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airline operation

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Posted over 8 years ago

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Hello, I am taking quotes for outsource this topic of my assignment. Please take time to advice quote for this assignment of mine. I need to get this done by oct 1st week. Please advice the best quote as i need to finalise it in 2- 3 days. topic- Assignment Question B737-800 Performance & Planning 1. You are a line pilot with Air Can-Do, a charter company which is planning to upgrade to B737-800 aircraft. The Company is based in Townsville. 2. The Chief Pilot has asked you as the Company Navigation Specialist to provide him with some performance and planning data for the B737-800. He is aware that you passed the 3510 NSC course at GU and is confident you know all about the performance and planning requirements for the B737-800. 3. The CP briefs you that he wants: A set of performance and planning data that will enable him to do some initial route planning and fuel planning for evaluation of the B737-800. Specifically he wants to know: a. The maximum cruise altitude based on 1.3g buffet margin for the top of climb weight b. The optimum cruise altitude for LRC for the top of climb weight c. Climb flight fuel based on the brakes release weight d. Minimum LRC flight fuel based on 4 hours in cruise based on top of climb weight e. Descent flight fuel based on estimated top of descent weight f. Alternate flight fuel based on 400nm alternate 4. The assumptions he wants you to base your figures on are at Annex A. 5. You need to focus purely on the B737-800 data available in the B737-800 Performance & Operating handbook. 6 Your report may be in ‘dot point’ format provided there is sufficient explanation. 7. The indicative word count is 1000 – 1500 words. However, the answers are the important items and there will be NO PENALTY for word count above 1500 or below 1000 words. Annex A A. Assume temperatures at ALL levels of ISA + 15ºC B. Assume Brakes Release Weight of 77,000kg (77t) C. Assume time in cruise of 240 minutes Marking Criteria Performance & Planning Item 1. The maximum cruise altitude based on 1.3g buffet margin for the top of climb weight 2. The optimum cruise altitude for LRC for the top of climb weight 3. Climb flight fuel based on the brakes release weight 4. Minimum LRC flight fuel based on 4 hours in cruise based on top of climb weight 5. Descent flight fuel based on estimated top of descent weight 6. Alternate flight fuel based 400nm alternate Marks Allocation = 5 marks per item. Total marks available is 6 x 5 = 30 marks 5 marks for correct answer [ ± 500 ft] 50% marks for ±1000ft 5 marks for correct answer [± 500 ft] 50% marks for ± 1000 ft 5 marks for correct answer [±100 kg 50% marks for ± 200kg 5 marks for correct answer ±200 kg 50% marks for ±400kg 5 marks for correct answer [±20 kg] 50% marks for ±40 kg 5 marks for correct answer [ ± 200 kg] 50% marks for ±400 kg
Project ID: 8485656

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