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)

24
Q

Max reverse torque

25
Max reverse ITT (*C)
760
26
Max reverse Np (RPM)
1650
27
Max reverse oil pressure (PSI)
90 to 135
28
Max reverse oil temp (*C)
10 to 105
29
(Note 1) 67P MAX CRUISE is limited to ___ PSI
36.95
30
(Note 2) Applies over a speed range of ___ to ___ Ng RPM.
50.7% to 61.4%
31
(Note 3) Oil temperature is limited to 10 minutes at ___ *C to ___ *C.
105 to 110
32
(Note 4) During steady state operation, operation from ___ to ___ RPM is permitted to allow for governing accuracy.
1670 to 1730
33
1. Stabilized operation of propeller on the ground between ___ and ___ RPM is not permitted.
350 and 950
34
2. 67P Gen 2 limited to ___ on the ground.
200A
35
3. Max fuel imbalance for takeoff:
3 LCD segments.
36
4. Max landing weight: ___ lbs. Max zero fuel weight: ___ lbs / ___ lbs (Trainer/EQ-EQ+)
9921, 9039, 9240
37
5. (Trainer) Max ramp weight: ___ lbs. Max T/O weight: ___ lbs.
10495, 10450
38
6. (EQ/EQ+) Max ramp weight: ___ lbs. Max taxi weight: ___ lbs. Max T/O weight: ___ lbs.
11400, 10979, 10,935
39
7. Above 10450 lbs, no ___ maneuvers, bank angle is limited to ___ maximum, make ___ transitions from climb or descent.
abrupt, 30*, slow
40
8. If landing above max landing weight, max touchdown descent rate is limited to ___ FPM.
300
41
MAX FLAP EXTENDED SPEED (VFE) <= 15*
163 KIAS
42
MAX FLAP EXTENDED SPEED (VFE) > 15*
130 KIAS
43
GEAR EXTEND/RETRACT SPEED (VLO)
177 KIAS
44
GEAR EXTENDED SPEED (VLE)
236 KIAS
45
MAX OPERATING SPEED (VMO)
236 KIAS (Trainer) 216 KIAS (EQ/EQ+)
46
In pusher ice mode with gross weight <= 9921/10450/10935 lbs: MAXIMUM FLAP EXTENSION
15* with de-ice boots 0* with de-ice boots
47
Pusher ice mode: MIN CLIMB SPEED, 0* FLAPS
130/135/145 KIAS
48
Pusher ice mode: MIN APPROACH SPEED, 15* FLAPS
108/111/114 KIAS
49
Pusher ice mode: MIN APPROACH SPEED, 0* FLAPS
134/140/145 KIAS
50
Crosswind: FLAPS 0*
30 KTS
51
Crosswind: FLAPS 15*
25 KTS
52
Crosswind: FLAPS 30*
20 KTS
53
Crosswind: FLAPS 40*
15 KTS
54
GENERATOR 1 RATING
28 V, 400 A
55
GENERATOR 2 RATING 67B/67P
28 V, 115 A/28V, 300 A
56
BATTERY RATING
24 V, 42 Ah
57
Engine automatic starting cycle shall be limited to the following intervals:
1. Sequence, 60 seconds OFF 2. Sequence, 60 seconds OFF 3. Sequence, 30 minutes OFF