pssa and saa framwwork 2014

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    Unified Framework forPSSA and SAA withRelevant Safety

    Requirements

    Dr. Ahmed Bassyouni

    Aerospace Consultant315 [email protected]

    Dr. Ahmed BassyouniAerospace Consultant

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    Preliminary System Safety Assessment (PSSA) is used to

    evaluate planned architecture against the SFHA

    requirements and allocate these and new derived safety

    requirements to equipment and ITEMS (software, AEH,

    hardware)

    The difference between the PSSA and the SSA is that the

    PSSA is a method to evaluate proposed architectures and

    derive system safety requirements for each; whereas theSSA is a verification that the implemented design meets

    both the qualitative and quantitative safety requirements

    defined in the AFHA, SFHA and PSSA.

    PSSA Structure and Function

    Dr. Ahmed BassyouniAerospace Consultant

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    Dr. Ahmed BassyouniAerospace Consultant

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    PSSA Structure and Function

    PSSA Structure and contents should follow the Templatesof the Japanese JCAP and the Federal FAA Organizations of

    Aircraft certifications.

    The basic structure of the PSSA shall include the following contents:

    1. Introduction

    2. System description

    3. System Boundary and Operations

    4. Hazard Assessment

    5. Safety Objectives6. Safety Assessment

    7. Derived Safety Requirements

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    PSSA

    Safety Obje for FMEA

    Define Mitg & Val

    Faults impact Safety

    FDAL & IDAL HW,SW

    DSR Derived Safety Req

    Define Severity Levels

    Define Mitig Method

    Define Val method

    Support Certificate

    FHA Func. Haz. Ana

    FTA Fault Tree Ana

    Failure Conditions

    Failure Rates/detect

    Prob. of Root Causes

    Severity Levels

    Safety Master Plan

    CCM Com Cause Ana

    Input & Output of PSSA

    PSSA has to provide the DSR and techniques to Eliminate Hazard

    Dr. Ahmed BassyouniAerospace Consultant

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    1. Identify the hazards and failure conditions for Aircraft

    Systems components2. Assess the Severity and Establish Safety Objectives system

    components

    3. Overview the System Reliability Analysis

    4. Develop FMEA, and FMES

    5. Develop Mitigation Strategies to reduce risk6. Determine Effectiveness of Mitigation Strategies

    [Acceptable Risk]

    7. Develop DSR for LG components

    8. Verify Implementation of Mitigation Strategies

    Safety Validation and verification Tasks

    1.Updating the PSSA/SSA Contents

    2.Updating the PASA/ASA Contents

    Dr. Ahmed BassyouniAerospace Consultant

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    Updating PSSA/SSA

    Dr. Ahmed BassyouniAerospace Consultant

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    PSSA

    DSR

    Safety Plan for Developing PSSA and SSA

    Dr. Ahmed BassyouniAerospace Consultant

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    Verify & Update

    SHFA , FC tables

    Update Equipment

    Tech. Specs. FC

    Tables

    Verify & Update

    FTA diagrams

    CCA(CMA, PRA,ZSA)

    FMEA

    SSA

    OCT

    NOV

    DEC

    MAR

    JAN

    FEB

    ATA-32 Landing Gear System

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    In addition to PSSA/SSA it is recommendedto perform a PASA/ASA

    PASA: Preliminary Aircraft Safety Assessment

    ASA: Aircraft Safety Assessment

    The PASA/ASA assesses the A/C level FC coming from aircraft level

    FHA that combine failures of several systems that are not studied

    or cannot be studied at system level.

    It allows identification of the Development Assurance Levels

    (DAL) for aircraft functions.

    Updating PSSA/SSA, PASA/ASA

    Dr. Ahmed BassyouniAerospace Consultant

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    Updating PSSA/SSA, PASA/ASA

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    System Safety Assessment (SSA)

    The SSAshall include quantitative analysis of critical failureconditions.

    Failure rates from FMEA documents and risk times shall be

    placed into FTAs to calculate the probability of failureconditions.

    The mitigated RPNs shall be considered for Risk Assessment

    Dr. Ahmed BassyouniAerospace Consultant

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