Canadian Aviation Regulations Practice Test 3 Of 6

All maintenance and elementary work carried out on an aeronautical product

Any maintenance, elementary work, or servicing carried out on an aeronautical product

Any maintenance carried out on an aeronautical product

Any maintenance carried out on an aeronautical product, with the exception of non- specialized maintenance carried out on private aircraft

The foreign airworthiness directive prevails

Both directives must be complied with

Compliance with either directive will satisfy the applicable standards

The Transport Canada AD prevails

The criteria used to determine whether an AD is to be issued

The definition of a reportable service difficulty

The definition of a defect in respect to journey log entries

The criteria used to determine whether a repair is a major modification or major repair

An aircraft with a type certificate in the restricted category

An aircraft that has been modified in such a manner that it no longer complies with the basis of its original type certificate

Both A and B

An aircraft involved in a flight testing program

Power-driven aircraft-day VFR

Power-driven aircraft - IFR

Gliders

All of the above

All Canadian aircraft, with the exception of ultra-lights and hang gliders must operate under a maintenance schedule approved under CAR 625

Only holders of an Air Operator Certificate must operate under an approved maintenance schedule

Only holders of an Air Operator Certificate and turbine-powered pressurized aircraft must operate under an approved maintenance schedule

All aircraft other than balloons must operate under an approved maintenance schedule

Through an appropriately rated AMO by the holder of an SCA

By an AME holding an E, S, or P licence appropriate to the type of specialized maintenance

By an appropriately rated AME authorized to sign a maintenance release under the MPM of an AMO approved for the type of specialized maintenance

By an appropriately rated AME or an RCA (Restricted Certification Authority)

The aircraft is away from base and the abnormal occurrence is not a hard landing

The inspection does not involve the disturbance of flight or engine controls

The pilot-in-command has received appropriate training in accordance with an MCM authorized pursuant to CAR 706

No disassembly is required

Operate transport category aircraft

Hold an AMO certificate

Establish a training program

Operate under Appendix B, Part I, of CAR 625

On privately registered aircraft under 12,566 lbs

Where no maintenance release is required pursuant to CAR 571

Both a and b

None of the above

7 days

5 working days

14 days

30 days

If the aircraft is a foreign aircraft, and is operated by a country that is a contracting state, or has an agreement or arrangement with Canada that provides for it.

If the aircraft is operated by a flight training unit, and the flight is conducted within 25 miles of the origin of that flight.

If the flight authority is a specific purpose flight permit, ferry flight, and the flight is conducted wholly in Canadian airspace.

If the flight authority is an experimental flight permit, and the aircraft is operated by a Canadian aircraft manufacturer

Within thirty days of the maintenance action

As soon as Practicable

As soon as practicable, but at least before the next flight

Pursuant to CAR 605, all maintenance must be entered in the journey log

Carry the last two entries forward into the new volume

Carry the last entry forward into the new volume

Ensure that the previous and new volumes are sequentially numbered

Make entries relating to the preceding volume to ensure that an unbroken chronological record is maintained.

CAR 625, Equipment and Maintenance Standard

CAR 605, General Operating and Flight Rules

CARs 571, Aircraft Maintenance Requirements

CARs 706, Commercial Air Service Standards

Service bulletins marked mandatory by the aircraft manufacturer

Transport Canada airworthiness directives

Progressive inspections pursuant to CAR 625

All of the above

Determine whether a damaged aircraft is acceptable for a flight permit issued by Transport Canada

Allow an aircraft to operate with defects, provided the aircraft are not passenger aircraft

Are determined by the manufacturer, and part of the type certificate data sheet

Are a list of systems and equipment in the aircraft showing the degree to which defects may be deferred

The journey log

Airframe log, engine log, propeller log

Empty weight and balance report

All of the above

When the damage is less than 12 inches in any direction

When the damage is less than 6 square inches

When the damage to the skin measures 6 inches or less in any direction

When the damage is confined to skin not part of a pressure bulkhead

For as long as the aircraft is registered

For 24 months

Until the aircraft is sold, de-registered, or.destroyed

For one year

The pilot in command

The person who discovers it

The owner of the aircraft or a person delegated by the owner

An appropriately rated AME

Not less than 19.68 inches high

Not less than 25 cm high

Displayed as far outboard as possible

Displayed parallel to the longitudinal axis of the aircraft

Special C of A - Ultra-light

Restricted C of A

Flight authority is not required

Specific purpose flight permit

Maintenance, providing the maintenance was non-specialized

Aircraft

CAR Part IV and CAR Part VII aircraft specialized and non-specialized maintenance

Airframes, engines, and related subsystems

The FAA

The CAA

The FAR

The DOT

An appropriately rated AME or other approved person

The person who performed the maintenance, or, where particulars are transcribed from the journey log, the aircraft owner

The aircraft owner

The person who performed the maintenance, or, where the maintenance has been entered in the journey log, further entries are not required.

6 months

12 months

24 months

Every 12 months, providing the aircraft is operated in class B airspace

10 hrs

10 hrs, or 10% of the interval, whichever is least

10% on calendar time only

There is no allowable tolerance

A properly rated AME or RCA

In the case of an AMO, an AME, or a person who is not an AME licence holder but is authorized by an ACA (Aircraft Certification Authority)

A properly rated AME, or an AME having training in any higher category than that of the aircraft being certified.

A properly rated AME, or in the case of an AMO, the holder of an SCA (Shop Certification Authority)

Every 12 months, when installed on commercial and flight training aircraft

Every 24 months, when installed on commercial and flight training aircraft

According to the ELT manufacturer's recommendations

According to Appendix C of AWM Chapter 571

3 working days of the defect occurring

48 hrs of the defect occurring

2 weeks of the defect occurring

7 days of the defect occurring

Defect control procedures

A quality assurance program

Technical dispatch procedure

All of the above

AWM chapter 571

CAR Part V, subpart 7

AWM Chapter 509

AWM chapter 507

Pursuant to the MPM of an appropriately rated AMO

By an AME E, S, or M engineer, provided the maintenance is non-specialized

By persons who have completed the appropriate training and performed the task at least once under the direct supervision of an AME

By the procedures set forth in CAR 625, Appendix H

In the absence of manufacturer's recommendations, every 3 years

Every 5 years

Every 4 years

In the absence of manufacturer's recommendations, every 10 years

Annually

Every three years

Within 30 days of any change in the regulations

On commencement of the operation of a new aircraft type

A quality assurance manager

A production manager

Both of the above

None of the above

Certificate of Airworthiness

Continuous flight permit

Special flight permit

Special C of A - limited

After an aircraft lightning strike

Every 12 months

After work is performed that may affect it

All of the above

Where there is a change in empty weight of over 2%

Where there is a change in MCTOW of more than 2%

Every five years

Where there is any change in weight or C of G

Every ten years, or 2500 hours air time, whichever comes first

Where the manufacturer has made recommendations regarding the air time between overhauls, at the interval recommended or every ten years, whichever comes first

According to the intervals in Appendix C, CAR 625, unless otherwise approved by an on-condition maintained under CAR 625, Appendix D

Every five years, intervals in Appendix C, CAR 625

Defects are recurring defects where a failure mode is repeated twice, on a particular aircraft, within 15 flight segments of a previous repair made in respect of that failure mode.

Defects are recurring defects where a failure mode is repeated on consecutive flights after a repair has been made in respect of that failure mode.

Defects are recurring defects where a failure mode is repeated on similar aircraft in an operator's fleet within a period of seven days.

Defects are recurring defects where a failure mode is repeated three times, on a particular aircraft, within 15 flight segments of a previous repair made in respect of that failure mode.

CAR 625, Appendix B, part I

CAR 571

CAR 605, Schedule I

CAR 571, Schedule II

Transport Canada advises compliance with the AD

Is mandatory for all aircraft with the exception of aircraft in the amateur built and owner maintenance category

Is mandatory for aircraft operated by the holder of an Air Operator Certificate

Is not mandatory in any case

CAR 571, Aircraft Maintenance Requirements

CAR 605, General Operating and Flight Rules

AWM Chapter 571

CAR 625,Equipment and Maintenance Standards

A maximum of 30 days

Flight Training Units and Commercial Air Services may not install borrowed parts on their aircraft

100 hours or 90 days, whichever is greater

30 days or 50 hours air time whichever is greater

An airworthiness limitation

Hard time

Mandatory maintenance procedure

Progressive maintenance

Temporary maintenance release only - subject to test flight

Subject to satisfactory test flight

Test flight required

If a test flight is required, or satisfactory testing may not be completed on the ground, no maintenance release may be signed before a test flight is carried out