FR 2021-03814

Overview

Title

Airworthiness Directives; Pratt & Whitney Canada Corp. Turboshaft Engines

Agencies

ELI5 AI

The FAA wants to use a different way to count how many times some parts inside certain airplane engines work, because the current system might not count correctly, and this could be unsafe. They want to make sure the counting is right to prevent any problems.

Summary AI

The Federal Aviation Administration (FAA) has proposed a new airworthiness directive aimed at certain models of turboshaft engines produced by Pratt & Whitney Canada Corp. This directive is a response to a potential issue where the Automated Damage Tracking System may underestimate the number of cycles completed by critical engine components, which might lead to their premature failure. To address this, the FAA is proposing to replace the automated system with a manual cycle-counting method to ensure accuracy. The FAA is inviting comments on this proposal until April 12, 2021, as part of efforts to enhance aviation safety and prevent any unsafe conditions related to these engines.

Abstract

The FAA proposes to adopt a new airworthiness directive (AD) for all Pratt & Whitney Canada Corp. (P&WC) PW210A and PW210S model turboshaft engines. This proposed AD was prompted by a report from the manufacturer that the Automated Damage Tracking System (ADTS) may under-count the number of cycles accrued by the impeller and the high- pressure compressor (HPC) rotor. The impeller and HPC rotor are both life-limited components and exceeding their published life limits could result in the failure of these components. This proposed AD would require the use of the manual low-cycle fatigue (LCF) counting method in place of the ADTS counting method to determine the number of cycles accrued by the impeller and HPC rotor. The FAA is proposing this AD to address the unsafe condition on these products.

Citation: 86 FR 11651
Document #: 2021-03814
Date:
Volume: 86
Pages: 11651-11653

AnalysisAI

The document in question is a proposed rulemaking by the Federal Aviation Administration (FAA), which seeks to implement a new airworthiness directive (AD) for Pratt & Whitney Canada Corp. turboshaft engines, specifically models PW210A and PW210S. The need for this directive arises from a reported issue where the Automated Damage Tracking System (ADTS) might not accurately count the cycles of certain components, possibly leading to their premature malfunction. The FAA proposes replacing this with a manual system to ensure the safety and reliability of these engine components.

Summary of the Document

The FAA is focused on enhancing safety by ensuring crucial components of aircraft engines do not exceed their life limits without detection. The components in question, the impeller and the high-pressure compressor (HPC) rotor, are integral for engine function and thus, their failure could have severe consequences. The proposed shift to a manual low-cycle fatigue (LCF) counting method is primarily a corrective and preventive measure against potential undercounting flaws in the existing automated system.

Significant Issues

There are several notable issues within the document that may warrant further discussion or clarification:

  • Cost of Compliance: The proposal does not clearly outline the financial implications for operators who must adhere to the manual counting method. This lack of detail could be a concern for stakeholders who need to evaluate operational costs.

  • Technical Jargon: The document uses industry-specific terms and legal references which might be difficult for the general public to comprehend, such as "low-cycle fatigue (LCF) counting method" and "Joint Aircraft System Component (JASC) Code 7230".

  • Confidential Business Information (CBI): While the document deals with issues around sensitive business information and freedom of information, the explanations presuppose a level of familiarity with these topics that a layperson might not have.

  • Preferred Methodology: There isn't a detailed explanation as to why the manual method is definitively preferred over the current automated system, raising questions about the decision-making process behind this change.

  • Lack of Alternatives: The proposal doesn't seem to consider or discuss potential alternatives or support mechanisms, which might be less burdensome for operators who use the ADTS.

Impact on the Public

Broadly speaking, the directive reinforces the FAA's commitment to aviation safety, which ensures greater peace of mind for the flying public. However, uncertainties regarding cost and implementation might affect operators' resources and subsequently, potentially increase costs for consumers.

Impact on Stakeholders

Operators and manufacturers are likely the most affected by this directive. While the emphasis on safety is understandable and commendable, the transition to a different system could require additional training and resources, about which the document remains silent. This shift might impose additional operational burdens. Moreover, reassuring these stakeholders through clearly articulated costs, resources for transition, and possibly exploring alternatives could help in securing their cooperation and maintain operational efficiency.

In conclusion, while the FAA's intention to safeguard engine performance is crucial, further clarity and consideration of implementation impacts could greatly enhance the effectiveness and acceptance of this directive among key stakeholders.

Issues

  • • The document does not specify the estimated cost for operators to comply with the proposed AD, which could be a concern for stakeholders evaluating the financial impact.

  • • Language related to 'Confidential Business Information' (CBI) may be confusing for some readers as it presumes understanding of FOIA without explaining it fully.

  • • The document includes legal references and technical jargon (e.g., 'low-cycle fatigue (LCF) counting method', 'Joint Aircraft System Component (JASC) Code 7230') that may not be easily understood by all readers.

  • • The proposal lacks a detailed explanation of why the manual LCF counting method is preferred or necessary over the existing Automated Damage Tracking System (ADTS).

  • • There is no mention of potential alternatives to the proposed manual LCF counting method that might be less burdensome for operators.

  • • It is unclear if there are any support or training resources available to help operators transition from ADTS to the manual LCF counting method.

Statistics

Size

Pages: 3
Words: 2,989
Sentences: 94
Entities: 315

Language

Nouns: 1,055
Verbs: 230
Adjectives: 107
Adverbs: 25
Numbers: 173

Complexity

Average Token Length:
4.54
Average Sentence Length:
31.80
Token Entropy:
5.55
Readability (ARI):
19.30

Reading Time

about 11 minutes