Limitations Flashcards

1
Q

Rough air speed

A

210 KIAS

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2
Q

Landing gear operating speed (Vlo)

A

200 KIAS

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3
Q

Takeoff or landing with the bypass doors open is prohibited at or above a maximum ambient temperature limitation of ___.

A

ISA +25C

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4
Q

Minimum Oil PSI

MaxStart Oil PSI

Normal Oil PSI

Transient (low ) Oil PSI

A

44 PSI

100 PSI

61 to 72 PSI

44 to 61 PSI

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5
Q

Minimum portable oxygen pressure for dispatch (2 crew/3crew)…and gives x hours?

A

1300 PSI (2 crew)

1800 PSI (3 crew)

2 Hours

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6
Q

AFCS is approved for autopilot approaches to… (what Category)

A

CAT I limits only.

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7
Q

Maximum operating altitude for takeoff and landing

A

10,000 ft

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8
Q

Maximum altitude for landing gear or wing flaps

A

15,000 ft

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9
Q

Maximum fuel imbalance

A

600 lbs

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10
Q

What ice is detected the AIRFRAME MODE SELECT selector must be…

A

positioned at FAST.

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11
Q

Autopilot must be disengaged…(conditions)

A

in severe icing. in severe atmospheric turbulence.

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12
Q

For all approaches the autopilot must be disengaged at or above

A

200 ft agl

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13
Q

Maximum operation speed (Vmo)245 KIAS

0 to 8,000 ft

8 to 10,000

10 to 18,000

18 to 20,000

20 to 25,000

A

0 to 8,000 ft 245

8 to 10,000 282

10 to 18,000 286

18 to 20,000 275

20 to 25,000 248

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14
Q

Airplane min / max operating ambient temperature limit

A

-50c to 50c or (ISA +35c)

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15
Q

The aircraft is only authorized for Cat __ approach minimums

A

I

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16
Q

Starting Max ITT

&

Max ITT normal

A

920 (20 seconds maximum)

880 Normal Max

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17
Q

Max reverse Max torque

A

35%

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18
Q

On a Single Engine approach the AP must be off …..

A

past the final approach fix or 1000 feet agl, whichever is lower

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19
Q

Fuel heater outlet temp limitation

A

operation with fuel heater outlet temperature below 0C or above 71 C is prohibited

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20
Q

Normal cabin pressure

differential limit

A

5.46 +/- 0.1 psi

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21
Q

APP mode, autopilot engaged approaches, is approved for what flap settings:

A

Flap 0, 5, 10, 15, and 35

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22
Q

Minimum SAT for engine relight

A

-40C

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23
Q

APU is approved for…

A

ground operations only.

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24
Q

Max reverse Max ITT

A

880C

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25
Wheel brake cooling limits apply when....and shorted time is.....
between a landing or a low-energy rejected takeoff and a subsequent takeoff to ensure that sufficient brake energy is available 15 Minutes min
26
Standby, Auxiliary, and Main Battery Maximum load meter reading for takeoff
0.1
27
With and Cargo in any compartment the airplane must no be.....
the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.
28
Minimum Nh% ground operation
64.2%
29
Definition of icing conditions
Icing conditions exist when the SAT on the ground and for takeoff is 10C or below, or SAT in flight is 5C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for takeoff is 10C or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
30
Engine intake bypass doors must be...(closed/open) in what conditions
open for engine operation in icing conditions.
31
APU ambient temperature limits
- 35 to +50C or (ISA +35C)
32
Maximum altitude for air-start
20,000 ft
33
Integrated Standby Instrument limitation (flight time)
With the ISI installed the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.
34
Maximum runway slopes approved for takeoff and landing
+ 2% to - 2%
35
Maximum cabin pressure differential limit during taxiing, takeoff and landing
0.5 psi
36
Maximum cabin altitude (pressurized flight)
8,000 ft
37
Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff
-20C
38
Route limitation (this is the general...how far/how long can you be ?)
The route of flight must be within ONE hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative.
39
Maximum tailwind component
10 kts
40
Minimum flight crew
One Pilot and One copilot
41
Starting Oil temperature
-40C min
42
Oil Temps Minimum for Starting Normal Icing
-40c 0 - 107c 55c; 65c in 3 min
43
Maximum cabin pressure differential limit
5.95 psi
44
Propeller make and model
Dowty Aerospace R408
45
Maximum tire speed
182 kts
46
For approach minimums on straight in and circle approaches the DHC-8-402 is a category __ aircraft.
C
47
Landing gear extended speed (Vle)
215 KIAS
48
Powerplant ambient temperature limitation
-54C to +50C or (ISA +35C)
49
Normal takeoff (NTOP) Max torque
(NTOP torque indication will be 90% or 91%)
50
APU starter cranking limits
60 secs on, 5 mins off 60 secs on, maintenance action is required
51
AC Gen, DC Gen, and TRU Maximum load air/ground
1.0
52
Powerplant starter cranking limits
70 secs on, 2 mins off 70 secs on, 2 mins off 70 secs on, 30 mins off
53
Center of gravity limits Fore and Aft
17% MAC 36% MAC
54
Maximum wind speed for ground operation with the nose of the airplane more than 30 degrees out of the wind
50 kts
55
Alternate gear extension speed
185 KIAS
56
Maneuvering speed (Va)
204 KIAS
57
FLAP Extension Speeds ## Footnote 5 10 15 35
5 200 10 181 15 172 35 158
58
Maximum Ramp weight Maximum takeoff weight Maximum Landing weight Maximum zero fuel weight
65,400 lbs 65,200 lbs 62,000 lbs 58,000 lbs
59
After takeoff or go around the minimum height for autopilot engagement is \_\_\_\_\_.
1000 ft agl
60
Autopilot and flight director only approaches are approved for glideslope angles of ___ to a maximum of \_\_\_.
2.5 degrees to a maximum of 4 degrees
61
Tank 1 and 2 auxiliary fuel pumps must be...
....on for takeoff and landing.
62
Max takeoff (MTOP) (limited to x mins)
10 Minute Engines
63
Maneuvering G limit load factors ## Footnote Flaps retracted Flaps extended
+ 2.5 g - 1.0 g ## Footnote + 2.0 g - -0.0 g
64
Contaminated runway definition
More than 25% of surface is covered by any standing water, ice, slush, or snow
65
Automatic takeoff power uptrim is ....TQ?
10% torque (nominal)
66
Powerplant make and model Horse Power
Pratt & Whitney PW150A 5071,
67
APU must not be operated unattended... APU must be of for....
with passengers onboard. during pressure refueling. Off for Gravity...
68
Maximum operating altitude
25,000 ft