Essays on Fundamentals In Aeronautical Engineering Assignment

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WEIGHT DISTRIBUTIONLOAD IN COMPARTMENTS 6977 1/2516 3/1677 4/1677 5/1107 PASSENGER/CABIN BAG 6923 AD/77 C/13 I/6 TTL 90+6TOTAL PAYLOAD 13900 LAST MINUTE CHANGESDRY OPERATING WEIGHT 42599 DEST SPEC CL/CPT +/- WEIGHTZERO FUEL WEIGHT ACTUAL 56499 MAX 61000 LTAKE OFF FUEL 12400TAKE OFF WEIGHT ACTUAL 68899 MAX 76931TRIP FUEL 9460LANDING WEIGHT ACTUAL 59439 MAX 64500TAXI OUT FUEL 115UNDERLOAD BEFORE L. M.C. 4501 LIMITED BY ZFW LMC TOTAL + / -BALANCING/TRIM CONDITIONSMACZFW 34.21%MACTOW 31.16% STAB TRIM: 0.6 DNMACLDW 34.89%MAC LIMITSZFW FWD 16.74% AFT 42.00%TOW FWD 17.00% AFT 42.00%LDW FWD 16.86% AFT 43.00%TRIM BY CABIN AREAA30.B30.C30CAPTAINS INFORMATION/NOTESSTD WEIGHTS USED ADULT/84 CHILD/35 INFANT/0BLOCK FUEL/ 12515 ( 15498 LITER)LANDG FUEL/ 2940 ( 3641 LITER)TAXI TIME 10 MINB737-700L O A D S H E E T ISSUED BY APPROVED DATE TIME 24 APR 2013 1445ALL WEIGHTS IN KILOGRAMS. .... ....

. .... .... . FROM/TO FLIGHT A/C REG A/C TYPE CONFIG LTBX/EGCC 3 DFR987 B737-700/CFM56-7B22 Y126 WEIGHT DISTRIBUTIONLOAD IN COMPARTMENTS 5099 1/2550 2/2549 PASSENGER/CABIN BAG 8246 AD/94 C/10 I/8 TTL 104+8TOTAL PAYLOAD 13345 LAST MINUTE CHANGESDRY OPERATING WEIGHT 37848 DEST SPEC CL/CPT +/- WEIGHTZERO FUEL WEIGHT ACTUAL 51193 MAX 54658 LTAKE OFF FUEL 11600TAKE OFF WEIGHT ACTUAL 62793 MAX 69626TRIP FUEL 9890LANDING WEIGHT ACTUAL 52903 MAX 58481TAXI OUT FUEL 115UNDERLOAD BEFORE L. M.C.

3465 LIMITED BY ZFW LMC TOTAL + / -BALANCING/TRIM CONDITIONSMACZFW 30.23%MACTOW 32.26% STAB TRIM: +4.9MACLDW 31.48%MAC LIMITSZFW FWD 22.90% AFT 40.45%TOW FWD 20.64% AFT 44.27%LDW FWD 22.58% AFT 42.45%TRIM BY CABIN AREAA39.B40.C25CAPTAINS INFORMATION/NOTESSTD WEIGHTS USED ADULT/84 CHILD/35 INFANT/0BLOCK FUEL/ 11715 ( 14508 LITER)LANDG FUEL/ 1710 ( 2118 LITER)TAXI TIME 10 MINTASK 3 EASA TCs A320-214 seriesType Certificate holderEngine type designation Modification TCDSN EASA. A.064 Issue 10, 08 June 2011Airbus CFM56-5B424251 (SAC combustor)TCDSN EASA. A.064 Issue 10, 08 June 2011AirbusCFM56-5B4, CFM56-5B4/PEngine intermix22 December 2012 Effective Date: Required as indicated, unless accomplished previously: Required Action(s) and Compliance Time(s): (1) Before next flight after the effective date of this AD, amend the applicable AFM to incorporate Airbus AFM A320 TR286 “AOA Blocked”, issue 1.0, inform all flight crews and thereafter operate the aeroplane accordingly.

(2) After modification of an aeroplane by replacing AoA sensor conic plates with AoA sensor flat plates in accordance with Airbus approved aeroplane modification instructions, the operational procedure as required by paragraph (1) of this AD is no longer applicable and shall be removed from the AFM of that aeroplane.

Contact Airbus to obtain the necessary approved modification instructions. EASA B737-700Maximum Certified Masses: 737-700*737-700 IGW** Taxi and Ramp 155,000 lbs. 70,307 kg, 171,500 lbs. 77,791 kg. Take-off 154,500 lbs. 70,080 kg. 171,000 lbs. 77,564 kg. Landing 129,200 lbs. 58,604 kg. 134,000 lbs. 60,781 kg. Zero Fuel 121,700 lbs. 55,202 kg. 126,000 lbs. 57,153 kg Fuel Tank FlammabilityReduction System (FRS): Aircraft which have made their first flight after 1 January 2012 must be equipped with a fuel tank Flammability Reduction System (EASA SIB 2010-10)Flammability Reduction Systems have been installed on aircraft line numbers 1820 and 1831 in December 2005, and then since mid-2008 on aircraft line number 2517, 2620 and on. This system shall remain installed and operative and can only be dispatched inoperative in accordance with the provisions of the MMELTask 4 ELEVATION = 0 (FT): A320-214/CFM56-5B4 : :: SLOPE = +0.00 (% ) : DATED 14 FEB 2013 21:43 UTC: ALL WEIGHTS IN: : T. O.R. A.

= 2500 (M ) : : KILOGRAMS (KG): : T. O.D. A.

= 2500 (M ) : AIR COND OFF: :: A. S.D. A. = 2500 (M ) : ANTI ICE OFF: NOT FOR: : LENGTH = 2500 (M ) : RUNWAY COND DRY: OPERATIONAL USE: : WIDTH = 45 (M ) : QNH 1013.25 HPA: :ELEVATION = 100 (FT): B737-700/CFM56-7B22 : :: SLOPE = +0.00 (% ) : DATED 24 APR 2013 18:38 UTC: ALL WEIGHTS IN: : T. O.R. A. = 2400 (M ) : : KILOGRAMS (KG): : T. O.D. A.

= 2400 (M ) : AIR COND ON: :: A. S.D. A. = 2400 (M ) : ANTI ICE OFF: NOT FOR: : LENGTH = 2400 (M ) : RUNWAY COND DRY: OPERATIONAL USE: : WIDTH = 45 (M ) : QNH 1013.25 HPA: Task 6FINDINGS AND RECOMMENDATION Airbus A320-214 is an aircraft manufactured by Airbus Company. The company has received 6,210 orders and so far it has delivered 3,274 between 1997 and 2012. By December 2012, the company delivered 82 aircrafts. The table below shows dimension of the plane.

The overall length of the plane is 37.57m. The drawings below show the illustrations of the A320-214 aircraft. The drawings show the front view, top view and side view of the aircraft.

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