FLYTECH AVIATION ACADEMYDGCA PAPER II MOCK TEST II1. When a manufacturer designs an aircraft who certifies it ?a. CAAb. FAAc. Either a or bd. FAA since 19582. Which of the aircrafts among the following required to be weighed and have their centre of gravity calculated every three years ?a. All general aviation airplanes b. Air taxi & charter twin engine airplanes operating under (14CFR) part 135.c. As in b or airplane with a seating capacity of 20 or more d. As in a or airplane with a maximum payload of 6000 lbs or more.3. MTCS a. The datum once considered must not be changed during the life of the aircraft.b. Aircraft weight and balance information are contained in Type Certificate Data Sheet which also includes the aircraft equipment list.c. Moment is the product of weight multiplied by its distance from C.G.d. None of the above.4. Which among the following produces a negative moment ?a. Weight being added aft of the datumb. Weight being removed forward of the datumc. Weight being added forward of the datumd. None of the above5. The center of gravity of an aircraft is :a. A point about which the nose heavy and tail heavy moments are exactly equal in magnitude.b. A point at which if the aircraft is suspended would have no tendency to rotate in either a nose-up or nose-down attitude.c. A point about which the weight of any airplane or an object is concentrated.d. All the above6. The heaviest weight an airplane can be loaded to without having any usable fuel in the tank :a. Maximum zero fuel weightb. Maximum ramp weightc. Maximum landing weightd. Maximum take off weight7. The empty weight is the weight supplied by a manufacturer which do not include any optional equipment that might be installed in a particular aircraft:a. Basic empty weightb. Standard empty weightc. Licensed empty weightd. None of the above

8. The useful load of an aircraft consists of :a. Fuel , baggage and passengers.b. Fuel , baggage, pilot, copilot and passengers.c. As in b and equals to sum of payload and fueld. None of the above9. If the total moment counts to 3400 in-lb and the total weight is 495 lbs determine its C.G :a. 6.87b. 5.87c. 6d. 5.5710. What are the possible sources of weight and balance data ?a. Aircraft specifications b. Aircraft operating limitations c. Aircraft flight manuald. All the above11. The weight and balance information found in Type Certificate Data Sheet includes :a. Maximum weightb. Fuel capacityc. Amount of fuel in empty weightd. All the above12. Aircraft empty weight includes :a. Weight of fully filled hydraulic reservoirs b. As in a & Weight of fully filled oil tanksc. As in a & Weight of fully filled water and waste tanks d. None of the above13. Given are the conditions for a loaded aircraft :Aircraft loaded weight = 3,034 lbsDistance out of limit = 0.6How much temporary ballast should be added in the baggage compartment which is located at 39 from the forward C.G limit ?a. 46.68b. 45.234c. 46d. 64.6814. In considering the forward weight and balance check the parameters considered are:a. Aircraft empty weight and C.Gb. As in a & the maximum weight added ahead of the forward C.G limitc. As in b & the maximum weight added rearward of the forward C.G limitd. As in a & the minimum weight added ahead of the forward C.G limit

15. If the weight of the loaded aircraft decreases where the rearward C.G limit is not affected :a. The C.G range gets smallerb. The C.G range gets largerc. Either of the above 16. Which of the following is not contained in type certificate date sheeta. Minimum fuel grade to be usedb. ADSc. Location of the datumd. Control surface adjustment17. Ballast is used fora. Bringing the C.G within C.G rangeb. Leveling the lateral arm on central pointc. Both a & bd. None18. MTCS regarding leveling of a/c :a. Lateral leveling of H/A is more critical than L/Ab. Jacking points are located on longitudinal axisc. Leveling is always done on longitudinal axisd. Leveling of lateral point is always done on longitudinal axis19. When weighing an aircraft :a. The brakes should be appliedb. The brakes should be released to avoid side loadsc. As in b & the tare weight should be deducted from the observed weight.d. None 20. Determine the %age of 80 MAC if the datum is located 130 from the leading edge & EWCG is 170 from datum.a. 25%b. 50%c. 88.83%d. None