Maintenance Publications

Question 1

8492. Airworthiness Directives are issued primarily to
      A— provide information about malfunction or defect trends.
      B— present recommended maintenance procedures for correcting potentially hazardous defects.
      C— correct an unsafe condition.

Answer 1

C— correct an unsafe condition

The FAA issues ADs to correct unsafe conditions that have been discovered on certificated aircraft, engines, propellers, or appliances.
An unsafe condition causes the device to fail to meet the conditions for its certification. An AD specifies the corrective action that must be taken to return the device to the conditions specified for its certification.

Question 2

8493. (1) A Supplemental Type Certificate (STC) 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 (TSO) system requires no further approval for installation in a particular aircraft. Regarding the above statements,
A— both 1 and 2 are true.
B— neither 1 nor 2 is true.
C— only 1 is true.

Answer 2

C— only 1 is true.

Statement 1 is true. More than one person may apply for a STC that covers the same change to an aircraft.
An STC is not a patent and it is not protected. Each applicant must furnish proof that their alteration meets all of the applicable airworthiness requirements.
Statement 2 is not true. A part produced according to a TSO requires specific approval for installation on a particular aircraft. Even though the part is built according to a TSO, it may be neither suitable nor approved for the particular aircraft.

Question 3

8493-1.
What does the acronym TSO mean regarding a type certificated aircraft part, material, component and/ or process?
A— Training Specific Organization.
B— Type Supplement Original.
C— Technical Standard Order.

Answer 3

C— Technical Standard Order.

A Technical Standard Order (TSO) is an approval for the manufacture of a component for use on certificated aircraft.

Question 4

8494. Primary responsibility for compliance with Airworthiness Directives lies with the
      A— aircraft owner or operator.
      B— certificated mechanic holding an Inspection Authorization who conducts appropriate inspections.
      C— certificated mechanic who maintains the aircraft.

Answer 4

A— aircraft owner or operator.

The aircraft owner or operator is responsible for determining that the aircraft continues to meet the requirements for its certification. This includes the compliance with all ADs.

Question 5

8495. An aircraft Type Certificate Data Sheet contains
      A— maximum fuel grade to be used.
      B— control surface adjustment points.
      C— location of the datum.

Answer 5

C— location of the datum.

Since the location of all items in an aircraft are measured from the datum and this datum can be at any location the aircraft manufacturer chooses, the technician must know exactly where this reference is located.
The location of the datum is included in the information furnished on a Type Certificate Data Sheet.

Question 6

8496. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? A— Propeller Specifications or Propeller Type Certificate Data Sheet.
      B— Aircraft Specifications or Aircraft Type Certificate Data Sheet.
      C— Alphabetical Index of Current Propeller Type Certificate Data Sheets, Specifications, and Listings.

Answer 6

B— Aircraft Specifications or Aircraft Type Certificate Data Sheet.

The Aircraft Specifications or Type Certificate Data Sheets list all of the allowable engine-propeller combinations approved for a specific aircraft.

Question 7

8497. When an aircraft is sold domestically, the Airworthiness Certificate
      A— must be surrendered to the local Flight Standards District Office.
      B— becomes invalid until the new owner makes application for a new Airworthiness Certificate.
      C— is transferred with the aircraft at the time of sale.

Answer 7

C— is transferred with the aircraft at the time of sale.

The Airworthiness Certificate issued to an aircraft is transferred with the aircraft to the new owner when the aircraft is sold.

Question 8

8498. The issuance of an Airworthiness Certificate is governed by
      A— 14 CFR Part 23.
      B— 14 CFR Part 21.
      C— 14 CFR Part 39.

Answer 8

B— 14 CFR Part 21.

14 CFR Part 21 entitled “Certification Procedures for Products and Parts” governs the issuance of an Airworthiness Certificate.

Question 9

8499. 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
      A— Aircraft Listing.
      B— Summary of Discontinued Aircraft Specifications.
      C— FAA Statistical Handbook of Civil Aircraft Specifications.

Answer 9

A— Aircraft Listing.

The certification specifications for aircraft of which there are fewer than 50 currently in service or of which there were fewer than 50 certificated are found in the Aircraft Listing.

Question 10

8500. Where are technical descriptions of certificated propellers found?
      A— Applicable Airworthiness Directives.
      B— Aircraft Specifications.
      C— Propeller Type Certificate Data Sheets.

Answer 10

C— Propeller Type Certificate Data Sheets.

Technical specifications for certificated aircraft propellers are found in the Propeller Type Certificate Data Sheets.

Question 11

8501. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets?
      A— Empty weight of the aircraft.
      B— Useful load of aircraft.
      C— Control surface movements.

Answer 11

C— Control surface movements.

The amount of control surface movement determines the structural loads that can be put on an aircraft and also the f light characteristics of the aircraft.
Because this information is so critical, it is included on the Type Certificate Data Sheets of an aircraft.

Question 12

8502. Placards required on an aircraft are specified in
      A— AC 43.13-1B.
      B— The Federal Aviation Regulations under which the aircraft was type certificated.
      C— Aircraft Specifications or Type Certificate Data Sheets.

Answer 12

C— Aircraft Specifications or Type Certificate Data Sheets.

Placards that furnish information vital to the safety of f light and that must be installed in a certificated aircraft are specified in the Type Certificate Data Sheets for the aircraft.

Question 13

8503. Technical information about older aircraft models, of which no more than 50 remain in service, can be found in the
      A— Aircraft Listing.
      B— Summary of Deleted and Discontinued Aircraft Specifications.
      C— Index of Antique Aircraft.

Answer 13

A— Aircraft Listing.

The certification specifications for aircraft of which there are fewer than 50 currently in service, or of which there were fewer than 50 certificated, are found in the Aircraft Listing.

Question 14

8503-1.
Which of the following are sometimes used as authorization to deviate from an aircraft’s original type design?
A— FAA Form 337, Supplemental Type Certificate, and Technical Standard Order.
B— Supplemental Type Certificate, Airworthiness Directive, and Technical Standard Order.
C— FAA Form 337, Supplemental Type Certificate, and Airworthiness Directive.

Answer 14

C— FAA Form 337, Supplemental Type Certificate, and Airworthiness Directive.

The FAA Form 337 is the form the FAA uses to authorize a major alteration that may deviate from the aircraft’s original type design.
An STC is an authorization for a major change in the type design that is not great enough to require a new application for a type certificate.
An AD identifies an unsafe condition that exists in a product and that is likely to exist or develop in other products of the same type design. ADs may require alterations that deviate from the aircraft’s original type design.
A TSO is a minimum performance standard used to evaluate an article. An article can be a material, part, component, process, or appliance (see 14 CFR §21.1(b) (2)). Each TSO covers a certain type of article. When authorized to manufacture an article to a TSO standard, this is referred to as a TSO authorization. Receiving a TSO authorization is both a design and production approval but is not used as an authorization to deviate from an aircraft’s original type design.

Question 15

8504. (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,
A— only 2 is true.
B— neither 1 nor 2 is true.
C— only 1 is true.

Answer 15

C— only 1 is true.

Statement 1 is true. After an aircraft has been altered in accordance with a Supplemental Type Certificate, it must be inspected for conformity with the information included in the STC before it can be approved for return to service.
Statement 2 is not true. Even though a part has been manufactured according to a Technical Standard Order, it is not necessarily approved for installation on a particular civil aircraft.

Question 16

8505. Which regulation provides information regarding instrument range markings for an airplane certificated in the normal category?
      A— 14 CFR Part 21.
      B— 14 CFR Part 25.
      C— 14 CFR Part 23.

Answer 16

C— 14 CFR Part 23.

Information regarding instrument range markings that must be used on aircraft certificated in the normal category is found in 14 CFR Part 23, “Airworthiness Standards: Normal, Utility, Acrobatic and Commuter Category Airplanes.”

Question 17

8505-1.
Which regulation provides the airworthiness standards for an airplane certificated in the normal category?
A— 14 CFR Part 27.
B— 14 CFR Part 25.
C— 14 CFR Part 23.

Answer 17

C— 14 CFR Part 23.

14 CFR Part 27 provides the airworthiness standards for normal category rotorcraft. Part 25 provides airworthiness standards for transport category airplanes. Part 23 provides airworthiness standards for normal, utility, acrobatic, and commuter category airplanes.

Question 18

8505-2.
What regulations are covered by 14 CFR Part 1?
A— Certification of airmen other than crewmembers.
B— General operating and flight rules.
C— Definitions and abbreviations.

Answer 18

C— Definitions and abbreviations.

14 CFR Part 1 covers definitions and abbreviations. This regulation is helpful for learning the legal terms and their associated meanings as well as the many acronyms used in aviation.

Question 19

8506. (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,

A— only 2 is true.
B— both 1 and 2 are true.
C— neither 1 nor 2 is true.

Answer 19

Statement 1 is false. Propellers are included in the Airworthiness Directive system.
Statement 2 is true. A certificated powerplant mechanic can make a minor repair to an aluminum propeller and can approve it for return to service.

Question 20

8507. 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?
      A— Airworthiness Directives.
      B— AC 43.13-2A.
      C— Supplemental Type Certificates.

Answer 20

B— AC 43.13-2A.

The FAA issues or approves two types of data for aircraft:
1. Regulatory data is approved data that specifies the way something will be done. It is specific and it must be complied with as it applies.
2. Data in Advisory Circulars, such as that in AC 43.132A, is advisory in nature and is “acceptable data.” While it shows a way that things can be done, it is neither specific nor mandatory. It is not considered to be “approved data.”

Question 21

8508. What is the maintenance recording responsibility of the person who complies with an Airworthiness Directive? A— Advise the aircraft owner/operator of the work performed.
      B— Make an entry in the maintenance record of that equipment.
      C— Advise the FAA office of the work performed, by submitting an FAA Form 337.

Answer 21

B— Make an entry in the maintenance record of that equipment.

When a technician complies with an Airworthiness Directive, it is his or her responsibility to make an entry in the maintenance record of the affected equipment. This entry must include the method of compliance and the date of compliance.

Question 22

8509. (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,

A— both 1 and 2 are true.
B— only 1 is true.
C— only 2 is true.

Answer 22

C— only 2 is true.

Statement 1 is not true. Not all manufacturer’s data is FAA approved and Advisory Circulars are not considered to be approved data.
Statement 2 is true. All of the items listed in this statement are considered to be approved data.

Question 23

8509-1.
A Technical Standard Order (TSO) is issued by whom?
A— The Aircraft industry.
B— Part manufacturers.
C— The Administrator.

Answer 23

C— The Administrator.

TSOs are issued by the Administrator under 14 CFR Part 21.

Question 24

8510. 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,

A— both 1 and 2 are true.
B— neither 1 nor 2 is true.
C— only 1 is true.

Answer 24

A— both 1 and 2 are true.

Statement 1 is true. The ATA Specification 100 is a standard for arranging and presenting technical data in maintenance manuals.
Statement 2 is also true. The ATA Specification 100 divides the aircraft into numbered systems and subsystems to simplify locating maintenance instructions.

Question 25

8511. Aviation Maintenance Alerts (formerly General Aviation Airworthiness Alerts)
      A— provide mandatory procedures to prevent or correct serious aircraft problems.
      B— provide information about aircraft problems and suggested corrective actions.
      C— provide temporary emergency procedures until Airworthiness Directives can be issued.

Answer 25

B— provide information about aircraft problems and suggested corrective actions.

Aviation Maintenance Alerts, formerly General Aviation Airworthiness Alerts, provide a common communication channel through which the aviation community can economically interchange service experience and thereby cooperate in the improvement of aeronautical product durability, reliability, and safety. The contents include items that have been reported to be significant but have not been evaluated fully by the time the material went to press.

Question 26

8512. (Refer to Figure 62, 62A, & 62B as necessary.) Which doubler(s) require(s) heat treatment before installation? A— -101.
      B — -102.
      C— Both.

Answer 26

B — -102.

Doubler -102 is made of .040 7075-O Alclad. This material is in its annealed (-O) condition, and it must be heat-treated to its -T6 condition before it is installed.
Doubler -101 is made of 2024-T3 Alclad which is already heat-treated.
According to General Notes-200 in Figure 62A, the - 102 doubler should be heat-treated to -T6 condition in accordance with Process Specification 5602.

Question 27

8512-1.
(Refer to Figures 62, 62A, and 62B as necessary.) How many parts will need to be fabricated by the mechanic in the construction and installation of one doubler?
A— 2.
B— 3.
C— 4.

Answer 27

B— 3.

The mechanic must fabricate three parts to install the doubler. For the -100 installation, one doubler -101 and two clips -103 are needed. For the -200 installation, one doubler -102 and two clips -103 are needed.

Question 28

8513. (Refer to Figure 62, 62A, & 62B as necessary.) Using only the information given (when bend allowance, set back, etc. have been calculated) which doubler is it possible to construct and install?
      A— -101.
      B — -102.
      C— Both.

Answer 28

A— -101.

There is enough information given here to construct and install the -101 doubler. There is not enough information to construct the stronger -102 doubler in the -200 installation. The -102 doubler requires certain Process Specifications that are not furnished.

Question 29

8514. (Refer to Figure 62.) The -100 in the title block (Area 1) is applicable to which doubler part number(s)?
      A— -101.
      B — -102.
      C— Both.

Answer 29

A— -101.

In Figure 62, follow the column for the -100 assembly upward to see the components it requires. The -101 doubler is in this column.

Question 30

8515. (Refer to Figure 63.) 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?
      A— 46.
      B— 200.
      C— 186.

Answer 30

C— 186.

The aircraft has less than 500 hours total time in service, so compliance with the AD falls in category I.
The AD has been complied with and the aircraft has operated for 14 hours since the compliance.
The AD must be complied with each 200 hours of time in service, so the aircraft can operate for another 186 hours before the AD note must be complied with again.

Question 31

8515-1.
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.”
A— Amendment.
B— Compliance.
C— Applicability.

Answer 31

B— Compliance.

“Within the next 25 hours time-in-service after the effective date of this AD,” is a statement of compliance time or date.

Question 32

8515-2.
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.
A— 1, 2, 3, and/or 4.
B— 1, 2, 3, and/or 5.
C— 1, 2, 3, 4, and/or 5.

Answer 32

A— 1, 2, 3, and/or 4.

The action required by an AD is described in the Compliance statement which specifies the action that is required by the AD, and specifies the method of compliance.
An AD does not specify an overall change in maintenance records.

Question 33

8515-3.
Type Certificate Data Sheets are issued for which of the following products?
A— Aircraft, engines, and propellers.
B— Aircraft, engines, and appliances.
C— Aircraft, engines, propellers, and appliances.

Answer 33

A— Aircraft, engines, and propellers.

Type Certificate Data Sheets and Specifications set forth essential factors and other conditions which are necessary for U.S. airworthiness certification of aircraft, engines and propellers.

Question 34

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
A— 260 knots.
B— 293 knots.
C— 139 knots.

Answer 34

C— 139 knots.

The maximum flap extended speed is marked on an aircraft airspeed indicator by the top of the white arc. The white arc would extend to 139 knots.

Question 35

8516-1.
When is a mechanic responsible for checking AD compliance?
A— Never, the owner or operator is solely responsible. B— When performing an inspection required under part 91, 125, or 135.
C— Anytime an aircraft or portion thereof is returned to service.

Answer 35

B— When performing an inspection required under part 91, 125, or 135.

It is the responsibility of the mechanic performing an inspection required under Part 91, 125, or 135 to determine the status of any AD affecting the airframe, engine, propeller, rotor, and any installed appliances.

Question 36

8516-2.
How long are AD compliance records required to be kept?
A— Until the work is repeated or superseded by other work.
B— For one year after the work is performed, or until the work is repeated or superseded by other work.
C— They shall be retained, and then transferred with the aircraft when it is sold.

Answer 36

C— They shall be retained, and then transferred with the aircraft when it is sold.

14 CFR §91.417(b)(2) states that the record of the current status of applicable AD including, for each, the method of compliance, the AD number, and revision date be retained and transferred with the aircraft at the time the aircraft is sold.

Question 37

8516-3.
What does the Type Certificate Data Sheet designation code “2 PCSM” mean? (K01)
A— Two place (number of seats), closed, sea, monoplane.
B— Two wing (biplane), primary category, semimonocoque (airframe).
C— Neither of the other two choices.

Answer 37

A— Two place (number of seats), closed, sea, monoplane.

The FAA uses coded information for the configuration of aircraft and engines in the Type Certificate Data Sheets. The code 2 PCSM identifies the aircraft as a two-place, closed, sea, monoplane.

Question 38

8516-4.
Which of the following includes all the regulatory definitions of “maintenance”?
A— Overhaul, repair, parts replacement, and preservation, and preventive maintenance.
B— Overhaul, repair, parts replacement, preservation, inspection, and preventive maintenance.
C— Overhaul, repair, parts replacement, inspection, and preservation.

Answer 38

C— Overhaul, repair, parts replacement, inspection, and preservation.

14 CFR Part 1 defines maintenance as inspection, overhaul, repair, preservation, and the replacement of parts, but excludes preventive maintenance.

Question 39

8516-5.
What is the maximum penalty for cheating or other unauthorized conduct when taking an FAA mechanic test?
A— Ineligibility to receive any certificate or rating for one year.
B— Ineligibility to receive any certificate or rating for one year, and suspension or revocation of any certificate held.
C— Ineligibility to receive any certificate or rating for one year, and suspension of any certificate held.

Answer 39

B— Ineligibility to receive any certificate or rating for one year, and suspension or revocation of any certificate held.

14 CFR §65.18(b) states that no person who cheats, gives or receives help from another, takes a part of the test for another, uses unauthorized material during the test is eligible for any airman or ground instructor certificate or rating for a period of one year after the date of that act. In addition, the commission of that act is a basis for suspending or revoking any airman or ground instructor certificate held by that person.

Question 40

8517. 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?

A— 100 hours.
B— 50 hours.
C— 125 hours.

Answer 40

A— 100 hours.

Since the valve mechanism is required to be inspected only every second 50-hour period, the engine can operate for 100 hours between valve mechanism inspections.

Question 41

8518. 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?

A— 150 hours.
B— 200 hours.
C— 250 hours.

Answer 41

A— 150 hours.

Since the thrust bearing nuts must be checked for tightness after the first 50 hours in service and then on every third 50-hour inspection, the engine can operate for 150 hours between inspections of tightness of the thrust bearing nuts.