CLASS REVIEW 1 CLASS REVIEW Computerized Testing Services

CLASS REVIEW 1

CLASS REVIEW Computerized Testing Services • Prescott, Phoenix or other large cities or larger flight schools • CATS: 800 -947 -4228 • PSI: 800 -733 -9267 • You must have 2 forms of ID, 1 with photo

CLASS REVIEW Computerized Testing • You may bring and use: – – – A flight computer (electronic or E 6 B) Plotter A clear plastic sheet with 90º lines drawn on it A simple calculator (no memory) Pencils • Pencils and paper will be supplied

CLASS REVIEW Computerized Testing • • • 60 questions 3 hours maxium You may skip or defer questions You are allowed bathroom breaks If you are found cheating, you will be denied to retake the test for at least one year.

http: //www. faa. gov/training_testing/test_questions/media/FAA-CT-8080 -2 E. pdf CLASS REVIEW

CLASS REVIEW Contents

CLASS REVIEW

CLASS REVIEW 0 on top 315º just read the needle 90º 225º 360º 45º 180º 270º 135º

CLASS REVIEW Place heading on top bearing TO: 240° Heading: 035° bearing TO: 030° Heading: 120° bearing TO: 185° Heading: 320° bearing TO: 135°

Heading is on top CLASS REVIEW 210º just read the needle 190º 295º 200º

CLASS REVIEW Place 0 on top RB: 240° RB: 25° RB: 340° RB: 235°

CLASS REVIEW Basic ADF rule: Bearing to: Relative bearing: 0 on top heading on top

CLASS REVIEW ADF tracking into crosswind Needle must point almost up Needle points downwind Wind

CLASS REVIEW

CLASS REVIEW What is the maximum amount of baggage that can be carried when the airplane is loaded as follows? Front seat: 387 lb Rear seat: 293 lb Fuel: 35 gal A: 220 pounds. B: 45 pounds. C: 63 pounds.

CLASS REVIEW Item Empty Weight Front seats Rear seats Baggage Fuel Weight (lbs) 2015 Arm (inches) ---- 387 85 293 45 121 140 75 210 2050 2905 Total Max gross weight: 2950 Moment (lb-in/100) 1554 329 355 63 158 2459

CLASS REVIEW What is the maximum amount of baggage that can be carried when the airplane is loaded as follows? Front seat: 387 lb Rear seat: 293 lb Fuel: 35 gal A: 220 pounds. B: 45 pounds. C: 63 pounds. From our calculations: GW: 2950 Moment: 2459

CLASS REVIEW Upon landing, the front passenger (180 pounds) departs the airplane. A rear passenger (204 pounds) moves to the front passenger position. What effect does this have on the CG if the airplane weighed 2, 690 pounds and the MOM/100 was 2, 260 just prior to the passenger transfer? A. The CG moves forward approximately 0. 1 inch. B. The CG moves forward approximately 3 inches. C. The weight changes, but the CG is not affected.

CLASS REVIEW Item Front seats Weight (lbs) 204 180 Arm Moment (inches) (lb-in/100) 85 173 153 121 --- 247 173 400 ---204 Rear seats Front + Rear 84 Original 81 -227 2260 2033 2510 2690 GW A. The CG moves forward approximately 0. 1 inch. B. The CG moves forward approximately 3 inches. New GW C. The weight changes, but the CG is not affected.

CLASS REVIEW With the airplane loaded as follows, what action can be taken to balance the airplane? Rear seat occupants 411 lb Rear seat occupants 100 lb Main wing tanks 44 gal A. Add a 100 -pound weight to the baggage compartment. B. Fill the auxiliary wing tanks. C. Transfer 10 gallons of fuel from the main tanks to the auxiliary tanks.

CLASS REVIEW Item Empty weight Front seats Rear seats Baggage Main fuel Aux fuel Total Weight (lbs) Arm (inches) 2015 ---- 411 100 85 121 140 75 94 264 2790 Moment (lb-in/100) 1554 349 121 198 2222

CLASS REVIEW With the airplane loaded as follows, what action can be taken to balance the airplane? Rear seat occupants 411 lb Rear seat occupants 100 lb Main wing tanks 44 gal A. Add a 100 -pound weight to the baggage compartment. B. Fill the auxiliary wing tanks. C. Transfer 10 gallons of fuel from the main tanks to the auxiliary tanks. From our calculations: GW: 2790 Moment: 2222

CLASS REVIEW Item Weight (lbs) Arm (inches) Moment (lb-in/100) Empty 2015 ---1554 weight 349 Front seats 411 85 121 Rear seats 100 121 100 140 Baggage 140 153 198 264 204 Main fuel 75 114 60 56 107 Aux fuel 94 2362 2233 2904 2790 2890 2329 Total C. Transfer 10 gallons of fuel from the main tanks to the auxiliary tanks. A. Add a 100 -pound weight to the baggage compartment. B. Fill the auxiliary wing tanks.

CLASS REVIEW With the airplane loaded as follows, what action can be taken to balance the airplane? Rear seat occupants 411 lb Rear seat occupants 100 lb Main wing tanks 44 gal A. Add a 100 -pound weight to the baggage compartment. GW: 2890 MOM: 2362 B. Fill the auxiliary wing tanks. GW: 2904 MOM: 2329 C. Transfer 10 gallons of fuel from the main tanks to the auxiliary tanks. GW: 2790 MOM: 2233 C A B

CLASS REVIEW Calculate the moment of the airplane and determine which category is applicable. Empty weight: 1, 350 lbs MOM: 51. 5 Pilot & front passenger: 310 lbs Rear passengers: 96 lbs Fuel: 38 gal Oil: 8 qt MOM: -0. 2 A. 81. 2, normal category. B. 79. 2, utility category. C. 80. 8, utility category. 25 Pilot and Front Seat Rear Passengers Fuel: 228 lbs Passenger Moment = 11. 5 lb. Moment = 7 lb-in / 1000 Moment = 11 lb-in / 1000

CLASS REVIEW Item Empty Weight Front seats Rear seats Baggage Fuel Oil Weight (lbs) Moment (lb-in/1000) 1350 51. 5 310 11. 5 96 7. 0 228 15 1999 11. 0 -0. 2 80. 8

CLASS REVIEW From our calculations: GW: 1999 Moment: 80. 8 / 1000 A. 81. 2, normal category B. 79. 2, utility category C. 80. 8, utility category 27

CLASS REVIEW Quantity scale 10 index Minute scale 60 index How far will an How fast is an How long will it What climb rate Hour/minute aircraft travel in aircraft flying if take to climb take to fly do we need to scale 2 -1/2 minutes 43 minutes with it covers 38 km it covers 72 km 13, 000 feet at 280 km at 126 reach 8500 ft with a a groundspeed in 18 min? in 35 min? 500 fpm? kts? from 1500 ft in groundspeed of of 118 knots? 12 minutes? 98 knots? Quantity Time

CLASS REVIEW FINIS