MODULE 10 - PART 1

A register of airlines operating on an AOC is maintained by the. ICAO. CAA. FAA.

What category of aircraft are 'break-in' markings required?. All public transport aircraft above 2300Kg. All public transport aircraft above 5700Kg. All aircraft registered in the UK.

A Part-145 approval covers. base maintenance. the major part of the organisation. only line maintenance.

For UK registered aircraft, components must be. maintained by a part-145 approved organisation. any appropriately approved organisation. maintained by a part-145 approved organisation registered in the UK.

Aircraft manufactured abroad, but registered in the UK. can fly with an export C of A. must have a C of A issued in the UK before it can fly. can fly with a foreign C of A.

To facilitate a repair, a drawing can be taken from. the CAA. the manufacturer. a part-145 organisation.

Documents to be carried on a specific aircraft for a specific purpose is given in. BCAR Section A and B. JAR-OPS. AOC.

Safe operation of the aircraft is the responsibility of the. part-M organisation. owner. operator.

The period of validity of a Certificate of Fitness for Flight under 'A' Conditions is. 7 days. 1 flight.1 flight. 2 days.

Where can be found the details of design of a particular aircraft?. The Maintenance Manual. The Declaration of Design and Performance. EASA Certification Specification 25.

The validity of an EASA permit to fly is. 12 months. 7 days. as stated on the certificate but not exceeding 14 days.

An engineer may issue a CRS if they. have a company approval.have a company approval.have a company approval. are LWTR and company approved on the appropriate type of aircraft. are type rated on any equivalent aircraft type.

Where would you normally train for licences?. At a Part-147 approved organisation. At a Part-145 approved organisation. At a technical training school.At a technical training school.At a technical training school.

By when do BCAR licensed aircraft maintenance engineers have to conform to EASA Part-66?. 28th September 2011. 28th September 2006. 28th September 2001.

By what date must all base maintenance certifying staff and B1 and B2 support staff for aircraft below 5700kg be part-66 qualified?. 28 September 2008. 28 September 2006. currently there is no date specified, such authorisations will always be covered by BCAR Section L.

If changes are made in a Part-66 license without the approval of the CAA,. the license is cancelled and an enquiry is conducted. the license is cancelled from the point of the CAA becoming aware of the changes. all certifications made under that licence are invalid from the date the changes were made.

If an engineer has a heavy cold, he/she,. must take only the medication which is prescribed specifically to him/her. may take medication without advice. must seek medical advice from a doctor.

To what does a B1-3 License apply to?. Helicopter with turbines, their engines, airframes and electrics. Light aircraft with piston engines. Helicopters with piston engines, their engines, airframes and electrics.

What can an A1 licensed engineer sign for?. Minor Scheduled Line Maintenance tasks on piston engined aircraft. Minor Scheduled Line Maintenance tasks on turbine engined aircraft. Minor Scheduled Line Maintenance tasks on turbine engined helicopters.

Who can sign a CRS?. Any licensed engineer. An appropriately licensed engineer. An unlicensed engineer who has permission from the Chief Inspector.

Where would you find the requirements and the syllabus for a maintenance license?. EASA Part-147. EASA Part-145. EASA Part-66.

An A1 licensed mechanic can sign for. Aeroplanes and Helicopters. Aeroplanes - Piston. Aeroplanes - Turbine.

From 28 September 2008, all engineers are required to be licensed in accordance with. EASA Part-66. ICAO. JAR 66.

A Part-66 licence can be used without amendment or exchange. only in the member state in which it was issued. throughout all member states. throughout the World.

A part-66 licence holder wishing to work in another member state apart from the one it was issued, must have a licence printed in. English. only the originating member state's language. the language of the member state which the holder wishes to work in.

Who issues a part-66 licence?. EASA. A part 145 organisation. The competent authority of the member state.

Who may amend or endorse a part-66 licence?. A part 145 organisation. The licence holder. A part 147 organisation.

Whose responsibility is it that no unauthorised entries are made in a part-66 licence?. EASA or the national aviation authority of the member state. The licence holder. The part-145 organisation.

EASA Form 26 is. the application for a part-66 licence. the application for an extension to a part-66 licence. the part-66 licence itself.

A part-66 licence is issued for. initially 2 years then re-issued for a period of 5 years. initially 5 years then re-issued for a period of 2 years. 5 years.

A B2 License applies to. line maintenance on airframe structure and powerplants. line maintenance on electrical systems and avionics. line maintenance on airframe structure.

Who carries out the practical task training required for a category A licence?. Either a part-145 or a part-147 organisation. A part-147 organisation only. A part-145 organisation only.

Who is responsible for the control and issue of engineers licenses?. EASA. CAA. JAA.

When can a LAE sign a CRS?. For any aircraft for which he has a type rating. For any aircraft for which his company has Part-145 approval. For any aircraft for which he has a type endorsement on his license and holds the appropriate company approval.

The time scale for retaining training records within a JAR-147 school is. five years after the candidate leaves the course. three years after the course. five years after the completion of the course.

A basic aircraft maintenance in category B1, B2 or C licence. does confer licensing responsibilities. allows you to sign a CRS but not CMR. does not confer any licensing responsibilities.

With reference to the licensing of aircraft maintenance engineers, the requirements for the issue of a licence without type rating can be found in. BCAR section L. EASA IR Part-66. Airworthiness Notices.

Within an aircraft maintenance organisation approved in accordance with IR Part-145, the limitations of an individual's certification rights are recorded upon. the personnel authorisation certificate. the aircraft maintenance licence. the personnel records.

In the future BCAR section L will be replaced by. EASA IR Part-66. JAA JAR-66. EASA IR Part-145.

The term 'Extension' of a Part-66 licence means. to extend its validity for a further period of time. to add an additional basic category. to add a type approval.

An aircraft type approval endorsement to a Part-66 licence is only provided after. adequate theoretical training. adequate theoretical and practical training. adequate practical training.

EASA IR Part-66 applies to aircraft. below 5700 kg only. above and below 5700 kg. above 5700 kg only.

An engineer's BCAR Section L licence for certification of aircraft above 5700 kg will, on 28 Sept 2006. automatically convert to EASA IR Part-66 without any action. remain usable but with restrictions if not converted to EASA IR Part-66. become invalidated if not converted to EASA IR Part-66.

In order to obtain a type approval on an aircraft, an engineer must. must work on aircraft for 12 months within the last 24 months. have a manufacturers course within the last 3 years. work on the type for 12 months in the last 24 months.

What experience is required for an A1 license?. 2 yrs or 1 yr if qualified in another profession. 3 yrs or 2 yrs if qualified in another profession. 5 yrs or 3 yrs if trained by 147 company.

The syllabus and requirements related to an aircraft maintenance engineers license for a light commercial air transport aircraft can be found in. BCAR Section L. JAR-66. IR Part-66.

An EASA category A licensed mechanic can. certify minor line tasks which he has done himself and for which he has approval. certify minor line tasks which he or other line mechanics have done and for which he has approval. certify line maintenance checks.

Which of the following are the sub-sections of a Part-66 maintenance licence in category A?. Aeroplanes - Piston, helicopters Piston, Aeroplanes -Turbine and Helicopters Turbine. Aeroplanes - Piston and helicopters Piston. Aeroplanes - Turbine and helicopters Turbine.

An A licence is automatically granted with the issue of which of the following?. B1 or B2. B1. B2.

IR Part-66 experience requirements may be reduced with. aircraft production experience. completion of training at a Part-147 approved school. completion of a university engineering degree.

A category C certifying staff authorisation permits the holder to issue a block CRS after. base maintenance. line maintenance and defect rectification. any line or base maintenance.

When did / will the EASA IR Part-66 licence become sole code?. 2011. 2003. 2006.

An EASA IR B1.2 engineer can certify. aircraft - turbine engined. aircraft -both turbine and piston engined. aircraft - piston engined.

An EASA IR B1.3 engineer can certify. helicopters - both turbine and piston engined. helicopters - piston engined. helicopters - turbine engined.

How long is an EASA part-66 licence valid?. 2 years once signed in ink. 5 years once signed and verified that the information contained in the licence is the same as that contained in the competent authority records. 5 years once signed in ink.

A Part-145 organisation based outside the EU, the competent authority is. the CAA. the NAA of the country it is located in. the EASA.

How many people sign a CRS after scheduled maintenance?. One in each category. One. Two.

The independent audit part of a QA department of a large Part-145 company. must be part of the company. can be combined with the planning department. can be contracted out to another company.

Maintenance documentation held by a Part-145 company is kept for. 2 years after they were raised. 5 years after they have expired. 2 years after the aircraft has been returned to the operator.

Who is a Part-145 approved organisation headed by?. The Technical Manager. The QA Manager. The Accountable Manager.

When the block CRS is finally issued for base maintenance at a Part-145 organisation, who is ultimately responsible for maintenance carried out during the check?. the Category B LAE. the Category C LAE. the Accountable Manager.

A Part-145 approval is not required to carry out. daily checks (as long as 48 hours has not passed. defect rectification. pre-flight checks.

An approved Part-145 organisation is one which is. of a standard acceptable to the CAA and the FAA. of a standard acceptable to the EU. of a standard as defined in the ANO.

How long does an licensed engineer have to produce his/her authorisation certification if asked by the CAA or EASA?. immediately. 7 days. 24 hours.

A Part-145 approved maintenance organisation is authorised to. approve major modifications. issue certificates for work completed in aircraft maintenance or overhaul. originate repair schemes and manufacture parts.

Who can sign the CRS?. LAE. LAE who has the permission from the chief inspector. LAE who is authorised to do so.

A situation is found which could hazard an aircraft, while it is undergoing maintenance by a Part-145 organisation. The situation must be reported within. 48 hours. 24 hours. 72 hours.

If you are required to produce your License, this must be done. immediately. within 24 hours. within a reasonable time.

How many people sign a CRS after scheduled maintenance?. Two, one for mechanical activities and one for the avionics. One in each category. One only.

A Part-145 organisation finds a condition on an aircraft which could be hazardous, they must inform the CAA within. 3 days. 24 hours. 7 days.

In a Part-145 company, who is responsible for keeping technical information on certifying staff?. Tech Records. Quality Assurance. Personnel Department.

Who monitors how a company is adhering to Part-145?. Base Maintenance Manager. Accountable Manager. Quality Manager.

For which type of maintenance do you not need a Part-145 approval?. Hangar Base Maintenance. Preflight inspection. Weekly Check.

CAA approval of a Part-145 organisation to undertake base maintenance of a particular aircraft type will be found in. the companys AOC data sheet. the company operations manual. the company limitation part of the approval schedule.

A Part-145 company is required to be headed by. a technical director. a licensed engineer. an accountable manager.

Implementation procedures for IR Part-145 may be found in. Airworthiness Notice 14. BCAR section A. Air Navigation Regulations.

Unserviceable aircraft equipment should not be stored. in a goods-in store. on unserviceable shelves around the hangar. with serviceable spares.

Under the Part-145 Approval System an A1 Rating relates to aircraft. on base maintenance only. of 5700 kg MTOM and below. exceeding 5700 kg MTOM.

The Approval Reference Number for a typical Part-145 company would be. AI/1234/94. CAA 00023. UK.145.00505.

Line maintenance under Part-145 is defined as typically. C and D checks. preflight maintenance. A and B checks.

Awards of the EASA Part-145 approval in the UK are made by the. ICAO. JAA. CAA.

The responsibility for reporting incidents and occurrences during a flight rests with the. aircraft commander. engineer clearing the tech log. air stewards.

Following the replacement and compensation of a direct reading compass certification is made in the form of a. certificate of compensation. certificate of conformity. CRS.

The minimum distribution of the Authorised Release Certificate EASA Form 1 is. 1, to remain with the component to which it refers. 2, one for the originator and one to remain with the component to which it refers. 1, to be retained by the originator.

The Authorised Release Certificate EASA Form 1 can. have several items entered onto it providing they are identical part numbers. have several items entered onto it of different part numbers. have only one item entered onto it.

Following satisfactory aircraft component replacement, adjustment, locking and functioning. Which of the following is issued?. Certificate of maintenance review. CRS. A maintenance statement.

The wording of a CRS issued by a Part-145 organisation can be found in. the ANO. EASA Part-145 Section A. The Acceptable Means of Compliance to EASA Part 145.

Independent audits of a department within a Part-145 approved organisation are to be carried out at least every. 6 months. 12 month. 24 months.

The EASA Form 1 is to be used when components are. both exported/imported and bought/sold domestically. exported or imported only. used bought and sold domestically only.

After a mandatory inspection has been carried out by a Licensed Engineer, what is issued?. Certificate of Release to Service. A Flight Release Certificate. A Certificate of Maintenance Review.

When an item is removed from an aircraft, then subsequently refitted. no certificate of release to service is required if it is the same item. only one certificate of release to service is required to cover both the removal and the re-fitment. two certificates of release to service is required to cover the removal and the re-fitment respectively.

For the purposes of EASA Part-145, a 'Large aircraft' is. over 13610 kg MTOM. over 2730 kg MTOM. over 5700 kg MTOM.

If a temporary wiring repair has to be carried out on an aircraft which is away from its Maintenance Organization, how would this be certified?. No Certification need be made. Aircraft would be certified as Fit for Flight under 'A' conditions. By signing a Certificate of Release to Service.

A company has approval reference of form EASA.145.00X? It is located. outside a European Member State. in the USA. within a European Member State.

On completion of the overhaul of an aircraft component by an overhaul organization. the worksheets with a certified CRS are retained by the overhaul organization and an EASA form 1 is issued to the customer. the worksheets with a certified CRS are placed in the aircraft file with the log books. the worksheets are retained by the overhaul organization in their own files.

A Part-145 approved organisation may subcontract specialist work to. any non-approved company. any BCAR approved company. any BCAR approved company that is listed in their Maintenance Organisation Exposition.

Signatories to the CRS will be found in. Airworthiness Notice No.3. the organization exposition. BCAR Section A-8/13, A-8/15, A-8/3.

EASA IR Part-145. lists the minimum requirements acceptable to the CAA. applies to all European Aircraft. replaces the relevant chapters of BCAR Section A.

Aircraft and aircraft component records must be retained by a Part-145 approved organization for a period of. three years after the aircraft component is permanently removed from service or destroyed. two years after the aircraft or aircraft component has been released from the Part-145 approved maintenance organization. 5 years after the aircraft or aircraft component has been destroyed or permanently removed from service.

The staffing requirements for an organization approved to undertake maintenance on commercial transport aircraft are to be found in. EASA IR Part-145.30. JAR E.25D. EASA IR Part-25.13.

EASA IR Part-145 approved organizations are approved to maintain. all UK registered aircraft used for commercial transport purposes. all UK registered aircraft used for commercial transport purposes and aircraft exceeding 5700 kg MTWA in any C of A category. all UK registered aircraft above 5700 kg MTWA.

The extent of an organisation's Part-145 approval is stated. on the approval certificate. in the CAA's list of approved organisations. in the organisation's exposition.

On a Certificate of Release for Service an adjustment to a control would come under the heading. replacement. repair. overhaul.

To comply with IR Part-145. the Acceptable Means of Compliance can be used. any additional national directives must be used. JAA Joint Circulars should be used.

The list of typical tasks which cat-A line maintenance mechanic may perform is contained in. Part 145. Part 147. Part 66.

An aircraft component which comes with an EASA form 1,. will not need a CRS when fitted as a form 1 is also a CRS. will also require a form 8130-3 if fitted to a British aircraft. will require a CRS to be issued when fitted to certify correct installation as the form 1 CRS applies only to the conformity of the component.

An organisation seeking approval to carry out maintenance on an aeroplane of 6000kg MTWA carrying cargo only, would apply for approval under. CS 25. IR Part-145. BCAR section A or B depending on country of origin of aeroplane.

Category C licensed engineers are backed up by. engineers holding existing BCAR section-L licence in the appropriate category. hanger based cat B1 and B2 licensed maintenance technicians and mechanics with appropriate type ratings. cat B1 and B2 technicians with type rating.

Since EASA IR Part-145 came into effect. it lists the minimum requirements acceptable to the CAA. it has replaced the relevant chapters of BCAR. it currently applies only to transport passenger aircraft.

Part-66 certifying staff must be. not less than 21 years of age. There is no Age limitation. not less than 18 years of age.

A Part-145 organisation's accountable manager is responsible for. ensuring that all line maintenance procedures are carried out. ensuring that all necessary resources are available to accomplish maintenance in accordance with Part 145.A.65 (a). ensuring that all base maintenance procedures are carried out.

The list of EASA Part-145 approved maintenance organisations is found in. the CAA list of approved organisations. the maintenance schedule. the company's exposition.

After a modification on an aircraft system, a certificate of release to service is issued. To do this you require. Part-21 Subpart H approval. ICAO approval. Part-145 approval.

What aircraft can an EASA part-145 company maintain?. Commercial Air Transport aircraft only. All aircraft over 5700 kg MTOM. All aircraft on its schedule of approval.

How long have you got, to produce a Part-66 licence when asked to do so?. Within 7 days. Within 5 days. Within 24 hours.

An aircraft has an unapproved repair. Issue a CRS to approve it. Issue a Fitness for Flight cert. It cannot be certified until the repair is approved.

The requirement for having a Quality Department to a maintenance organisation are set out in. IR Part 21. IR Part M. IR Part-145.

The responsibility for regularly weighing aircraft rests with the. operator. Part-145 maintenance organisation. CAA.

Documents to be carried include. Certificate of Registration, Airworthiness, Insurance and Radio License. C of A, Permit to Fly, radio License, Crew Licenses, and C of R. Crew licenses, radio licence and aircraft dealers certificate.

The requirement for re-weighing an aircraft under JAR-OPS is. at manufacturer, then two years and five yearly thereafter. at manufacturer and then four yearly intervals. at manufacturer and then five yearly intervals.

Aircraft types which an operator can fly are listed in the. Aircraft Flight Manual. Air Operators Certificate. Company Maintenance Schedule.

Where can information on the aircraft documents to be carried be found?. ECAR Part-145. JAR-OPS subpart B. ANO schedule 3.

An aircraft registered in the UK and operating in the transport category will normally be operated. by the holder of an AOC. Under B conditions. by the owners.

In which book would you expect to find all the following: a CMR, a maintenance statement, a sector record and a deferred defect?. Technical log book. Flight manual. Aircraft Log book.

Amendments to JAR OPS are by way of. orange pages. grey pages. blue pages.

Deferred defects are recorded in. the Deferred defect manual. the Technical Log. the Technical Manual.

Which of the following documents must be carried on an aircraft?. Certificate of Registration. Air operators Certificate. Engine Log Book.

Large Aircraft Maintenance Schedules are produced by. manufacturer with CAA approval. operator. CAA Safety Regulation Group.

Aircraft over 5700kg MTOM are weighed. at the renewal of the Certificate of Airworthiness. prior to entry into service and then every 4 years. annually.

JAR OPS subpart J covers. maintenance. instruments and equipment. mass and balance.

JAR OPS 3 applies to. commercial transport. aeroplanes. helicopters.

Which of the following form part of the aircraft Technical Log?. Future maintenance program for the pilots information. Pilots name and number. CRS and weight and balance information.

Which of the following documents are to be carried on an aircraft?. Tech log, full Operations Manual and Flight Manual. Tech Log and parts of the Operations Manual. Full Operations Manual and Flight Manual.

Who approves the aircraft Technical Log?. The Part-145 organisation maintaining the aircraft. The operator. The National aviation authority.

The documents to be carried on an aircraft are stated in the. flight manual. JAR OPS. appropriate ANO article.

What is the minimum legal decision height for Cat I auto landing?. 100 to 200 ft. 200 to 300 ft. 400 to 500 ft.

A type certificate is. issued after a Certificate of Registration. issued before a Certificate of Airworthiness. issued after a Certificate of Airworthiness.

A Type Certificate is a. requirement prior to the issue of a C of A for aircraft in the Transport Category. requirement for aircraft above 2730Kg MTWA. prerequisite to the issue of a C of A.

A design organisation is approved in accordance with. IR Part-21. IR Part-145. BCARs.

The standard to which the B747-400 was certified to was. BCAR section D. JAR-25. JAR-21.

A Type Certificate is issued to. an aircraft type and its variants. all aircraft of a type (e.g. A340). each aircraft of a type.

A Certificate of design is raised. by the CAA. by the manufacturer. by the operator.

Certificates of design certify. that a major mod has been designed adequately. that a company has design approval. that the aircraft meets current stated design requirements BCARs/EASA as specified.

An aircraft manufacturer approved to EASA Part-21, may maintain aircraft and issue certificates of release to service. for any aircraft providing it is on its schedule of approval. only if it holds a Part-M or Part-145 approval also. only for the aircraft that it has produced.

A type certificate issued to an aircraft by the CAA. shows approval of the design by the CAA only. shows approval of the design by the CAA and would be approved under EASA. shows approval of the design by the CAA but will not necessarily be approved under EASA.

An EASA Part-145 organisation may classify repairs as major or minor if approved in accordance with. EASA Part-145. EASA Part-21 subpart J. JAR OPS subpart M.

A type certificate is issued to. aircraft identical in all major areas to a previous approved aircraft. aircraft similar to a previous aircraft but with design differences. a prototype aircraft.

What BCAR covers Noise Certification requirements?. Section D now replaced by EASA CS-25. Section A and B. Section N.

Which of the following does not require a Noise Certificate?. A helicopter under 5700 kg. A small business jet aircraft. A fixed wing aircraft under 2730 kg.

To what stage of flight is a Noise Certificate applicable?. Take-off and landing. All stages of flight. Take-off only.

What could invalidate a Noise Certificate?. A modification. An unauthorised or unapproved repair is carried out. Once issued, nothing can invalidate it.

When is a Noise Certificate required to be carried aboard the aircraft?. At all times. When flying in UK airspace only. When flying in UK or any EU member state airspace.

On completion of a major modification to an EASA aircraft, for the purposes of a flight test. issue a Certificate of Fitness to Fly since the C of A has been invalidated. the C of A is valid providing it is still within the date shown on it. issue a Permit to Fly.

The Flight Manual is part of the. JAA Form 1. Certificate of Airworthiness. Certificate of Registration.

What Certificate must an Operator have who flies for public transport and cargo carrying?. Air Navigation Certificate. Air Transport Licence. Air Operators Certificate.

The validity of a C of A extends for. six months. as stated on the certificate. the life of the aircraft or a change of ownership.

A certificate of airworthiness is a requirement of. IR Part-21. JAR OPS. IR Part-M.

What is the period of validity for a Certificate of Registration?. Until a change of ownership or maintenance arrangements. Until a change of ownership. The same as for the aircrafts C of A.

A series EASA aircraft flying for the approval of a major modification flies under. A conditions. a permit to fly. B conditions.

When preparing a weight and C of G schedule, the variable load can be calculated from the. weight of the pilots and any special equipment that they carry. weight of A.P.S. and payload. Nothing.

A non-expiring EASA C of A will be issued by the CAA after. 28 September 2005. 28 September 2008. 28 September 2007.

A Certificate of Approval of Aircraft Radio Installation is awarded. before the aircraft obtains a C of A. after the aircraft obtains a C of A. regardless of the aircraft's C of A status.

A certificate of fitness for flight. clears an aircraft for a scheduled flight. permits the aircraft to fly under A condition. permits the aircraft to fly under B conditions.

A Certificate of Clearance can be issued by organisations with BCAR approval. A8-13. A8-9. Primary Companies.

A flight manual. must be carried on all public transport aircraft. forms part of the C of A. is sometimes called the operations manual.

A radio station license becomes invalid. whenever a radio Flight test is required. upon change of ownership of aircraft. when the c of a is due for renewal.

A certificate of approval of Aircraft Radio Installation is issued to. an aircraft. an air operator. a company approved for such installations.

A C of A for export is. to allow an aircraft to be flown away on export. A statutory document. necessary for each exported aircraft.

The purpose for which an aircraft may be flown on a special category C of A is. applicable to ex military aircraft only. stated on the certificate. for private use only.

The period of validity of a Permit Flight Release Certificate is. stated on the permit to fly. until the end of the days flying. stated in the maintenance schedule.

A permit to fly is valid. for 12 months. until the date stated on it. only for evaluating a modification.

C of As for EASA aircraft are. necessary for all aircraft. required by IR Part 145. required by ANO.

The period of validity of an EASA C of A is. as stated on certificate. 36 months. indefinite.

An aircraft with a Standard category C of A may be used for. any purpose. carrying passenger and/or freight only. carrying passengers only.

A Cof R is renewable. when aircraft is sold abroad. every year. when ownership changes in U.K. only.

A C.of R. is issued by Ministry of Trade and Industry. may not be issued if aircraft could be more suitable registered elsewhere. is valid only in country of origin.

A Noise certificate is valid for. unlimited duration. until a change in ownership of the aircraft to an owner located in another member state. until a change in ownership of the aircraft.

Categories with respect to the C of A are. Transport, Aerial Work, Passenger and Special. Standard and Special. Transport (Passenger) and Passenger (Cargo).

When is a Certificate of Fitness for Flight under A conditions required?. To allow an unregistered aircraft to fly for air test. After a Certificate of Maintenance Review has been signed. To allow an aircraft to fly on air test to check out a modification.

An aircraft Radio License has to be renewed. every three years. every five years. only on change of aircraft ownership.

An aircraft is awaiting spares. What effect has this on the Certificate of Maintenance Review?. Deduct time. Remains unchanged. Add time.

An aircraft with a transport category C of A cannot be flown for hire and reward except. under the terms of an air operators certificate. under the terms of an aerial work certificate. under the terms of an aircraft dealers certificate.

If an EASA aircraft is required to be flown without a C of A, for the issue of a C of A. an EASA Permit to Fly is applied for. it can be flown with special permission from the competent authority. it can be flown under A Conditions.

A British aircraft manufacturer must apply for a Certificate of Airworthiness. to the Department of Trade and Industry. to the I.C.A.O. to the C.A.A.

A Noise Certificate is a requirement of. IR Part-21. JAR OPS. IR Part-M.

Variable load is weight of. fuel, oil and non-expendable equipment relevant to role. crew, their baggage and equipment relevant to role. basic weight plus operating weight.

A Flight Manual is. part of the Certificate of Registration. part of the Certificate of Airworthiness. for information of the crew only.

What is the period of validity of a C of A for an aircraft in the Special Category below 2730 kg?. On-going, provide the aircraft is maintained to an Approved Maintenance Schedule. 1 Year. 3 Years.

A new imported series aircraft requires flight testing prior to the issue of its first UK C of A. this flight test should be carried out under. A Conditions of the A.N.O. an EASA Permit to Fly. B Conditions of Schedule 2 of the A.N.O.

Which of the following would an EASA Permit to Fly NOT be used for?. To proceed to a place where the aircraft will be painted. To fly passengers or cargo domestically. To check a modification.

Part A of the Weight Schedule refers to. the aircraft prepared for service weight. the variable load. the basic weight.

How many copies of the Certificate of Registration are required?. Two copies, one for the flight manual, one for the filing system. Two copies, one for the owner, one for the aircraft. one copy for the owner/operator.

Details of aircraft weight and C of G may be obtained from information given in. CAA Publication CAP 562. Section 1-8. CAA Publications CAAIP Leaflet 1-4. Schedule 4 of the ANO.

When preparing a weight and C of G schedule, the variable load can be calculated from the. weight of the passengers plus fuel and cargo. weight of the pilots and any special equipment that they require. weight of the APS and payload.

When a major defect occurs during an aircraft's Certificate of Airworthiness period of validity. the C of A immediately becomes invalid. the C of A is suspended until the defect is rectified. the C of A is not affected.

Before an aircraft, issued with a Permit to Fly is flown, the aircraft and its equipment must be certified as fit for flight by the certification of. a Fitness for Flight Certificate. a Certificate of Release to Service. a Permit Flight Release Certificate.

The aircraft weight schedule must be preserved by the operator. for a maximum period of nine months. for a period of six months following the next occasion on which the aircraft is weighed. for a minimum period of three months.

Mandatory equipment required to be fitted on an aircraft would be found in. BCAR Section C. BCAR Section K or EASA Part-21 CS 25. BCAR Section E.

How many copies must be made of the load sheet?. Three. One. Two.

Who is responsible for making a recommendation for a C of A renewal?. The approved organization maintaining the aircraft to an Approved Maintenance Schedule. The type rated engineer. The CAA Surveyor.

When does a C of G schedule need to be renewed?. At manufacturer then at 5 yearly intervals. Whenever the weight and/or C of G are known to have changed. Every 3 years.

At C of A renewal. the aircraft never needs to we reweighed. the aircraft needs to be reweighed. the aircraft only needs to be reweighed if it is due for re-weighing.

An aircraft's Weight and CG schedule contains. aircraft's weight, CG, period of validity and dates. aircraft's weight and CG only. aircraft's weight, CG and data used for loading.

The certificate of registration becomes invalid if. the AOC is termed invalid. it is found that the aircraft is registered in another country. the C of A is invalid.

A radio installation is. a C of R requirement. an operational requirement. a C of A requirement.

When does a noise certificate not have to be carried?. When leaving and arriving at the same aerodrome. When in UK. When in an EC member state.

In a company with a Part-M approval, an Airworthiness Review Certificate may be signed by. any employee holding an appropriate licence. qualified persons nominated by the company. no-one, it is not required under Part-M.

What is the retention time for a Technical Log?. 2 years after the last entry. 2 years. 3 years after the last entry.

Can a person not employed by an approved organisation sign the CRS?. Only in certain situations. No. Yes.

Tasks which may be completed without the certification of a CRS is given. EASA Part-66 Appendix VI. EASA Part-145 Appendix III. EASA Part-M Appendix VIII.

Maintenance of large aircraft must be carried out by. a part-M approved organisation. a part-145 approved organisation. a part-147 approved organisation.

All outstanding deferred defect rectifications are recorded in. the flight manual. the operator's technical log. the appropriate Log Book.

An airworthiness review certificate, when issue, is valid for. 1 year. 3 years. indefinitely, until varied, suspended or revoked.

Aircraft components released for service from an EASA Part-M approved organization must do so under cover of. EASA Form 1. Form 268A. EASA Form 10.

The technical log is a requirement of. IR Part-145. IR Part-M. IR Part-21.

Which of the following is not contained in a Tech Log?. List of acceptable deferred defects. Weight and C.G. Schedule. Certificate of Maintenance Review.

A staff member of a Part-M organisation authorised to issue or recommend issue of an airworthiness review certificate. need not be part 66 qualified. must be both Part-66 qualified and have an aeronautical degree. must be Part-66 qualified.

The persons authorised to issue or recommend issue of an airworthiness review certificate are listed. in the company exposition. on the airworthiness review certificate. on the Part-M Certificate of Approval.

An airworthiness review certificate is necessary after. refuelling an aircraft. a specified number of hours from the issue of the previous one. any task affecting airworthiness of the aircraft.

The operator of an aircraft used for commercial air transport. need not be approved to IR Part-145 providing they are contracted to a Part-145 organisation. must be approved to IR Part-M only. must be approved to IT Part-145.

Who produces and prints maintenance schedules?. CAA for Air Operators Certificate Organizations. CAA and approved by the manufacturer. The Part-M approved organisation.

An EASA approved maintenance organisation in the category B rating, is approved to carryout maintenance on. aircraft. engines. aircraft and engines.

An airworthiness review certificate can be extended. twice only. once only. It cannot be extended, it must be re-issued.

Which of the following documents forms part of a tech log?. Maintenance Statement. Air Operators Certificate. Type certificate data sheet.

Tasks which may be completed without clearance on a CRS are listed in. EASA Part-M. the ANO. the approved maintenance schedule.

Continued airworthiness is the responsibility of. the owner or lessee. the part-M company. the part-145 company.

A pre-flight inspection. can be carried out only by an A, B1 or B2 licensed, type rated and Part-145 company approved engineer. can be carried out only by an A or B1 licensed, type rated and Part-145 company approved engineer. does not require Part-145 approval for carrying-out.

Under EASA how long does the Technical Log have to be retained?. 5 years after the last entry. 2 years after the last entry. 3 years after the last entry.

The requirement for an EASA aircraft to be maintained in accordance with an Approved Maintenance Programme is set out in. EASA IR Part 21. JAR OPS (Subpart M). The Air Navigation Order.

The application for approval of a maintenance schedule, presents to the Authority a Maintenance Schedule which is based upon whose recommendation?. The operator. An approved design organisation. The Type Certificate holder.

How many copies of a maintenance schedule are submitted to the Authority for approval?. 1. 2. 3.

Where is the period of validity of CMR stated?. In the maintenance schedule. On the CMR. In the maintenance statement.

An operator adds a new aircraft to its fleet. An amendment to its Approved Maintenance Schedule must be applied for, only if the aircraft differs in any way to the aircraft already in its fleet. An amendment to its Approved Maintenance Schedule must be applied for, only if the aircraft is a totally different Type to any of the aircraft already in its fleet. An amendment to its Approved Maintenance Schedule must be applied for, even if the aircraft is identical to the aircraft already in its fleet.

The pilot of an aircraft can sign. the second part of a duplicate inspection providing he is licensed on any similar aircraft type. the first part of a duplicate inspection providing he is licensed on the respective aircraft type. the second part of a duplicate inspection providing he is licensed on the respective aircraft type.

If, at a major check, there is too much documentation to go into the log book. a CRS is raised to cover the documentation, and the documentation is then discarded. a new log book is raised. the documentation is stored elsewhere and the logbook is cross referred to it.

Scheduled maintenance can be extended by authority written into the. Approved Maintenance Schedule. Aircraft Maintenance Manual. Approved Maintenance Document.

Vital points are. parts of the aircraft where a single malfunction could cause catastrophic failure. a check on every maintenance schedule input. when an engine/fuel system is disturbed.

How many items can be entered on an Approved Certificate?. Only 1. As many as there is room for providing they are similar items. As many as there is room for providing each entry is perfectly readable.

An incident must be reported within. 96 hours. earliest convenient time. 24 hours.

What approval would you need to maintain airships?. BCAR A8 18. Part-145 with two sections of BCAR A8 18. JAR A.

Details of all placards and markings on an aircraft will be found in. the Maintenance Manual. the Operations Manual. the Flight Manual.

Whom would you inform of an Occurrence/Incident?. The Department of Trade. QA department of your organisation. The CAA.

When a modification is carried out on an aircraft, details are entered in. the Log Book. the Modification Record Book. both the Log Book and the Modification Record Book.

How long is a Technical Log retained for a non-EASA aircraft?. Until the CAA has given authorisation for them to be destroyed. Three (3) years after the aircraft has been destroyed or permanently withdrawn from service. Two (2) years after the aircraft has been destroyed or permanently withdrawn from service.

All aircraft which fly in UK airspace must be registered, with the exception of. none. kites, captive balloons and aircraft under B conditions. kites, balloons, gliders and variant aircraft.