Flt. Lt. Alexandre Jay Parr · Prevention of Future Deaths report

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Issued 2 Jan 2019•Wiltshire and Swindon

Published report and response evidence

This report’s concerns and statements found in recipients’ published responses. Statements are included even where no link to an individual concern is recorded. A link shows an evidence connection; it does not assign responsibility.

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Concerns
3

Raised in this report

Recipients
1

Named on the report

Responses found
1

Of 1 recipient

Stated actions
7

Described in responses

Recipients and published responses

Full report text

This is the full text from the original published report.

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Concerns and recipient responses

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Report evidence summary

Concerns raised3

  1. Failure to communicate the emergency fuel-primer-pump cycle rate to YAK pilots
  2. Failure to apply a 20-year engine-overhaul limit to all piston engines
  3. Failure of the emergency fuel-primer-pump instructions to specify the required cycle rate
    Part of recurring concern: Failure to ensure clear and followed instructions for safe equipment use

Stated actions An action is something a recipient says it has done, is doing, or plans to do in response to a concern raised.7

  1. Civil Aviation Authority

    Discuss YAK fuel-primer-pump use during power loss at the next CAA-led YAK and Nanchang Continuing Airworthiness Forum and consider whether additional UK guidance would be useful and effective.

  2. Civil Aviation Authority

    Replace the YAK-52 engine life directive with requirements reinforcing the 2,250-hour limit and informing owners of a maximum calendar life.

  3. Civil Aviation Authority

    Review YAK-52 engine-failure accident data and specialist overhaul data to assess whether engine age or maintenance contributed to failures.

  4. Civil Aviation Authority

    Publish a revised Safety Notice on safety-harness replacement and assessment guidance in the second quarter of 2019.

  5. Civil Aviation Authority

    Enhance Safety Notice 2018/005 with harness calendar-life guidance and aircraft-specific assessment checks that may prompt withdrawal before expiry.

  6. Civil Aviation Authority

    Require calendar-based engine overhaul periods for low-utilisation National Permit to Fly aircraft alongside or instead of flying-hour maintenance tasks.

  7. Civil Aviation Authority

    Consult general aviation industry on whether to mandate replacement lives for safety harnesses.

Respondent positions A position is what a recipient says about a concern when it does not describe a specific action.4

  1. Civil Aviation Authority

    A single mandatory safety-harness replacement life is not appropriate because varied aircraft configurations and use could make safety worse.

    No action considered necessaryThe respondent said that no further action was needed.
  2. Civil Aviation Authority

    Requesting the manufacturer to specify a fuel-primer-pump rate is not appropriate because technical and human factors may make use counterproductive.

    No action considered necessaryThe respondent said that no further action was needed.
  3. Civil Aviation Authority

    The applicability of Leaflet 70-80 does not need extending following the review of YAK-52 engine-failure data and overhaul findings.

    No action considered necessaryThe respondent said that no further action was needed.
  4. Civil Aviation Authority

    UK YAK-52 engine-failure reports did not identify engine age or inadequate maintenance as contributory factors; conventional wear drives replacement.

    Disputes the concernThe respondent disagreed with part of the concern or the basis for it.

Source evidence

How this individual concern was interpreted

PFD Monitor created a concise, searchable interpretation from the report wording shown below. Response links show a clear evidence connection; they do not assign responsibility.

PFD Monitor interpretation

Failure to communicate the emergency fuel-primer-pump cycle rate to YAK pilots

Wider context from the report

“c) THE USE OF THE FUEL PRIMER PUMP IN AN EMERGENCY. Whilst the primer pump may not have originally been specifically designed for use in an emergency I understand from the AAIB investigators that the manufacturer's state in their manual that the pump can be used in an emergency, for example should the fuel pump fail. Regrettably, I also understand that the manufacturer's manual gives no indication as regards the cycle rate for the use of the primer pump in these emergency circumstances. When G-YAKB experienced a loss of engine power and Alex sitting in the front cockpit used the primer pump he was pumping at a rate of 1 cycle every 3 to 4 seconds. This was found to be insufficient to provide sufficient fuel to the engine in order to regain power. When the AAIB investigators attempted to ascertain a sufficient cycle rate they found that a significantly higher rate was required in order to provide sufficient fuel to the engine. That rate was 1.3 cycles per second. I am unclear, aside from the findings of the AAIB report, as to how this potentially important piece of information can be communicated to the YAK user population in the United Kingdom. It seems to me that this information is important and may be unknown to many YAK pilots and I am concerned that if the intention is that YAK 52 pilots are required to read this AAIB Report concerning this incident, then this particular piece of information may be missed if a pilot does not research this particular incident. I would respectfully ask you to consider how best to communicate this information to the wider YAK pilot community in the United Kingdom. ”

Is this part of a recurring concern?

No recurring-concern membership is currently published.

Open source report

Source evidence

How this individual concern was interpreted

PFD Monitor created a concise, searchable interpretation from the report wording shown below. Response links show a clear evidence connection; they do not assign responsibility.

PFD Monitor interpretation

Failure to apply a 20-year engine-overhaul limit to all piston engines

Wider context from the report

“a) OVERHAUL OF ENGINE. This particular aircraft G-YAKB a YAK 52 was manufactured in 1992 and had an initial manufacturer's life span of 20 years. The life span was extended in 2013 for a period of 10 years following an overhaul carried out in accordance with CAA Regulations. The manufacturer's specification was that an overhaul of the engine was required at 750 hours. At the time of the crash even though the aircraft was approximately 24 years old the original piston engine had only logged 516 hours. I understand having heard Mr. Hawkins that currently there is a CAA leaflet number 70/80 that requires a 20-year calendar limit in relation to an engine overhaul irrespective as to whether or not the manufacturer's specified number of hours usage has been reached however leaflet 70/80 only applies to engine with more than 400 horsepower. I understand from the AAIB investigators that your organisation is conducting a review as to whether or not this should be extended to all piston engines. Whilst accepting the evidence of the AAIB that there was not an issue with this particular engine this observation made by the AAIB investigators may lend sense to me from a safety perspective and I would be grateful if you could please advise me as regards the state of this review and ultimately notify me as to whether leaflet 70/80 is to be extended or how the issue is to be resolved through other means. If there is to be no change then please indicate why and how you reached that decision. ”

Is this part of a recurring concern?

No recurring-concern membership is currently published.

Open source report

Source evidence

How this individual concern was interpreted

PFD Monitor created a concise, searchable interpretation from the report wording shown below. Response links show a clear evidence connection; they do not assign responsibility.

PFD Monitor interpretation

Failure of the emergency fuel-primer-pump instructions to specify the required cycle rate

Wider context from the report

“c) THE USE OF THE FUEL PRIMER PUMP IN AN EMERGENCY. Whilst the primer pump may not have originally been specifically designed for use in an emergency I understand from the AAIB investigators that the manufacturer's state in their manual that the pump can be used in an emergency, for example should the fuel pump fail. Regrettably, I also understand that the manufacturer's manual gives no indication as regards the cycle rate for the use of the primer pump in these emergency circumstances. When G-YAKB experienced a loss of engine power and Alex sitting in the front cockpit used the primer pump he was pumping at a rate of 1 cycle every 3 to 4 seconds. This was found to be insufficient to provide sufficient fuel to the engine in order to regain power. When the AAIB investigators attempted to ascertain a sufficient cycle rate they found that a significantly higher rate was required in order to provide sufficient fuel to the engine. That rate was 1.3 cycles per second. I am unclear, aside from the findings of the AAIB report, as to how this potentially important piece of information can be communicated to the YAK user population in the United Kingdom. It seems to me that this information is important and may be unknown to many YAK pilots and I am concerned that if the intention is that YAK 52 pilots are required to read this AAIB Report concerning this incident, then this particular piece of information may be missed if a pilot does not research this particular incident. I would respectfully ask you to consider how best to communicate this information to the wider YAK pilot community in the United Kingdom. ”

Is this part of a recurring concern?

Yes — Failure to ensure clear and followed instructions for safe equipment use.

Open source report

Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Discuss YAK fuel-primer-pump use during power loss at the next CAA-led YAK and Nanchang Continuing Airworthiness Forum and consider whether additional UK guidance would be useful and effective.

Verbatim wording from the response

“manufacturer to specify a rate. The use of the YAK Fuel Primer Pump in the event of a loss of power, will be included for discussion at the next CAA led YAK & Nanchang ‘Continuing Airworthiness Forum’ due to be held by the end of the second quarter of 2019 and attended by key owners and maintainers of the affected types. The Group will consider whether additional guidance to UK users would be useful and effective.”

Source location

2019-0001-Response-by-CAA
Page 3 · response
Published 23 May 2019

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Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Replace the YAK-52 engine life directive with requirements reinforcing the 2,250-hour limit and informing owners of a maximum calendar life.

Verbatim wording from the response

“Additionally, Mandatory Permit Directive, MPD 1998-001R2, which limits the life of the YAK-52 engine to 2250 flying hours has been superseded by a new MPD 2019-002 which reinforces the replacement lifespan of this engine and now also ensures owner/operators are aware of the need for a maximum calendar life, even if engine utilisation (flying hours) is low.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

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Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Review YAK-52 engine-failure accident data and specialist overhaul data to assess whether engine age or maintenance contributed to failures.

Verbatim wording from the response

“The CAA has reviewed the UK accident safety data related to engine failure on YAK-52 aircraft and confirmed that none of the reports (five in total between January 2003–January 2019) cited engine age or lack of maintenance as a contributory factor. Additionally, the CAA has reviewed recent overhaul data from a specialist Approved Organisation in Hungary which is responsible for the maintenance overhaul of 40-50 of this engine type per year. This review concluded that conventional (flight hour-related) component wear is the main reason for replacement at overhaul, rather than age.”

Source location

2019-0001-Response-by-CAA
Page 1 · response
Published 23 May 2019

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Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Publish a revised Safety Notice on safety-harness replacement and assessment guidance in the second quarter of 2019.

Verbatim wording from the response

“The CAA is working with industry stakeholders on enhancing the existing Safety Notice 2018/005 to emphasise the need to take into account any manufacturer’s specified ‘calendar’ lives for safety harnesses as well as to provide more guidance on individual aircraft-specific harness assessments/checks that could lead to withdrawal from use before such calendar periods expire. The CAA intends to publish a revised Safety Notice in the second quarter of 2019.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

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Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Enhance Safety Notice 2018/005 with harness calendar-life guidance and aircraft-specific assessment checks that may prompt withdrawal before expiry.

Verbatim wording from the response

“The CAA is working with industry stakeholders on enhancing the existing Safety Notice 2018/005 to emphasise the need to take into account any manufacturer’s specified ‘calendar’ lives for safety harnesses as well as to provide more guidance on individual aircraft-specific harness assessments/checks that could lead to withdrawal from use before such calendar periods expire. The CAA intends to publish a revised Safety Notice in the second quarter of 2019.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

Open published response

Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Require calendar-based engine overhaul periods for low-utilisation National Permit to Fly aircraft alongside or instead of flying-hour maintenance tasks.

Verbatim wording from the response

“The CAA’s requirements for all National Permit to fly Aircraft[1] now includes an expectation that appropriate calendar periods for engine overhaul should complement or replace flying hour-related maintenance tasks in the aircraft maintenance programme for individual aircraft in the case of low utilisation. Any such calendar period(s) for engine overhaul are expected to be determined by consideration of manufacturers recommendations, usage, environmental conditions (e.g. hangarage) and type of operation (safety risk).”

Source location

2019-0001-Response-by-CAA
Page 1 · response
Published 23 May 2019

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Source evidence

How this respondent action was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Consult general aviation industry on whether to mandate replacement lives for safety harnesses.

Verbatim wording from the response

“As part of the follow-up action to AAIB Recommendation 2017-021 (11-2017) the CAA consulted with GA industry on the potential for mandating a replacement life (or lives) for safety harnesses on all GA aircraft. Following the outcome of this consultation, the CAA concluded that mandating a single life for the wide variety of GA aircraft configurations and types of utilisation may, in fact be counter-productive, in some cases safety harnesses requiring replacement and non-serviceable harnesses continuing to be utilised. Instead of mandating a replacement life (or lives) for safety harnesses, the CAA will improve the current guidance material to enable a more informed decision to be made by both maintenance organisations and aircraft owners, on an ongoing use basis as to when the replacement of individual harness installations is appropriate.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

Open published response

Source evidence

How this respondent position was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

A single mandatory safety-harness replacement life is not appropriate because varied aircraft configurations and use could make safety worse.

Verbatim wording from the response

“As part of the follow-up action to AAIB Recommendation 2017-021 (11-2017) the CAA consulted with GA industry on the potential for mandating a replacement life (or lives) for safety harnesses on all GA aircraft. Following the outcome of this consultation, the CAA concluded that mandating a single life for the wide variety of GA aircraft configurations and types of utilisation may, in fact be counter-productive, in some cases safety harnesses requiring replacement and non-serviceable harnesses continuing to be utilised. Instead of mandating a replacement life (or lives) for safety harnesses, the CAA will improve the current guidance material to enable a more informed decision to be made by both maintenance organisations and aircraft owners, on an ongoing use basis as to when the replacement of individual harness installations is appropriate.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

Open published response

Source evidence

How this respondent position was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

Requesting the manufacturer to specify a fuel-primer-pump rate is not appropriate because technical and human factors may make use counterproductive.

Verbatim wording from the response

“The CAA has established there are a number of different technical and human factors that would have an impact on the effectiveness of utilisation of the Fuel Primer Pump, particularly in emergency situations where it’s use may, in certain circumstances be counter-productive. For this reason, the CAA has concluded it would not be appropriate for CAA to request the”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

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Source evidence

How this respondent position was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

The applicability of Leaflet 70-80 does not need extending following the review of YAK-52 engine-failure data and overhaul findings.

Verbatim wording from the response

“As a consequence of the review conducted by the CAA and the findings set out above, the applicability of Leaflet 70-80 does not need to be extended.”

Source location

2019-0001-Response-by-CAA
Page 2 · response
Published 23 May 2019

Open published response

Source evidence

How this respondent position was interpreted

PFD Monitor created a concise, searchable interpretation from the published response wording shown below.

PFD Monitor interpretation

UK YAK-52 engine-failure reports did not identify engine age or inadequate maintenance as contributory factors; conventional wear drives replacement.

Verbatim wording from the response

“The CAA has reviewed the UK accident safety data related to engine failure on YAK-52 aircraft and confirmed that none of the reports (five in total between January 2003–January 2019) cited engine age or lack of maintenance as a contributory factor. Additionally, the CAA has reviewed recent overhaul data from a specialist Approved Organisation in Hungary which is responsible for the maintenance overhaul of 40-50 of this engine type per year. This review concluded that conventional (flight hour-related) component wear is the main reason for replacement at overhaul, rather than age.”

Source location

2019-0001-Response-by-CAA
Page 1 · response
Published 23 May 2019

Open published response
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Information checked against the published report and official responses · Data reviewed 7 Sep 2026 · About data quality and limitations

Official responses located
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Data last updated 7 September 2026