aerodynamics

Question 1

SMACFUM

Answer 1

standard day
max power
aft cg
critical engine inop and windmilling
flaps and gear
up to 5 degrees bank
most unfavorable weight

Question 2

PAST

Answer 2

p-factor
accelerated slipstream
spiraling slipstream
torque

Question 3

service ceiling

Answer 3

both engines: max density that altitude that 100 fpm can be maintained
single engine: ax density altitude that 50 fpm can be maintained

Question 4

absolute ceiling

Answer 4

single/both engines: max density altitude that ANY climb can be maintained
drift down if above when an engine fails

Question 5

loading, balance, spin awareness

Answer 5

engines located on wings not nose -> more weight is father aft on twins -> CG is more aft -> more susceptible to flat spins