Unit of Competency Mapping – Information for Teachers/Assessors – Information for Learners

AVIY5023A Mapping and Delivery Guide
Operate multi-engine fixed wing aeroplane

Version 1.0
Issue Date: April 2024


Qualification -
Unit of Competency AVIY5023A - Operate multi-engine fixed wing aeroplane
Description This unit involves the skills and knowledge required to carry out take-off and departure procedures as pilot-in-command of a multi-engine aeroplane during visual, instrument and night conditions in normal, abnormal and emergency situations. Licensing, legislative, regulatory or certification requirements are applicable to this unit.
Employability Skills This unit contains employability skills.
Learning Outcomes and Application Work must be carried out in compliance with the relevant licence and aircraft rating requirements of the Civil Aviation Safety Authority (CASA); and/or ADF, airspace control requirements and VFR, Instrument Flight Rules (IFR); and aircraft control principles, regulations, safety codes, protocols and procedures required when operating a multi-engine fixed wing aeroplane.Use for ADF Aviation is to be in accordance with relevant Defence Orders and Instructions and applicable CASA compliance.Operations are conducted as part of commercial and military aircraft activities across a variety of operational contexts within the Australian aviation industry.Work is performed under limited supervision.This unit is nominally packaged at Certificate V.
Duration and Setting X weeks, nominally xx hours, delivered in a classroom/online/blended learning setting.
Prerequisites/co-requisites Not applicable.
Competency Field Y - Aircraft Operation and Traffic Management
Development and validation strategy and guide for assessors and learners Student Learning Resources Handouts
Activities 		Slides
PPT 		Assessment 1 Assessment 2 Assessment 3 Assessment 4
Elements of Competency Performance Criteria              
Element: Operate a multi-engine aeroplane in all phases of flight
  • Normal operations of multi-engine aeroplane type on the ground and in flight are conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
  • Asymmetric operations for all phases of flight are anticipated and contingencies are planned
  • A plan of action is self-briefed or briefed to crew members that will ensure the safest outcome in the event of asymmetric operations
       
Element: Manage engine failure /malfunction in flight
  • (In simulated conditions) Maintain and/or re-gain control of aeroplane
  • Failed/malfunctioning engine is identified and confirmed
  • Power set on serviceable engine/s and aeroplane configuration is adjusted to achieve desired aeroplane performance
  • Failed/malfunctioning engine is managed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
  • Indicated airspeed is maintained above VMCA
  • ATC or another agency capable of assistance are advised of situation and intentions
  • Recovery to aerodrome is evaluated and conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
       
Element: Manage engine failure/malfunction after take-off
  • (In simulated conditions) Engine failure/malfunction is managed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures after take-off while heading is maintained
  • Initial climb not less than best engine out angle of climb speed (VX) or best engine out rate of climb speed (VY) until clear of obstacles, then VY is maintained
  • Recovery to aerodrome is evaluated and conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
       
Element: Perform rejected take-off
  • Take-off is aborted prior to V1 or at a point during the take-off where the abort procedure can be initiated and the aeroplane stopped on the remaining runway/stopway
  • Power is reduced smoothly and promptly
  • Spoilers, prop fine/reverse, thrust reverse, wheel brakes and other drag and braking devices are activated
  • Positive control is maintained to bring the aeroplane to a safe stop
  • Engine failure procedures and/or checklists are initiated and completed
       
Element: Manage engine failure /malfunction during approach/landing
  • (In simulated conditions) Control of aeroplane is maintained
  • Engine inoperative approach is performed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
  • Decision is made to continue or abort approach/landing
  • Decision height for landing is nominated
  • ATS or other agencies capable of providing assistance are advised of situation and intentions
  • Flight profile is flown from which a controlled landing could be achieved
       
Element: Conduct go-around or missed approach with engine failure
  • (In simulated conditions) Engine failure in a multi-engine aeroplane during a go-around or missed approach is identified and confirmed
  • Control of aeroplane is maintained
  • Engine inoperative go-around is performed from decision height in accordance with aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures
       


Evidence Required

List the assessment methods to be used and the context and resources required for assessment. Copy and paste the relevant sections from the evidence guide below and then re-write these in plain English.

The Evidence Guide provides advice on assessment and must be read in conjunction with the performance criteria, required knowledge and skills, the range statement and the assessment guidelines for this Training Package.

Critical aspects for assessment and evidence required to demonstrate competency in this unit

The evidence required to demonstrate competency in this unit must be relevant to and satisfy all of the requirements of the elements and performance criteria of this unit and include demonstration of applying:

the underpinning knowledge and skills

relevant legislation and workplace procedures

other relevant aspects of the range statement

Context of and specific resources for assessment

Performance is demonstrated consistently over a period of time and in a suitable range of contexts

Resources for assessment include:

a range of relevant exercises, case studies and/or other simulated practical and knowledge assessment, and/or

access to an appropriate range of relevant operational situations in the workplace

In both real and simulated environments, access is required to:

relevant and appropriate materials and equipment, and

applicable documentation including workplace procedures, regulations, codes of practice and operation manuals

Method of assessment

Assessment of this unit must be undertaken by a registered training organisation

As a minimum, assessment of knowledge must be conducted through appropriate written/oral tests

Practical assessment must occur:

through activities in an appropriately simulated environment at the registered training organisation, and/or

in an appropriate range of situations in the workplace

Submission Requirements

List each assessment task's title, type (eg project, observation/demonstration, essay, assignment, checklist) and due date here

Assessment task 1: [title]      Due date:

(add new lines for each of the assessment tasks)

Assessment Tasks

Copy and paste from the following data to produce each assessment task. Write these in plain English and spell out how, when and where the task is to be carried out, under what conditions, and what resources are needed. Include guidelines about how well the candidate has to perform a task for it to be judged satisfactory.

REQUIRED KNOWLEDGE AND SKILLS

This describes the essential knowledge and skills and their level required for this unit.

Required knowledge:

Airspeed limitations including: VNO, VA, VX and VY, VNE, VFE, VLO, VLE, VLO2 (landing gear operations down), maximum crosswind, turbulence penetration speed and maximum load factor

Emergency airspeeds including: VMCA, VSSE, engine(s) inoperative climb, approach and final speed, emergency descent and best glide range speeds

Emergency procedures for: engine failure after take-off, engine fire on the ground and airborne, engine failure in the cruise, waste gate failure (if applicable) and propeller/turbine over-speed

Safety implications of asymmetric flight below VMCA

Power, flight and configuration requirements that apply to VMCA

Methods of regaining control of an aeroplane with a failed engine that is flying at a speed less than VMCA

Conditions that would increase V1

Performance the aeroplane can achieve after reaching VY or V2 during asymmetric flight

Markings on the airspeed indicator that apply to failed engine operations

Relevant sections of Civil Aviation Safety Regulations and Civil Aviation Orders

In ADF context, relevant Defence Orders and Instructions

Relevant OH&S procedures and regulations

Normal and crosswind take-off/landing procedures: climb, cruise, descent procedures including, airspeeds, configurations, method of drift allowance, setting of flight instruments and non-normal/emergency procedures

Technique and procedures used during engine failure on take-off, the appropriate reference airspeeds, and the specific pilot actions required

Technique and procedure for carrying out a rejected take-off after a engine/system(s) failure/warnings, including related safety factors

Technique and procedures used to conduct a go-around or missed approach during engine failure on take-off, the appropriate reference airspeeds, and the specific pilot actions required

Required skills:

Calculate accelerate/stop distance

Calculate V1 for any specified take-off conditions

Calculate initial rate of climb and climb gradient for one engine inoperative after take-off

Calculate fuel flow and true airspeed with one engine inoperative

Determine if the range of the aeroplane increases or decreases following an engine failure

Calculate PNR and ETP/CP for one engine inoperative with maximum fuel

Extract, calculate and apply all performance information applicable to the aeroplane

Identify, and manage emergency and abnormal situations while maintaining control of the aeroplane, in accordance with Flight Manual/POH

Identify the critical engine

Control and manage the aeroplane during flight with failed engine(s), in accordance with Flight Manual/POH

Maintain compliance with relevant regulatory requirements

Set priorities and manage workload to ensure safe task completion in the time available

Apply relevant air safety practices and regulations

Communicate effectively with others when operating a multi-engine fixed wing aeroplane

Read and interpret instructions, regulations, procedures and other information relevant to operating a multi-engine fixed wing aeroplane

Interpret and follow operational instructions and prioritise work

Complete documentation related to operating a multi-engine fixed wing aeroplane

Operate electronic communication equipment to required protocol

Work collaboratively with others when operating a multi-engine fixed wing aeroplane

Adapt appropriately to cultural differences in the workplace, including modes of behaviour and interactions with others

Promptly report and/or rectify any identified problems that may occur when operating a multi-engine fixed wing aeroplane in accordance with regulatory requirements and workplace procedures

Implement contingency plans for unexpected events that may arise when operating a multi-engine fixed wing aeroplane

Apply precautions and required action to minimise, control or eliminate hazards that may exist when operating a multi-engine fixed wing aeroplane

Monitor and anticipate operational problems and hazards and take appropriate action

Monitor work activities in terms of planned schedule

Modify activities dependent on differing workplace contingencies, situations and environments

Work systematically with required attention to detail without injury to self or others, or damage to goods or equipment

Adapt to differences in equipment and operating environment in accordance with standard operating procedures

Select and use required personal protective equipment conforming to industry and OH&S standards

Implement OH&S procedures and relevant regulations

Identify and correctly use equipment required to operate a multi-engine fixed wing aeroplane

The range statement relates to the unit of competency as a whole. It allows for different work environments and situations that may affect performance.

Tasks may be undertaken in:

VMC

IMC

VMC with simulated IMC conditions

Performance may be demonstrated in:

multi-engine aeroplane

multi-engine synthetic training device approved by appropriate authority

variable air traffic conditions

variable weather conditions

variable flight situations

abnormal situations

classes of airspace as designated by the Civil Aviation Safety Authority

Crew may include:

single pilot

multi crew

Instruments may be:

fitted flight instruments

head up display

Limitations may be imposed by:

local noise abatement requirements and curfews

airspace endorsements

Classes of airspace may be:

as designated by the regulator

restricted and danger areas

military control zones

Air Defence Identification Zones

Conditions may include:

a method of simulating IMC

simulated icing conditions

moderate turbulence

simulated hazardous weather

Autopilot/Flight Director

FMS/ other NAV system

simulation of emergency and abnormal procedures

Dependent on the type of organisation concerned and the local terminology used, workplace procedures may include:

company procedures

enterprise procedures

organisational procedures

established procedures

standard operating procedures

Information/documents may include:

relevant sections of Civil Aviation Safety Regulations and Civil Aviation Orders

in ADF context, relevant Defence Orders and Instructions

Manual of Standards - Pilot Licensing (MOS-PL)

Flight Manual/ Pilot's Operating Handbook (POH)

Aeronautical Information Publication (AIP)

relevant sections of the Civil Aviation Advisory Publications (CAAP)

performance charts

operations manuals

approved checklists

workplace procedures and instructions and job specification

induction and training materials

conditions of service, legislation and industrial agreements including workplace agreements and awards

Applicable regulations and legislation may include:

relevant Civil Aviation Safety Regulations and Civil Aviation Orders

in ADF context, relevant Defence Orders and Instructions

relevant state/territory OH&S legislation

relevant Australian Standards

Performance includes tolerances specified in either of:

relevant licence and aircraft rating requirements of the Civil Aviation Safety Authority (CASA) such as:

Day VFR Syllabus

Manual of Standards

relevant Defence documentation such as:

Defence Orders and Instructions

approved curricula and training documentation

Copy and paste from the following performance criteria to create an observation checklist for each task. When you have finished writing your assessment tool every one of these must have been addressed, preferably several times in a variety of contexts. To ensure this occurs download the assessment matrix for the unit; enter each assessment task as a column header and place check marks against each performance criteria that task addresses.

Observation Checklist

Tasks to be observed according to workplace/college/TAFE policy and procedures, relevant legislation and Codes of Practice Yes No Comments/feedback
Normal operations of multi-engine aeroplane type on the ground and in flight are conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 
Asymmetric operations for all phases of flight are anticipated and contingencies are planned 
A plan of action is self-briefed or briefed to crew members that will ensure the safest outcome in the event of asymmetric operations 
(In simulated conditions) Maintain and/or re-gain control of aeroplane 
Failed/malfunctioning engine is identified and confirmed 
Power set on serviceable engine/s and aeroplane configuration is adjusted to achieve desired aeroplane performance 
Failed/malfunctioning engine is managed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 
Indicated airspeed is maintained above VMCA 
ATC or another agency capable of assistance are advised of situation and intentions 
Recovery to aerodrome is evaluated and conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 
(In simulated conditions) Engine failure/malfunction is managed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures after take-off while heading is maintained 
Initial climb not less than best engine out angle of climb speed (VX) or best engine out rate of climb speed (VY) until clear of obstacles, then VY is maintained 
Recovery to aerodrome is evaluated and conducted in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 
Take-off is aborted prior to V1 or at a point during the take-off where the abort procedure can be initiated and the aeroplane stopped on the remaining runway/stopway 
Power is reduced smoothly and promptly 
Spoilers, prop fine/reverse, thrust reverse, wheel brakes and other drag and braking devices are activated 
Positive control is maintained to bring the aeroplane to a safe stop 
Engine failure procedures and/or checklists are initiated and completed 
(In simulated conditions) Control of aeroplane is maintained 
Engine inoperative approach is performed in accordance with the aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 
Decision is made to continue or abort approach/landing 
Decision height for landing is nominated 
ATS or other agencies capable of providing assistance are advised of situation and intentions 
Flight profile is flown from which a controlled landing could be achieved 
(In simulated conditions) Engine failure in a multi-engine aeroplane during a go-around or missed approach is identified and confirmed 
Control of aeroplane is maintained 
Engine inoperative go-around is performed from decision height in accordance with aeroplane Flight Manual, Pilot's Operating Handbook (POH) and company operating procedures 

Forms

Assessment Cover Sheet

AVIY5023A - Operate multi-engine fixed wing aeroplane
Assessment task 1: [title]

Student name:

Student ID:

I declare that the assessment tasks submitted for this unit are my own work.

Student signature:

Result: Competent Not yet competent

Feedback to student

 

 

 

 

 

 

 

 

Assessor name:

Signature:

Date:

Assessment Record Sheet

AVIY5023A - Operate multi-engine fixed wing aeroplane

Student name:

Student ID:

Assessment task 1: [title] Result: Competent Not yet competent

(add lines for each task)

Feedback to student:

 

 

 

 

 

 

 

 

Overall assessment result: Competent Not yet competent

Assessor name:

Signature:

Date:

Student signature:

Date: