Phenom Limits & SOPs 5.0 Inc Flashcards
Max Operating Altitude
41,000 PA
Max Landing Gear Operation V LO
180 KIAS
(250 KIAS Emergency)
Max Landing Gear Extended V LE
275 KIAS
Min Control Speed - T/O
V MC
97 KIAS
Min Control speed - landing
V MC
86 KIAS
(97 KIAS Icing)
Max Operating Speed
V MO / M MO
Up to 28,000ft
275 KIAS - 0.70M
Max Operating Manoeuvring Speed
Vo
186KIAS
Max flap extend Speed
V FE
(1-4)
Flap 1 - 200 KIAS
Flap 2 - 160 KIAS
Flap 3 - 160 KIAS
Flap 4 - 145 KIAS
Max Alt Flap Extend
YD Operating: 15,000 ft
YD Inoperative: 12,000 ft
Max Tyre Ground Speed
139 Kts
Max time @ max thrust
10 mins
Max time @ TOGA
5 minutes
MAX ITT
Max thrust: 845°C
TOGA/CONTCLMB: 830°C
MAX N2 (%)
100.4 %
MAX ITT Start
830°C
830 - 950°C for 5 seconds
Minimum oil temp for engine start
-40°C
Normal Oil Temp range
14 - 130°C
Max Oil Pressure
170 PSI
170 - 250 PSI allowed up to 500 seconds
Start motor attempts vs cool down (1-4)
Attmpt 1: 1 min cool dwn
Attmpt 2: 1 min cool dwn
Attmpt 3: 15 min cool dwn
Attmpt 4: 30 min cool dwn
Min BAT VOLT for eng start
24 V
Min GPU V to charge the BATS
27 V
Max GEN load on ground
250 A each
Max GEN load in flight above 34,000’
250 A each
Max GEN load in flight below 34,000’
300 A each
Max fuel capacity
1292.8 Kg
Total unusable fuel
20 Kg
Max imbalance between tank
100 Kg
Min Fuel Tank Temp
– 37°C
Max Fuel Tank Temp (flight)
+ 80°C
Max Fuel Tank Temp (ground)
+ 52°C
Max Diff. Pressure
8.3 PSI
Max Diff. Overpressure
8.6 PSI
Max Diff. Neg Pressure
- 0.4
Max Diff. Pressure (TO/Landing)
0.2
Max TO/Landing Tailwind Component
10 Kts
Max x-wind component TO/Landing (inc. gusts)
25 Kts
Air conditioning system operation on the ground requires 1 of either 2 criteria to be met:
1) GPU must be used
or
2) Both Generators operating
YD to be engaged above __,___ ft and/or above ___ Kts
Above 25,000ft and/or 250 Kts
Autopilot / YD min engagement height (duel eng)
500 ft AGL
Autopilot / YD min engagement height (OEI)
1000 ft AGL
Autopilot / YD min use height
195 ft AGL
Autopilot / YD Altitude Loss
54 ft
Spin??
nah lol
Max AoB
60°
Manoeuvring at AoAs near the stall, or full application of rudder, elevator and aileron is not to occcur above __ speed.
Vo = 186 KIAS
G-force limitations with flaps up
-1.2 to +3.27 g
G-force limitations with flaps Extended
0 to +2.00 g
Runway Slope range
-2% to +2%
Permissible runway surfaces
Paved
Permissible runway conditions (3)
Dry / Wet / Contaminated
Can we trample arrestor cables?
Nah
Instrument approach category?
B
Min temp for WINGSTAB operation:
– 40°C
Min airspeed for WINGSTAB swith activation (Flap 0 and Gear up)
150 KIAS
Min airspeed for Holding (Flap 0 and Gear up)
160 KIAS
Following an aborted TO over 80 KIAS, min brake cooling time is:
50 mins
Max tailwind for Engine Start
10 kts
Local TRG flight Min Oxy PSI
1050
Minimum Significant Weather avoidance (nm)
10nm
Take-brief mnemonic:
T Type of TO
S Speeds from Tape
S Standard PM duties
R Rejection reasons
E Emergency intentions post V1
D Departure briefed
S Safety Alt, TA
Max landing weight
4480
Stabilised approach criteria
Maintaining runway centreline
On desired approach path
Between Vref and Vref +20
Appropriate trim in all axes
In briefed landing config
Must call stab by 200ft
EFATO / SEFATO Accel Height
As calculated from planning tools. MIN 400 ft AGL
(1000ft requested only in FFS)
TOGA ‘event’ Limit?
12 TOGA Events / per engine / per sortie
Post Abort Actions?
Inform crew
F - FRCs
A - After Ldg Cxs
B - Brake Cooling Time
Consider Vacating - ATC
Final 1000ft Climb AP Engaged Work Cycle
A - Altimeter - correct setting
A - ALT SEL Active, ALT armed
A - Air Speed
NITS message format?
N - Nature of emergency
I - Intent
T - Time
S - Special instructions / Services required
FL above which Windshields must be selected ON
Above FL150
Min distance to go to initiate GA?
3000ft
Target Storm Penetration Speed
180 KIAS
