Assessor Resource

AVIH0019
Manage aircraft performance and load

Assessment tool

Version 1.0
Issue Date: May 2024


You may want to include more information here about the target group and the purpose of the assessments (eg formative, summative, recognition)

Submission Requirements

List each assessment task's title, type (eg project, observation/demonstration, essay, assingnment, 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: