ppl flight test Flashcards
engine fire on ground
crank starter
hold brakes
if engine starts 1700 for 2 mins, then shutdown and inspect
if engine does not start:
full throttle
mixture ICO
keep cranking starter
fuel selector off
master off
mags off
check checklist
cabin fire
master off
close all vents
use fire extinguisher
vent cabin
land asap
check checklist
engine fire in flight
mixture ICO
fuel selector off
master off
close cabin heat and air
keep outside vent open
airspeed 100 KT
forced approach
check checklist
electrical fire in flight
master off
all other switches off
close all vents
use fire extinguisher
if fire gone: master on, slowly turn on other switches and radios, land as soon as practicable
if fire remains: forced approach
check checklist
engine failure on ground
throttle idle
brakes
flaps up
mixture ICO
mags off
master off
check checklist
engine failure takeoff
airspeed 80 mph
mixture ICO
fuel selector off
mags off
flaps as required
master off
check checklist
engine failure in cruise
airspeed 80 and carb heat hot
pick field
engine check no fire
cause check:
mixture rich
fuel selector both
mags cycle then both
primer locked
throttle idle
attempt restart
mayday
passenger briefing
shutdown engine:
mixture ICO
fuel selector off
mags off
flaps down
master off
unlatch doors
check checklist
wing fire
nav lights off
strobe lights off
pitot heat off
side slip away from burning wing
forced approach
how much fuel can we have in our tanks and how much is usable
42 total, 38 usable
oil capacity in sump vs total
8 qt in sump
9 qt total
Vx, Vy , Va , Vs , Vso (landing config) , Vno , Vne , Vr , Vglide , Vmax flaps, max cross wind, max takeoff weight
Vx = 68
Vy = 91
Va = 115
Vs = 50
Vso = 40
Vno = 142
Vne = 179
Vr = 60
V glide = 80
V max flaps = 100
max xw = 15
max takeoff weight = 2300 lbs
static RPM is between
2270-2370
max takeoff weight for normal vs utility
normal = 2300
utility = 2000
G load factor limits for normal vs utility catagory (with and without flaps)
normal: +3.8g -1.52g
normal with flaps: +3.0g
utility: +4.4g -1.76g
utiltiy with flaps: +3.0g
what to do if you encounter ice?
pitot heat on
turn around or descend to lower altitude (hopefully warmer)
cabin heat and defroster
full throttle = increase engine speed and limit ice build up on propellers
monitor RPM for intake ice
land ASAP
do NOT use flaps (because turbulent airflow hitting icy elevators is no bueno)
how to land when you have a flat main tire
approach normally and touchdown with good tire
check checklist
how can you tell you have a static port blockage?
what do you do to fix it
altimeter freezes at the last altitude
VSI remains zero
ASI: when climbing, ASI extra slow. when descending, ASI shows extra fast
pull alternate static source
check checklist
what does a fully and partially blocked pitot look like on your instruments?
fully blocked pitot:
ASI shows fast during climb and slow during descent
partially blocked pitot: ASI = 0
what do you do if your low voltage light illuminates in flight?
- avionics OFF
- master OFF then ON again
- if light turns off, you’re good to turn avionics on again and relax :)
- if light stays on (ammeter discharge - battery only)
- alternator OFF
- conserve battery (turn off non essential electronics)
- land as soon as practical
check checklist
what to do if you see excessive charge on ammeter?
alternator off
non essential electrics off
land as soon as practical
check checklist
landing with ice
increase landing speed due to icing conditions
flaps RETRACTED
left window open and slip for improved visibility
check checklist
low oil pressure and high oil temperature
use minimum power
land asap and expect engine failure
short field takeoff and landing procedures
takeoff: line up edge of runway, hold brakes, full power, check gauges, release brakes
landing: flaps up, back pressure and brake
soft field takeoff and landing procedures:
takeoff: back pressure, throttle idle, just rudder to get lined up. when lined up, keep back pressure and full throttle. after rotation, parallel until gain speed then Vy
landing: when flare, add 100 rpm power to slow descent rate, keep back pressure and roll down runway until stop
does certificate of airworthiness expire? explain
NO the CoA does not expire but to keep it valid you must follow MAPS
MAPS
maintenance schedule
ADs
POH G loading
Snags (defects)
certificate of registration invalid when
changes to purpose, address, owner, registration
accident/destroyed
something changes on your certificate of registration. how long do you have to update TC
7 days
day VFR equipment list
MAATE
mag compass
ASI
altimeter
time
engine gauges: oil temp, pressure, tachometer, fuel gauges
what type of ailerons do we have
frise = up-aileron has more drag
differential = goes up more than down
describe the engine
- lycoming model O320 engine that is 4 cylinder, horizontally opposed, air cooled, carbureted with a wet sump oil system
- 150 hp at 2700 rpm
describe the engine oil system
- wet sump oil system (stored below engine)
- the engine-driven oil pump sucks the oil from the sump to the filter (if the oil is hot, it goes to a cooler before the filter)
- from the filter, oil gets sent to various engine parts and excess oil returns to sump by gravity flow
how is the engine cooled?
cool outside engine: ram air enters cowling and directed to cylinders via fins
cool inside engine: oil
what is the purpose of the battery?
start the alternator
backup if alternator fails
uh oh, there’s impact ice around by air intake vent. what ever shall i do?
alternate air intake - from inside of cowling