Phenom 100 Limitations Flashcards
1
Q
Maximum Takeoff Weight
A
10472lbs
2
Q
Maximum Ramp Weight
A
10516lbs
3
Q
Maximum Landing Weight
A
9766lbs
4
Q
Maximum Zero Fuel Weight
A
8444lbs
5
Q
Max Nose Baggage Compartment Weight
A
66lbs
6
Q
Max Wardrobe Compartment Weight
A
55lbs
7
Q
Max Lavatory Compartment Weight
A
33lbs
8
Q
Max Aft Baggage Compartment Weight
A
353lbs
9
Q
Max No of occupants
A
9
10
Q
Max No of passengers
A
7 including 1 lap child
11
Q
Vmo
A
275KIAS
12
Q
Mmo
A
0.70Mach
13
Q
Vo(maneuvering)
A
186KIAS
14
Q
Vlo
A
180KIAS
15
Q
Vlo (Emergency)
A
250KIAS
16
Q
Vle
A
275KIAS
17
Q
Vf (1)
A
200KIAS
18
Q
Vf (2) and (3)
A
160KIAS
19
Q
Vf (full)
A
145KIAS
20
Q
Max flap extension altitude
A
15000 Yaw Damper operative
12000 Yaw Damper inoperative
21
Q
Vmca
A
97KIAS
22
Q
Vmc landing
A
86KIAS
23
Q
Vmc landing icing conditions
A
97KIAS
24
Q
Max Tail Wind
A
10 Knots
25
Max demostrated crosswind
17 knots not limiting
26
Max Tyre Speed
139 KIAS
27
Minimum oxygen pressure for dispatch
730 PSI(but consult chart in AFM for min based on no of pax for charter or rpt ops)
28
Oxy masks extend in PAX AUTO at
14500 +250 -500 feet
29
Maximum runway slope
+/-2%
30
Electrical system operating voltage
28VDC
31
Battery voltage
24VDC
32
Min battery voltage for start
24VDC
33
GPU voltage range
26-29VDC
34
Min GPU voltage to charge batteries
27VDC
35
Max Generator load
250 AMPS but 300 AMPS permissible below FL340 in flight
36
Start/Generator disengage/engage speed
44% N2
37
ELT Battery replacement time
6 years or as required by the regulating authority
38
Total fuel capacity
2850lbs
39
Useable Fuel per tank
1403lbs
40
Unuseable Fuel per tank
22lbs
41
Max Fuel Imbalance
220lbs
42
Min Fuel Temperature
-37 Deg C
43
Max Fuel Temperature (Ground)
52 Deg C
44
Max Fuel Temperature (Flight)
80 Deg C
45
Max load limits
Flaps Up plus 3.27G Flaps Down plus 2G
46
Yaw Damper must be on
Above 25000 feet or above 250 KIAS
47
Static Wicks required for dispatch
12 (3 per aileron 2 on rudder and 2 per elevator)
48
Maximum Differential Pressure
8.3PSI
49
Maximum Negative Differential Pressure
-0.4PSI
50
Maximum Differential Overpressure
8.6PSI
51
Maximum Diff Press TO and LDG
0.2PSI
52
Starter Cycle Limits
60 Seconds Off
60 Seconds Off
15 Minutes Off
30 Minutes Off
53
Max ITT(SE)
845 Deg C
54
Max ITT TO/GA
830 Deg C
55
Max ITT Cont Climb
830 Deg C
56
Max ITT start
830 Deg C(892 for 5 seconds)
57
Max ITT Transient
830 Deg C
862 Deg C for 20 Seconds Normal and ATR mode
845 Deg C for ATR mode only
58
Max Thrust
Not intended for normal operations
59
Cold Start Idle Time
Idle Thrust for 3 minutes after oil reaches 14 Deg C
60
Engine Anti Ice
SAT/TAT plus 5 to 10 Deg C EAI must be on
SAT/TAT below 5 Deg C Windshield.Engine and Wing anti ice must all be on
Ice Formation (despite Temperature )
Windshield, Engine and Wing anti ice must all be on
61
Min Temperature to Operate Wing and Stabiliser Boots
-40 Deg C
62
Min Speed in Icing Conditions
150KIAS
63
Min Altitude to engage Auto Pilot (2 engines)
500 feet AGL
64
Min Altitude to engage Auto Pilit (1 engine)
1000 feet AGL
65
Min Auto Pilot altitude use (on approach)
195 feet AGL
66
Max Allowable Auto Pilot Altitude Loss
54 feet
67
Auto Pilot Use prohibited if
1. Severe Icing Conditions
2. Unusual Control force or deflection or unusually large control forces required to move flight controls
3. Indications of frequent autopilot retrimming during straight and level flight
68
Vra Turbulence Penetration (Not a Limitation)
230 kts at or below 28000'
230/0.59M above 28000'
SIGNS/OUTLET Switch......PED-BELTS/OFF
