---
title: "Bow-Tie Risk Assessment in Aviation: A Worked Example · Avioverse"
description: "A full bow-tie for a tool left in an engine intake: threats, barriers with owners, consequences, escalation factors, residual risk and SPIs."
url: "https://avioverse.aero/articles/bow-tie-risk-assessment-aviation-example"
---

# Bow-Tie Risk Assessment in Aviation: A Complete Maintenance Example

A full bow-tie for a tool left in an engine intake: threats, barriers with owners, consequences, escalation factors, residual risk and SPIs.

[Dionysis Kefalas](https://avioverse.aero/articles/author/dennis-kefalas) 25 Sep 2026 13 min read

On this page

05:40 at ExampleMRO's line station. The end-of-shift tool check comes up one short: kit 14's inspection torch is not on its shadow. Kit 14 was last used for a fan blade inspection on XX-EXA's number 2 engine, and XX-EXA is due off stand at 06:30. Whether that torch is found was settled months ago, by the barriers around one hazard.

A **bow-tie risk assessment** draws those barriers. It maps one hazard around a single top event: the moment control is lost. Threats that can cause it sit on the left, consequences on the right. Preventive barriers stop threats; recovery barriers stop or limit consequences. Escalation factors weaken barriers and get barriers of their own. To build one, name the hazard, fix the top event, list threats and consequences, place barriers on every line, judge each barrier, score the current risk, then add barriers and forecast the residual risk.

## What goes into a bow-tie

| Element                   | Plain meaning                                                                        | In the ExampleMRO bow-tie                                         |
| ------------------------- | ------------------------------------------------------------------------------------ | ----------------------------------------------------------------- |
| Hazard                    | Part of normal work that can cause harm                                              | Hand tools used inside an engine intake                           |
| Top event                 | The moment control is lost, before any damage                                        | A tool stays in the intake after the task is closed               |
| Threat                    | Can cause the top event on its own                                                   | A technician is called away and leaves a spanner on the inlet lip |
| Preventive barrier        | Stops a threat reaching the top event                                                | Tool count against the shadow board before sign-off               |
| Consequence               | Where the top event can lead                                                         | Engine failure on the take-off roll                               |
| Recovery barrier          | After the top event, stops a consequence or limits it (then often called mitigating) | Shift-end tool reconciliation that holds the release              |
| Escalation factor         | Makes a barrier fail more often                                                      | Time pressure late in a night shift                               |
| Escalation-factor barrier | Protects a barrier from that condition                                               | No release while the reconciliation is open                       |

Read it left to right, as time. Left of the knot is prevention. Right of it assumes prevention has already failed.

## Does EASA require a bow-tie?

No. The rules require the work, not the method. Part-145 point [145.A.200](https://avioverse.aero/regulations/easa/continuing-airworthiness/part-145/section-a-technical-and-organisation-requirements/145-a-200) asks for a management system that includes, at (a)(3):

> the identification of aviation safety hazards entailed by the activities of the organisation, their evaluation and the management of the associated risks, including taking actions to mitigate the risks and verify their effectiveness

That text names no bow-tie and no risk matrix. Two EASA user guides, one for foreign Part-145 expositions and one for CAMEs, mention the bow-tie as one option among several: "Regardless of the method used (ICAO safety risk matrix, ARMS, BOW-TIE, etc.), it is important to customize the risk assessment matrix so as to reflect the operational profile." A user guide is not rule text. The [hazard identification and safety risk management guide](https://avioverse.aero/guides/easa-hazard-identification-safety-risk-management) sets out the rules and AMC themselves.

For a bow-tie, the end of that text matters most: the mitigating actions are barriers, and verifying their effectiveness is the barrier judgement and the SPIs below.

## The worked example: a tool left in an engine intake

ExampleMRO maintains narrow-body jets for ExampleAir and other operators. Fan blade inspections and probe changes put spanners, torches and mirrors inside an intake most weeks. ExampleMRO is fictional, and so are its counts, verdicts, severities and likelihoods below: copy the structure, then score with your own data and definitions.

![Bow-tie diagram for a tool left in an engine intake: threats T1 to T4 on the left pass through preventive barriers P1 to P7 to the top event in the centre; consequences C1 to C3 on the right are guarded by recovery barriers R1 to R4](https://avioverse.aero/article-images/bow-tie-tool-left-in-engine-intake.svg)

The whole bow-tie on one page. The steps below build it line by line.

### Step 1: fix the hazard and the top event

- **Hazard:** hand tools and equipment used inside an engine intake.
- **Top event:** a tool or item of equipment stays in the intake after the task is closed.

While someone is still working in the intake, the tool is under control. Once the task card is signed, only a later check stands between the tool and a running engine. "Engine damage" would be too late for a top event; it is a consequence. "Tools in the intake" is too early; that is the hazard during normal work.

### Step 2: threats and preventive barriers

Each threat must be able to cause the top event on its own. Barriers sit on the threat lines they interrupt, and one barrier can sit on several.

| Threat                                                                                    | Preventive barriers on this line                                                                               |
| ----------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------- |
| T1. Task interrupted; a tool is put down inside the intake and forgotten                  | P1 shadow-board kit · P2 tool count before sign-off · P6 independent close-up inspection · P7 intake entry log |
| T2. Task handed over at shift change with tools or equipment still in the intake          | P3 handover sheet · P6 independent close-up inspection · P7 intake entry log                                   |
| T3. A tool from outside the kit: personal, borrowed, a loaned special tool, a spare torch | P4 loaned and personal tools issued through the tool store · P7 intake entry log                               |
| T4. A tool dropped into a part of the inlet the technician cannot see                     | P5 tethered tools · P2 tool count before sign-off · P6 independent close-up inspection                         |

### Step 3: consequences and recovery barriers

Severity is the worst credible outcome on each line, using ExampleMRO's own severity definitions. ExampleMRO grades severity by the safety outcome for people and the flight, not by repair cost, so an engine damaged on the ground with nobody hurt is Minor even when the repair bill is large. If your definitions count major equipment damage as Hazardous, as the ICAO wording does, C1 scores higher; the top score still rests on C2.

| Consequence                                                                                              | Worst credible severity | Recovery barriers on this line                                                                                  |
| -------------------------------------------------------------------------------------------------------- | ----------------------- | --------------------------------------------------------------------------------------------------------------- |
| C1. Tool ingested at engine start or ground run; engine damaged, aircraft still on the ground            | Minor (D)               | R1 shift-end tool reconciliation holds the release · R2 intake inspection before any engine start or ground run |
| C2. Tool ingested on the take-off roll; engine failure, then a high-speed rejected or continued take-off | Hazardous (B)           | R1 · R3 walk-around torch check of each intake before the first flight · R4 crew engine-failure procedures      |
| C3. Tool works loose in climb or cruise and is ingested; in-flight shutdown and diversion                | Major (C)               | R1 · R3 · R4                                                                                                    |

R3 and R4 belong to ExampleAir. They are interface barriers: ExampleMRO can ask for evidence that they work but does not run them. R4 is also mitigating; it limits what follows an engine failure.

### Step 4: escalation factors and their barriers

An escalation factor does not cause the top event. It makes a barrier fail.

| Escalation factor                                         | Barriers it weakens | Escalation-factor barrier                                                                                              | Owner                    |
| --------------------------------------------------------- | ------------------- | ---------------------------------------------------------------------------------------------------------------------- | ------------------------ |
| E1. Time pressure in the last half hour of a night stop   | P2, P6, R1          | No release to service while the tool reconciliation is open; the shift lead has written authority to hold the aircraft | Line maintenance manager |
| E2. Contract technicians new to ExampleMRO's tool control | P1, P4              | No kit issued until tool-control induction is recorded; personal toolboxes booked in at the tool store                 | Tool store supervisor    |

## How to judge whether a barrier is any good

Ask four questions of every barrier:

- **Does it work on its own?** A barrier detects, decides and acts. If it cannot stop the sequence alone, it is not a barrier.
- **Is it independent?** Of the threat, and of the other barriers on its line. P2 and P6 fail together if one tired technician does both at 05:30, which is why P6 needs a second person.
- **Is it effective?** How often it works when called on, shown by spot checks, lost-tool reports and audit samples, not opinion.
- **Who owns it?** A named role that keeps it working and hears when it degrades. "All staff" is not an owner.

ExampleMRO's barrier register today:

| Barrier                                                | Owner                       | Verdict today             | Evidence or gap                                                                                                           |
| ------------------------------------------------------ | --------------------------- | ------------------------- | ------------------------------------------------------------------------------------------------------------------------- |
| P1 Shadow-board kits signed out to a named technician  | Tool store supervisor       | Effective                 | A gap shows at a glance                                                                                                   |
| P2 Tool count before sign-off                          | Shift lead                  | Weak                      | Same person, same moment as the work; count not recorded                                                                  |
| P3 Handover sheet                                      | Shift leads                 | Weak                      | No line for tools left in the intake                                                                                      |
| P4 Loaned and personal tools via the tool store        | Tool store supervisor       | Partly in place           | Loaned special tools bypass it                                                                                            |
| P5 Tethered tools for intake work                      | Engineering                 | Not in place              | None                                                                                                                      |
| P6 Independent close-up inspection with a torch        | Base maintenance manager    | Effective when done       | Recorded on the task card; squeezed by E1                                                                                 |
| P7 Intake entry log: tools in, tools out               | Shift lead                  | Not in place              | None                                                                                                                      |
| R1 Shift-end reconciliation and lost-tool procedure    | Tool store supervisor       | Effective for kit tools   | Caught all three lost kit tools in 12 months (one, the kit 14 torch, in XX-EXA's intake); blind to tools outside the kits |
| R2 Intake inspection before engine start or ground run | Ground-run authorised staff | Effective                 | A step in the run-up procedure                                                                                            |
| R3 Walk-around torch check of each intake              | ExampleAir                  | Unknown                   | Evidence requested                                                                                                        |
| R4 Crew engine-failure procedures                      | ExampleAir                  | Not ExampleMRO's to judge | Limits severity only                                                                                                      |

The R1 row is the one to read twice. The reconciliation only sees tools on a shadow board. A torch a technician brought from home was never on one, so the 05:40 check has nothing to miss. T3 runs straight past R1.

## Current risk and residual risk

Current risk credits only barriers that exist and work today. ExampleMRO scores the bow-tie on its worst credible consequence, C2 at Hazardous (B). The top event has happened once in twelve months: the kit 14 torch, caught by R1. The T3 path bypasses R1 entirely, which leaves R3, a barrier ExampleMRO cannot see into, as the last line before take-off. ExampleMRO calls that Remote (3). **Current risk: 3B.**

The planned barriers close P4 for loaned tools, add P5 and P7 to every intake task, add a tools line to P3, and put the two escalation-factor barriers in place. If they are implemented and work, likelihood drops to Improbable (2). Severity stays at B: preventive barriers change how often a tool stays behind, not what a spanner does to a fan at take-off power. **Residual risk forecast: 2B.**

On the ICAO Doc 9859 default matrix, 3B and 2B both sit in the tolerable band. The cell moved; the colour did not. That shows what a matrix cannot do: decide whether 2B is acceptable to ExampleMRO. [AMC1 145.A.200(a)(3)](https://avioverse.aero/regulations/easa/continuing-airworthiness/part-145/section-a-technical-and-organisation-requirements/145-a-200#amc1-145-a-200-a-3) puts that decision with specified levels of management:

> (2) The levels of management who have the authority to make decisions regarding the tolerability of safety risks, in accordance with (b)(1)(ii), should be specified.

The residual score stays a forecast until the new barriers exist and prove themselves. Scoring detail, including worst credible versus worst imaginable outcomes, is in the [risk matrix article](https://avioverse.aero/articles/aviation-risk-matrix-likelihood-severity).

## Turning weak barriers into leading SPIs

The bow-tie shows which barriers carry the load; an SPI shows whether they still do. Measure the barrier, not the accident. Tool-caused engine failures are too rare to steer by. Skipped reconciliations are not.

| Barrier watched              | Leading SPI (monthly)                                                                             | What a bad month means                   |
| ---------------------------- | ------------------------------------------------------------------------------------------------- | ---------------------------------------- |
| R1 Shift-end reconciliation  | Shifts with the reconciliation complete before the first release, as a % of shifts with a release | The last ground barrier is being skipped |
| P2 Tool count                | Kits found incomplete at unannounced spot checks, per 100 kits checked                            | Counts are being signed without counting |
| P4 Loaned and personal tools | Tools found in use without a tool-store record                                                    | The T3 path around R1 is open again      |
| P6 Independent close-up      | Intake close-up inspections signed by the technician who did the work, as a % of intake tasks     | Independence is eroding under E1         |

Lost-tool reports per 1,000 task cards show how often the recovery side is called on. Set targets and alert levels once you have a baseline; the [SPI worked example](https://avioverse.aero/articles/spi-targets-alert-levels-worked-example) shows how. The same four barriers belong on the next internal audit checklist, and the [audit programme guide](https://avioverse.aero/guides/compliance-monitoring-audit-programme-part-145-camo) shows where they fit.

## Common mistakes

- **Barriers that are wishes.** "Be careful in the intake", "tool awareness", "follow procedures". Ask what it detects, who owns it and how an auditor would see it fail. No answer means a wish. The barrier is the count, log or tether that makes care happen.
- **Threats that are consequences.** "FOD ingestion" drawn on the left of "tool left in intake" is an outcome, not a cause. Test: does it happen before the knot?
- **Escalation factors drawn as threats.** Time pressure leaves no tool in an intake by itself. It makes P2, P6 and R1 fail, so draw it under them.
- **Planned barriers in the current risk.** Tethers not yet bought do not lower today's score.
- **A hazard too broad.** "Maintenance error" yields forty threats and no usable barrier. Keep one top event per bow-tie; an unsecured fan cowl on the same engine is a second bow-tie.

For starting points on other hazards, the public [SMS hazard library](https://avioverse.aero/risks) groups sample hazards by SMS domain.

## Doing this in Avioverse

In **Risks**, **New assessment** offers **Create manually** or **Draft with Metis**. One assessment can hold several bow-ties (**Add bow-tie**). Each is drawn as lines: every threat's line runs through the preventive barriers that stop it into the **Top event**, and from the top event a line runs through the recovery barriers that limit each consequence. A threat that no barrier stops shows as a dashed line, so the gap is plain to see. Selecting a barrier lights up its lines and opens its details beside the diagram.

Each barrier says whether it is **In place** or **Planned**. You set **Current risk** and the **Residual risk forecast** yourself by picking a matrix cell. Current risk credits only in-place barriers; planned ones count only towards the forecast, and the page says so: "Residual risk is a forecast, conditional on planned controls being implemented." A planned barrier can become a task with **Create task**. When the task is done, the page asks whether the barrier is in place (**In place** or **Not yet — reopen task**); completing the task alone does not lower the risk. In place means implemented. Whether the barrier works is recorded separately, in the **Barriers** tab, with **Confirm effectiveness**.

The band and its colour come from the **Workspace risk matrix**, a fixed 5×5 whose default bands follow ICAO Doc 9859. Workspace owners and admins can re-band cells and choose band colours; nobody can resize the matrix or rename its axes. A later matrix edit changes the band on saved assessments too, finalised ones included.

Saving (**Create assessment**, then **Save changes**) and **Finalise** are separate steps. Finalising records who finalised the assessment and when, and the confirmation dialog calls a finalised assessment "signed off". It is not a second person's approval, and it is not your organisation's acceptance of the risk. **Reopen & edit** returns it to draft. The PDF export includes the change history. Avioverse is not your SMS record; the PDF is what you file in it.

An assessment can also start from an audit finding, through **Create new** in the finding's risk decision. The finding cannot close until that assessment is finalised.

Metis can draft a bow-tie from your description and save it as a draft when you ask. It cannot finalise it.

The grid has no column for escalation factors and no owner field on a barrier, so keep both in your barrier register. SPIs are set up in their own module and do not link to the assessment.

## Frequently asked questions

### What is a bow-tie risk assessment in aviation?

It maps one hazard around a single top event, the moment control is lost. Threats and the preventive barriers that stop them sit on the left. Consequences and the recovery barriers that stop or limit them sit on the right. Escalation factors show what weakens a barrier.

### Does EASA require a bow-tie analysis?

No. Part-145 point 145.A.200 asks for hazard identification, evaluation and risk management, but it names no method. Two EASA user guides mention the bow-tie as one option among several; a user guide is not rule text.

### What is the difference between a threat and an escalation factor?

A threat can cause the top event on its own, such as a tool put down in an intake during an interrupted task. An escalation factor causes nothing by itself. It makes a barrier fail more often, such as time pressure at the end of a night shift.

### What is the difference between current risk and residual risk?

Current risk credits only the barriers that exist and work today. Residual risk is a forecast that assumes the planned barriers are implemented and effective, so it stays a forecast until they are.

### How do bow-tie barriers become SPIs?

Pick the barriers that carry the most load or look weakest, and measure each month whether they work. One example is the share of shifts where the tool reconciliation was complete before the first release.

### Does finalising a bow-tie in Avioverse mean the risk is accepted?

No. Finalising records who finalised the assessment and when. It is not a second person's approval, and it is not the organisation's acceptance of the risk. That decision stays with the people your safety management system names.

## Related

- [Hazard Identification and Safety Risk Management under EASA Guide · 17 min](https://avioverse.aero/guides/easa-hazard-identification-safety-risk-management)
- [Aviation Risk Matrix: Likelihood, Severity and EASA Article · 12 min](https://avioverse.aero/articles/aviation-risk-matrix-likelihood-severity)
- [SPI Alert Levels and Targets: A Worked Example Article · 12 min](https://avioverse.aero/articles/spi-targets-alert-levels-worked-example)
- [Occurrence Analysis and Follow-up in the SMS Guide · 5 min](https://avioverse.aero/guides/occurrence-analysis-follow-up-sms)
- [EASA Safety Management AI Prepares the Work Article · 10 min](https://avioverse.aero/articles/ai-for-easa-safety-management)

Written by Dionysis Kefalas. Retired Hellenic Air Force Captain and founder of Avioverse. [About the author](https://avioverse.aero/articles/author/dennis-kefalas)

[Request early access →](https://avioverse.aero/register?redirect=https%3A%2F%2Fapp.avioverse.aero%2Frisks)

Build the bow-tie by hand or have Metis prepare a first draft, score it on your workspace matrix, and finalise it yourself when you are satisfied. Opens in October 2026.

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