WorksheetsLEZZ GO CHARLIE
Total questions: 78
Worksheet time: 49mins
What is the designed gross weight of T41B in lbs?
(a)
What is the fuel capacity of R172K in gallons?
(a)
How many quarts is the oil capacity of the t41D, t41B and R172K?
(a)
What is the engine model of all the t41 aircraft (D/B/K)?
(a)
What is the pressure rating of the Main Wheel Tire of T41 in psi?
(a)
What is the pressure rating of the nose wheel tire of t41D and T41B in psi?
(a)
What is the pressure rating of the Nose Wheel tire of the R172K in psi?
(a)
What is the pressure rating of all the t41 aircrafts' nose gear strut in psi?
(a)
T41 Specifications:
Supply the missing data.
3 to 5 degrees
3.5 to 5 degrees
3 to +/-1 degrees
3.1 to 5 degrees
What is the wings span of the t41D and t41B?
36'2"
35.82'
36'28"
38'2"
What is the wing span of the R172K?
36'2"
35'82"
38'52"
36'18"
what is the tail span of the t41D and t41B?
11'4"
11'26"
11'46"
11'24"
What is the tail span of r172K?
11'4"
11'26"
11'24"
11'42"
What is the length of the t41D and t41B?
26'4.5"
27.26'
27'26"
11'4"
What is the length of the R172K?
27.26'
27'26"
26'4.5"
27.27'
What is the fin height of the t41D and t41B?
8'9.5"
8.79'
8'7.5"
8.95'
What is the fin height of the R172K?
8.79'
8.95'
8'9"
8'9.5"
What is the track width of the t41D and t41B?
7'2"
8.13'
7.2'
7'8"
What is the firing order of the ignition?
163254
254163
123456
654321
What is the compression ratio of the t41 engine?
8.5:1
8:1
8:1.5
8:2
The ability of cylinder and piston to compress ________ cc of fuel/air mixture at bottom dead center (BDC) to 1,000 cc at top dead center (TDC) thus 8.5:1
8500
8600
8700
8000
What fuel does AETDC use?
AVGAS100LL
AVGASLL100
AVGAS111LL
AVGAS110LL
What system has a handle and ratchet mechanism that is connected by a cable to linkage at the master cylinder.
(a)
What system works when you pull out the handle that depresses both master cylinder piston rods and the ratchet locks the handle in this position until the handle is turned and released?
(a)
___________ consists of housing, piston, pressure plate, back plate, linings riveted on pressure plate and back plate.
Brake Assembly
Parking Brake System
Parking Brake
Brake
What should be replaced when they are worn to a minimum thickness of 3/32 inch?
(a)
What is the allowable thickness of brake disc in inches?
(a)
This is locate just forward of the pilot rudder pedal, actuated by applying toe pressure on the rudder pedal and has a small reservoir is incorporated with each master cylinder.
Master Brake Cylinder
Brake Disc
Brake Lining
Brake Cylinder
Are rigid aluminum tubing, except of flexible hoses used at master cylinders and at wheel brake assemblies and have a separate line is used to connect each master cylinder to its corresponding wheel brake cylinder.
Hydraulic Brake Lines
Master Brake Cylinder
Torque Link
Brake Disc
What is the Flap Operating Range (white arc)?
56-100MPH
145-182MPH
64-145MPH
182PMH
What is the maximum allowable (red line) air speed?
182MPH
145-182MPH
64-145MPH
56-100MPH
What is the caution range (yellow arc) of air speed?
182MPH
145-182MPH
64-145MPH
56-100MPH
What is the normal range (green arc) of airspeed?
182MPH
145-182MPH
64-145MPH
56-100MPH
How many RPM is the category 1 for Engine Limits?
3000
3300
more than 3300
less than 3300
How many RPM is the category II for Engine Limits?
3300
3000
more than 3300
less than 3300
Category III is defined as Excessive Overspeed that is?
3000
3300
less than 3300
more than 3300
Airframe Limitation for Utility Category:
Supply the missing data
4.5
4.4
4.3
4.2
Airframe Limitation Normal Category
Supply the missing data.52
-1.52g
1.53g
1.52g
-1.53g
I provide comfortable control forces and ease of maneuvering of the aircraft.
(a)
I consist of aileron, elevator, and rudder, utilized to control attitude and directional control of the aircraft and my
output from the cockpit controls is transmitted to the flight control surfaces through cable runs and/or mechanically linkage.
WHAT AM I?
(a)
Used to cut off fuel from the tank to the engine and located at the floor board of copilot side.
(a)
The Aux Pump on R172K is located at the floorboard beneath the (a) .
Used for engine starting, vapor purging and for engine operation whenever the engine-driven fuel pump fails.
(a)
The Aux pump of R172E and H is located at the firewall enclosed by a (a) .
When the fuel drops to 9 gallons in either fuel tank, this sensing unit will illluminate.
(a)
This is located at the instrument panel. It illuminates when the engine manifested a metal in the oil system, this is connected to a chip detector plug in the oil drain sump.
(a)
Normal operating range of the Manifold pressure.
15-25 inches Hg
4.5-11.5 GPH
18.5 psi
3.0 psi
Minimum psi for Fuel Flow.
3 psi
4.5-11.5 gph
18.5 psi
15-25 inches HG
Normal Operating Range for Fuel Flow.
4.5-11.5 GPH
3.0 psi
18.5 psi
15-25 inches Hg
Maximum for Fuel Flow?
3.0 psi
4.5-11gph
18.5 psi
100 psi
How many RPM is the maximum limits for Tachometer?
2800
2200-2600
2600
2200
How many RPM is Normal Operating Range for the Tachometer?
2200-2600
2600
2800
2200
How many Fahrenheit is the maximum limit for the CHT?
160
460
200-460
240
How many Fahrenheit is the Normal Operating Range of the CHT?
200-460
100
240
200
How many Fahrenheit is the maximum allowable for the Oil Temperature?
240
100-240
212
160
How many Fahrenheit is the normal operating range for the Oil Temperature?
100-240
240
100-212
160-240
What is the normal operating range for the suction?
4.6-5.4 Inches Hg
4-5 Inches Hg
5.4-6.5 Inches Hg
3-4.5 Inches Hg
How many psi is the Minimum Idling for Oil Pressure?
10
30-90
30-60
100
What is the normal operating range for the Oil Pressure?
10
30-60
60-90
100
How many psi is the maximum for Oil Pressure?
100
30-60
60
10
I consist the aileron, elevator and rudder and utllized to control attitude and directional control of the aircraft what am I?
Primary Flight Control System
Secondary Flight Control System
Flight Control
Flight Control Surface
Output from the cockpit controls is transmitted to the flight control surfaces through cable runs and/or mechanical linkages.
Primary Flight Control System
Secondary Flight Control System
Flight Control
Flight Control Surface
__________ are hinged on the trailing edge outboard of each wing controlled by the control wheel via series of sprockets, chains, pulleys, cables, bell cranks and push pull tubes.
Aileron
Rudder
Trim Tab
Elevator
____________ is automatically determined when rudder are rigged against return springs 6.50 inches from firewall
Torque Effect
Torsion
Cable Tension
Surface Tension
________ is hinged at the trailing edge of the vertical stabilizer.
Rudder
Aileron
Flaps
Elevator
________ is hinged on the trailing edge of the horizontal stabilizer.
Elevator
Trim tab
Aileron
Rudder
_________ is installed on the right elevator.
Trim tab
Flap
Rudder Tab
Strut
What consist wing flaps, elevator trim tab, rudder trim. Likewise, ailerons and rudders are provided with tabs adjustable on the ground only.
Primary Flight Control System
Secondary Flight Control System
Flight Control
Trim Tab System
What operates the wing flaps?
Electrical Switch
Yoke
Rudder pedals
Master Switch
What are located at the inboard trailing edge of both wings?
Aileron
Trim tab
Flaps
Rudder
What 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.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
What is operated by forward and aft movement of the control yoke and transmit power to the elevators through a push pull tubes, cables and bell cranks.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
What is consist of rudder pedals, cables and pulleys which link the pedals to the rudder and nose wheel steering.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
What consists of 2 (two) control wheels attached to columns and linked by universal joints to the control “U” behind the instrument panel.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
In flight, when the control wheel is steered to the left, the tip of the left aileron goes up and the tip of the right aileron goes down resulting the aircraft to bank to the left and vice versa.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
During taxiing, pushing the right pedal to the right steered the nose wheel to the right and the trailing edge of the rudder also move to the right and vise versa. On flight, the nose wheel automatically locked at neutral position and rudder is controlled by the rudder pedals.
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
The aft and forward control of the yoke moved the elevator. When the control wheel is moved forward the elevator trailing edge move down and vice versa
Aileron Control System
Rudder Control System
Elevator Control System
Wing Flap Control System
Longitudinal trimming of the aircraft is controlled by operating the control wheel. Rotating the top of the control wheel aft, the trailing edge of the tab should go down and vise versa
Aileron Control System
Rudder Control System
Elevator Trim Tab Control System
Wing Flap Control System
