T-1 Boldface And Ops Limits Flashcards

1
Q

Engine fire during ground operations

A

THROTTLES - CUTOFF

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2
Q

Engine fire during flight
-If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist

A

THROTTLE - IDLE
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

Engine - Takeoff - Time Limit (Minutes)

A

5

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7
Q

Engine - Takeoff - Maximum Observed ITT (C)

A

700

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8
Q

Engine - Takeoff - N2%

A

96

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9
Q

Engine - Takeoff -N1%

A

104

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10
Q

Engine - Takeoff -Oil Pressure (2) PSI

A

60 to 83

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11
Q

Engine - Takeoff - Oil Temperature (C)

A

10 to 121

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12
Q

Engine - Maximum Continuous - Time Limit (Minutes)

A

Continuous

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13
Q

Engine - Maximum Continuous - Maximum Observed ITT (C)

A

680

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14
Q

Engine - Maximum Continuous - N2%

A

96

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15
Q

Engine - Maximum Continuous - N1%

A

104

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16
Q

Engine - Maximum Continuous - Oil Pressure (2) PSI

A

60 to 83

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17
Q

Engine - Maximum Continuous - Oil Temperature (C)

A

10 to 121

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18
Q

Engine - Idle - Time Limit (Minutes)

A

Continuous

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19
Q

Engine - Idle - Maximum Observed ITT (C)

A

580

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20
Q

Engine - Idle - N2%

A

52 (Min)

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21
Q

Engine - Idle - Oil Pressure (2) PSI

A

40 (Min)

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22
Q

Engine - Idle - Oil Temperature (C)

A

-40 to 121

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23
Q

Engine - 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

Engine - Starting (4) - Oil Temperature (C)

A

-40 (Min)

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25
Q

Engine - Transient - Maximum Observed ITT (C)

A

(720 2 SEC Max)

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26
Q

Engine - Transient - N2%

A

96

27
Q

Engine - Transient - N1%

A

106

28
Q

Engine - Transient - Oil Pressure (2) PSI

A

95 for
90 SEC

29
Q

Engine - Transient - Oil Temperature (C)

A

135 (Max)
(15 MIN Max)

30
Q

(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 the safe recovery of the flight, preferably at reduced power setting. Oil pressure below ____ PSI is unsafe.

A

60
83
60
60
40

31
Q

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

A

83
95
90

32
Q

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

A

550

33
Q

Normal hydraulic pressure ____ to ____ PSI

A

1350
1550

34
Q

Normal nitrogen pressure ____ to ____ PSI

A

1350
1650

35
Q

Normal oxygen pressure ____ to ____ PSI

A

1600
1850

36
Q

Min battery voltage for battery start ____ volts

A

22

37
Q

Max gen load prior to starting second engine ____ amps

A

150

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

30, 5
30,15
30, 60

39
Q

Emergency fuel / Minimum fuel ____ lbs / ____ lbs

A

300 / 500

40
Q

Maximum fuel imbalance - T.O. / Touch & Go ____ lbs

A

100

41
Q

Max fuel imbalance - Flight ____ lbs

A

300

42
Q

Max fuel imbalance - Landing ____ lbs

A

300

43
Q

Fuel crissfeed with 2 engines operating is limited to level flight with less than ____ lbs of fuel remains in the wing tank supplying fuel

A

600

44
Q

Max ramp weight ____ lbs

A

16,300

45
Q

Max takeoff weight ____ lbs

A

16,100

46
Q

Max landing weight ____ lbs

A

15,700

47
Q

Extend flaps to 10 degrees ____ KIAS

A

200

48
Q

Extend flaps > 10 degrees ____ KIAS

A

170

49
Q

Flaps extended > 10 degrees ____ KIAS

A

165

50
Q

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

A

330
.78

51
Q

Landing gear / Lights ____ KIAS / FL ____

A

200 / 200

52
Q

Wipers ____ KIAS

A

200

53
Q

Tire ____ Knots GS

A

165

54
Q

Max tailwind ____ Knots

A

10

55
Q

Max crosswind ____ Knots Max

A

25

56
Q

Crosswind (Wet) ____ Knots Max

A

15

57
Q

Crosswing (Icy) ____ Knots Max

A

10

58
Q

Max operating altitude FL ____

A

410

59
Q

Yaw damper required operable for flight above FL ____

A

280

60
Q

Do not use autopilot below ____ FT AGL

A

200

61
Q

Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ____ (C)

A

10

62
Q

Do not operate surface anti-ice systems in flight at ram air temperatures above ____ (C)

A

10

63
Q

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

A

70