53 What is the maximum baggage weight that can be loaded on the aeroplane so that the center of gravity remains within limits?(Fig FPP07)
Empty Weight = 1350 lb moment(/1000) = 51,5., Pilot and front passengers = 250 lb, Rear Passengers =400lbs, Fuel = (30

54 calculate the moment/1.000 of the following aircraft and check if it is loaded within the CG envelope limits.(Fig FPP07)], Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 310 lb. Επιβάτ

55 What is the maximum amount of fuel which can be loaded on the aeroplane before take off, so that the total moment remains within the envelope limits? (Fig FPP07)]. Βάρος κενό/ Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/P

56 Calculate the total moment and check if it is within the envelope limits. (Fig FPP07)]. Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 340 lb. Επιβάτες πίσω/Rear Passengers = 310lbs.

57 Calculate the CG position and check if it is located within the envelope limits.(Fig FPP07)]. Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 380 lb. Αποσκευές/Baggage = 45 lb. Καύσιμο/

110 Consult Fig.4. Refering to this graph, the flight for maximum range in a piston engined aircraft is achieved by flying:

114 (Refer to Fig.8). What is the effect of a temperature increase from -4?C to +10°C on the density altitude if the pressure altitude remains at 5,000 feet?

115 (Refer to Fig.8). What is the effect of a temperature increase from +4?C to -15°C on the density altitude if the pressure altitude remains at 10,000 feet?

116 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22" at standard temperature.

117 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,820 feet MSL with an altimeter setting of 30.58" at standard temperature.

118 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................29.25"
Runway temperature...........................................+27°C
Airport elevation......................................5,250 ft MSL

119 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................30.15"
Runway temperature........................................... -1°C
Airport elevation......................................4,610 ft MSL

120 (Refer to figure 8.) Determine the pressure altitude at an airport that is 4,563 feet MSL with an altimeter set¬ting of 29.96".

121 (Refer to figure 8.) What is the effect of a temperature increase from -1?C to 10°C on the density altitude if the pressure altitude remains at 3,000 feet MSL?

122 (Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97".

123 (Refer to figure 8.) Determine the density altitude for these conditions:
Altimeter setting...................................................30.35"
Runway temperature........................................... -4°C
Airport elevation......................................3,894 ft MSL

124 (Refer to Fig.9) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

125 (Refer to Fig.9) Determine the maxi¬mum wind velocity for a 45° crosswind if the maxi¬mum crosswind component for the airplane is 25 knots.

126 (Refer to Fig.9) Determine the maxi¬mum wind velocity for a 50° crosswind if the maxi¬mum crosswind component for the airplane is 23 knots.

127 (Refer to Fig.9) What is the maximum wind velocity for a 30? crosswind if the maximum crosswind component for the airplane is 12 knots?

128 (Refer to Fig.9) What is the maximum wind velocity for a 35 ? crosswind if the maximum crosswind component for the airplane is 17 knots?

129 (Refer to Fig.9) With a reported wind of north at 20 knots, which runway (6, 29, or 32) is acceptable for use for an airplane with a 13-knot maxi¬mum crosswind component?