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TEST BORRADO, QUIZÁS LE INTERESEModulo 10.7a. Applicable National and International Req.

COMENTARIOS ESTADÍSTICAS RÉCORDS
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Título del test:
Modulo 10.7a. Applicable National and International Req.

Descripción:
Applicable National and International Requirements

Autor:
Helbert Arias
(Otros tests del mismo autor)

Fecha de Creación:
01/02/2024

Categoría:
Personal

Número preguntas: 136
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Temario:
An engineers licence is valid for. 2 years once signed in ink. Iinitially 2 years, then subsequently 5 years once signed in ink 5 years once signed in ink.
The requirement for an EASA aircraft to be maintained in accordance with an Approved Maintenance Programme is set out in. JAR OPS (Subpart M). EASA IR Part 21. The Air Navigation Order. .
The application for approval of a maintenance schedule, presents to the Authority a Maintenance Schedule which is based upon whose The Type Certificate holder. The operator. An approved design organisation.
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. In the maintenance statement. On the CMR.
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.
Aircraft of mass greater than 5700 kg are weighed. At manufacture and at the annual inspection. At manufacture and then at periods not exceeding 5 years At manufacture and then at 2 years and then at periods not exceeding 5 years.
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. The documentation is stored elsewhere and the logbook is cross referred to it. A new log book is raised.
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 Approved Certificate must have.. Three (3) duplicate copies. The date of manufacture of the component to which it refers An Approved signature.
An incident must be reported within. 96 hours. Earliest convenient time. 24 hours.
What approval would you need to maintain airships?. Part-145 with two sections of BCAR A8 18. JAR A. BCAR A8 18.
Details of all placards and markings on an aircraft will be found in. The Maintenance Manual. The Operations Manual. The Flight Manual.
If a repair is made on an aircraft down route, but cannot be certified. The person completing the repair can authorise it to fly to a place where it can be certified. An LAE can authorise it to be flown to a place where it can be certified The pilot (with certain conditions) can authorise it to fly to a place where it can be certified.
A Service Bulletin contains. Information concerning the airworthiness of aircraft and are distributed by the CAA. A list of maintenance tasks to be carried out on a particular aircraft A detailed description of a problem and corrective action to be taken.
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.
The Air Navigation Order applies to. Commonwealth and UK registered aircraft. British manufactured aircraft registered in a contracting state UK registered aircraft operating anywhere in the world.
Schedules of the Air Navigation Order. Are explained in more detail by the Articles. Explain in more detail parts of the General Regulations Explain in more detail parts of the articles.
All aircraft which fly in UK airspace must be registered, with the exception of. Kites, captive balloons and aircraft under B conditions. None. Kites, balloons, gliders and variant aircraft.
An aircraft need not be registered if it is a non-EASA aircraft and being operated by. An operator using the aircraft solely for aerial work. An aircraft dealer, demonstrating the aircraft overseas An aircraft dealer, not taking the aircraft overseas.
A Certificate of Maintenance Review is retained. For six (6) months from date of issue. Until two (2) years after the aircraft has been destroyed or Permanently withdrawn from service. For two (2) years from date of issue.
Authority to amend a maintenance schedule is given by the. Local CAA surveyor. Operator. CAA with written consent. .
A Licensed Engineer will sign a CRS when. The job is complete and properly recorded. He is happy that all physical aspects of the job are finished. He is sure that he has company approval.
A Certificate of Maintenance Review is. Is required for all aircraft over 5300kg MTWA. Required for all transport aircraft maintained under Part-145 Is not required for transport aircraft maintained under Part-145.
Scheduled Maintenance can be extended by. Authority written into the approved maintenance document. Authority written into the approved maintenance manual. Authority written into the approved maintenance schedule.
What is an Exposition?. A document which sets out details of the maintenance schedule. A document which sets out details of how maintenance work is carried out A document which sets out details of an organisation.
If a design amendments is made to a drawing. A new issue number and date is allocated to the drawing. The old issue number is retained with a new amendment date added. No change in issue number is necessary.
An AOC is issued by the CAA for aircraft in the. Transport categories. Transport and Aerial Work 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. Bbar 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. Operations Manual. Approved Maintenance Manual. ATA Chapter 11 of the AMM.
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.
When does a Radio Licence become valid?. When the C of A is issued. Once the Certificate of Registration has been issued OR After the radio station has been approved and the Certificate of Approval issued After the radio station has been approved and the Certificate of Approval issued.
The telecommunications log book is considered to be part of the. Public Address Licence. Radio approved document. Radio Licence.
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. EASAs. ANO.
Certificates of Fitness for Flight are signed by. A CAA surveyor. An Inspector or QA Engineer. An appropriately licensed engineer. .
Under what conditions can you fly when a C of A has expired?. C conditions. B conditions. A conditions. .
Flying times are recorded from. Take off to touch down. Chock to chock. Engine start to shut down. .
Equipment required to be carried on aircraft flying for the purpose of Public Transport is specified in the. Air Navigation (General) Regulations, Schedule 9. Air Navigation Order (Rules of the Air), Schedule 2. Air Navigation Order, Schedule 4. .
Flying under A conditions is carried out by aircraft in the. Series aircraft group. Proto-modified Group. Variant 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. When the repair has not previously been approved by the CAA and FAA. When the repair has not previously been approved by the FAA. .
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. Over 3600Kg MTWA. Under 2300Kg MTWA. Under 2730Kg MTWA. .
Where are scales of equipment to be carried found?. Airworthiness Notices. Air Navigation (General) Regulations. Air Navigation Order, schedule 4. .
If a modification is carried out on an aircraft, it is entered. Both aircraft and modification log books. The modification record book. 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. Tech log. Maintenance schedule. Log book..
Companies with design approval can be found in. Part-145 list of companies. Front of the maintenance schedule. The company exposition.
Certificate of Airworthiness for International flight on transport aircraft. Must not be flown with aircraft. Must be carried. 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 A N(G)R. In ANO. In BCARs.
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. A detailed description of a problem and corrective action to be taken. Information concerning the airworthiness of aircraft and are distributed by the CAA. .
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 if necessary the deferred defects column. Tech Log and if necessary the deferred defects column. .
An MMEL is compiled by. The manufacturer and the CAA after joint consultation. An air operator and approved by he CAA. The manufacturer and the AOC company after joint consultation and then approved by the CAA. .
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. On the AOC. In the approved maintenance schedule. In the Company Exposition. .
An aircraft may fly unregistered. Under B conditions. Under A conditions. For export purposes. .
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. Can sign the 2nd part of the duplicate inspection if the aircraft is away from base. Cannot sign the 2nd part of a duplicate inspection. Can sign the 2nd part of a duplicate inspection if licensed on that particular type.
Aircraft above 5700 kg are weighed. At manufacture then after 2 years then every 5 years after manufacture. Every five years. Two years after manufacture thereafter every five years.
Who issues a C of A for export?. The manufacturer. The CAA - SRG. The Approved Organisation. .
CAP 393 is. Air Operators Certificate. AWNs. The ANO and regulations.
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 FAA. Are published by the CAA.
The minimum number of battery powered megaphones required for an aircraft capable of carrying more than 199 passengers is. 5 7 3.
Life jackets not equipped with a whistle are. Acceptable for children under 3 years old. Acceptable for one passenger of a pair. Not acceptable.
Maintenance Manuals in cassette/CDs have the advantage of being easier to. Store. Amend. Read.
It is the responsibility of the person accepting parts for use on an aircraft to ensure that. Those parts conform to the required standard and are serviceable. A green serviceable label is attached. Those parts are designed to the appropriate Authorised Release Certificate. .
Mandatory markings for flight instruments, or placards are annotated in the. Aircraft Maintenance Schedule. Aircraft Maintenance Manual. Flight manual or Certificate of Airworthiness. .
Consumable items such as split pins, nuts, nuts bolts etc are usually identified by a. Batch number on each item. Batch/part number on the containing bag. Release note on each item.
CAP 360 relates to. EASA aircraft only. Public Transport aircraft. Crop spraying aircraft only. .
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. CAA. EASA. 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. ANO schedule. BCAR section A. AWN 3.
Vital points identified and included in the maintenance documents. Relate to areas in which all work must be carried out by a suitably licensed engineer. Relate to points subject to a duplicate inspection. 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. Maintenance requirements. Mandatory operational restrictions. Modified component or system. .
Technical limitations of work and authority with reference to Aircraft Maintenance Engineers are laid down in. Airworthiness Notice 3. BCAR Section L. 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 USA. The former USSR. Europe.
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 undercarriage. Each engine and VP propeller. 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. B conditions. A conditions. .
Mandatory modification of UK origin are identified by the CAA. AAD. AAN. AD number.
The check cycle for an aircraft is. Stated in the approved maintenance schedule. The same for all aircraft maintained by one operator. 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 inspection item on the AMS. A check on the check cycle. Each check A for aircraft not exceeding 2730Kg MTWA.
A CMR must be completed on aircraft exceeding 2730Kg at. Every 4 months. Every 12 months. Periods not exceeding 4 months.
A duplicate inspection must be the last. Check before issue of a CRS for the task. CRS issue. Signature after a CRS for the task.
A maintenance statement is. Part of the tech log. The approval for a maintenance schedule. 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. BCAR section L. CAP 747. CAAIPs.
Information on Air Operators Certification is to be found in ANO. Article 10. Article 9. Article 6. .
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 conform to required standard. Materials and parts come from an approved source.
B.C.A.R.s. Detail mandatory requirements for aircraft design and construction. Contain minimum requirements to be met. Are issued by Ministry of Trade and Industry.
C.A.A.I.Ps. Contain approved inspection procedures. Contain mandatory instructions. Are issued by CAA.
A Major Modification. Will always require air testing after embodiment. Must be certified in the Modification Record Book. Is approved by an A.A.N.
An Approval Authority Reference number. Is issued by Ministry of Trade and Industry. Must be included on all Approved Certificates. Will be of specific form.
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. Must have a C of A. Does not need 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. Propulsive control system only. Control system and anything that controls propulsive force. .
A Certificate of Release to service states that. The aircraft has been maintained to an approved schedule. An operator has satisfied the CAA of his competence. A task has been carried out in accordance with the ANO.
A CMR is raised after. Major overhaul. Defect rectification. Scheduled servicing at specified intervals. .
Occurrences should be reported to. Department of Trade & Industry. Chief Inspector of Accidents. CAA. .
Compliance with the ANO is restricted to. Aircraft and their equipment which are on the UK & Commonwealth Civil Registers. All civil aircraft and their equipment on the International Civil Register. Aircraft and their equipment which are on the UK Civil Register only.
A quarantine store is a part of an approved store where. Aircraft parts are placed, once they have been proven to conform to specification. Aircraft parts are placed, whilst awaiting delivery to the customer. Aircraft parts are placed, until they have been proven to conform to specification.
Which of the following manuals would be referred to when checking the airworthiness directive on a British constructed engine?. CAP 476 Mandatory Aircraft Modifications and Inspections Summary. CAA Additional Directives CAP 473. FAD Volume 3 CAP 474.
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 Aircraft Log Book. The Modification Record Book. The Engine Log Book.
If an Airworthiness Directive has not been complied with within the flying hour limitations given on the directive, what effect would this have on the engine?. The aircraft can be certified fit for flight under A conditions of the ANO and continue operation for the period of validity of the certificate. The approved engineer can award an extension to the compliance time to enable the engine to remain in operation. The engine and thus the aircraft is grounded until the directive has been complied with.
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.
An alert bulletin printed by the manufacturer of a British constructed engine is. A recommended modification to the aircraft/engine. Classified as mandatory by the manufacturer and must be incorporated before further flight. Classified as mandatory by the CAA and will be followed by incorporation in the publication Mandatory Aircraft Modifications and Inspection Summary.
The information in the ANO is given in the form of. Chapters, each one dealing with a different aspect of Civil Aviation, these chapters being backed up by the Schedules Regulations, each one covering a different aspect of Civil Aviation and as such is mandatory. Articles of Law, some of which are further clarified by Schedules.
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. FAA Airworthiness Directives Volume 1. FAD Volume 3. FAA Airworthiness Directives Volume 2. .
An airworthiness directive has the identification number 91-10-05 on it. This indicates. The year followed by the weekly period followed by the directive number. The chapter followed by the section followed by the subject or directive number in accordance with ATA 100. The year followed by the bi-weekly period followed by the directive number.
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