O File C/Users/duron/Downloads/M7 Weight,and Balance Worksheet 1.pdf Wolght 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. An upgraded engine was installed at station -62 inches from the datum and weighing 185 pounds. (25 Points) Current aircraft weight and CG Weight lbs 998 Arm inches Moment ins/T000 C.G. nches 13.48 Basic Empty Weight before the modification Weighe, Moment and C G from speoiic acat Waight&Balance as ammended) (includes unusable fvel and fu o) Calculate the new weight of the aircraft and CG of the aircraft after modification: Aircraft Old Engine New Engine Total Final Basic weightF Final Aircraft CG 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 caiculated 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 instalied 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) pe here to search t eN @ Assi, i E75. DVX AP4 ETop. G54 |G8Log l@Taxp |MailEMai C File | C/Users/duron/Downloads/M7 weight and-Balance Worksheet ladf E01 |OSew | G an. F Emr | G Cak I.Wey: I 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 m pound seats located at station +71 were required to be removed. A new odified. Two 15 cabinet weighing 97 pounds was installed in place of the 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 1-1 Now Cabinet New Seat New Radio Equip, l Total -l: L 1 Final Basic weight Final Aircraft CG 3) An owner brought the aircraft into our hanger for an annual inspection. In addition to the inspection, the owner requested the aircraft weight and balance be verified. It was discavered that the aircraft was out of CG range The aircraft weighed 4954 pounds and the CG was caloulated to +30 5 inches of arm. The manual shows the CG should be within a range of +32 10 +42 1 inches. Ballast will have to be added to station +162 (arm) but you now will have to caicware the comet wight of the badast prior to adding it. (25 Points) instructions. Use the Ballast Formula which is explained ri pages 386 through 389 Shifting the CG } 10 calculate the weight ofthe File l C/Users/duron/Dornioads Mr-weight and-Baance worksheet pain Total Final Basic weight Final Aircraft CG 3) An aircraft weight and balance be venfied. It was discovered that the aircraft was out of CG range. The aircraft weighed 4954 pounds and the CG was calculated to +30.5 inches of arm. The manual shows the CG should be within a range of +32 to +42.1 inches Balast will have to be added to station +162 (am) but you now wil have 10 iare me correct we att ofthe balast prior to adding it (25 Points) Instructions: Use the Ballast Formula which is explained in pages 386 through 389 (Shifting the CG') to calculate the weight of the ballast to be added. You may use a calculator. This is also explained in the AMT General Handbook FAA FAA-H-8083-30A: owner brought the aircraft into our hanger for an annual inspection. In addition to the inspection, the owner requested the Total w. x dist, needed to shift CG Dist, between ballast and desired CG Ballast needed Show your work: Total Weight x Distance needed to shift CG Balast Weight needed Distance between Ballast and desred CG Type here to search O File C/Users/duron/Downloads/M7 Weight,and Balance Worksheet 1.pdf Wolght 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. An upgraded engine was installed at station -62 inches from the datum and weighing 185 pounds. (25 Points) Current aircraft weight and CG Weight lbs 998 Arm inches Moment ins/T000 C.G. nches 13.48 Basic Empty Weight before the modification Weighe, Moment and C G from speoiic acat Waight&Balance as ammended) (includes unusable fvel and fu o) Calculate the new weight of the aircraft and CG of the aircraft after modification: Aircraft Old Engine New Engine Total Final Basic weightF Final Aircraft CG 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 caiculated 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 instalied 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) pe here to search t eN @ Assi, i E75. DVX AP4 ETop. G54 |G8Log l@Taxp |MailEMai C File | C/Users/duron/Downloads/M7 weight and-Balance Worksheet ladf E01 |OSew | G an. F Emr | G Cak I.Wey: I 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 m pound seats located at station +71 were required to be removed. A new odified. Two 15 cabinet weighing 97 pounds was installed in place of the 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 1-1 Now Cabinet New Seat New Radio Equip, l Total -l: L 1 Final Basic weight Final Aircraft CG 3) An owner brought the aircraft into our hanger for an annual inspection. In addition to the inspection, the owner requested the aircraft weight and balance be verified. It was discavered that the aircraft was out of CG range The aircraft weighed 4954 pounds and the CG was caloulated to +30 5 inches of arm. The manual shows the CG should be within a range of +32 10 +42 1 inches. Ballast will have to be added to station +162 (arm) but you now will have to caicware the comet wight of the badast prior to adding it. (25 Points) instructions. Use the Ballast Formula which is explained ri pages 386 through 389 Shifting the CG } 10 calculate the weight ofthe File l C/Users/duron/Dornioads Mr-weight and-Baance worksheet pain Total Final Basic weight Final Aircraft CG 3) An aircraft weight and balance be venfied. It was discovered that the aircraft was out of CG range. The aircraft weighed 4954 pounds and the CG was calculated to +30.5 inches of arm. The manual shows the CG should be within a range of +32 to +42.1 inches Balast will have to be added to station +162 (am) but you now wil have 10 iare me correct we att ofthe balast prior to adding it (25 Points) Instructions: Use the Ballast Formula which is explained in pages 386 through 389 (Shifting the CG') to calculate the weight of the ballast to be added. You may use a calculator. This is also explained in the AMT General Handbook FAA FAA-H-8083-30A: owner brought the aircraft into our hanger for an annual inspection. In addition to the inspection, the owner requested the Total w. x dist, needed to shift CG Dist, between ballast and desired CG Ballast needed Show your work: Total Weight x Distance needed to shift CG Balast Weight needed Distance between Ballast and desred CG Type here to search