US Department 

of Transportation 

Federal Aviation 

Administration 

Advisory 

Circular 

Subject: Propeller Critical Parts Date: 1 I 1 7 I 13 

------------------ Initiated By: ANE-111 

ACNo: 35.16-1 

Change: 

1. Purpose. This advisory circular (AC) provides guidance and acceptable methods, but not the 

only methods, that may be used to demonstrate compliance with the propeller critical parts 

requirements ofTitle 14 ofthe Code ofFederal Regulations (14 CFR) § 35.16. This AC 

provides information about what a propeller critical part is, the identification of propeller critical 

pmis by applicants, and engineering processes, manufacturing processes, and maintenance 

processes for those parts. 

2. Applicability. 

a. The guidance provided in this document is directed to propeller applicants, manufacturers, 

modifiers, foreign regulatory authorities, and Federal Aviation Administration (FAA) designated 

engineering representatives. 

b. This material is neither mandatory nor regulatory in nature and does not constitute a 

regulation. It describes acceptable means, but not the only means, for demonstrating compliance 

with the applicable regulations. We ("the FAA'') will consider other methods an applicant may 

present to demonstrate compliance. Terms such as "should," "shall," "may," and "must" are 

used only in the sense of ensuring applicability of this particular method of compliance when the 

method in this document is used. While these guidelines are not mandatory, they are derived 

from extensive FAA and industry experience in determining compliance with the relevant 

regulations. If we find that following this AC would not result in compliance with the applicable 

regulations, we will not be bound by this AC, and we may require additional substantiation as the 

basis for finding compliance. 

c. This material does not change, create any additional, authorize changes in, or permit 

deviations from existing regulatory requirements. 
1117/13 AC35.16-1 

3. Related regulations. Please check the FAA's website at http://ecfr.gpoaccess.gov for part 

35 ofTitle 14 ofthe Code of Federal Regulations (14 CFR). 

a. 14 CFR 3 5.15, Safety analysis. 

4. Definitions. For the purpose of this AC, the following definitions apply: 

a. Approved Life. The mandatory replacement life of a part that is approved by the FAA and 

is listed in the airworthiness limitation section (ALS) of the instructions for continued 

airworthiness (ICA). 

b. Engineering Process. The process that defines the integrity of propeller critical parts 

throughout their service life. 

c. Manufacturing Process. The process that identifies the requirements to produce propeller 

critical parts consistent with the engineering process. 

d. Primary Failure. Failure of a part that is not the result of prior failure of another part or 

system. 

e. Propeller Critical Part. A part on the propeller whose primary failure can result in a 

hazardous propeller effect, as determined by the safety analysis required by § 3 5.15. 

f. Service Management Process. The process that identifies the continued airworthiness 

requirements of propeller critical parts as required by the engineering process. 

5. Introduction. 

a. The failure of a propeller critical part could result in a hazardous propeller effect as defined 

by§ 35.15. Accordingly, applicants must meet the requirements of§ 35.16 for propeller critical 

part management. Section 35.16 requires that applicants establish the integrity of propeller 

critical parts through defined engineering, manufacturing, and service management processes. 

These three processes form a closed-loop system linking design intent, as defined by the 

engineering process, to part manufacture and service management. Engineering, manufacturing, 

and service management work together as an integrated system that recognizes actions in one 

area may affect all. 

b. The engineering process defines the requirements, technical data, and actions necessary to 

establish and maintain the integrity of propeller critical parts throughout their service life. The 

engineering process and the part life are established before the part is introduced into service. 

The engineering process is updated as new information becomes available. 

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1117113 AC35.16-1 

c. The manufacturing process is a compilation of the controls and procedures, such as the 

drawings, procedures, specifications, and instructions required to produce and inspect a propeller 

critical part, as defined by the engineering process. 

d. The service management process identifies the procedures for in-service maintenance, 

overhaul, and repair to ensure that a propeller critical part achieves the requirements defined by 

the engineering process. The service management process forms the basis for in-service 

maintenance, overhaul, and repair that are conveyed through the ICA, and the ALS of the ICA 

constant with the engineering process. 

6. General. 

a. The engineering, manufacturing, and service management processes should provide clear 

information for propeller critical part management. "Process" in the context of the proposed 

requirement does not mean that all the required technical information is within a single 

document. When relevant information exists elsewhere, the process documents may reference 

for example, drawings, material specifications, process specifications, as appropriate. These 

references should be clear enough to sufficiently identify the referenced document so as to allow 

the design history of an individual part to be traced. 

b. When a critical part is inseparable from an assembly, the assembly is identified as a critical 

part. Both the inseparable part(s) and the assembly should be included in the engineering, 

manufacturing, and service management processes. This does not limit applicants from defining 

separable assemblies containing propeller critical parts as a propeller critical part in support of 

the engineering process. 

7. Defining an engineering process. 

a. Introduction. The engineering process includes procedures and requirements for how 

propeller critical parts are identified, associated life analysis is determined, and mandatory 

inspection intervals. Each of these is discussed in more detail below. 

b. Identifying Propeller Critical Parts. Section 35.15 Safety analysis requires the 

identification of all propeller critical parts. The engineering process should have the drawing(s) 

distinguish propeller critical parts. 

c. Life Analysis. The engineering process should establish the methodology for determining 

what propeller critical parts are life limited, if any. For those that require a life limit, the 

approved life is published in the ICA Airwmihiness Limitations Section (ALS). 

( 1) Establishing the Propeller Critical Part Life. The applicants engineering process should 

provide a systematic and uniform methodology to predict part life. The applicants life prediction 

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1117113 AC 35.16-1 

methodology should consider: airplane operating conditions, engine compatibility, stress 

analysis, materials data, safe life analysis and/or damage tolerance analysis, wear analysis and 

service experience. Any in-service inspections identified as required to maintain the part life 

should be incorporated into the ICA ofthe ALS. 

(2) Maintaining the Propeller Critical Part Life. The engineering process should include a 

provision for incorporating design, manufacturing and service data, relative to the condition of 

propeller critical parts, into the part life methodology. This is to assure that design changes and 

changes introduced during manufacture or service will be evaluated, and if necessary, corrective 

action taken to restore or maintain part life. 

d. Mandatory Inspection Interval. The engineering process should include a methodology for 

determining any mandatory inspection intervals, and for incorporating them into the ALS of the 

I CA. 

8. Defining a manufacturing process. 

a. Introduction. The manufacturing process identifies the requirements to consistently 

produce propeller critical parts as required by the engineering process. The requirements 

established by the manufacturing process should include engineering requirements, and apply 

controls to ensure that manufacturing and inspection methods and processes are maintained. The 

manufacturing process can be broadly grouped as process and source approvals, and part 

marking. Each is discussed below: 

b. Manufacturing Process Approval. 

(1) The essential manufacturing processes should be reviewed and approved by the 

appropriate engineering, quality and manufacturing personnel established by the applicant. 

Changes to the manufacturing processes should be subject to the same or similar review and 

approval process. The review and approval of changes should include an assessment of the 

impact on the life of the critical part. The applicant may integrate the manufacturing process 

with the quality system to assure conformance for all propeller critical parts. 

(2) The applicant should identity the appropriate inspection personnel who will ensure the 

manufactured product is consistent with the requirements of the engineering process. This group 

of personnel should also evaluate and approve non-conformance dispositions, and all propeller 

critical part manufacturing sources. 

(3) The level of detail in the inspection process may vary depending on the process step 

being considered, the sensitivity of the step, and the level of control necessary to achieve the 

propeller critical part requirements. 

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1/17/13 AC 35.16-1 

c. Source Approval. The applicant should impose source approval requirements on suppliers 

of parts, materials or processes that are incorporated into critical parts. Approval means the 

source has successfully demonstrated to the applicant that they have the capability to produce 

parts or materials that satisfy the requirements of the critical part established in the engineering 

and manufacturing processes. 

d. Part Marking. Propeller critical parts marking should be consistent with 14 CFR part 45. 

Propeller critical parts not addressed in part 45 do not require part number and serial number 

markings. The procedures for marking propeller critical parts should be defined in the 

manufacturing or engineering process, as applicable. 

9. Defining a service management process. 

a. Introduction. The service management process is part of the process to maintain propeller 

critical parts throughout their service life. The service management process identifies and 

conveys the requirements for in-service repair, maintenance, and overhaul to remain consistent 

with the requirements contained in the engineering process. 

(1) The I CAs and ALS of the ICA, operation and maintenance manuals, bulletins and other 

service documents are part of the service management process. The service management process 

has been developed with the expectation that general procedures such as pre-flight or other 

periodic inspections and overhauls will be accomplished in accordance with the published 

service documents and do not need to be in the ALS of the ICA. 

(2) Critical parts should be identified in the service documents. 

b. Elements of a Service Management Process. The service management process should 

include the following: 

(1) Service requirements and procedures to maintain continued airworthiness. 

(2) Propeller installation, maintenance and overhaul procedures. 

(3) Airworthiness limitations. 

( 4) Repair procedures. 

(5) Maintenance intervals 

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1/17/13 AC 35.16-1 

c. Determining the Acceptability of Repair, Maintenance and Overhaul Processes. 

( 1) Repair, maintenance, and overhaul should be reviewed and approved by the appropriate 

engineering, quality and manufacturing personnel established by the applicant. The review 

should include an assessment of the impact on the life of the critical part. Changes to repair, 

maintenance, and overhaul should be subject to the same or similar review and approval process. 

d. ICA Statement. 

(1) To ensure a closed-loop between the in-service parts and the engineering process, the 

applicant should highlight the importance of limits to the repair and maintenance of propeller 

critical parts in the propeller maintenance manuals. Applicants may use the following wording in 

the propeller maintenance manual, or something similar, to highlight the criticality of repairs on 

propeller critical parts, or parts that affect propeller critical parts: 

"The following maintenance and repair instructions have been substantiated based 

on engineering analysis that expects this product will be operated and maintained 

using the procedures and inspections provided in the ICA supplied with this 

product." 

I J ....... 

L/Robeti ~~ Ganley, 

.tJV 1 Acting Manager, Engine and Propeller Directorate 

Aircraft Certification Service 

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