module 10 - part 2

Authority to amend a maintenance schedule is given by the. local CAA surveyor. CAA with written consent. operator.

A Licensed Engineer will sign a CRS when. he is happy that all physical aspects of the job are finished. he is sure that he has company approval. the job is complete and properly recorded.

If a design amendments is made to a drawing. the old issue number is retained with a new amendment date added. a new issue number and date is allocated to the drawing. no change in issue number is necessary.

An AOC is issued by the CAA for aircraft in the. transport and Aerial Work categories. transport categories. transport passenger category.

If an exit becomes unserviceable, the action to be taken is to fly to the nearest place where a repair can be carried out, and. radio ahead for spares. bar the exit with a white disc with NO EIT in red. bar the exit with a red disc with NO EIT in red in a white bar.

Details of placards and markings on aircraft will be found in. ATA Chapter 11 of the AMM. Operations Manual. Approved Maintenance Manual.

The legal responsibility for ensuring that the aircraft load is not excessive and has been properly loaded rests with. Commander of the aircraft. Load Master. Chief Pilot.

The telecommunications log book is considered to be part of the. Public Address Licence. Radio Licence. Radio approved document.

For what period of time must a load sheet be kept?. Five years. Two years. Six months.

Information about identification markings can be found in. CAAIPs and ANO. ANO. EASAs.

Certificates of Fitness for Flight are signed by. A CAA surveyor. An appropriately licensed engineer. An Inspector or QA Engineer.

Under what conditions can you fly when a C of A has expired?. conditions. conditions. conditions.

Flying times are recorded from. take off to touch down. chock to chock. engine start to shut down.

Flying under A conditions is carried out by aircraft in the. proto-modified Group. variant Group. series aircraft group.

The period of validity for a Certificate of Fitness for Flight is. not exceeding the validity of the C of A. a maximum of ten days. a maximum of seven days.

When is a flight test certificate signed?. After a test flight. Before a test flight. Whenever an aircraft is flown.

When is a 'Permit Flight Release Certificate' issued?. Before an aircraft is flown with a valid C of A. Before an aircraft is test flown with a permit to fly. Before a series aircraft is flown.

The minimum equipment list is found in the. Flight manual. Maintenance manual. Maintenance schedule.

When would a repair scheme be treated as a modification?. When the repair has not previously been approved by the CAA and FAA. When the repair has not previously been approved by the FAA. When the repair has not previously been approved by the CAA.

A letter of transmittal is. authorisation to use an Approved Maintenance Schedule. authorisation to amend a Maintenance Manual. a record of accepting a type certificate.

A LAMS schedule applies to aircraft. under 2730Kg MTWA. over 3600Kg MTWA. under 2300Kg MTWA.

Where are scales of equipment to be carried found?. Air Navigation Order, schedule 4. Airworthiness Notices. Air Navigation (General) Regulations.

If a modification is carried out on an aircraft, it is entered. the modification record book. both aircraft and modification log books. the aircraft log book.

On completion of a modification to a non-EASA aircraft, for the purpose of a test flight. a Permit to Fly is issued. the C of A is valid so long as it is still in date. a Certificate of Fitness for Flight is issued as the C of A has been invalidated.

Deferred defect pages are kept in the. maintenance schedule. log book. tech log.

Companies with design approval can be found in. front of the maintenance schedule. Part-145 list of companies. the company exposition.

Certificate of Airworthiness for International flight on transport aircraft. must be carried. must not be flown with aircraft. does not have to be carried.

The check cycle for aircraft operating to the LAMS schedule, is. 50hr, 100hr annual and star inspections. 75hr, 150hr and star inspection. 50hr, 150hr, annual and star inspection.

A CAA issued capability list gives. details of the operational restrictions placed on an aircraft with a C of A. details of the scope & extent of a type rated engineers license. details of the scope & extent to which an organisations approval is given.

Tasks which may be completed without the certification of a CRS is given. in ANO. in BCARs. in A N(G)R.

An aircraft operator's MEL. can be more restrictive than the MMEL. can be less restrictive than the MMEL. can be more restrictive with certain limitations.

A service bulletin contains. a list of maintenance tasks to be carried out on a particular aircraft. information concerning the airworthiness of aircraft and are distributed by the CAA. a detailed description of a problem and corrective action to be taken.

Condition Monitoring is. not a preventative process, having neither Hard Time nor On-Conditioning elements. a combination of Hard Time and Flexi-time working practices. a preventative process.

An allowable deficiency is listed in the. Tech Log and Cabin Defect Log Book. Tech Log and deferred defect column. Tech Log and if necessary the deferred defects column.

An MMEL is compiled by. an air operator and approved by he CAA. the manufacturer and the AOC company after joint consultation and then approved by the CAA. the manufacturer and the CAA after joint consultation.

Flight manual amendments. can be done by the operator. must have written consent of the CAA. can be done by the manufacturer.

Registration of aircraft operated by a company can be found. in the approved maintenance schedule. in the Company Exposition. on the AOC.

An aircraft may fly unregistered. under A conditions. for export purposes. under B conditions.

Foreign Airworthiness Directives, Volume 1 & 2 cover. aircraft above and below 2730Kg MTWA. aircraft above and below 5700lbs and equipment fitted to them. aircraft above and below 5700Kg MTWA and equipment fitted to them.

If the second copy of the Tech Log can not be left on the ground, it should. be flown in an approved (by the CAA) box on the aircraft. be carried by the pilot. be flown on a different aircraft.

The pilot of an aircraft. cannot sign the 2nd part of a duplicate inspection. can sign the 2nd part of the duplicate inspection if the aircraft is away from base. can sign the 2nd part of a duplicate inspection if licensed on that particular type.

Aircraft above 5700 kg are weighed. every five years. two years after manufacture thereafter every five years. at manufacture then after 2 years then every 5 years after manufacture.

Who issues a C of A for export?. The CAA - SRG. The manufacturer. The Approved Organisation.

CAP 393 is. the ANO and regulations. Air Operators Certificate. AWNs.

AWN 3 is. related to engineers personal responsibility when medically unfit. related to engineers licence type rating. related to the responsibilities of licensed engineers.

Volume 1 and 2 of FADs. relate to aircraft from countries other then USA and UK. are published by the CAA. are published by the FAA.

The minimum number of battery powered megaphones required for an aircraft capable of carrying more than 199 passengers is. 3. 5. 7.

Life jackets not equipped with a whistle are. acceptable for one passenger of a pair. not acceptable. acceptable for children under 3 years old.

Maintenance Manuals in cassette/CDs have the advantage of being easier to. amend. store. read.

It is the responsibility of the person accepting parts for use on an aircraft to ensure that. a green serviceable label is attached. those parts conform to the required standard and are serviceable. those parts are designed to the appropriate Authorised Release Certificate.

Mandatory markings for flight instruments, or placards are annotated in the. Aircraft Maintenance Schedule. Flight manual or Certificate of Airworthiness. Aircraft Maintenance Manual.

Consumable items such as split pins, nuts, nuts bolts etc are usually identified by a. batch/part number on the containing bag. batch number on each item. release note on each item.

CAP 360 relates to. EASA aircraft only. crop spraying aircraft only. Public Transport aircraft.

Holding a Licence Without type (LWTR) only affords the holder. automatic company approval. limited certification ability. no certification rights.

All reports received by the CAA under the MOR scheme are processed by the. EASA. CAA. Air Accident Investigation Branch.

In respect of an aircraft exceeding 2730kg maximum total mass, a CRS is required. when a component has been replaced even if it is the same component. when an item of workshop test equipment is submitted for an annual check. only if component replacement in an aircraft involves a different component.

The full extent of the certification responsibilities of a licence engineer with regard to the CRS will be found in. AWN 3. ANO schedule. BCAR section A.

Vital points identified and included in the maintenance documents. relate to points subject to a duplicate inspection. relate to areas in which all work must be carried out by a suitably licensed engineer. identify areas or components subject to timed life.

A Master Minimum Equipment List (MMEL) is. more restrictive than a Minimum Equipment List. is a list of items that may be inoperative on an aircraft. originated by the aircraft operator.

An airline's MEL contains an additional note (M). This indicates a. Mandatory operational restrictions. Maintenance requirements. Modified component or system.

Technical limitations of work and authority with reference to Aircraft Maintenance Engineers are laid down in. BCAR Section L. Airworthiness Notice 3. ANO.

An A or C Type rated aircraft maintenance engineer may issue a CRS relating to an associated electrical system within limitations laid down in. BCARs section L. ANO. AWN 3.

When completing a Certificate of Maintenance Review, which of the following must be completed?. C of A. CRS. A maintenance statement in the tech log.

An aircraft of less than 2730Kg operating in the private category would normally be maintained I.A.W. the manufactures maintenance schedule. LAMS. the owners wishes.

Foreign AD volume 2 is applicable to aircraft, engines, propellers, and equipment manufactured in. the former USSR. Europe. the USA.

With reference to engineer licensing, aircraft for which type rating can not be obtained are found in. Airworthiness Notice No 10. BCAR section L. EASA IR Part-145.

The ANO states that the Log Book shall be kept for the aircraft and one for. each engine and VP propeller. each engine and undercarriage. its radio and navigation equipment.

An airline wishes to fly an aircraft to a contractor within the UK with all the passengers seats removed ready for refurbishment and painting. The flight may be authorised using. A special request procedure to the CAA. A conditions. B conditions.

Mandatory modification of UK origin are identified by the CAA. AAD. AAN. AD number.

The check cycle for an aircraft is. the same for all aircraft maintained by one operator. stated in the approved maintenance schedule. the same for all aircraft of one type.

For a simple aircraft the CAA LAMS Schedule may need to be amended by. deleting non application items. completing the supplementary texts. rewriting it.

A CRS is not required on completion of. each check A for aircraft not exceeding 2730Kg MTWA. each inspection item on the AMS. a check on the check cycle.

A CMR must be completed on aircraft exceeding 2730Kg at. periods not exceeding 4 months. every 4 months. every 12 months.

A duplicate inspection must be the last. CRS issue. check before issue of a CRS for the task. signature after a CRS for the task.

A maintenance statement is. the approval for a maintenance schedule. part of the tech log. used to certify a pre-flight check.

MAMIS lists mandatory inspections and service bulletins of aircraft manufactured in. Europe (not including the UK). the UK. USA.

Guidance with respect to Part-145 and CAA national requirements can be found in. BCAR section A. CAAIPs. AWN 14.

An aircraft maintenance engineer licence does not include unlimited certification in NDT testing. Guidance with respect to NDT personnel can be found in. CAP 747. BCAR section L. CAAIPs.

Information on Air Operators Certification is to be found in ANO. Article 6. Article 9. Article 10.

An Air Operators Certificate must be issued by the CAA. before an airline can. carry passengers and/or freight for reward. carry freight for reward. carry fare paying passengers.

An approved certificate certifies that. items are serviceable on delivery. materials and parts come from an approved source. materials and parts conform to required standard.

B.C.A.R.s. contain minimum requirements to be met. detail mandatory requirements for aircraft design and construction. are issued by Ministry of Trade and Industry.

CAAIPs. contain approved inspection procedures. contain mandatory instructions. are issued by CAA.

A Major Modification. will always require air testing after embodiment. is approved by an A.A.N. must be certified in the Modification Record Book.

An Approval Authority Reference number. is issued by Ministry of Trade and Industry. will be of specific form. must be included on all Approved Certificates.

Technical and Administrative information is officially circulated to L.A.M.E.S. in. AWNs. CAIPs. B.C.A.R.s.

A glider being used privately, and not crossing boundaries of countries. must have a Permit to Fly. does not need a C of A. must have a C of A.

An approved store. is required by every approved organization. is the responsibility of Quality Assurance Department. must contain at least a bonded store.

On a duplicate inspection on a helicopter, what checks are carried out?. Control system only. Control system and anything that controls propulsive force. Propulsive control system only.

A CMR is raised after. major overhaul. scheduled servicing at specified intervals. defect rectification.

Occurrences should be reported to. Department of Trade & Industry. Chief Inspector of Accidents. CAA.

Which of the following manuals would be referred to when checking the airworthiness directive on a British constructed engine?. CAA Additional Directives CAP 473. FAD Volume 3 CAP 474. CAP 476 Mandatory Aircraft Modifications and Inspections Summary.

An Airworthiness Directive carried out to an engine of American construction fitted to British built aircraft below 5700 kg MTWA would be certified in. the Engine Log Book. the Aircraft Log Book. the Modification Record Book.

When related to aeronautical engineering, the term Inspection is defined in the publication. ANO Article 11. BCAR Section L. Airworthiness Notice (AWN) 3.

Mandatory modifications are. modifications which ensure continued airworthiness. modifications which are approved on an airworthiness approval note. modifications of an urgent nature.

Air Navigation (General) Regulations are to be found in. CAA Printed Manual CAP 393. British Civil Airworthiness Requirements Section A. Airworthiness Requirements CAP 455.

British Civil Airworthiness Requirements. are printed by the CAA and are of an advisory nature. form the Technical requirements for the design and operation of aircraft and their equipment. interpret the ANO and form the Technical requirements for the design, construction, operation and maintenance of aircraft and their equipment.

Airworthiness directives for American built engines fitted to aircraft not exceeding 5700 kg would be found in. FAD Volume 3. FAA Airworthiness Directives Volume 1. FAA Airworthiness Directives Volume 2.

Airworthiness Notices are amended by. issue numbers and dates as necessary. monthly issue numbers. CAA yellow pages.

An airworthiness directive must be complied with. before further flight. as soon as practicable following receipt of the directive. within the time or flying hours limitations given on the directive.

Information contained in the ANO is. of a legal nature in all sections and is therefore mandatory. written in compliance of the Civil Aviation Act of 1943 ratifying the ICAO Convention. of a mandatory nature where safety is concerned.

What documents should be carried when flying an aircraft overseas for the purpose of exportation?. C of A for export, a C of R, and a validation certificate. C of A for export, a ferry certificate and a permit to fly. C of A for export, a C of A for Ferry Purposes and a C of R.

The responsibilities of licensed engineers for certification of aircraft are laid down in. ANO. ANO (General) Regulations. Airworthiness Notice 3.

Maintenance Schedules are issued. in a folder with the operators name on the cover. with an approval certificate by the CAA. by the operator with CAA approval.

When nil defects are entered by the captain in a Tech Log. A Certificate of Release to Service must be issued, noting nil defects. All copies of this entry must be renewed before flight. One copy is kept on the ground.

Who can sign a Certificate of Maintenance Review?. The Captain of the aircraft if he holds an A.T.P.L. A Flight Engineer licensed for the aircraft type. A multi categorized type rate Licensed Engineer or person approved by the CAA.

Above what weight is an Air Operators Certificate required?. All aircraft flying for public transport. 3600 kg. 2300 kg.

Who approves Maintenance Manuals?. The Department of Trade and Industry. The Board of Trade. The CAA.

If an engine is inhibited. Where is this recorded?. Airframe Log Book. Engine Log Book. Flight Manual.

When extra documents are used for maintenance recovery and are too numerous to list in the aircraft Log Book, what action is taken?. Obtain new Log Book and cross refer to the original Log Book. Enter brief details in Log Book and retain documents. Enter brief details in the Log Books and cross refer to a work pack.

You are a passenger of an aircraft which sustains major damage facilitating major repair or component replacement. Who would you inform?. CAA. Chief Inspector of Accidents. Board of Trade.

An Airworthiness Directive carried out to an engine of American construction fitted to British built aircraft below 5700 kg M.T.W.A. would be certified in. The Engine Log Book. The Aircraft Log Book. The modification record book.

The certification requirements for scheduled and non-scheduled mandatory inspections, overhauls and repairs are to be found in. the organization's schedule of approval. the aircraft maintenance manual. the approval document to the aircraft maintenance schedule.

The purpose of the CRS is. to comply with article 15 of the ANO which states that an aircraft must not fly unless it is properly equipped for the intended flight. to turn a log book or job card entry into a legal document and to ensure that the signatory takes full responsibility for the work done. to ensure that the log book entry is complete.

A hard time engine inspection involves. replacement with a new or overhauled component. removal of an engine component, it's inspection and refitting. an in-situ function test.

If an engine fuel control is disturbed. the whole fuel control system must be inspected again in duplicate. the part disturbed must be inspected again in duplicate. the part disturbed must be inspected again.

An aircraft technical log forms. a permanent history of the aircraft. a part of the certificate of airworthiness for transport category aircraft. a day to day history of the aircraft.

Log books are initially provided by. the manufacturer. the C.A.A. the operator.

You would expect to find information on ground handling of aircraft in the. Flight Manual. Aircraft Maintenance Manual. Aircraft Overhaul Manual.

A.T.A. Specification No. 100 is. an internationally agreed form of Maintenance Schedule. a system of numbering chapters and sections of Manuals. a statement of international airworthiness.

Where would you find legislation governing Nationality and Registration Marks on U.K. registered aircraft?. C.A.A.I.P. B.C.A.R. A.N.O.

A Quarantine Store. holds life controlled items only. holds materials and parts until proved to conform to specification. holds parts and materials received from overseas.

A concession is. authority not to embody a modification. authority for a permanent reduction of a requirement. authority to accept a limited quantity of parts which may not be strictly in accordance with the relevant drawings or specifications.

Which of the following is typical of the number granted to an approved organization under BCARs. A N/0000/67. A I/0000/103. A I/0000/83.

Technical Logs are mandatory for the following groups: Private plus Special Category. Transport Category plus private category. Transport Category plus aerial work category.

Rectification of defects should be entered in appropriate logs. before expiration of Certificate of Maintenance Review. immediately reported. within seven days of expiration of Certificate of Maintenance Review.

A Certificate of Maintenance Review must be retained for. two years after expiry of period of validity. two years after date of issue. six months after date of issue.

Where would you find inspection and classification of damage and repair?. Repair Manual. Flight Manual. Maintenance Manual.

Are C.A.A.I.P.s mandatory?. Yes, but only for six months at a time. Only selected parts which are in B.C.A.R. No, nothing in C.A.A.I.P. is mandatory.

The aircraft captain records the aircraft hours flown and defects in. Aircraft Log Book. Technical Log. Maintenance Statement.

Air Navigation Regulations are originated by. CAA. Privy Council. Department of Trade and Industry.

A Technical Log is originated by. Manufacturer. CAA. Operator.

Details of International Aircraft Markings on the U.K. register will be found in. ANO. Flight Manual and Certificate Organizations. B.C.A.R.

When a minor adjustment to a control system has been made away from base, a pilot or flight engineer may sign, if licensed for the type concerned. neither part of the duplicate inspection. the second part of the duplicate inspection. both parts of the duplicate inspection.

After a modification to an aircraft, what has to be raised?. Certificate of Release to Service. Certificate of Modification. Certificate of Maintenance Review.

What work has to be recorded and signed for?. Only work involving replacements. All work carried out. Only work which entails a duplicate inspection.

Who can sign the Certificate of Release to Service? gineer or approved inspector. A licensed engineer or approved inspector. Only a licensed engineer. Anyone who has worked on the particular task.

What should not be kept in Quarantine or Bonded Store?. Engine Spares. Commercial Supplies. Aircraft spares.

Where can information on overhaul and replacement periods be found?. Flight Manual. Technical Log. Maintenance Manual.

An operator who uses his aircraft for the transportation of cargo must do so under the terms of an. Aerial Application Certificate. Aerial Dealers Certificate. Air Operators Certificate.

An Alert Service Bulletin is issued by. the Manufacturer, notifying aircraft owners and Maintenance Organizations of an urgent major modification. the CAA giving notification of a mandatory modification. the Manufacturer notifying aircraft owners and Maintenance Organizations of a modification affecting aircraft airworthiness.

CAA Approval for a major modification is given on. an Airworthiness Approval Note. Form AD 282. Form AD 261.

After a reportable occurrence involving an aircraft, for how long must the operator retain the relevant Flight Data records?. 7 days. 14 days. 2 years.

The Light Aircraft Maintenance Schedule is used for aircraft below the maximum total weight authorized of. 2300 kg. 2730 kg. 6000 kg.

Technical Logs are raised. only if aircraft is to land away from home. in triplicate. in duplicate.

A four (4) Engined Turbo-Prop Aircraft requires. 1 - Combined Log Book. 5 Statutory Log Books. 9 Statutory Log Books.

The Commander records defects. on the C of R. on the C of A. in the Technical Log.

Airworthiness Notices 3 and 10 deal with. maintenance. approvals. licensing.

The standard Format for Maintenance Manuals is defined in. ATA 100. B.C.A.R.s. A.N.O. and A.N.R.s.

In the A.T.A. 100 System, Pages 1 -100 for Chapters in Maintenance Manuals covers. description and operations. maintenance practices. description.

A.T.A. 100 is used in. repair manuals. fuel specifications. technical and administrative Publications.

The captain can sign for a Duplicate Inspection. if away from base. if A and C Licensed. if there are two Engineers.

Storage conditions are critical in the. special equipment Store. Quarantine Store. Bonded Store.

Fuel Flow results are entered in the. Aircraft Log Book. the Fuel Uplift column of the Tech Log. Engine Log Book.

Additional equipment which must be installed according to the circumstances in which an aircraft is flown is listed in. the Forth Schedule of the A.N.O. Part A of the Weight Schedule. the Certificate of Airworthiness.

The number of electrical fuses of a particular rating required to be carried in an aircraft is. 5 amp or less 3, off 5 amp or more 10 off. 3% of each rating or 10, whichever is the greater. 10% of each rating or 3, whichever is the greater.

Mandatory Aircraft Modifications and Inspection Summary is divided into. 4 parts: aircraft, engines and propellers, radio stations, equipment. 3 parts: aircraft, engines and propellers, radio and equipment. 2 parts: aircraft and equipment, engines and propellers.

A letter of Transmittal. records acceptance of a Type Certificate. authorizes an amendment to a Maintenance Manual. authorizes a Maintenance Schedule by the CAA.

The total engine hours expended may be determined from information given in. the Maintenance Statement. the Technical Log. the Engine Log Book.

When an unserviceable component is removed from an aircraft and replaced with a different component to carry out the same function it is classified as. a repair. a modification. a replacement.

The definition of a Reportable Accident is given in. CAA Air Regulations number 11 CAP 393. Civil Aviation (Investigation of Accidents). ANO Article 94.

Where is the overhaul period of an aircraft component found?. In the Approved Maintenance Schedule. In the Maintenance Manual. In the Overhaul Manual.

The Certificate of Fitness for Flight is issued in. 1 copy: for the Aircraft. 2 copies: for Aircraft and File. 3 copies: for Tech Log, File and Aircraft.

The aircraft owner's Name Plate must be fixed. near the main entrance of the aircraft. on the instrument panel. on the rear fuselage.

In the ATA 100 format, what would the third element of the reference number refer to?. Chapter or system. Section or sub section. Subject or component.

Air Navigation General Regulations are to be found in. British Civil Airworthiness Requirements Section A. CAA printed manual CAP 393. Airworthiness Requirements CAP 455.

Information on the procedures adopted by an approved B1 organization for controlling matters directly affecting airworthiness and technical standards will be laid down in. the organization's exposition. BCAR Chapter A8-3. EASA Part-145.

Duplicate inspections are required to be made following the disturbance of. all engine and propeller controls and any vital points. all engine & propeller components and any vital points. aircraft, engine & propeller controls and any vital points.

The wording of the Duplicate inspection statement is given in. ANO Article 2. BCAR Section A & B/6-2. Airworthiness Notice No.3.

A duplicate inspection is defined as an inspection made and certified by. a qualified person and subsequently repeated by that person. a qualified person and subsequently by another qualified person. an unqualified person and then by a qualified one.

BCAR Organizations which automatically have design approval are. M1 Maintenance organizations. Primary companies. M3 Maintenance organizations.

Certificates of release to service. are kept for 2 years. can be signed by company approved engineers. are signed before each flight.

BCAR Section A applies to. aircraft on the UK civil register manufactured outside the UK. all aircraft on the UK civil register. aircraft on the UK civil register manufactured in the UK.

What happens to a Hard Time component when removed from an aircraft?. Scrapped or returned for overhaul. Placed in quarantine store. Inspected and if serviceable can be replaced.

CAP 393 - Air Navigation - The Order and the Regulations. is fully authoritative and would be referred to in a court of law. only Part 1 is fully authoritative and would be referred to in a court of law, whereas the General Regulations are not authoritative. is not considered authoritative and would not be referred to in a court of law.

BCAR A8-8 E3 will. be added to Part-145 ratings on application to the CAA. transfer to JAR OPS (M) when an AOC is awarded. not transfer when JAR-21 becomes the legal code.

The requirement to fly an aircraft properly equipped and that the equipment fitted is to be serviceable, is given in. Article 8 of the ANO. schedule 4 of the ANO. Article 14 of the ANO.

Engine and propeller log book requirements are covered in. Schedule 6 of the ANO. JAR E. Article 11 of the ANO.

The current ANO has. 101 Articles, 11 Schedules. 123 Articles, 14 Schedules. 168 Articles, 15 Schedules.

CAA Additional Airworthiness Directives are printed on. Blue Papers. White Papers. Yellow Papers.

Which of the following publications contains additional directives for German built aircraft on the British Register?. CAP 474. CAP 475. CAP 476.

Condition monitoring. permits in-life until failure occurs. is a time lifed method of maintenance. is a preventative maintenance process.

The allowable deficiency list is normally included in an aircrafts. approval document to the aircraft maintenance schedule. modifications record book. operations manual.

The master minimum equipment list is compiled by. the manufacturer and the air operator after joint consultation and then approved by the CAA. the air operator and approved by the CAA. the manufacturer and the CAA after joint consultation.

An aircraft operators MEL. can be more restrictive than the aircrafts MMEL. can be less restrictive than the aircrafts MMEL. must be the same as the aircrafts MMEL.

Information on Air Operators Certificate is to be found in the Air Navigation Order. Article 6. Article 9. Article 20.

If, as the result of a reported occurrence, an error in general engineering practices was established, this would be circulated by the CAA to all organizations and persons concerned by. CAA publication CAP 479, Engineering Safety Practices. an amendment to CAA publication CAP 562 Civil Aircraft Airworthiness. an airworthiness notice.

The wording for the Certificate of Fitness for Flight is to be found in. Chapter (A&B) 3-8 of BCAR. Chapter A6-2 of BCAR. Chapter (A&B) 6-7 of BCAR.

Companies holding C.A.A. design and Inspection Approval for the manufacture and overhaul of complete aircraft are defined as. primary companies. material manufacturers. suppliers.

An Additional Airworthiness Directive is issued by the C.A.A. for certain aircraft, which are. British constructed aircraft. American constructed aircraft on the British Register. Any foreign aircraft on the British Register.

The signals to be used when ground marshalling an aircraft can be found in. C.A.I.P.s Pt. 1. Air Navigation Rules - Aerodrome Traffic Rules. B.C.A.R.s Sect. D.

Who normally carries out the maintenance on an aircraft under 2730kg in the private category?. A Part-145 approved organisation. A company with BCAR approval only until 28th September 2008. A Part M organisation.

CAP 395 - modification record book is required for. American aircraft only. all aircraft. all aircraft over 2,730 kg.

On a light aircraft with a 3 year C of A, a Star Inspection must be carried out. at each annual inspection. at the third annual inspection. at every 150 flying hours.

A Certificate of Maintenance Review for an aircraft over 2,730 kg has a maximum period of validity of. 4 months. 6 months. 1 year.

Certification responsibilities of Licensed Engineers and Approved Inspectors can be found in. CAIPs pt 111. EASA IR Part-66. Airworthiness Notices 3 and 10.

How many times must the nationality and registration marks appear on an aircraft?. 3 times. 4 times. 5 times.

An aircraft can fly without registration markings. under an EASA Permit to Fly. under B conditions. under A conditions.

Privately owned aircraft over 5700 kg must be maintained by. an A8-13 company. a Part-145 company. an engineer independent of a Part-145 company.

Aircraft over 5700 kg must be weighed. within 2 years of manufacture. at every major check. annually.

The Overhaul Manual. allows you to comply with the Maintenance Schedule. allows you to comply with the Maintenance Manual. allows you to repair, test or overhaul a component.

The requirement for an aircraft to be weighed is. when required by the CAA. as specified in the Maintenance Schedule. prior to a C of A renewal.

Where are the A and B conditions of flight testing stated?. AWNs. ANO. BCARs.

CAA Additional Airworthiness Directives. supersede existing Ads. are means of amending FADs by CAA. are included in MAMIS.

An aircraft under 5700 kg is being operated privately in the UK. Who may sign for maintenance?. A suitably licensed engineer independent of a Part-145 organisation. An approved member of an A8-13 organisation. An unlicensed member of a Part-145 organisation.

When an aircraft is on a hangar check the CMR. continues to run irrespective. is suspended whilst on check. has to be renewed at the end of the check.

Scheduled maintenance inspection time or hour limits. can be extended by a LAME with respect to the extension limits of the maintenance schedule. can never be exceeded. can be exceeded in extraordinary circumstances.

Information on bogus parts may be found in. IEM 145.30 to JAR145.30. AWN 19. BCAR section A.

If a defect is raised in the tech log and deferred. it is transferred to the aircraft log book. it is left on the tech log page until rectified. it is transferred to the ADD sheets which form part of the tech log.

Where would you find details of the tasks that the holder of a private pilot's licence can do on his own aircraft if it has a C of A in the private category?. AN(G)R's. BCAR A8-15. EASA IR Part-145.

What airworthiness notice applies to propellers used on British registered aircraft?. 4. 14. 75.

The responsibility to keep and maintain aircraft log books lies with. the owner. the operator. the Part-145 organisation maintaining the aircraft.

The modification record book logs all modifications. to the aircraft only. to the aircraft, engines and propellers. only mandatory modifications.

Aircraft components require overhauls at times stated in the. maintenance schedule. overhaul manual. maintenance manual.

The overhaul manual gives you information on. how to maintain a component on an aircraft. overhaul, repair and bench test. when to overhaul a component.

A major mod is carried out. The C of A. is suspended until the mod is carried out and the time is added on to the C of A. is not effected. becomes invalid.

To what does Airworthiness Notice 60 refer?. Toilet flush motors. Cabin and toilet fire protection. Bogus parts.

The minimum requirements for recording a modification are. title page, mod no, description of mod, issue no. and date. mod. no., issue no. and date. mod. no. and date.

What covers engineers responsibilities with reference to a CRS?. AWN 3. BCARs. ANO.

The CMR covers all work including. scheduled maintenance, modifications, defects and any deferred defects. scheduled maintenance, defect rectifications. scheduled maintenance, modifications.

What modifications are recorded in the aircraft log book?. Aircraft only. Engine, propeller and aircraft. Engine and propeller.

Aircraft which must fly under an AOC are. aircraft registered in the UK. aircraft in the transport categories. any aircraft in UK airspace.

Category 2 autoland with a decision height of 100 ft has a visual line up approach limit of. 300 meters. 400 meters. 500 meters.

An operator's ETOPS approval will lapse if they cease extended range operations for a period of. 12 months. 13 month. ETOPS approval does not lapse providing the aircraft continues to meet the equipment requirements.

Extended Range Operations (ETOPS) is defined as flight conducted over a route that contains a point further than. one hour's flying time (in still air) at the normal cruise speed from an adequate aerodrome. one hour's flying time (in still air) at the normal one-engine-inoperative cruise speed from an adequate aerodrome. three hour's flying time (in still air) at the normal one-engine-inoperative cruise speed from an adequate aerodrome.

The 'Threshold Time' for an ETOPS approved aircraft is. 60 minutes. 90 minutes. 120 minutes.

Independent and reliable electrical power should be available to an ETOPS aircraft from at least. two sources at all times. one source at all times. three sources.

Any time limited system on an ETOPS aircraft should be available for. the Rule Time minus 15 minutes. the Rule Time. the Rule Time plus 15 minutes.

If an operator wishes to apply for ETOPS approval, modifications are most likely to be required of. the aircraft design, MEL, and AMS. the MEL, AMS and engineer training programme. the aircraft design, MEL, AMS and engineer training programme.

An instrument landing system requires. both airborne equipment and airport ground equipment. airport ground equipment only. airborne equipment only.

A Category 2 landing is. a decision height of 30 M (100ft) or more. a decision height of 60 M (200ft) or more. a decision height of 120 M (300ft) or more.

A Category 3 landing is. a decision height of 30 M (100ft) or less. a decision height of 60 M (200ft) or more. a decision height of 60 M (200ft) or less.

The excess ILS deviation light is coloured. amber and continuous. amber and flashing. red and flashing.

In a landing system, decision height is recognised by. a sonar altimeter. a barometric servo altimeter. a radio altimeter.

A register of airlines operatoring 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.

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. 1 flight. 2 days. 7 days.

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

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