This five-day course is a continuation of the Aircraft Structural Repair for Engineers Part I. It uses a combination of lectures, practice exercises and discussion to further enhance the ability of the engineer to understand, design and assess repairs to metallic airframe structure.
This course focuses on the design of repairs to structure loaded in compression. Concepts of bending and column stability will be discussed. Repairs to airplane structural members will be analysed for beam bending, buckling and crippling failure modes.
Prerequisites: Engineering degree or equivalent experience and Structural Repair for Engineers Part I.
This course satisfies ATA 104 Level IV objectives. Upon completion of the course, the student will be able to:
» Analyse beam structural repairs for bending
» Analyse structural repairs for Euler column and inter-fastener buckling failure modes
» Analyse structural repairs for crippling and Johnson-Euler column failure modes
» Apply Part I and Part II analysis methods to the design of typical floor beam repairs.
An exam will be administered for this course.
Details
DATE: 16 - 20 May, 2016
8am - 4pm
VENUE: Level 4, 210 Kings Way, South Melbourne VIC 3205
COST: $4,500 per person + GST
Please note – if registering for Part I & Part II a 20% discount will be applied
to the total price.
REGISTRATION CLOSES: 15 April, 2016
STUDENTS RECEIVE: Course materials, morning tea, light lunch, afternoon tea and certificate.
REGISTRATION: Register online at www.QTTraining.com.au