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XPW 24-14 > T-1 Boldface And Ops Limits > Flashcards

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
Engine - Transient - Maximum Observed ITT (C)
(720 2 SEC Max)
26
Engine - Transient - N2%
96
27
Engine - Transient - N1%
106
28
Engine - Transient - Oil Pressure (2) PSI
95 for 90 SEC
29
Engine - Transient - Oil Temperature (C)
135 (Max) (15 MIN Max)
30
(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.
60 83 60 60 40
31
(3) Under cold starting conditions, oil pressure between ____ PSI and ____ PSI is limited to ____ seconds.
83 95 90
32
(4) The ITT during ground starts should normally not exceed ____ (C).
550
33
Normal hydraulic pressure ____ to ____ PSI
1350 1550
34
Normal nitrogen pressure ____ to ____ PSI
1350 1650
35
Normal oxygen pressure ____ to ____ PSI
1600 1850
36
Min battery voltage for battery start ____ volts
22
37
Max gen load prior to starting second engine ____ amps
150
38
Motoring of the starter is limited to: First, ____ seconds then ____ minutes cooling Second, ____ seconds then ____ minutes cooling Third, ____ seconds then ____ minutes cooling
30, 5 30,15 30, 60
39
Emergency fuel / Minimum fuel ____ lbs / ____ lbs
300 / 500
40
Maximum fuel imbalance - T.O. / Touch & Go ____ lbs
100
41
Max fuel imbalance - Flight ____ lbs
300
42
Max fuel imbalance - Landing ____ lbs
300
43
Fuel crissfeed with 2 engines operating is limited to level flight with less than ____ lbs of fuel remains in the wing tank supplying fuel
600
44
Max ramp weight ____ lbs
16,300
45
Max takeoff weight ____ lbs
16,100
46
Max landing weight ____ lbs
15,700
47
Extend flaps to 10 degrees ____ KIAS
200
48
Extend flaps > 10 degrees ____ KIAS
170
49
Flaps extended > 10 degrees ____ KIAS
165
50
Aircraft is limited to ____ KIAS or ____ MACH, whichever is less
330 .78
51
Landing gear / Lights ____ KIAS / FL ____
200 / 200
52
Wipers ____ KIAS
200
53
Tire ____ Knots GS
165
54
Max tailwind ____ Knots
10
55
Max crosswind ____ Knots Max
25
56
Crosswind (Wet) ____ Knots Max
15
57
Crosswing (Icy) ____ Knots Max
10
58
Max operating altitude FL ____
410
59
Yaw damper required operable for flight above FL ____
280
60
Do not use autopilot below ____ FT AGL
200
61
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ____ (C)
10
62
Do not operate surface anti-ice systems in flight at ram air temperatures above ____ (C)
10
63
To ensure proper wing anti-ice operation, the throttles must be kept at ____ % N2 minimum
70

XPW 24-14 (2 decks)

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