General Flashcards
What are Icing Conditions?
How do we set up the Plane?
<10C AOT & Visible Moisture
Prop Heat ON, Boots ON, Inertial Sep. OPEN
Icing Limitations & Vspeeds
No Flight into FZ precip or Severe Icing
All Ice systems must work;
105- Landing
135- Flaps 0 climb
145-175 Holding speed
De-Ice Boots Description and Limits
On leading edge of Wings and Horizontal Stabilizer.
5 sections: H-Stab, Lower Inner, Upper Inner, Lower Outer, Upper Outer
Cycle: 8 secs per section = 40 secs full cycle, then repeat depending on mode
Modes OFF/3 Min/ 1Min
OAT limit -40C to 40C
Wind Shear
To and Land N/A when RWY specific alert issued
+/- 15kts Execute Memory Item
PCL- Full
Flaps 30 or less
AOA-Centered
De-Ice and Anti-Ice Fluids
Can use type 1-4
Type-1 Deice. Must be applied hot. Applied everywhere (excepts intakes and windshield)
Type-4 Anti-Ice: Will not remove ice, may only be applied after Deice. Applied to airfoils only.
Take off with Pusher Ice Vspeeds if type 4 applied
Fuel Type
Jet-A, Jet A1, Jet-B, JP-4
Must use PRIST (Antifreeze)
6.8lbs/Gal @ 15C
quick convert lbs to Gal
drop last decimal and add 50%
ex: 500lbs = 75 Gallons
Overwater OPs
Lifevest with Light for all occupants (under seat)
91K - Liferaft required when 100NM or 30mins from shore (whichever is less)
135 - Must have liferaft, Must remain in glide dist during cruise.
Flight in Heavy Precip
Inertial Sep. Open
Ignitors ON
Precision Approach Mins.
1800 RVR
200 AGL
Climb speeds
180kts @ Sea Level
decreases 10kts per 5000ft.
160 @ 10000
140 @ 20000
Passenger Oxygen
Switch must be in AUTO with Passengers
flow will start at 13500 Cabin ALT
7 masks (6 cabin, 1 lav)
Prop Heat
Electrical.
Switch is ON/OFF
3 modes dependant on OAT
>0C OAT - STBY
0Cto-16C OAT cycle (45-odd/45-evn/90-off)
< -16C OAT cycle (90-odd/90-even)
Ice Protection Components
Prop Heat
Boots
Probe and AoA Heat
Windshield heat
Inertial Seperator
Intake Lip Heat (always ON)
Aircraft Dimensions
14’ H
47’3” L
53’4” W
14’10” Wheelbase
39’ Turning Radius
Stabilized Approach
Fully Configured (flaps and gear)
& Stabilzed (Power, speed, descent) by:
1000’ IFR
500’ VFR
Circling App. (higher of 500agl or Mins)