Studied by 6 people(1) Manufacturer's data and FAA publications such as Airworthiness Directives, Type Certificate Data Sheets, and advisory circulars are all approved data. (2) FAA publications such as Technical Standard Orders, Airworthiness Directives, Type Certificate Data Sheets, and Aircraft Specifications and Supplemental Type Certificates are all approved data. Regarding the above statements,
only No. 2 is true.
Type Certificate Data Sheets are issued for which of the following products?
Aircraft, engines, and propellers.
Where are technical descriptions of certificated propellers found?
Propeller Type Certificate Data Sheets.
Technical information about older aircraft models, of which no more than 50 remain in service, can be found in the
Aircraft Listing.
An aircraft Type Certificate Data Sheet contains
location of the datum.
What is the maintenance recording responsibility of the person who complies with an Airworthiness Directive?
Make an entry in the maintenance record of that equipment.
(1) Propellers are NOT included in the Airworthiness Directive system. (2) A certificated powerplant mechanic may make a minor repair on an aluminum propeller and approve for return to service. Regarding the above statements,
only No. 2 is true.
A complete detailed inspection and adjustment of the valve mechanism will be made at the first 25 hours after the engine has been placed in service. Subsequent inspections of the valve mechanism will be made each second 50-hour period. From the above statement, at what intervals will valve mechanism inspections be performed?
100 hours.
An aircraft has a total time in service of 468 hours. The Airworthiness Directive given was initially complied with at 454 hours in service. How many additional hours in service may be accumulated before the Airworthiness Directive must again be complied with? The following is the compliance portion of an Airworthiness Directive. 'Compliance required as indicated, unless already accomplished. I. Aircraft with less that 500-hours' total time in service: Inspect in accordance with instructions below at 500-hours' total time, or within the next 50-hours' time in service after the effective date of this AD, and repeat after each subsequent 200 hours in service. II. Aircraft with 500-hours' through 1,000-hours' total time in service: Inspect in accordance with instructions below within the next 50-hours' time in service after the effective date of this AD, and repeat after each subsequent 200 hours in service. III. Aircraft with more than 1,000-hours' time in service: Inspect in accordance with instructions below within the next 25-hours' time in service after the effective date of this AD, and repeat after each subsequent 200 hours in service.'
186
What does the Type Certificate Data Sheet designation code '2 PCSM' mean?
Two place (number of seats), closed, sea, monoplane.
(Refer to Figure 62, 62A, & 62B as necessary.) How many parts will need to be fabricated by the mechanic in the construction and installation of one doubler?
3.
Airworthiness Directives are issued primarily to
correct an unsafe condition.
Which regulation provides the airworthiness standards for an airplane certificated in the normal category?
14 CFR Part 23.
Which of the following includes all the regulatory definitions of 'maintenance'?
Overhaul, repair, parts replacement, inspection, and preservation.
How long are AD compliance records required to be kept?
They shall be retained, and then transferred with the aircraft when it is sold.
Check thrust bearing nuts for tightness on new or newly overhauled engines at the first 50-hour inspection following installation. Subsequent inspections on thrust bearing nuts will be made at each third 50-hour inspection. From the above statement, at what intervals should you check the thrust bearing nut for tightness?
150 hours
Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source?
Aircraft Specifications or Aircraft Type Certificate Data Sheet.
Under the Federal Aviation Regulations, an aviation maintenance technician is required to perform maintenance on an aircraft so that it
is at least equal to its original or properly altered condition.
When is a mechanic responsible for checking AD compliance?
When performing an inspection required under part 91, 125, or 135.
What does the acronym TSO mean regarding a type certificated aircraft part, material, component and/or process?
Technical Standard Order.
(1) The Federal Aviation Regulations require approval after compliance with the data of a Supplemental Type Certificate. (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. Regarding the above statements,
only No. 1 is true.
What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets?
Control surface movements.
Placards required on an aircraft are specified in
Aircraft Specifications or Type Certificate Data Sheets.
When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate
is transferred with the aircraft.
The Air Transport Association of America (ATA) Specification No. 100 (1) establishes a standard for the presentation of technical data in maintenance manuals. (2) divides the aircraft into numbered systems and subsystems in order to simplify locating maintenance instructions. Regarding the above statements,
both No. 1 and No. 2 are true.
Specifications pertaining to an aircraft model manufactured under a type certificate, of which less than 50 are shown on the FAA Aircraft Registry, can be found in the
Aircraft Listing.
The issuance of an Airworthiness Certificate is governed by
14 CFR Part 21.
The following words are an example of what kind of statement in an AD? 'Required within the next 25 hours time-in-service after the effective date of this AD, unless already accomplished.
Compliance
The following is a table of airspeed limits as given in an FAA-issued aircraft specification: Normal operating speed 260 knots Never-exceed speed 293 knots Maximum landing gear operation speed 174 knots Maximum flap extended speed 139 knots The high end of the white arc on the airspeed instrument would be at
139 knots.
What regulations are covered by 14 CFR Part 1?
Definitions and abbreviations.
Primary responsibility for compliance with Airworthiness Directives lies with the
aircraft owner or operator.
Which regulation provides information regarding instrument range markings for an airplane certificated in the normal category?
14 CFR Part 23.
What is the maximum penalty for cheating or other unauthorized conduct when taking an FAA mechanic test?
Ineligibility to receive any certificate or rating for one year, and suspension or revocation of any certificate held.
The action required by an AD may take what form? 1. Inspection. 2. Part(s) replacement. 3. Design modification. 4. Change in operating procedure(s). 5. Overall change in the content, form and disposition of aircraft maintenance records.
1, 2, 3, and/or 4.
(1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement. (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. Regarding the above statements,
only No. 1 is true.
An aircraft mechanic is privileged to perform major alterations on U.S. certificated aircraft; however, the work must be done in accordance with FAA-approved technical data before the aircraft can be returned to service. Which is NOT approved data?
AC 43.13-2A.
A Technical Standard Order (TSO) is issued by whom?
The Administrator.
Which of the following are sometimes used as authorization to deviate from an aircraft's original type design? 1. FAA Form 337. 2. Supplemental Type Certificate. 3. Airworthiness Directive. 4. Technical Standard Order
1, 2, and 3.
(8535) The replacement of a damaged engine mount with a new identical engine mount purchased from the aircraft manufacturer is considered a
minor repair.
(8521) The replacement of fabric on fabric-covered parts such as wings, fuselages, stabilizers, or control surfaces is considered to be a
major repair even though no other alteration or repair is performed.
(8516) The following is a table of airspeed limits as given in an FAA-issued aircraft specification: Normal operating speed 260 knots Never-exceed speed 293 knots Maximum landing gear operation speed 174 knots Maximum flap extended speed 139 knots The high end of the white arc on the airspeed instrument would be at
139 knots.
(8447) Which is an appliance major repair?
Overhaul of a hydraulic pressure pump.
(8449) Which maintenance action is an airframe major repair?
The repair of portions of skin sheets by making additional seams.
(8527) The replacement of a damaged vertical stabilizer with a new identical stabilizer purchased from the aircraft manufacturer is considered a
minor repair.
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