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FTU > OLs > Flashcards

OLs Flashcards

1
Q

Takeoff max torque

A

44.34 psi

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2
Q

Takeoff max ITT (*C)

A

800/850

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3
Q

Takeoff max Np

A

1700 RPM

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4
Q

Takeoff oil pressure

A

90 to 135 psi

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5
Q

Takeoff oil temp (*C)

A

10 to 110

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6
Q

Max cont. climb or max cruise torque (Note 1)

A

36.95/44.34

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7
Q

Max cont. climb or max cruise max ITT (*C)

A

760/820

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8
Q

Max cont. climb or max cruise %NG

A

104

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9
Q

Max cont. climb or max cruise Np

A

1700 RPM

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10
Q

Max cont. climb or max cruise oil pressure (psi)

A

90 to 135

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11
Q

Max cont. climb or max cruise oil temp (*C)

A

10 to 105

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12
Q

Min idle max ITT (*C) (note 2)

A

750

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13
Q

Min idle %NG

A

50.7 ground idle, 64 flight idle

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14
Q

Min idle oil temperature (*C)

A

-40 to 110

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15
Q

Min idle oil pressure (psi)

A

60 min

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16
Q

Starting max ITT (*C)

A

1000 (5 sec limit)

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17
Q

Starting oil pressure (psi)

A

200 max

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18
Q

Starting oil temp (*C)

A

-40 min

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19
Q

Transient (20 sec limit) torque (psi)

A

61

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20
Q

Transient (20 sec limit) max ITT (*C)

A

870

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21
Q

Transient (20 sec limit) Np (RPM)

A

1870

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22
Q

Transient (20 sec limit) oil pressure (PSI)

A

40 to 200

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23
Q

Transient (20 sec limit) oil temperature (*C) (Note 3)

A

110 max

24
Q

Max reverse torque

A

34.25

25
Q

Max reverse ITT (*C)

A

760

26
Q

Max reverse Np (RPM)

A

1650

27
Q

Max reverse oil pressure (PSI)

A

90 to 135

28
Q

Max reverse oil temp (*C)

A

10 to 105

29
Q

(Note 1) 67P MAX CRUISE is limited to ___ PSI

A

36.95

30
Q

(Note 2) Applies over a speed range of ___ to ___ Ng RPM.

A

50.7% to 61.4%

31
Q

(Note 3) Oil temperature is limited to 10 minutes at ___ *C to ___ *C.

A

105 to 110

32
Q

(Note 4) During steady state operation, operation from ___ to ___ RPM is permitted to allow for governing accuracy.

A

1670 to 1730

33
Q
  1. Stabilized operation of propeller on the ground between ___ and ___ RPM is not permitted.
A

350 and 950

34
Q
  1. 67P Gen 2 limited to ___ on the ground.
A

200A

35
Q
  1. Max fuel imbalance for takeoff:
A

3 LCD segments.

36
Q
  1. Max landing weight: ___ lbs. Max zero fuel weight: ___ lbs / ___ lbs (Trainer/EQ-EQ+)
A

9921, 9039, 9240

37
Q
  1. (Trainer) Max ramp weight: ___ lbs. Max T/O weight: ___ lbs.
A

10495, 10450

38
Q
  1. (EQ/EQ+) Max ramp weight: ___ lbs. Max taxi weight: ___ lbs. Max T/O weight: ___ lbs.
A

11400, 10979, 10,935

39
Q
  1. Above 10450 lbs, no ___ maneuvers, bank angle is limited to ___ maximum, make ___ transitions from climb or descent.
A

abrupt, 30*, slow

40
Q
  1. If landing above max landing weight, max touchdown descent rate is limited to ___ FPM.
A

300

41
Q

MAX FLAP EXTENDED SPEED (VFE) <= 15*

A

163 KIAS

42
Q

MAX FLAP EXTENDED SPEED (VFE) > 15*

A

130 KIAS

43
Q

GEAR EXTEND/RETRACT SPEED (VLO)

A

177 KIAS

44
Q

GEAR EXTENDED SPEED (VLE)

A

236 KIAS

45
Q

MAX OPERATING SPEED (VMO)

A

236 KIAS (Trainer)
216 KIAS (EQ/EQ+)

46
Q

In pusher ice mode with gross weight <= 9921/10450/10935 lbs:
MAXIMUM FLAP EXTENSION

A

15* with de-ice boots
0* with de-ice boots

47
Q

Pusher ice mode: MIN CLIMB SPEED, 0* FLAPS

A

130/135/145 KIAS

48
Q

Pusher ice mode: MIN APPROACH SPEED, 15* FLAPS

A

108/111/114 KIAS

49
Q

Pusher ice mode: MIN APPROACH SPEED, 0* FLAPS

A

134/140/145 KIAS

50
Q

Crosswind: FLAPS 0*

A

30 KTS

51
Q

Crosswind: FLAPS 15*

A

25 KTS

52
Q

Crosswind: FLAPS 30*

A

20 KTS

53
Q

Crosswind: FLAPS 40*

A

15 KTS

54
Q

GENERATOR 1 RATING

A

28 V, 400 A

55
Q

GENERATOR 2 RATING 67B/67P

A

28 V, 115 A/28V, 300 A

56
Q

BATTERY RATING

A

24 V, 42 Ah

57
Q

Engine automatic starting cycle shall be limited to the following intervals:

A
  1. Sequence, 60 seconds OFF
  2. Sequence, 60 seconds OFF
  3. Sequence, 30 minutes OFF

FTU (6 decks)

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