Safety assessment
ARP4761A safety-assessment support for airborne systems
ARP4761A safety-assessment support helps an avionics or equipment supplier show that the safety analysis behind a system actually closes the safety objectives it set. It is used by systems and safety teams whose FHA, PSSA, and SSA were built across a program and may not connect to the failure-condition classifications, the DAL assignment, or the architecture that emerged. The work reviews the functional hazard assessment, the preliminary and final safety assessments, the fault tree and failure modes analyses, and the link to development assurance levels and the safety requirements driven down to software and hardware. You receive a safety-assessment gap assessment, a traceability view from hazard to objective to evidence, and a prioritized list of the safety analysis to close.
When this review is needed
- A system is approaching review and the safety assessment chain has to be checked end to end, from hazard to objective to evidence.
- The FHA classified the failure conditions early and the architecture has since changed, so the PSSA and SSA may no longer reflect the design.
- Quantitative objectives in the fault trees rely on failure rates and exposure times that need to be confirmed against the latest data.
- Common cause analysis was deferred and whether the independence claimed in the fault trees actually holds needs to be established.
- A supplier wants an independent read of the safety assessment before it drives the DAL assignment in a wider submittal.
The problem
ARP4761A is the analysis that everything else hangs from, and its weakest link is usually continuity. The FHA classifies failure conditions, the PSSA derives the safety requirements and the architecture to meet them, and the SSA is supposed to show the built system actually does, but the three are often written at different times by different hands. Fault trees inherit independence assumptions that the common cause analysis never confirmed, and the derived safety requirements that the analysis produced do not always reach the software and hardware that must implement them.
What gets reviewed
- The functional hazard assessment and the failure-condition classifications it sets
- The preliminary safety assessment and the safety requirements and architecture it derives
- The system safety assessment and how it demonstrates the objectives are met
- Fault tree analyses and the quantitative objectives and exposure times behind them
- Failure modes and effects analyses and how they feed the fault trees
- Common cause analysis, including zonal, particular risks, and common mode
- Derived safety requirements and their flow-down to software and hardware items
What gets validated
- Each failure condition in the FHA carries a classification and a safety objective tied to it
- The PSSA architecture and safety requirements meet the objectives the FHA set
- The SSA demonstrates the built system meets each objective, not only the planned one
- Fault tree independence assumptions are confirmed by the common cause analysis
- Quantitative objectives use failure rates and exposure times traceable to a defensible source
- Latent failures and their exposure intervals are identified and bounded
- Derived safety requirements reach the software and hardware items that must implement them
Evidence normally required
- The functional hazard assessment and its failure-condition classifications
- The preliminary and final safety assessments and the safety requirements they produced
- The fault tree, FMEA, and common cause analyses assembled so far
- The architecture description the safety assessment was performed against
- The failure rate, exposure, and reliability data behind the quantitative claims
- The traceability from derived safety requirements to software and hardware items
Common discrepancies
- Fault tree independence assumed but never confirmed by the common cause analysis
- An SSA that demonstrates the planned architecture rather than the system as built
- Failure rates or exposure times in the fault trees with no traceable source
- Latent failures with no defined exposure interval or detection means
- Derived safety requirements that never reached the items meant to implement them
- Failure-condition classifications in the FHA inconsistent with the DALs they drive
- An FMEA that does not feed the failure modes the fault trees rely on
What is at stake
When the safety assessment does not close its objectives, the development assurance levels it drives are exposed, and the assurance claimed for the software and hardware can collapse with them. A latent failure that the common cause analysis missed, or an objective the SSA never demonstrates, can force redesign at the architecture level late in the program, where the cost lands on every item the safety assessment touches and on the certification schedule.
Move from findings to resolution
Identify gaps against the means of compliance.
How the work runs
Walk the chain
Confirm the FHA classifications flow into the PSSA objectives and architecture and that the SSA demonstrates them.
Test the independence
Reconcile the fault tree independence assumptions against the common cause analysis and flag what is unconfirmed.
Trace the requirements
Confirm the derived safety requirements reach the software and hardware items meant to implement them.
Package the gaps
Produce a safety-assessment gap assessment and a prioritized closure list ready for the system review.
What the buyer receives
Who uses the output
- Certification leads preparing the safety-assessment submittal or review
- Safety engineering teams closing the analysis and common cause gaps
- Systems engineering teams reconciling the architecture with the analysis
How the work fits into the transaction or program
The support strengthens the safety assessment that drives the development assurance levels, so the DALs the rest of the program depends on rest on analysis that closes its objectives. It pairs directly with ARP4754B development-assurance support, since the safety requirements flow from here into the system and item development.
Start with a single asset
Confirm requirements trace through verification.
Aircraft-specific considerations
The safety assessment is performed against a function in a specific system and aircraft, so the same equipment can carry different failure-condition classifications depending on what its loss or malfunction means in that installation. A function that is catastrophic in one aircraft may be hazardous or major in another, which changes the safety objectives, the architecture needed to meet them, and the DALs the analysis drives, so the assessment cannot be lifted unchanged from one installation to the next.
Regulatory limits
Endeavor Elements supports the applicant's safety-assessment data. It does not act as the authority or a delegate, make compliance findings, issue any approval, make airworthiness determinations, or guarantee acceptance. The applicant and the authority keep their roles, and the classifications and objectives remain the applicant's, supported by the analysis.
What this review does not cover
- Making official compliance findings, airworthiness determinations, or acting as the authority
- Issuing any approval, authorization, or design approval
- Performing the system design or generating the underlying reliability data itself
Specific to this review
- ARP4761A structures the work as a chain, FHA to PSSA to SSA, so a break at any link leaves the safety objectives unproven even when each document looks complete on its own.
- Fault tree analyses depend on independence between branches, and the common cause analysis, zonal, particular risks, and common mode, is what either confirms or invalidates that independence.
- Latent failures matter because a hidden failure plus a later one can defeat redundancy, so the analysis has to define exposure intervals and detection means rather than assume the redundancy holds.
- Quantitative safety objectives are expressed as probabilities per flight hour tied to the failure-condition classification, so a misclassification in the FHA changes the entire quantitative target downstream.
Sources
U.S. Government (eCFR). Type certificates, STCs (Subpart E), TSO authorizations (Subpart O), PMA (Subpart K), and export airworthiness approvals (Subpart L).
SAE International. Safety assessment methods (FHA, PSSA, SSA, FTA, FMEA) supporting development assurance level assignment.
SAE International. Development assurance process at aircraft and system level, including requirements capture and validation.
Federal Aviation Administration. FAA type certification process, certification basis establishment, and compliance findings.
Frequently asked questions
Do you set the failure-condition classifications for us?
No. The classifications and the safety objectives are the applicant's. The review checks that the FHA, PSSA, and SSA are internally consistent, that the analysis closes the objectives, and that the common cause work supports the independence the fault trees assume.
Relevant glossary terms
Related pages
Where this fits
Talk to an engineer who has done this work
We will walk through your current state, the records or evidence involved, and a scoped first engagement.
Walk through your situation with an engineer who has done this work.