The company flew an aircraft to Mobile Alabama for Maintenance, Repair, and Overhaul (MRO) service. The aircraft basic weight was 2886 and had a Moment calculated at 101673.78.
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The company flew an aircraft to Mobile Alabama for Maintenance, Repair, and Overhaul (MRO) service. The aircraft basic weight was 2886 and had a Moment calculated at 101673.78. While in the hanger the aircraft was required to be modified. Two 15 pound seats located at station +71 were required to be removed. A new cabinet weighing 97 pounds was installed in place of the seats (at station +71). Also at station +71, an upgraded seat weighing 20 pounds was installed. As part of the new modification, new radio equipment was installed at station +94 weighing 30 pounds. Reference textbook pages 382 – 385. (50 Points) Calculate the new weight of the aircraft and CG of the aircraft after modification: Aircraft 2886 * Not Used = 101673.78 Old seats New Cabinet New Seat New Radio Equip. Total * Not Used = Final Basic weight Final Aircraft CG
Adi S.
2) The company flew an aircraft to Mobile Alabama for Maintenance, Repair, and Overhaul (MRO) service. The aircraft basic weight was 2886 and had a Moment calculated at 101673.78. While in the hanger the aircraft was required to be modified. Two 15 pound seats located at station +71 were required to be removed. A new cabinet weighing 97 pounds was installed in place of the seats (at station +71). Also at station +71, an upgraded seat weighing 20 pounds was installed. As part of the new modification, new radio equipment was installed at station +94 weighing 30 pounds. (50 Points) Calculate the new weight of the aircraft and CG of the aircraft after modification: Aircraft __________*__________ = __________ Old seats __________*__________ = __________ New Cabinet __________*__________ = __________ New Seat __________*__________ = __________ New Radio Equip. _________*__________ = ___________ Total __________ = __________ Final Basic weight Final Aircraft CG
Supreeta N.
Weight and Balance Worksheet (You may use a calculator as needed) 1) During maintenance and modification of an aircraft, the engine was changed out to an upgraded engine package. The original engine weight was 175 pounds and was removed at Station -62. An upgraded engine was installed at station -62 inches from the datum line and weighing 185 pounds. Reference textbook pages 382 – 385. (25 Points) Current aircraft weight and CG: Weight lbs: 998 Arm Inches: Moment lb-ins/1000: C.G. Inches: 13.48 Basic Empty Weight before the modification (Weight, Moment, and C.G. from specific aircraft Weight & Balance, as ammended) (includes unusable fuel and full oil) Calculate the new weight of the aircraft and CG of the aircraft after modification: Aircraft 998 * 13.48 = Difference Old /New Engine * = Total * Not Used = Final Basic weight Final Aircraft CG
Sri K.
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