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Airframe Finals

CAR Part V (Airworthiness) - Standard 571, is divided into 13 different sections, which section is 571.03?

Application, Reserved

Maintenance and Elementary Work Performance Rules

Recording of Maintenance and Elementary Work

Specialized Maintenance

CAR Part V, Airworthiness - Standard 571, is divided into 13 different sections, which section is 571.11?

Application, Reserved

Persons Who May Sign a Maintenance Release

Recording of Maintenance and Elementary Work

Specialized Maintenance

What is the abbreviation CAR?

Canadian Aircraft Rules

Canada Air Rules

Canadian Atmosphere Regulations

Canadian Aviation Regulations

CAR Standard 571.10 (d) references …

Maintenance Releases

Work that disturbs Engine or Flight Controls.

An operational check for proper sense and range of motion of the Engine or Flight Controls has been accomplished, by at least two persons, and the technical record contains the signatures of both persons

All of the above

Which of the Dirty Dozen Human Factors is the most dangerous one?

All 12 are equally dangerous to cause errors, it depends on the circumstance and context, more-so if several combine together!

Complaceny

Lack of Knowledge

Both B and C

Select the answer that best describes the following quote: “I’ve looked back there a thousand times and never found a flight control fault”

Complacency

Train yourself to always look for a fault

Never sign for anything you didn’t inspect properly

A false sense of security

All of the above is true

Select the correct answer describing a LINK in the chain.

An error can add a link to the chain and increase the risk of an incident

Correcting someone else’s error can break the link to possibly stop an incident or prevent its severity

A link can be created by anyone supporting the aircraft

All of the above

Select the correct answer describing a SAFETY NET.

Using the applicable MM and IPC to repair an aircraft

Getting training on the aircraft you are maintaining

Getting a good night’s sleep

Being aware of the Dirty Dozen

All of the above

In the term W.H.M.I.S, the “H” and “M” stand for?

Hazardous Materials

Hazardous Metals

Helpful Materials

Harmful Materials

Select the correct answer why W.H.I.M.I.S. System is in place at the workplace?

To train employees to be more productive and profitable

To provide employees information to handle hazardous goods and materials safely

To train and license employees to drive vehicles (like forklifts & trucks) safely while in the workplace

Is an optional program for the employer to provide employees information about handling workplace materials

In this HAZARD LABLE what is indicated by the ‘G’ in the white square at the bottom?

Fire Hazard Index

Personal Protection Equipment

Explosiveness of Material

Type of Driver’s License required to transport this material

Select the answer that best describes the PRIMARY FLIGHT CONTROLS.

AILERONS

ELEVATOR

RUDDER

ALL OF THE ABOVE

Which FLIGHT CONTROL rotates the aircraft around the Vertical Axis?

AILERONS

ELEVATOR

RUDDER

FLAPS

Which Axis is affected by the Ailerons?

LATERAL

DIAGONAL

VERTICAL

LONGITUDINAL

An aircraft is flying, if the Lift = Weight, the aircraft will …

Aircraft will maintain steady state altitude

Aircraft will gain altitude (ascend)

Aircraft will increase airspeed

Aircraft will bank (roll) to the left

If you pull the flight deck control yoke (control wheel) aft, which axis will the aircraft rotate around?

LATERAL

DIAGONAL

VERTICAL

LONGITUDINAL

What is a Stabilator?

Stabilator rotates the aircraft around the Vertical Axis.

It is the horizontal stab and the elevator combine into one unit

It provides an assist to the ailerons to roll the aircraft

All of the above

Select the true statement regarding Angle Of Attack?

The chord line of the wing is changed when lowering the Flaps changing the AOA.

It is a rusultant of the Chordline and the relative wind

Is affected by the camber of the wing

All of the above

Select the answer stating an example of a Secondary Flight Control.

Trim Tabs

Flaps

Slats

All of the above

Select the correct answer the best describes AOA. (Angle Of Attack).

The angle created by the Chord-line and the relative wind

Is the degrees of bank angle during a coordinated turn

The angle between the Vertical and Longitudinal Axis

Is the angle created when flaps are lowered to max degrees

Select the correct answer describing Fowler Flaps.

They extend from the wing leading to increase lift.

They can have 3 different surfaces within a single unit

They allow the aircraft to fly faster in cruise

Fowler flaps change & rotate the angle of the entire wing

Select the correct answer describing Trim Tabs.

Are trailing edge devices on Ailerons, Elevators and Rudders

Can balance a flight control for hands free flight

Can reduce pilot fatigue

All of the above

Select the correct answer regarding a ‘SERVO’ Trim Tab.

It deflects in the opposite direction of the primary flight ctl

Is an ‘assist’ device to help the primary flight control move

Can act as a back up system if the main control system fails

All of the above

Select the correct answer describing Wing Slots.

Slots are trailing edge devices that assist the flaps

Slots are a fixed surface on the leading edge to prevent stall Slots are a fixed surface on the leading edge to prevent stall

Slots slide out on tracks from the leading edge to increase lift

Slots are either hydraulically or electrically actuated

What is the function of SPOILERS?

To assist Ailerons in roll functions

In-flight air-braking for speed reduction

To dump lift at landing allowing full weight of the aircraft on the wheels.

All of the above

What is the function of THS? (Trimmable Horizontal Stabilizer)

To stabilize Pitch trim forces by trimming the stab

The entire Horizontal Stabilizer pivots (degrees of motion)

The Horizontal Stabilizer is actuated by a jackscrew

All of the above

What is the purpose of a Wing Fence?

The Wing Fence works with the Ailerons for roll control.

The Wing Fence creates lift with the Flaps for Landing

The Wing Fence prevents raccoons from getting into the airplane

The Wing Fence prevents span wise air movement at hi AOA The Wing Fence prevents span wise air movement at hi AOA

What is the purpose of a Vortex Generator?

To create electricity

To prevent turbulence on the wing

To generate aerodynamic vortices

To generate additional vortex lift at take-off and landing

Select the correct answer the best describes AOA sensor (Angle Of Attack).

Measures the angle between the fuselage and relative wind

Some AOA sensors are Probe Type

Some AOA sensors are Vane Type

All of the above

Select a common Stall Warning system.

Pneumatic type

Electric vane type

Stick shaker

All of the above

Select the best answer for TCDS?

Type Certificate Data Sheet

Has info for degrees of Flight Control Travels

Has Weight & Balance information

All of the above

Select the best answer for 7x19?

Is a very flexible aircraft flight control cable

Has 7 Strands

Each Strand has 19 wires

All of the above

Select the best answer for Flight Control cable end terminations?

Nicopress Type

Swage Type

Hand Woven Type

All of the above

What is the part AN100?

Nicopress Sleeve

Thimble

Turnbuckle barrel

Flight Control cable pulley

What is the ‘ring’ circling around one end of the turnbuckle barrel?

Left Hand Thread

Shows where you must lockwire for safetying

It is where all the flight control cables attach

It is where the Flight Control cable pulley attaches

What is “in safety” for the turnbuckle?

Torqued very tight

No more than 3 threads visible where both cables attach

Using fiberlock AN safety nuts with turnbuckle

A chain locking device is attached

What is the function of a flight control Pulley?

To allow the flight control cable to change its direction

The cable pushes the flight control surface into desired deflection

To structurally ‘pull’ (hold) the aircraft’s fuselage together

To pull the flight control cable

This is a Pulley troubleshooting question: If the Pulley has very deep cable grooves cut throughout, what is the cause of this?

Pulley is side-loaded by the cable.

Cable tension is excessively tight.

Cable diameter is to large for the pulley.

This is normal wear and tear on a pulley.

Select the true statement about the Tensiometer?

It has three risers called #1, #2 and #3.

It measures the tension of the flt control cable in pounds.

A chart is used to determine the actual cable tension.

All of the above.

In the Tensiometer kit seen here in the diagram, what is the red device for?

It measures the turnbuckle for ‘maximum 3 threads for safety’.

It measures the diameter of the flt control cable.

It is a spacer 1/8” (0.125”) thick to measure cable clearances.

It is a chart for converting cable tension values in pounds (lbs).

What is the purpose of the Inclinometer as seen here in the diagram?

It measures the aileron’s angle of incidence

It measures the aileron’s weight and balance

It measures the aileron for symmetry

It measures the aileron’s degrees of up/down travel from neutral

What is the general process when using an Inclinometer to check this aileron?

Ensure the Aileron is in the neural position iaw the MM

Place Inclinometer on the aileron and adjust to zero degrees.

Move aileron to full up-down positions and measure deflection

All of the above is logical in general terms

Select the correct answer regarding the push-pull tube in a flight control system?

It has adjustable rod ends to adjust the flight control position

It pushes and pulls to transmit movement to a flight control

The rod ends are locked (torqued) using a checknut

All of the above

What is the cable tension for the Cessna 172N elevator cable?

Cable tension is not measured, it is accomplished thru springs

100 pounds +-10

30 lbs +-10

40 lbs +-10

Where is the data plate located on a Cessna 172?

Inside the front left door frame

On the engine

On the control column

On the floor behind the rudder pedals

What is neutral for the Cessna 172 Elevator?

Elevator’s counterweight must be even with the horizontal stab

Elevator must flush with horizontal stab

All degrees are measured from full down deflection

Elevator must be at 0-degrees when even with the horizon

Select the true answer about Cessna 172 Elevator bellcrank(s)?

Elevator has 1 forward bell crank

Elevator has 1 aft bell crank

Elevator has 2 bell cranks, fwd and aft

Elevator has 3 bell cranks, fwd, mid, aft

The Cessna 172 Elevator deflection specs are 28 deg up (+1 -0) and 23 deg down (+1 -0), where is this info?

MM Chapter 8, Elevator Section

Chapter 1 MM, specs section

MM Chapter 6, Aileron Section

Chapter 1 or the TCDS

What info is found in the Cessna 100 SERIES MM?

Cessna 150’s, 170’s and 180’s

The Cessna 172 aircraft

All applicable Part numbers

Servicing Standards and Part Numbers

What info does the Cessna 100 SERIES MM troubleshooting section provide?

Probable Cause

Isolation Procedures

Remedy

All of the above

What does the term ‘applicability’ mean when maintaining a Cessna 172?

Applying all maintenance tasks iaw the correct model of aircraft

Applying all maintenance tasks iaw the correct s/n of aircraft

Applying all maintenance tasks iaw with applicable mm and ipc

All of the above

What is “in safety” for the turnbuckle?

Torqued very tight

Max 3 threads visible where both cables attach to the barrel

Using fiberlock AN safety nuts with turnbuckle

A chain locking device is attached

What is the cable tension for the Cessna 172N Rudder cable?

Cable tension is not measured, it is accomplished thru springs

20 lbs +-10

30 lbs +-10

40 lbs +-10

Where is the data plate located on our Cessna 172?

Inside the front left door frame

On the engine

On the control column

On the floor behind the rudder pedals

What is neutral for the Cessna 172 Rudder?

Rudder’s counterweight must be even with the landing gear

It is set with two 2x4 boards and 2 wooden spacers

Degrees of deflection are 22.5 deg up and 19 degs down

Elevator must be at 0-degrees when even with the horizon

Select the true answer about Cessna 172 RUDDER bellcrank(s)?

RUDDER has 1 forward bell crank

RUDDER has 1 aft bell crank

RUDDER has 2 bell cranks, fwd and aft

RUDDER has 3 bell cranks, fwd, mid, aft

Select the correct Cessna 172 approved reference?

The C172 MM, Chapter 10, Rudder Section

C172 IPC

TCDS

All of the above

What document will you find information about maintain and rigging the C172N rudder?

Cessna 172 MM

Cessna 172 IPC

All of the above

What info does the Cessna 172 MM (aka Servicing Manual) provide in the troubleshooting section?

Probable Cause

Isolation Procedures

Remedy

All of the above

What does the term ‘applicability’ mean when maintaining a Cessna 172?

Applying all maintenance tasks iaw the correct model of aircraft

Applying all maintenance tasks iaw the correct s/n of aircraft

Applying all maintenance tasks iaw with applicable mm and ipc

All of the above

What document will you find information about maintaining and rigging the Mooney M20 rudder?

Mooney M20 MM

Mooney M20 IPC

TCDS

All of the above

What is the function of the PUSH-PULL Rod?

To have various Rod-End options to adapt to many designs

To provide 2 way force, push and pull

To provide linear force

All of the above

What is the function of the Push-Pull tube Witness Hole?

To inspect for corrosion (to witness corrosion)

You should be able to see straight thru to signify ‘In Safety’

For Safety you must not be able to pass a lockwire thru the hole

It is an alignment hole to ensure the Push-Pull tube is straight

What is the function of the Torque Tube?

To provide rotary action to transmit forces

To provide 2 way force, push and pull

To measure the tightness (torque) of aircraft hardware

To provide linear force

Select the true statement regarding Corrosion Inspection for PUSH-PULL Tubes?

Ferrous Tubes (steel, iron) are susceptible to oxidization (aka rust)

Non-Ferrous Tubes (commonly Alum Alloys) are susceptible to various corrosion types incl Pitting, Uniform Etch, Galvanic, Intergranular, Exfoliation, Filiform etc.

The applicable MM or AC43.13 are approved Corrosion manuals

All of the above are true

Select the correct answer regard the Mooney M20 stabilizer trim system?

You turn the Trim wheel on the floor to transmit forces

The Trim wheel cranks a chain

The chain rotates the Stab Trim torque tube that is connected to the stabilizer

The entire Empennage of the aircraft rotates (changes its angle)

All of the above

Select the true statement regarding the diagram here?

This is the aircraft’s Data Plate

Model and Serial Number identify the aircraft’s manufacturing data and applicability info

Use the MM and IPC iaw the aircraft Model and Serial No. info

All of these statements are true

The rod-ends of the Push-Pull tube are adjustable, how would you secure (lock) the rod end after adjustments were made?

Rod-Ends are locked using a Checknut

Rod-Ends are self adjusting to be ‘In Safety’, no locking is needed

For Safety you must use LockTite to chemically lock the rod-end

The Rod-End must be welded after adjustments to lock in place

Select the answer that best decribe Push-Pull tube inspection?

Rod-End is threaded far enough – Witness inspection hole

Tube us straight, not bent

Check jam nut is tight

Ball end is free to move

All of these statements are true

Select the correct answer regarding LPI?

Can only detect surface cracks only

Works on Ferrous Metals

Works on non-Ferrous Metals

All of the above are correct

Select the correct answer regarding MPI?

Can detect surface cracks.

Can detect slightly sub-surface cracks.

Works on ferrous metals only.

All of the above are correct.

Be careful with ‘Step 3’ of the LPI process, can void the entire LP Inspection, select the correct process?

Spray a large volumes of cleaner directly onto the part to clean off developer to ensure easy visibility during inspection

Dwell time is always less than 5 minutes

Spray cleaner directly on cloth only and then clean/wipe the parts surface

Always use the red dye penetrant, the fluorescent type is not reliable

Regarding LPI, select the correct answer for Dwell time?

This is the degrees of cam rotation while the points are closed

10-30 minutes depending on the type of faults & cracks

Dwell time is acceptable as long it is greater than 5 minutes

Greater than 60 minutes is minimum Dwell time

The pilot adjust the left ailerontrim tab trailing edge upward, how will this affect the aircraft during flight?

The aircraft will roll to the right

The aircraft will pitch down

The aircraft will pitch up

The aircraft will roll to the left

Select the answer that correctly describes this NIcopress assembly

Flight control cable

Nicopress Sleeve

Thimble AN100

All of the above

Select the correct answer for the Flt Control Cable diagram?

1x21

3x21

3x1

3x7

Select the true answer regard the 3 rectangular pieces just above the red tool in this Tensiometer kit. (see diagram here)

They are risers to adjust the tensiometer to different cable diameters

They are spacers to measure acceptable cable clearance from aircraft structure

They are spare anvils to replace warn parts in the tensiometer

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