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Development of
Airshuttle AS-202
Prakhar Gupta (19BSPHH01C0798)
Subhodip Pal (19BSPHH01C1244)
Ashish Dadhwal (19BSPHH01C0215)
Shivani Ambekar (19BSPHH01C1124)
Biswadeep Guha Roy (19BSPHH01C1465)
Debpratik Ghosh (19BSPHH01C0323)
Hitesh Sharma (19BSPHH01C1478)
Sabyasachi Bhar (19BSPHH01C1578)
Group-7
Sector: Commercial Aircraft
Introduction
NOTE- BAL Airshuttle is a Hypothetical Organization
 Bharat Aeronautics Limited (BAL)
 What is Airshuttle?
 Plants of Airshuttle
 Competitors of Airshuttle
 AS-101
 Need for AS-202 (Business Problem)
Objectives of the Project
 To reduce the fuel consumption by the aircrafts.
 To develop a sensor system for auto-stabilization of the aircraft.
 To update the existing cockpit console in terms of hardware and software.
 To provide a newly designed cabin with customizable LED lights and a digital
system for Cabin Crew.
 To develop new simulation units in order to train the pilots with new all-digital
console system and newly added stabilization sensor system.
Constraints
 Time constraint (Major):
 Airshuttle has to manufacture and test the new AS-202 to their customers as
soon as possible in order to retain their market share in the Indian Commercial
Airline market.
 Cost Constraint (Minor):
 The development of AS-202 had to be done in a way so as to keep the cost of
the aircrafts for the customers lower than the price of foreign offering
Root Cause Analysis
Project Charter
Project Charter
Project Title DEVELOPMENT OF AIRSHUTTLE AS-202
Project Manager
Prakhar
Gupta
Project Start Date 24-Apr-14 Project end date 15-Mar-20
Business Need
To be a leader in commercial aerospace, strengthen market position and focus on profitability,
value creation and to develop the most comprehensive & safe aircraft in response to customer
needs.
Project Scope Deliverables
1.) To reduce the fuel consumption by the aircrafts.
2.) To develop a sensor system for auto-stabilization
of the aircraft.
3.) To update the existing cockpit console in terms of
hardware and software.
4.) To provide a newly designed cabin with
customizable LED lights and a digital system for
Cabin Crew.
5.) To develop new simulation units in order to train
the pilots with new all-digital console
system and newly added stabilization sensor system.
1.) Airshuttle AS-202.
2.) Simulation Unit.
3.) Training Module for the Pilots.
Risk and Issues Assumptions/Dependencies
1.) Technical Risk
2.) Economic Risk
3.) Staffing Risk
4.) Schedule Risk
5.) Quality & Testing Risk
1.) Cross Functional Dependencies
between different manufacturing units.
2.) Administrative support by regulatory
body
3.) Financial Aid from external bodies.
Financials
Airshuttle needs a funding of 1100 Crore INR from external bodies
Milestone Schedule
Milestone Target Completion Date Actual Date
Engine Development 28-Oct-17 28-Oct-17
Propulsion System Development 13-Dec-14 13-Dec-14
Sensor Unit Development 02-Jan-17 02-Jan-17
Cockpit Design and Manufacture
20-Dec-17 20-Dec-17
Cabin Design and Manufacture
Body Manufacture
Software Development 25-Mar-18 25-Mar-18
Software and Hardware Integration 04-Jun-18 04-Jun-18
Assembly of AS-202 23-Feb-19 23-Feb-19
Simulation and testing 06-May-19 06-May-19
Quality Assurance and Certifications 16-Jan-20 16-Jan-20
Project Team Approval/Review Committee
Project Manager Prakhar Gupta Sponsor *****
Team Members 1.) Ashish Dadhwal
2.) Biswadeep Guha Roy
3.) Shivani Ambekar
4.) Subhodip Pal
5.) Debpratik Ghosh
6.) Hitesh Sharma
7.) Sabyasachi Bhar
Business Division Head Shivani Ambekar
Business Unit head
Biswadeep Guha
Roy
Finance Manager Subhodip Pal
[ Project Charter Continued ]
Organization Breakdown Structure
Work Break-down Structure
Network Diagram
Critical Path Method
Gantt Chart
Responsibility Matrix (RACI)
Responsible
Accountable
Consulted
Informed
Risk Breakdown Structure
Severity Analysis
Activity ID Activity Description Risk
A FPR-1 Financial Risk
Risk Description Likelihood Weightage Impact
A1 R&D cost exceeding the estimation 0.3 0.025 0.5
A2 Need for external investment 0.15 0.045 0.35
0.07
CLF 0.01425
CIF 0.02825
Severity 0.000403
Likelilhood 0.45
B FPR-2 R&D Timeline Risk
Risk Description Likelihood Weightage Impact
B1 Delay in Designing 0.1 0.025 0.7
B2 Delay in Engine Development 0.25 0.085 0.8
B3 Delay in Sensor Unit R&D 0.25 0.08 0.75
B4 Delay in Software Development 0.35 0.085 0.8
B5 Delay in Cockpit R&D 0.2 0.065 0.7
B6 Delay in Assembly 0.15 0.08 0.7
0.42
CLF 0.0985
CIF 0.315
Severity 0.031028
Likelihood 1.3
C FPR-3 Operational Risk
Risk Description Likelihood Weightage Impact
C1 Cross-Functional Risk 0.3 0.065 0.45
C2 Logistic Risk 0.2 0.04 0.45
C3 Resource Utilization Risk 0.15 0.035 0.6
0.14
CLF 0.03275
CIF 0.06825
Severity 0.002235
Likelihood 0.65
D FPR-4 Technical Risk
Risk Description Likelihood Weightage Impact
D1 Software - Hardware Integration Risk 0.4 0.08 0.7
D2 Assembly Risk 0.1 0.06 0.55
D3 Simulation Unit Co-ordination Risk 0.2 0.04 0.45
D4 Testing Risk 0.3 0.055 0.3
0.235
CLF 0.0625
CIF 0.1235
Severity 0.007719
Likelihood 1
E FPR-5 Quality Assurance Risk
Risk Description Likelihood Weightage Impact
E1 Safety Norms Risks 0.3 0.06 0.4
E2 Delay in Approval and Certification 0.2 0.075 0.5
0.135
CLF 0.033
CIF 0.0615
Severity 0.00203
Likelihood 0.5
Total Weight 1
Total CLF 0.241
Total CIF 0.5965
Severity 0.143757
Risk Severity Matrix
LIKELIHOOD
Rare Unlikely Possible Likely Certain
CONSEQUENCE
Extensive
Major B1 B2, B3, B5, B6 B4, D1,
Medium D2 C2, C3, D3, E2 A1, C1, E1
Minor Impact A2 D4
No Impacct
Likelihood Scale Impact Scale
Rare 0 to 0.1 No Impacct 0 to 0.2
Unlikely 0.1 to 0.25 Minor Impact 0.2 to 0.4
Possible 0.25 to 0.5 Medium 0.4 to 0.6
Likely 0.5 to 0.8 Major 0.6 to 0.8
Certain 0.8 to 1 Extensive 0.8 to 1
Likelihood Scale
Rare 0 to 0.1
Unlikely 0.1 to 0.25
Possible 0.25 to 0.5
Likely 0.5 to 0.8
Certain 0.8 to 1
Cost Estimation
Activity Percentage Cost Cost Estimate (in Cr)
Engine Development 37% 407
Propulsion System Development 4% 44
Sensor Unit Development 8% 88
Cockpit Design and Manufacture 9% 99
Cabin Design and Manufacture 6% 66
Body Manufacture 10% 110
Software Development 6% 66
Software and Hardware Integration 4% 44
Assembly of AS-202 7% 77
Simulation and testing 3% 33
Quality Assurance and Certifications 6% 66
Total Cost Estimate 100% 1100
Earned Value Analysis
Activity
Planned
Completion
Cost Estimate (in
Cr) (PV)
Actual Work
Completed (EV) (SV)
Scheduled
Performance
Index AC CV
Cost
Performance
Index
Engine Development 0.82 333.74 0.82 333.74 0 1 340.30 -6.6 0.980722892
Propulsion System Development 1 44.00 1 44.00 0 1 40.00 4.0 1.1
Sensor Unit Development 1 88.00 1 88.00 0 1 98.00 -10.0 0.897959184
Body Manufacture 1 110.00 1 110.00 0 1 112.00 -2.0 0.982142857
Phase 1
0 to 984
Activity
Planned
Completion
Cost Estimate (in
Cr) (PV)
Actual Work
Completed (EV) (SV)
Scheduled
Performance
Index AC CV
Cost
Performance
Index
Engine Development 1 73.26 1 73.26 0 1 75.00 -1.7 0.9768
Cockpit Design and Manufacture 1 99.00 1 99.00 0 1 105.00 -6.0 0.942857143
Software Development 1 66.00 1 66.00 0 1 85.00 -19.0 0.776470588
Phase 2
984 to 1431
Earned Value Analysis
Activity
Planned
Completion
Cost Estimate (in
Cr) (PV)
Actual Work
Completed (EV) (SV)
Scheduled
Performance
Index AC CV
Cost
Performance
Index
Software and Hardware Integration 1 44.00 1 44.00 0 1 54.00 -10.0 0.814814815
Assembly of AS-202 1 74.00 1 74.00 0 1 78.00 -4.0 0.948717949
Phase 3
1431 to 1766
Activity
Planned
Completion
Cost Estimate (in
Cr) (PV)
ActualWork
Completed (EV) (SV)
Scheduled
Performance
Index AC CV
Cost
Performance
Index
Simulation and testing 1 33.00 1 33.00 0 1 35.00 -2.0 0.942857143
Quality Assurance and Certifications 1 66.00 1 66.00 0 1 70.00 -4.0 0.942857143
Phase 4
1766 to 2093
Conclusion
 The Project was completed as planned as it was a highly time constrained Project.
 The Project went over budget by 65.30 crore, which was spent in fast-tracking the
activities that were lagging in meeting the deadlines.
Activity Extra Cost (crore)
Engine Development 8.3
Sensor Unit Development 10.00
Body Manufacture 2.00
Cockpit Design and Manufacture 6.00
Software Development 19.00
Software and Hardware Integration 10
Assembly of AS-202 4
Simulation and testing 2
Quality Assurance and Certifications 4
Total 65.3
Thank you

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Development of Airshuttle AS-202

  • 1. Development of Airshuttle AS-202 Prakhar Gupta (19BSPHH01C0798) Subhodip Pal (19BSPHH01C1244) Ashish Dadhwal (19BSPHH01C0215) Shivani Ambekar (19BSPHH01C1124) Biswadeep Guha Roy (19BSPHH01C1465) Debpratik Ghosh (19BSPHH01C0323) Hitesh Sharma (19BSPHH01C1478) Sabyasachi Bhar (19BSPHH01C1578) Group-7 Sector: Commercial Aircraft
  • 2. Introduction NOTE- BAL Airshuttle is a Hypothetical Organization  Bharat Aeronautics Limited (BAL)  What is Airshuttle?  Plants of Airshuttle  Competitors of Airshuttle  AS-101  Need for AS-202 (Business Problem)
  • 3. Objectives of the Project  To reduce the fuel consumption by the aircrafts.  To develop a sensor system for auto-stabilization of the aircraft.  To update the existing cockpit console in terms of hardware and software.  To provide a newly designed cabin with customizable LED lights and a digital system for Cabin Crew.  To develop new simulation units in order to train the pilots with new all-digital console system and newly added stabilization sensor system.
  • 4. Constraints  Time constraint (Major):  Airshuttle has to manufacture and test the new AS-202 to their customers as soon as possible in order to retain their market share in the Indian Commercial Airline market.  Cost Constraint (Minor):  The development of AS-202 had to be done in a way so as to keep the cost of the aircrafts for the customers lower than the price of foreign offering
  • 6. Project Charter Project Charter Project Title DEVELOPMENT OF AIRSHUTTLE AS-202 Project Manager Prakhar Gupta Project Start Date 24-Apr-14 Project end date 15-Mar-20 Business Need To be a leader in commercial aerospace, strengthen market position and focus on profitability, value creation and to develop the most comprehensive & safe aircraft in response to customer needs. Project Scope Deliverables 1.) To reduce the fuel consumption by the aircrafts. 2.) To develop a sensor system for auto-stabilization of the aircraft. 3.) To update the existing cockpit console in terms of hardware and software. 4.) To provide a newly designed cabin with customizable LED lights and a digital system for Cabin Crew. 5.) To develop new simulation units in order to train the pilots with new all-digital console system and newly added stabilization sensor system. 1.) Airshuttle AS-202. 2.) Simulation Unit. 3.) Training Module for the Pilots. Risk and Issues Assumptions/Dependencies 1.) Technical Risk 2.) Economic Risk 3.) Staffing Risk 4.) Schedule Risk 5.) Quality & Testing Risk 1.) Cross Functional Dependencies between different manufacturing units. 2.) Administrative support by regulatory body 3.) Financial Aid from external bodies. Financials Airshuttle needs a funding of 1100 Crore INR from external bodies Milestone Schedule Milestone Target Completion Date Actual Date Engine Development 28-Oct-17 28-Oct-17 Propulsion System Development 13-Dec-14 13-Dec-14 Sensor Unit Development 02-Jan-17 02-Jan-17 Cockpit Design and Manufacture 20-Dec-17 20-Dec-17 Cabin Design and Manufacture Body Manufacture Software Development 25-Mar-18 25-Mar-18 Software and Hardware Integration 04-Jun-18 04-Jun-18 Assembly of AS-202 23-Feb-19 23-Feb-19 Simulation and testing 06-May-19 06-May-19 Quality Assurance and Certifications 16-Jan-20 16-Jan-20 Project Team Approval/Review Committee Project Manager Prakhar Gupta Sponsor ***** Team Members 1.) Ashish Dadhwal 2.) Biswadeep Guha Roy 3.) Shivani Ambekar 4.) Subhodip Pal 5.) Debpratik Ghosh 6.) Hitesh Sharma 7.) Sabyasachi Bhar Business Division Head Shivani Ambekar Business Unit head Biswadeep Guha Roy Finance Manager Subhodip Pal [ Project Charter Continued ]
  • 14. Severity Analysis Activity ID Activity Description Risk A FPR-1 Financial Risk Risk Description Likelihood Weightage Impact A1 R&D cost exceeding the estimation 0.3 0.025 0.5 A2 Need for external investment 0.15 0.045 0.35 0.07 CLF 0.01425 CIF 0.02825 Severity 0.000403 Likelilhood 0.45 B FPR-2 R&D Timeline Risk Risk Description Likelihood Weightage Impact B1 Delay in Designing 0.1 0.025 0.7 B2 Delay in Engine Development 0.25 0.085 0.8 B3 Delay in Sensor Unit R&D 0.25 0.08 0.75 B4 Delay in Software Development 0.35 0.085 0.8 B5 Delay in Cockpit R&D 0.2 0.065 0.7 B6 Delay in Assembly 0.15 0.08 0.7 0.42 CLF 0.0985 CIF 0.315 Severity 0.031028 Likelihood 1.3 C FPR-3 Operational Risk Risk Description Likelihood Weightage Impact C1 Cross-Functional Risk 0.3 0.065 0.45 C2 Logistic Risk 0.2 0.04 0.45 C3 Resource Utilization Risk 0.15 0.035 0.6 0.14 CLF 0.03275 CIF 0.06825 Severity 0.002235 Likelihood 0.65 D FPR-4 Technical Risk Risk Description Likelihood Weightage Impact D1 Software - Hardware Integration Risk 0.4 0.08 0.7 D2 Assembly Risk 0.1 0.06 0.55 D3 Simulation Unit Co-ordination Risk 0.2 0.04 0.45 D4 Testing Risk 0.3 0.055 0.3 0.235 CLF 0.0625 CIF 0.1235 Severity 0.007719 Likelihood 1 E FPR-5 Quality Assurance Risk Risk Description Likelihood Weightage Impact E1 Safety Norms Risks 0.3 0.06 0.4 E2 Delay in Approval and Certification 0.2 0.075 0.5 0.135 CLF 0.033 CIF 0.0615 Severity 0.00203 Likelihood 0.5 Total Weight 1 Total CLF 0.241 Total CIF 0.5965 Severity 0.143757
  • 15. Risk Severity Matrix LIKELIHOOD Rare Unlikely Possible Likely Certain CONSEQUENCE Extensive Major B1 B2, B3, B5, B6 B4, D1, Medium D2 C2, C3, D3, E2 A1, C1, E1 Minor Impact A2 D4 No Impacct Likelihood Scale Impact Scale Rare 0 to 0.1 No Impacct 0 to 0.2 Unlikely 0.1 to 0.25 Minor Impact 0.2 to 0.4 Possible 0.25 to 0.5 Medium 0.4 to 0.6 Likely 0.5 to 0.8 Major 0.6 to 0.8 Certain 0.8 to 1 Extensive 0.8 to 1 Likelihood Scale Rare 0 to 0.1 Unlikely 0.1 to 0.25 Possible 0.25 to 0.5 Likely 0.5 to 0.8 Certain 0.8 to 1
  • 16. Cost Estimation Activity Percentage Cost Cost Estimate (in Cr) Engine Development 37% 407 Propulsion System Development 4% 44 Sensor Unit Development 8% 88 Cockpit Design and Manufacture 9% 99 Cabin Design and Manufacture 6% 66 Body Manufacture 10% 110 Software Development 6% 66 Software and Hardware Integration 4% 44 Assembly of AS-202 7% 77 Simulation and testing 3% 33 Quality Assurance and Certifications 6% 66 Total Cost Estimate 100% 1100
  • 17. Earned Value Analysis Activity Planned Completion Cost Estimate (in Cr) (PV) Actual Work Completed (EV) (SV) Scheduled Performance Index AC CV Cost Performance Index Engine Development 0.82 333.74 0.82 333.74 0 1 340.30 -6.6 0.980722892 Propulsion System Development 1 44.00 1 44.00 0 1 40.00 4.0 1.1 Sensor Unit Development 1 88.00 1 88.00 0 1 98.00 -10.0 0.897959184 Body Manufacture 1 110.00 1 110.00 0 1 112.00 -2.0 0.982142857 Phase 1 0 to 984 Activity Planned Completion Cost Estimate (in Cr) (PV) Actual Work Completed (EV) (SV) Scheduled Performance Index AC CV Cost Performance Index Engine Development 1 73.26 1 73.26 0 1 75.00 -1.7 0.9768 Cockpit Design and Manufacture 1 99.00 1 99.00 0 1 105.00 -6.0 0.942857143 Software Development 1 66.00 1 66.00 0 1 85.00 -19.0 0.776470588 Phase 2 984 to 1431
  • 18. Earned Value Analysis Activity Planned Completion Cost Estimate (in Cr) (PV) Actual Work Completed (EV) (SV) Scheduled Performance Index AC CV Cost Performance Index Software and Hardware Integration 1 44.00 1 44.00 0 1 54.00 -10.0 0.814814815 Assembly of AS-202 1 74.00 1 74.00 0 1 78.00 -4.0 0.948717949 Phase 3 1431 to 1766 Activity Planned Completion Cost Estimate (in Cr) (PV) ActualWork Completed (EV) (SV) Scheduled Performance Index AC CV Cost Performance Index Simulation and testing 1 33.00 1 33.00 0 1 35.00 -2.0 0.942857143 Quality Assurance and Certifications 1 66.00 1 66.00 0 1 70.00 -4.0 0.942857143 Phase 4 1766 to 2093
  • 19. Conclusion  The Project was completed as planned as it was a highly time constrained Project.  The Project went over budget by 65.30 crore, which was spent in fast-tracking the activities that were lagging in meeting the deadlines. Activity Extra Cost (crore) Engine Development 8.3 Sensor Unit Development 10.00 Body Manufacture 2.00 Cockpit Design and Manufacture 6.00 Software Development 19.00 Software and Hardware Integration 10 Assembly of AS-202 4 Simulation and testing 2 Quality Assurance and Certifications 4 Total 65.3