10 FLIG. PER. EXAM. PREP.

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267 When an aircraft is in flight, to achieve a greater climb angle:

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268 The definition of gross weight is:

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269 Refer to the diagram (Fig.2). For the Utility category, what is the acceptable combination of both aircraft weight in pounds and moment arm in inches?

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270 Refer to the diagram (Fig.2). For the Utility category, what is the acceptable combination of both aircraft weight in pounds and moment arm in inches?

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271 Refer to the diagram (Fig.2). For the Utility category, what is the acceptable combination of both aircraft weight in Kilograms and moment arm in millimeters .Conversion formula: (lb-in) x 11.5 = (Kgr-mm)

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272 If an aircraft at maximum Take-off Weight (MTOW) is loaded in a manner that positions its C of G at or beyond its aft limit it will:

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273 An aircraft with a C of G out of its forward limit may experience that:

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274 If the angle of attack is increased from 4° to 8°:

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275 Taking off from a strip where the field length is critical and limits the take-off weight:

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276 (Fig.3) Calculate the rate of climb (VY) for an aircraft operating at 9000 ft with ΟΑΤ 0°.

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277 (Fig.3). Calculate the rate of climb (VY) for an aircraft operating at 7000 ft με ΟΑΤ 20° C.

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278 The length of a runway available plus the addition of the clearway is named:

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279 In a banked turn:

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280 One effect during the cruise of operating with partial flap extension would be:

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281 Lift being produced by the wing of an aircraft maintaining a constant true air speed(TAS) will:

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282 The speed at which the aircraft wheels leave the ground during take off is:

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283 The selection of take-off flap prior to an aircraft departure will:

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284 A wing evenly contaminated with only a small amount of ice will produce:

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285 The maximum demonstrated cross wind component for the aircraft is 11kt.Given a 16kt wind speed, by how many degrees can a runway heading differ from the wind direction before the surface cross wind component equals 11kt? See.Fig.9

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286 The maximum demonstrated cross wind component for your aircraft is 15kts. Given a 19kts wind speed, by how many degrees can a runway heading differ from the wind direction before the surface cross wind component equals 15kts. (Use CRP-1 or consult Fig. 9)

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287 Loading manifest sheet and C.G. envelope graph for Class "B" aircraft in passenger configuration, is given in Fig.6.
Front occupants……………………………..340 lb
Middle row occupants ………………….340 lb
Baggage comp. Zone "B"……………….200 lb
Fuel Loaded ...............................................58 USG
Trip Fuel ......................................................40 USG

Determine if take-off, landing mass and associated C.G.s are within limits and choose the correct answer.

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288 Loading manifest sheet and C.G. envelope graph for Class "B" aircraft in cargo configuration, is given in Fig.6.
Front occupants……………………………..200 lb
3rd & 4th seats pax…………………….missing
Baggage comp. Zone "A"……………… 520 lb
Baggage comp. Zone "B"……………… 300 lb
Baggage comp. Zone "C"……………… 100 lb
Fuel loaded.....................................................48 USG
Trip fuel ...........................................................44USG
Determine if take-off, landing mass and associated C.G.s are within limits and choose the correct answer.

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291 Determine from the "loading graph" in Fig.35, if aircraft's total moments are within envelope? (Max. MTOW 3600 Lb)
ITEM MASS (lb) TOTAL MOMENTS/1000 (lb-in)
BEM 2122 75.9
Pilot 270 -
Cargo "A" 300 -
Cargo "B" 340 -
Cargo "C" 320 -
Fuels[40USG] 240 -

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292 Determine from the "loading graph" in Fig.35, if aircraft can be allowed to take-off for max. MTOW of3600 lb?
ITEM MASS (lb) TOTAL MOMENTS/1000 (lb-in)
BEM 2122 75.9
Pilot 270 -
Cargo "A" 350 -
Cargo "B" 380 -
Cargo "C" 320 -
Fuels[40USG] 240