Prefect Limits Flashcards

1
Q

Max Take Off AUM

A

1515

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2
Q

Max Landing AUM

A

1515

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3
Q

Max AUM for Aerobatics

A

1440

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4
Q

Max Baggage Hold Mass

A

50

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5
Q

Max Positive g Aeobatic

A

+6

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6
Q

Maximum Negaive g Aerobatic

A

-4

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7
Q

Max Positive g Utility

A

+4.4

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8
Q

Max Negative g Utility

A
  • 1.7
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9
Q

Maz angle of bank Utility

A

60°

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10
Q

Max Positive g flaps down

A

+3.8

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11
Q

Minimum g flaps down

A

0

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12
Q

Max Operating speed Vmo

A

238

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13
Q

Max Landing Gear extension Speed

A

182

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14
Q

Max Speed with Gear extended

A

182

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15
Q

Max Manoeuvre speed - Aerobatic

A

164

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16
Q

Max Manoeuvre speed utility

A

143

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17
Q

max speed flaps at take off

A

151

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18
Q

Max speed landing gear retraction

A

137

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19
Q

Max speed flaps beyond take off

A

114

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20
Q

Marking for: 115% Max transient TQ (10secs)

A

not marked

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21
Q

Marking for: 111% Max Take off power TRQ (5 mins at T/O)

A

Red line above yellow

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22
Q

Marking for: 92% Max continuous TRQ

A

Top of green

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23
Q

Marking for: 927° Max engine start TOT

A

Red Diamond

24
Q

Marking for: 899° Max transient TOT

A

Red arrow

25
Q

Marking for: 810° Max T/O Power TOT (5 mins)

A

Red line above yellow

26
Q

752° Max Continuous TOT

A

Top of green

27
Q

Marking for: 106% N1 Max Transient

A

Red arrow

28
Q

Marking for: 105% N1 max continuous N1

A

Red Line

29
Q

Marking for: 2132 rpm Max Continuous N2

A

Red line

30
Q

Marking for: 1850 rpm Max N2 - crosswind >10kt

A

not marked

31
Q

Marking for: N2 speed avoidance range

A

yellow band

32
Q

Max fuel asymmetry

A

45.3 kgs

33
Q

Max Fuel pressure

A

25psi

34
Q

min fuel pressure

A

12 psi

35
Q

min lamding fuel on QTY gauge

A

25 kgs

36
Q

Max AUW aerobatics

A

144p

37
Q

Aerobatics fuel tanks selector must be:

A

LEFT

38
Q

Aerobatics: Fuel Transfer Pump must be

A

not operating

39
Q

max fuel in each tank for aeros

A

115 kg

40
Q

Max time in pitch attitude in excess of 45 degs, inverted ot wing down or knife edge flight?

A

30 seconds

41
Q

How long must aircraft be flown at positive g, pitch less than 45, following inverted/wing down floght?

A

For atleast the same time spent in restricted attitude

42
Q

Max no of turns in a spin

A

8

43
Q

Pitch limitations with Emergency transfer

A

15 degs nose up

10 degs nose down

44
Q

Engine start cooling periods

A

start 1. starter on 30s, cooling 1 min
start 2. starter on 30s, cooling 1 min
start 3. starter on 30s, cooling 30 mins

45
Q

How long is normal start cycle before starter diengages at 58% N1

A

15 secs

46
Q

Max time to BLOW engine if tot more than 150

A

15 secs

47
Q

When must power lever not be retarded below FI?

A

during flight

48
Q

Airspeed range Landing REVerse thrust

A

40-80 KIAS

49
Q

Take off and landing crosswind limitations

A

25 kts

50
Q

max crosswind for brake release take off

A

20 kts

51
Q

take off. flaps up in crosswinds above:

A

20 kts

52
Q

severe turulence airspeed

A

140-180

53
Q

when can canopy be open or unlocked in flights

A

in emergency conditions

54
Q

max canopy opening speed

A

110

55
Q

max speed canopy open

A

120

56
Q

ESI. Flight in IMC not permitted with:

A

Amber battery synbol

Amber or Red X over the battery symbol

CAL DUE message by battery symbol

57
Q

in visible mosityre or rain, what temp must:
P/S Heat ON
Comp Intake BOTH

A

4 degs