BF/Ops Flashcards

1
Q

Engine Fire During Ground Operations

A

THROTTLES - CUTOFF

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2
Q

Engine Fire During Flight

A

THROTTLE - IDLE

If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist:

THROTTLE - CUTOFF
ENGINE FIRE SWITCH - PUSH
BOTTLE ARMED SWITCH - PUSH

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3
Q

Smoke Or Fumes In Aircraft

A

OXYGEN MASKS - DON / 100%

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4
Q

Pitch Trim/Roll Trim/Rudder Trim Runaway

A

TRIM INT & A/P DISENGAGE SWITCH - PUSH AND HOLD

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5
Q

Low Cabin Pressure

A

OXYGEN MASKS - DON / 100%

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6
Q

Takeoff - Time Limit (Minutes)

A

5 (1) Time limit starts when throttles first advanced for takeoff thrust.

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7
Q

Takeoff -
Maximum Observed ITT °C

A

700

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8
Q

Takeoff - N2 %

A

96

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9
Q

Takeoff - N1 %

A

104

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10
Q

Takeoff - Oil Pressure (2) PSI

A

60 to 83

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11
Q

Takeoff - Oil Temperature (° C)

A

10 to 121

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12
Q

Maximum Continuous - Time Limit (Minutes)

A

Continuous

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13
Q

Maximum Continuous - Maximum Observed ITT °C

A

680

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14
Q

Maximum Continuous -
N2 %

A

96

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15
Q

Maximum Continuous -
N1 %

A

104

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16
Q

Maximum Continuous - Oil Pressure (2) PSI

A

60 to 83

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17
Q

Maximum Continuous - Oil Temperature (°C)

A

10 to 121

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18
Q

Idle - Time Limit (Minutes)

A

Continuous

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19
Q

Idle - Maximum Observed ITT °C

A

580

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20
Q

Idle - N2 %

A

52 (Min)

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21
Q

Idle - Oil Pressure (2) PSI

A

40 (Min)

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22
Q

Idle - Oil Temperature (°C)

A

-40 to 121

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23
Q

Starting (4) - Maximum Observed ITT °C

A

550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC

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24
Q

Starting (4) - Oil Temperature (°C)

A

-40 (Min)

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25
Q

Transient - Maximum Observed ITT °C

A

(720 2 SEC Max)

26
Q

Transient - N2 %

A

96

27
Q

Transient - N1 %

A

106

28
Q

Transient - Oil Pressure (2) PSI

A

95 for
90 SEC

29
Q

Transient - Oil Temperature (°C)

A

135 (Max)
(15 MIN Max)

30
Q

Notes
(2) Normal Flight: Normal oil pressure is ____ to ____ PSI at N2 speeds above ____%. Oil pressure below ____ PSI is undesirable and should be tolerated only for safe recovery of the flight, preferably at reduced power setting. Oil pressure below ____ PSI is unsafe.

A

60 to 83 PSI
60%
60 PSI
40 PSI

31
Q

Notes
(3) Under cold starting conditions, oil pressure between ____ PSI and ____ PSI is limited to ____ seconds.

A

83 PSI and 95 PSI
90 seconds

32
Q

Notes
(4) The ITT during ground starts should normally not exceed ____ °C.

A

550° C

33
Q

Normal hydraulic pressure ____ to ____ PSI

A

1350 to 1550 PSI

34
Q

Normal nitrogen pressure ____ to ____ PSI

A

1350 to 1650 PSI

35
Q

Normal oxygen pressure ____ to ____ PSI

A

1600 to 1850 PSI

36
Q

Min battery voltage for battery start

A

22 volts

37
Q

Max gen load prior to starting second engine

A

150 amps

38
Q

Motoring of the starter is limited to:
First, ___ seconds then ___ minutes cooling.
Second, ___ seconds then ___ minutes cooling.
Third, ___ seconds then ___ minutes cooling.

A

(1) 30 seconds, 5 minutes
(2) 30 seconds, 15 minutes
(3) 30 seconds, 60 minutes

39
Q

Emergency Fuel / Minimum Fuel

A

300 lbs / 500 lbs

40
Q

Maximum Fuel Imbalance - T.O./Touch & Go

A

100 lbs

41
Q

Max Fuel Imbalance - Landing

A

300 lbs

42
Q

Fuel crossfeed with 2 engine operating is limited to level flight with less than ___ lbs of fuel remains in the wing tank supplying fuel.

A

600 lbs

43
Q

Max Ramp Weight

A

16,300 lbs

44
Q

Max Takeoff Weight

A

16,100 lbs

45
Q

Max Landing Weight

A

15,700 lbs

46
Q

Extend flaps to 10 degrees

A

200 KIAS

47
Q

Extend flaps > 10 degrees

A

170 KIAS

48
Q

Flaps extended > 10 degrees

A

165 KIAS

49
Q

Aircraft is limited to ____ KIAS or ____ MACH, whichever is less.

A

330 KIAS
.78 MACH

50
Q

Landing Gear/Lights

A

200 KIAS / FL 200

51
Q

Wipers

A

200 KIAS

52
Q

Tire

A

165 Knots GS

53
Q

Max Tailwind

A

10 Knots

54
Q

Max Crosswind (Dry)

A

25 Knots

55
Q

Max Crosswind (Wet)

A

15 Knots

56
Q

Max Crosswind (Icy)

A

10 Knots

57
Q

Max Operating Altitude

A

FL 410

58
Q

Yaw Damper required operable for flight above FL ____

A

FL 280

59
Q

Do not use autopilot below ____ FT AGL

A

200 FT AGL

60
Q

Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___ ° C.

A

10° C

61
Q

To ensure proper wing anti-ice operation, the throttles must be kept at ___% N2 minimum.

A

70% N2 minimum

62
Q

Do not operate surface anti-ice systems in flight at ram air temperatures above ___ ° C.

A

10 ° C