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105-MAGS > Prefect limitations Aug 21 > Flashcards

Prefect limitations Aug 21 Flashcards

1
Q

VMO (Max Operating Speed)

A

238

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2
Q

MMO (Max operating Mach Number

A

0.45MN

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3
Q

V LOE (Max speed landing gear oppression extend)

A

182

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4
Q

V LE (Max speed landing gear extend)

A

182

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5
Q

VO (Aerobatic) (Max manoeuvre speed up to 1440kg AUM)

A

164

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6
Q

VO (Utility) (Max manoeuvre speed 1440 to 1515 kg AUM)

A

143

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7
Q

VFE - T/O (Max speed flaps extended at take off position)

A

151

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8
Q

V LOR (Max speed landing gear operation retract)

A

137

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9
Q

VFE (Max speed flaps extended beyond take off position)

A

114

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10
Q

Power lever must not be retarded below __ during flight

A

Flight Idle

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11
Q

Max airspeed to apply reverse thrust during landing

A

80

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12
Q

Min airspeed for use of Reverse thrust during landing

A

40

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13
Q

Take off and landing cross wind component limitations

1) Take off and landing ___
2) maximum crosswind for break release take off __
3) flaps should be up in crosswinds grater than __

A

25
20
20

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14
Q

Recommended cruise airspeed during severe turbulence?

A

140-180

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15
Q

Max opening speed of the canopy in flight

A

110

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16
Q

Max speed with canopy open in flight

A

120

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17
Q

Max take off AUM

A

1515

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18
Q

Max landing AUM

A

1515

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19
Q

Max aerobatics AUM

A

1440

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20
Q

Max zero fuel AUM

A

1370

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21
Q

Min flying AUM

A

1170

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22
Q

Max baggage compartment Mass

A

50kg

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23
Q

Pitch attitude limitations, when fuel tank selector in emergency transfer
Max nose up ___
Max nose down ___

A

15

10

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24
Q

Aerobatic (<1440kg) max G limits

A

-4 to +6

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25
Utility (<1515) G limits
-1.7 to +4.4
26
Flaps down max positive G Flaps down min G
+3.8 0
27
Max OAT on the ground
+38c
28
Max OAT
ISA + 23c
29
Min OAT
-54c
30
Reduced power - OAT operating limitation minimum
ISA - 15c
31
OAT <4c in visible rain or moisture
P/S Heat - On | Comp intake - Both
32
What must fuel contain when OAT is below 4c
FSII
33
Min battery voltage for engine start
24v
34
Max transient TRQ (10 Seconds)
115%
35
Max T/O Power TRQ (5 min at T/O) cumulative per sortie
111%
36
Max continuous TRQ
92%
37
Max engine start TOT
927c (10 seconds over 810c)
38
Max transient TOT
899c (6 seconds over 810c)
39
Max T/O power TOT
810 (5 min at T/O, cumulative per sortie)
40
Max continuous TOT
752c
41
Taxi and landing might limitation OAT > +38c =
Max 40 minutes (min 30 mins cool time)
42
Max transient limit (Propeller RPM)
2233 N2 (15 seconds max above 2130 N2)
43
Max continuous speed of propeller RPM
2132
44
Max static ground ops propeller RPM
1850 N2
45
N2 must not be allowed to stabilise within the ___
N2 speed avoidance range
46
The N2 speed avoidance range is
Stabilised for longer than 1 second between 1523 and 1786 RPM with more than 20% TRQ
47
Speed avoidance range applied in both
Forward and reverse thrust
48
Accumulated time spent in the N2 speed avoidance range must be recorded in __
The engine logbook
49
Gas generator RPM Max transient N1 Max continuous N1
106% N1 (max 15 sec >105%) | 105% N1
50
``` Oil pressure Max transient (cold weather / engine start) ```
150 PSI
51
Oil Pressure max
130 PSI
52
Oil pressure min at an N1 greater than 94%
120 | 105 (Beta)
53
Oil pressure min at N1 85% to 94%
``` 90 PSI 75 PSI (Beta) ```
54
Oil pressure N1 <85%
``` 50 PSI 35 PSI (Beta) ```
55
Oil temperature max limit at TRQ <40%
107c
56
Oil temperature Max transient TRQ >40% (5min)
107c
57
Oil temperature at max continuous TRQ >40%
82c
58
Min oil temperature
0c
59
Min oil temperature before starting
-40c
60
Total Fuel Capacity
282.7kg
61
LH collector tank capacity
16.8kg
62
Unusable fuel left wing
6.3kg
63
Unusable fuel right wing
1.4kg
64
Usable fuel
275kg
65
Max tank asymmetry
45.3kg
66
Max fuel in each wing for aerobatics
115kg
67
Max fuel pressure
25 PSI
68
Min fuel pressure
12 PSI

105-MAGS (4 decks)

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