What is the max take off and landing weight of t41 under normal category in pounds?

(a)  

I am located at the instrument panel, illuminated when the engine manifested a metal in the oil system and connected to a chip detector plug in the oil drain sump.

What am I?

(a)  

When the fuel drops to 9 gallons in either fuel tank, the sensing unit will illuminate the applicable low fuel warning light.

What am I?l

(a)  

Both pilots are required a headset to have communication to each other. Press to talk are integrated at each control yoke for press to talk function. Pressing toggle switch fore transmit outside the aircraft and aft for the intercom.

What am I?

(a)  

Removal of cabin door is accomplished either removing the screws which attached the hinges or by removing the jettisonable hinge pins.

(a)  

In case of emergency removal of cabin doors is accomplished by pulling out the jettison handle on both side of the pilots.

(a)  

I provide comfortable control forces and ease of maneuvering of the aircraft. Control wheel (yoke) and pedals are of conventional type. Connected to the movable surface by cables and rods.

What am I?

(a)  

I am utilized to control attitude and directional control of the aircraft. Output from the cockpit controls surfaces through cable runs and/or mechanically linkage.

(a)  

T41 Aircraft Rudder Control System

Supply the missing data.

(a)  

What is automatically determined when rudder are rigged against return springs 6.50 inches from the firewall?

(a)  

I am operated by forward and aft movement of the control yoke.

What am I?

(a)  

I am installed on the right elevator?

WHAT AM I?

(a)  

I consist the wing flaps, elevator trim tab and the rudder trim. My output from the cockpit controls is transmitted to the flight control surfaces through cable runs and/or mechanical linkage.

What am I?

(a)  

I consist of switch, and position indicator located in the instrument panel, electric motor transmission assembly, drive pulleys, push pull rods, cable and follow-up control.

(a)  

I consist of trim wheel inside the cockpit, trim tab which is hinged at the inboard trailing edge of the right elevator, chains cable and actuator.

What am I?

(a)  

ELEVATOR TRIM TAB CONTROL SYSTEM

A mechanical pointer, adjacent to the (a)   indicates tab position.

What controls the longitudinal trimming of the aircraft?

(a)  

Control surface of the aircraft do you check for the condition and security of hinge cotter pin?

(a)  

What is the fuel grade used in T41?

(a)  

I may be integral or cell type. Vented to the outside through the filler cap or through a tube extending through the surface of the wing, to maintain atmospheric pressure inside the tank.

(a)  

I include an overflow drain that may stand alon or be collocated with the fuel tank vent which allows fuel to expand with increases in temperature without damage to the tank itself.

(a)  

How many gallons is the fuel tank capacity of the t41B/D

(a)  

How many gallons is the fuel tank capacity of t41K?

(a)  

I allow the selection of fuel from various tanks. The position may be used to balance the amount of fuel remaining in each wing tank.

What am I?

(a)  

FUEL SELECTOR VALVE

Selecting this option will allow fuel feed from both tanks.

(a)  

I am used to cut-off fuel from the tank to the engine and located at the floor board of copilot side.

What am I?

(a)  

What should be drained before each flight?

(a)  

I am used for engine starting, vapor purging and for engine operation whenever the engine-driven fuel pump fails.

(a)  

Auxiliary Pump

On R172E & H, located at the firewall enclosed by a (a)   .

AUXILIARY PUMP

On R172K, located at the floorboard beneath the (a)   .