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T-1A > OPS limits > Flashcards

OPS limits Flashcards

0
Q

What is the time limit for idle thrust?

A

Continuous

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1
Q

What is the max ITT during takeoff

A

700

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2
Q

What is the max time limit for maximum continuous thrust

A

continuous

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3
Q

Max ITT with max continuous thrust settings

A

680

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4
Q

Max ITT with idle thrust

A

580

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5
Q

Max N2% with max continuous thrust

A

96

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6
Q

Max ITT during start

A

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

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7
Q

Max ITT with transient thrust settings

A

720 2 seconds

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8
Q

Min N2% in idle thrust

A

52

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9
Q

Max N2% with takeoff thrust

A

96

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10
Q

N1% with takeoff thrust

A

104%

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11
Q

N1% with transient thrust

A

106%

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12
Q

Min oil pressure in idle

A

40 psi

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13
Q

oil pressure with max continuous thrust

A

60-83 psi

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14
Q

N1% with max continuous thrust

A

104%

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15
Q

Under cold starting conditions, oil pressure between___ and ____ is limited to _____ seconds

A

83,95,90

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16
Q

Oil pressure during transient thrust settings

A

95 psi for 90 sec

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17
Q

Normal oil pressure is___to___ at N2 speeds above_____

A

60-83 psi

60 %

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18
Q

What is the max time limit for takeoff thrust

A

5 minutes

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20
Q

Oil temperature with max continuous thrust

A

10-121C

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21
Q

Oil temperature in idle

A

-40 to 121C

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22
Q

Oil temperature during takeoff

A

10-121C

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22
Q

Min Oil temperature during start

A

-40C

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24
Q

oil pressure during engine start

A

60-83 psi

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24
Oil temperature with transient thrust
135 C (max) for 15 min (max)
24
Oil pressure below _____PSI is undesirable and should not be tolerated, other than to safely recover the flight
60
25
Oil pressure below ______is unsafe
40 psi
27
Normal Oxygen pressure
1600-1850 PSI
28
Normal hydraulic pressure
1350-1550 psi
29
The ITT during ground starts should normally not exceed_____C
550
30
N2% with transient thrust
96
31
Min battery voltage for battery start
22V
32
Motoring of the starter is limited to:
30 seconds, 5 minutes cooling 30 seconds, 15 minutes cooling 30 seconds, 60 minutes cooling
33
Maximum fuel imbalance -- T/O, touch and go
100 lbs
34
Normal nitrogen pressure
1350-1650 psi
35
Emergency fuel/Minimum fuel
300 / 500 lbs
36
Max fuel imbalance in flight
300 lbs
37
Max gen load prior to starting second engine
150 amps
38
Max fuel imbalance---landing
300 lbs
39
Extend flaps more than 10 degrees____KIAS
170
40
Max ramp weight
16,300
41
Low Cabin Pressure
OXYGEN MASKS-DON/100%
42
Fuel crossfeed with 2 engines operating is limited to level flight with less than ____lbs of fuel remains in the wing tank supplying fuel
600 lbs
43
Max takeoff weight
16,100
44
Extend flaps to 10 degrees____KIAS
200
45
Max landing weight
15,700
45
aircraft limit to ____KIAS or ____MACH whichever is less
330, .78
46
Landing gear/lights_____KIAS/FL____
200 KIAS, FL200
48
Flaps extended more than 10 degrees___KIAS
165 KIAS
48
Tire____KIAS
165 Knots GS
50
Wipers___KIAS
200 KIAS
51
Max tailwind
10 kts
52
Max operating altitude
FL410
53
Yaw damper required operable for flight above FL____
FL280
54
Max crosswind (dry)
25 kts
55
Pitch Trim / Roll Trim/ Rudder Trim Runaway
TRIM INT & A/P DISENGAGE SWITCH-PUSH AND HOLD
56
Max crosswind (wet)
15 kts
58
Do not use autopilot below ____Ft AGL
200
59
To ensure proper wing anti-ice operation, the throttles must be kept at _____% N2 minimum
70 %
60
Max crosswind (icy)
10 kts
61
Do not operate surface anti-ice systems in flight at ram air temperatures above ____C
10 C
62
Smoke Or Fumes In Aircraft
OXYGEN MASKS-DON/100%
63
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___C
10 C
63
Engine Fire During Ground Operations
THROTTLES-CUTOFF
64
Engine Fire During Flight
THROTTLE-IDLE if condition persists THROTTLE-CUTOFF ENGINE FIRE SWITCH-PUSH BOTTLE ARMED SWITCH-PUSH

T-1A (9 decks)

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