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AERONAUTICAL ENGINEERING
nehru INSTITUTE OF TECHNOLOGY,COIMBATORE.
DEPARTMENT OF AERONAUTICAL ENGINEERING
Certified that this is the bonafide record of work done
by…………………………………………………… in the Aircraft Component Drawing of this
institution, as prescribed by Anna University, for the second Year / Fourth
Semester during the year 2012-2013.
Staff-in-charge Head of the Department
University Register No: ………………………
Submitted for the Second year / Fourth semester Examination of this Institution
conducted on ………………………
Internal Examiner External Examiner
EXPT. NO. DATE NAME OF THE EXPERIMENT
PAGE
NO Marks Signature
1
Design and Drafting of Riveted
Joints
2
Design and Drafting of Welded
Joints
3
Design and Drafting Control
Components Cam.
4
Design and Drafting Control
Components Bell Crank.
5
Design and Drafting Control
Components Gear.
6
Design and Drafting Control
Components Push-Pull Rod.
7
Three View Diagram of a Typical
Aircraft.
8 Layout of Typical Wing Structure.
9
Layout of Typical Fuselage
Structure.
10 Layout of Control System.

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  • 1. AERONAUTICAL ENGINEERING nehru INSTITUTE OF TECHNOLOGY,COIMBATORE. DEPARTMENT OF AERONAUTICAL ENGINEERING Certified that this is the bonafide record of work done by…………………………………………………… in the Aircraft Component Drawing of this institution, as prescribed by Anna University, for the second Year / Fourth Semester during the year 2012-2013. Staff-in-charge Head of the Department University Register No: ……………………… Submitted for the Second year / Fourth semester Examination of this Institution conducted on ……………………… Internal Examiner External Examiner
  • 2. EXPT. NO. DATE NAME OF THE EXPERIMENT PAGE NO Marks Signature 1 Design and Drafting of Riveted Joints 2 Design and Drafting of Welded Joints 3 Design and Drafting Control Components Cam. 4 Design and Drafting Control Components Bell Crank. 5 Design and Drafting Control Components Gear. 6 Design and Drafting Control Components Push-Pull Rod. 7 Three View Diagram of a Typical Aircraft. 8 Layout of Typical Wing Structure. 9 Layout of Typical Fuselage Structure. 10 Layout of Control System.