PPC Flashcards
When must PPC be “re-computed”
Increase of:
FAT: +5ºC
PA: +500ft
WT: +200 lbs
How do you convert kg to lbs ?
Kg * 2.205
MAX PA & TEMP will be used for all computations excepts
GO/NO GO TQ
Predicted hover TQ
How is “Zero fuel weight” on the PPC computed ?
Aircraft GWT - Total fuel weight
GWT - Fuel weight= zero fuel weight
Why are we concerned with:
if MAX TQ avail AEO is below/above 97%
If it’s below (high PA): We can never achieve 97% (MAX TQ)
If it’s above (low PA): We can easily exceed 97% and will have to be careful when raising the collective
During Hover PWR check, if “3ft-HOVER-TQ” is above/ below go-no go what does this mean to us?
1. IGE above
2. IGE below
3. OGE above
IGE above 3’ TQ Over max gross weight
IGE below 3’ TQ below max gross weight
OGE above 3’ TQ Aircraft is to heavy to perform OGE
What is the significance of knowing
“MAX GWT OGE w/MCP”
If actual aircraft weight is above this number you can expect to be in the 5 min PWR T/O range (>8.5 FLI) while performing OGE maneuvers
1% TQ is approx. ____ lbs
90 lbs
What is the significance of knowing
“H/V altitude (AGL)”
Hovering OGE (0 airspeed)
At or above this altitude: Safe landing expected after Single engine failure
Below this altitude: Safe landing NOT to be expected after Single engine failure (avoid+stay minimum time)
CRUISE
What A/S + TQ will you use for:
1. Staying on stations as long as possible
2. Climb as fast as possible
- Max endurance
- MAX TQ available + 45kts (Vx) to 65kts (Vy)
OBS IAS > 65 KIAS = OVER TQ
What’s the significance of
“OEI IAS - min/max”
Minimum: When doing practice OEI landings attempt to hold this airspeed with max FLI (close to touchdown speed)
Maximum: This airspeed you can expected when obtaining 12 FLI (obs vne OEI 110 kts)
When does arrival data have to be computed ?
FAT: +5ºC
PA: +500ft
Weight: +200 lbs
Why is DA important ?
It determines the aircrafts performance
ATM TASK
Compute PPC values:
Weight ± ?
Fuel flow ± ?
Airspeed ± ?
TQ ± ?
Weight ± 22 kg / 50 lbs
Fuel flow ± 50 lbs/hr
Airspeed ± 5 kts
TQ ± 2 %