeing 767-300 is designed to: Aid in braking during landing. Prevent damage to the aft fuselage if the tail hits the ground. Improve directional stability on the ground.

Which of the following is protected by the Rain Protection system?. Engine Inlet Vanes. Windshield Wipers. Wing Leading Edges.

Which system provides air for engine starting and ground operations?. Bleed air from the flight deck. APU (Auxiliary Power Unit) or external ground source. Cabin environmental control system.

What is the distribution of Spoilers on each wing?. 2 inboard and 2 outboard. 2 inboard and 4 outboard. 4 inboard and 2 outboard.

The 'stabilizer trim (when used or air or ground speed brakes)' is classified as: Primary Flight Control. Secondary Flight Control. Landing Gear System component.

What is the maximum nose wheel steering angle when using the rudder pedals?. 65 degrees. 30 degrees. 7.5 degrees.

The Lavatory fire system is generally operated: Manually by the flight crew. Automatically. By a dedicated ground crew.

What is the purpose of the wheel well overheat detection system?. To extinguish fires in the wheel well. To alert the crew to excessive temperatures in the wheel well area. To cool the brakes after landing.

Which of the following is NOT a primary flight control?. Rudder. Elevator. Flap.

How many actuators are responsible for moving the rudder?. 2. 3. 4.

Which system helps improve forward visibility in rain?. Ice Protection System. Rain Protection System (Windshield Wipers). Pneumatic System.

How many fire extinguisher bottles protect the cargo compartment?. 1. 2. 3.

Which panel is used to discharge the APU fire extinguisher?. Panel 8 fire control panel. Panel 40 apu fire control panel. Both Panel 8 apu remote control panel and Panel 40 apu fire control panel.

How many wheels are on the Main Landing Gear (MLG)?. 4. 6. 8.