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

AVIH0019 Mapping and Delivery Guide
Manage aircraft performance and load

Version 1.0
Issue Date: May 2024


Qualification -
Unit of Competency AVIH0019 - Manage aircraft performance and load
Description
Employability Skills
Learning Outcomes and Application
Duration and Setting X weeks, nominally xx hours, delivered in a classroom/online/blended learning setting.
Prerequisites/co-requisites
Competency Field
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: Apply weight and balance control to flight planning
  • Components of weight, balance and control are considered and applied in flight planning activities
       
Element: Weight and control limitations are included in flight planning calculations
       
Element: Required fuel and payload quantities, including minimum fuel reserves, maximum allowable payloads and fuel quantity limitations, are considered when calculating weight and balance
       
Element: Calculated aircraft weight centre of gravity (CG) is within aircraft limits and is established for take-off, cruise and fuel economy calculation purposes
       
Element: Ground handling of baggage and cargo is minimised through load distribution and loading sequence planning
       
Element: Weight and CG are derived and calculated using basic data methods and applied to flight planning calculations
       
Element: Comprehensive loadsheet is compiled that includes all required flight performance and load planning data
       
Element: Identify constraints affecting load planning
  • Implications of advanced sales on payload, weight and control limitations are considered
       
Element: Aircraft, route, fuel required and performance limitation planning factors are assessed for potential constraints to load planning activities
       
Element: Hazards are identified, risks are assessed and hazard management implemented
       
Element: Operator advance index tables and potential impact of weight and fuel minima during seasonal change are identified and considered
       
Element: Unusual conditions when advanced allotment tables may be exceeded, the operational impacts and associated contingency planning factors are considered
       
Element: Load planning constraints and limitations are prioritised based on operational and regulatory requirements
  • Aircraft design and weight, taxi, take-off, landing and zero-fuel weights (ZFW) are reviewed and applied to load planning activities
       
Element: Operational load planning factors affecting a restriction on weight, operational (phase of flight), environmental, equipment, airspace and airport/aerodrome are considered and applied as required to aircraft load planning
       
Element: Aircraft operating weight and passenger weight limits are summarised within load planning documentation
       
Element: Weight of minimum fuel based on ZFW, quantity, fuel type and specific gravity (including fuel quantity conversions) are reviewed and applied to load planning calculations
       
Element: Available payload based on specific conditions affecting a flight, including maximum take-off weight (MTOW), regulated take-off weight (RTOW), minimum fuel and taxi fuel requirements, are determined
       
Element: Manual loadsheet, including payload location and last-minute changes, is prepared
       
Element: Loadsheet, including payload location and last-minute changes, is interpreted and automated
       
Element: Apply principles of aircraft balance and longitudinal stability to load planning
  • Load planning factors, including balance, CG (variations), balance on the ground, principles of lift and centre of pressure, mean aerodynamic chord (MAC) and functions of stabilisers, are identified and considered when calculating aircraft performance and load
       
Element: Aircraft point of balance is calculated using aircraft data and aircraft balance principles, and is applied to load planning calculations
       
Element: Identify aircraft structural limitations
  • Satisfactory aircraft balance calculations are achieved ensuring aircraft is safely loaded, floor strengths have not been exceeded and load/cargo is capable of being satisfactorily restrained
       
Element: Fuselage structural limits over, forward and aft of the wing, and weight limitations for associated loading zones are considered and applied to load planning activities
       
Element: Maximum allowable package sizes are determined using aircraft tables
       
Element: Methods of restraint and the effect on passengers and crew, damage and CG, including principles of inertia and forces applied to load, are considered and applied to load planning activities
       
Element: Advantages and limitations of certified and non-certified cargo pallets and containers, and methods of load security are considered when calculating aircraft load limitations
       
Element: Identify aircraft weight and performance planning safety factors
  • Aircraft certification considerations, including structural strength, loads, speed limitations, operating environment, performance capability, runway lengths and terrain, are considered and applied to aircraft weight and performance calculations
       
Element: Aircraft certification standards, including categories, state-based variations, operating weight or CG never exceeding limits, and aircraft flight manual restrictions are considered and applied to aircraft weight and performance calculations
       
Element: Environmental considerations, including certified aircraft operating envelope, pressurisation capabilities, system limitations and aircraft flight manual envelope charts, are considered and applied to aircraft performance calculations
       
Element: Determine aircraft weight and speed limitations
  • Positive and negative load factor limitations, including normal and ultimate (structural), speed limitations and differing express terms of speed, are considered and applied to aircraft performance calculations
       
Element: Boundaries of aircraft operating envelope for a specific weight are determined using flight strength diagrams, illustrating effect of wind gusts, margins of speed limits and turbulence penetration considerations
       
Element: Calculate take-off runway requirements
  • Turbo-jet aircraft take-off requirements are determined considering clearways and stop-ways, runway requirements and alternatives to balanced field length methods
       
Element: Critical engine failure speeds, flap positions and reduced thrust take-off stopping distance at critical engine failure speeds are calculated
       
Element: Calculate climb performance
  • Take-off flight path, climb segments; including terrain and obstacle avoidance; and the effects of weight, altitude and temperature are determined
       
Element: En route considerations affecting climb performance, such as take-off weight, en route alternate selection and terrain, are considered and applied to aircraft performance calculations
       
Element: Approach and landing requirement planning factors, including terrain and obstacle avoidance, and effects of weight, altitude and temperature, are considered and applied to aircraft performance calculations
       
Element: Calculate landing runway requirements
  • Runway landing distance requirements are determined, including effect of aircraft configuration, available stopping distance, and effects of marginal conditions
       
Element: Landing distance based on varying environmental conditions, effect of obstacles and braking systems is calculated
       
Element: Determine aircraft buffet boundary and speeds
  • Aircraft buffet characteristics, and the effect of variations of a given weight and speed are identified and applied to aircraft performance calculations
       
Element: Permissible buffet for a range of aircraft speeds for combinations of weight and altitude, including safe operating margins, is calculated
       

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.
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
Components of weight, balance and control are considered and applied in flight planning activities 
 
 
 
 
 
 
Implications of advanced sales on payload, weight and control limitations are considered 
 
 
 
 
Aircraft design and weight, taxi, take-off, landing and zero-fuel weights (ZFW) are reviewed and applied to load planning activities 
 
 
 
 
 
 
Load planning factors, including balance, CG (variations), balance on the ground, principles of lift and centre of pressure, mean aerodynamic chord (MAC) and functions of stabilisers, are identified and considered when calculating aircraft performance and load 
 
Satisfactory aircraft balance calculations are achieved ensuring aircraft is safely loaded, floor strengths have not been exceeded and load/cargo is capable of being satisfactorily restrained 
 
 
 
 
Aircraft certification considerations, including structural strength, loads, speed limitations, operating environment, performance capability, runway lengths and terrain, are considered and applied to aircraft weight and performance calculations 
 
 
Positive and negative load factor limitations, including normal and ultimate (structural), speed limitations and differing express terms of speed, are considered and applied to aircraft performance calculations 
 
Turbo-jet aircraft take-off requirements are determined considering clearways and stop-ways, runway requirements and alternatives to balanced field length methods 
 
Take-off flight path, climb segments; including terrain and obstacle avoidance; and the effects of weight, altitude and temperature are determined 
 
 
Runway landing distance requirements are determined, including effect of aircraft configuration, available stopping distance, and effects of marginal conditions 
 
Aircraft buffet characteristics, and the effect of variations of a given weight and speed are identified and applied to aircraft performance calculations 
 

Forms

Assessment Cover Sheet

AVIH0019 - Manage aircraft performance and load
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

AVIH0019 - Manage aircraft performance and load

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: