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Dash-8 > Limitations > Flashcards

Limitations Flashcards

1
Q

Kinds of operations?

A
  • Day and night VFR
  • IFR
  • Icing conditions
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2
Q

Weight and Loading:

Max ramp weight?

A

64,700 lbs

65,400 lbs

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3
Q

Weight and Loading:

Max takeoff weight?

A

64,500 lbs

65,200 lbs

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4
Q

Weight and Loading:

Max landing weight?

A

61,750 lbs

62,000 lbs

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5
Q

Weight and Loading:

Max zero fuel weight?

A

57,000 lbs

58,000 lbs

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6
Q

Maneuvering Limit Load Factors:

Flaps retracted?

A

+2.5 g

-1.0 g

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7
Q

Maneuvering Limit Load Factors:

Flaps extended?

A

+2.0 g

0.0 g

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8
Q

Maximum fuel imbalance?

A

600 lbs

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9
Q

Airspeed Limitations:

0-8,000 ft?

A

245 KIAS

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10
Q

Airspeed Limitations:

10,000 ft?

A

282 KIAS

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11
Q

Airspeed Limitations:

18,000 ft?

A

286 KIAS

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12
Q

Airspeed Limitations:

20,000 ft?

A

275 KIAS

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13
Q

Airspeed Limitations:

25,000 ft

A

248 KIAS

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14
Q

Airspeed Limitations:
Flap Extended:
Flap 5º?

A

200 KIAS

160 KIAS min

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15
Q

Airspeed Limitations:
Flap Extended:
Flap 10º?

A

181 KIAS

150 KIAS min

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16
Q

Airspeed Limitations:
Flap Extended:
Flap 15º?

A

172 KIAS

145 KIAS min*

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17
Q

Airspeed Limitations:
Flap Extended:
Flap 35º?

A

158 KIAS

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18
Q 
Airspeed Limitations:
Maneuvering Speed (Va)?
A

204 KIAS

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19
Q

Airspeed Limitations:

Landing gear operating (Vlo)?

A

200 KIAS

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20
Q

Airspeed Limitations:

Landing gear extended (Vle)?

A

215 KIAS

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21
Q

Airspeed Limitations:

Rough Air Speed?

A

210 KIAS

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22
Q

Airspeed Limitations:

Alternate Gear Extension?

A

185 KIAS

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23
Q

Performance:

Max operating altitude?

A

25,000 ft

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24
Q

Performance:

Max altitude for takeoff and landing?

A

10,000 ft

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25
Q

Performance:

Max runway slope?

A

+2% uphill

-2% downhill

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26
Q

Performance:

Max tailwind component approved for takeoff with flaps 10º/15º or landing with 35º?

A

20 kts

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27
Q

Performance:

Max tailwind component approved for takeoff with flaps 5º or landing with 10º/15º?

A

10 KTS

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28
Q

Performance:

Min width of runway?

A

100 feet

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29
Q

Performance:
Max crosswind component approved for takeoff and landing…
•Hard, dry or wet runway?

A

32 kts

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30
Q

Performance:
Max crosswind component approved for takeoff and landing…
•Dry loose snow?
(4.0 in for takeoff, 5.1 in for landing)

A

18 kts

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31
Q

Performance:
Max crosswind component approved for takeoff and landing…
•Standing water, slush, or wet snow?

A

14 kts

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32
Q

Airplane Performance:

Max operating ambient temperature?

A

50º C or ISA +35º C

Whichever is lower

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33
Q

Airplane Performance:

Min operating ambient temperature?

A

-54º C

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34
Q

Performance:
Takeoff power setting limitation…
•Setting takeoff power prior to brake release, with nose of of airplane more than 45º out of wind, is prohibited for wind speeds greater than what?

A

8 kts

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35
Q

Performance:

Taxi limitations?

A
  • Single engine taxi is prohibited
  • Reverse taxi is not authorized
  • Max taxi speed is 30kts
  • Max taxi speed in low visibility is 10kts
  • Low vis is anything one mile or less
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36
Q

Aux fuel pumps:

A

Must be ON for T/O and landing

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37
Q

Fuel Heater:

Continuous operation with the fuel heat outlet temperature below___ or above___ is prohibited.

A

Below 0º C and above 71º C

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38
Q

Oil Limitations:
Oil Pressure General
-Minimum?
-Normal operating range?

A

44 psi

61 - 72 psi

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39
Q

Oil Limitations:
Oil Pressure General
-Transient min psi?

A

44 - 61 psi

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40
Q

Oil Limitations:
Temperature for start
-Min oil temperature?

A

-40º C

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41
Q

Oil Limitations:
Temperature for start
-Min oil temp to unfeather the prop?

A

-18 C

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42
Q

Oil Limitations:
Temperature for start
-Min oil temp above FLT IDLE?

A

0º C

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43
Q

Oil Limitations:
Temperature at DISC
-Minimum oil temp?

A

-40º C

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44
Q

Oil Limitations:
Temperature at DISC
-Max oil temp PLA between Disc and FLT IDLE?

A

125º C

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45
Q

Oil Limitations:
Temperature at DISC
-Maximum oil temp?

A

107º C

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46
Q

Oil Limitations:
Temperature above Flight Idle
-Minimum oil temp?

A

0º C

55º C for takeoff in icing conditions

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47
Q

Oil Limitations:
Temperature above Flight Idle
-Max oil temp?

A

107º C

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47
Q

Oil Limitations:
Temperature above Flight Idle
-Max continuous oil temp?

A

107º C

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48
Q

Performance:

Aircraft approach category?

A

Category C

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48
Q

Oil Limitations:

Min oil temp required to ensure engine air inlet ice protection, prior to takeoff?

A

55º C

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49
Q

Oil Limitations:
Min oil temp required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting takeoff power?

A

65º C

50
Q

APU Limitations:

General?

A
  • APU approved for ground ops only
  • APU must be shutdown prior to TO
  • APU must not be operated unattended with pax onboard
  • APU must not be operated unattended during pressure refueling
  • APU must not be operated during gravity refueling
51
Q

APU Limitation:

-Max ambient temp?

A

+50º C or ISA +35º C

Whichever is lower

52
Q

APU Limitation:

-Min ambient temp?

A

-35º C

53
Q

Max temp with APU louvers installed?

A

21º C

54
Q

APU Limitation:

-Starter Cranking Limits?

A
  1. 60 secs ON / 5 min OFF

2. 60 secs ON / MX action required

55
Q

Propeller:

Manufacturer and model?

A
  • Dowty Aerospace

* R408

56
Q

Powerplant:

Manufacturer?

A

Pratt & Whitney

57
Q

Powerplant:

Model?

A

PW 150A

58
Q

Powerplant:

-Ambient temp limitations?

A

Minimum: -54º C

Maximum: +50º C or ISA +35º C
Whichever is lower

59
Q

Powerplant:

Takeoff/landing or setting MTOP/MCP in flight with bypass doors opens prohibited at or above:

A

ISA +25º C

60
Q

Powerplant:

Max altitude for Airstart?

A

20,000 ft

61
Q

Powerplant:

Automatic Takeoff Power Uptrim?

A

10% torque (nominal)

62
Q

Engine Rating Limitations:

Max Takeoff MTOP (5071 SHP)?

A

106% TRQ

Max power on operating engine certified and is time limited to 5 minutes.

63
Q

Engine Rating Limitations:

Maximum Continuous MCP?

A

100% TRQ
Max continuous power rating is the max power certified for continuous use.
This rating should only be used when required to ensure safe flight.

64
Q

Engine Rating Limitations:

Normal Takeoff NTOP (4580 SHP)

A

90.3% TRQ

Takeoff power developed under normal takeoff conditions.

64
Q 
Power Plant Limitations:
MTOP (limited to 5 mins)...
Max TRQ?
Max ITT?
Max Nl % rpm?
Max Nh % rpm?
Max Np rpm?
Oil PSID?
Oil temp?
A 
Max TRQ% - 106%
Max ITT - 880º C
Max Nl% - 100%
Max Nh% - 100%
Max Np rpm - 1020 (max cont 1071)
Oil psi - 61 to 72
Oil Temp - 0º to 107º C
64
Q 
Power Plant Limitations:
NTOP....
Max TRQ?
Max ITT?
Max Nl % rpm?
Max Nh % rpm?
Max Np rpm?
Oil PSID?
Oil temp?
A 
Max TRQ - 90.3
Max ITT - varies
Max Nl % rpm - varies
Max Nh % rpm - varies
Max Np rpm - 1020 (1071 cont)
Oil PSID - 61 to 72
Oil temp - 0º to 107º C
64
Q 
Power Plant Limitations:
MCP (max continuous)...
Max TRQ?
Max ITT?
Max Nl % rpm?
Max Nh % rpm?
Max Np rpm?
Oil PSID?
Oil temp?
A 
Max TRQ - 100%
Max ITT - 880º C
Max Nl % rpm - 100%
Max Nh % rpm - 100%
Max Np rpm - 1020 (1071 max cont)
Oil PSID - 61 to 72
Oil temp - 0º to 107º C
64
Q 
Power Plant Limitations:
Starting...
Max ITT?
Oil PSID?
Oil temp?
A

Max ITT - 920º C (20 secs max)
Oil PSID - 100 (165 at DISC with OAT below 0º C)
Oil Temp - -40º C

64
Q 
Power Plant Limitations:
Transient (20 secs max)...
Max TRQ?
Max ITT?
Max Nl % rpm?
Max Nh % rpm?
Max Np rpm?
Oil PSID?
Oil temp?
A 
Max TRQ - 135
Max ITT - 920º
Max Nl % rpm - 102.3%
Max Nh % rpm - 101.2%
Max Np rpm - 1173
Oil PSID - 44 to 61 / 72 to 100
Oil temp - 125º max (5 secs max for TRQ value above idle and less than 55%)
64
Q

Power Plant Limitations:

Starter cranking limits…

A
  1. 70 secs ON / 2 min OFF
  2. 70 secs ON / 2 min OFF
  3. 70 secs ON / 30 min OFF
65
Q

Usable Fuel per tank:

A

5,862 lb per tank

11724 lb total

66
Q

Engine and Propeller Ground Ops Limitations:

Max Torque?

A

100%

67
Q

Engine and Propeller Ground Ops Limitations:

Min Nh?

A

64.2%

68
Q

Engine and Propeller Ground Ops Limitations:

Max wind speed for ground ops, with nose of the airplane more than 30º out of wind?

A

50 kts

69
Q

Engine and Propeller Ground Ops Limitations:
For winds greater than 8 kts, with nose of airplane more than 30º out of wind, max power for ground ops is?
(Ground Maneuvering)

A

MAX POWER SETTING
(Ground Maneuvering)
09 to 20 kts - FLIGHT IDLE (may be momentarily increase above flight idle for acceleration)
21 to 35 kts - FLIGHT IDLE
36 to 50 kts - FLIGHT IDLE (Power Levers must be at DISC with airplane static)

70
Q

Engine and Propeller Ground Ops Limitations:

What must be done in winds greater than 50 kts and within 24 hours?

A

Max wind speed must be recorded and provided to maintenance.

71
Q

Engine and Propeller Ground Ops Limitations:
For winds greater than 8 kts, with nose of airplane more than 30º out of wind, max power for ground ops is?
(Ground Static Operations)

A 
MAX POWER SETTING
(Ground Static Operation)
09 to 20 kts - Power levers angle at 60º
21 to 35 kts - FLIGHT IDLE
36 to 50 kts (gusts up to 55) - DISC
72
Q

Engine Airborne Ops Limitations:

In-flight ops of POWER levers aft of FLIGHT IDLE gate is…?

A

PROHIBITED

73
Q

Electrical System:
Battery…
Min battery temperature for takeoff?

A

-20º C

74
Q

Electrical System:
AC GEN, DC GEN, TRU…
Max load air/ground?

A

1.0

75
Q

Landing Gear and Flap Systems:

Max altitude for extending or extended landing gear or wing flap?

A

15,000 ft

76
Q

Maximim Tire Speed?

A

182 kts groundspeed

77
Q

Air Conditioning and Pressurization:

Normal Cabin psi differential limit?

A

5.46 +-0.1 psi

78
Q

Air Conditioning and Pressurization:

Max Cabin psi differential limit?

A

5.95 psi

79
Q

Air Conditioning and Pressurization:

Max Cabin psi differential limit during taxiing, takeoff, and landing?

A

0.5 psi

80
Q

Air Conditioning and Pressurization:

Max Cabin altitude?

A

8,000 ft

81
Q

Wheel Brake Cooling Limits?

A

Brake cooling times must be observed between a landing, or a low energy RTO and a subsequent takeoff.

82
Q

Ice Protection:
Engine intake bypass doors must be open for engine ops in icing conditions.
When ice is detected, AIRFRAME MODE SELECT must be positioned at?

A

FAST

83
Q

Definition of Icing Conditions?

A

SAT on ground and fir takeoff is 10º C or below.
SAT in flights is 5º C or below, and visible moisture in any form is present (such as clouds, fog and visibility if 1 mile or less, rain, snow, sleet or ice crystals).
SAT on ground and for takeoff is 10º C or below when operating on contaminated ramps that may be ingested by engines or freeze on engines, nacelle, or engine sensor probes.

84
Q

Automatic Flight Control System (AFCS):

AFCS is approved for auto approaches to CAT?

A

CAT I only

86
Q

Automatic Flight Control System (AFCS):

APP mode, autopilot engaged approaches, is approved for (flaps)?

A

Flap 0º (min alt: 1,000 ft AGL)

Flap 5º, 10º, 15º, and 35º

88
Q

Automatic Flight Control System (AFCS):

Autopilot must be _______ in severe icing?

A

DISENGAGED

88
Q

Automatic Flight Control System (AFCS):

During autopilot ops, pilot must be seated at controls with harness ________?

A

SECURED

89
Q

Automatic Flight Control System (AFCS):

Use of VOR without associated DME is prohibited in _____ mode?

A

APP

90
Q

Automatic Flight Control System (AFCS):

After takeoff or go-around, min height for autopilot engagement is?

A

1,000 ft AGL

91
Q

Automatic Flight Control System (AFCS):

For non-precision approaches the autopilot must be be disengaged at or above?

A

200 ft AGL

92
Q

Automatic Flight Control System (AFCS):

Flight conditions of severe atmospheric turbulence with autopilot engaged is?

A

PROHIBITED

92
Q

Automatic Flight Control System (AFCS):

An autopilot approach must not be continued past the final approach fix or 1000 AGL, whichever is lower with?

A

An INOPERATIVE engine

93
Q

Automatic Flight Control System (AFCS):

Autopilot and Flight Director only approaches are approved for glideslope angles of?

A

2.5º to a max of 4º

93
Q

Automatic Flight Control System (AFCS):

Autopilot approaches have been demonstrated in crosswind components up to ?

A

18 kts

This is not considered limiting

94
Q

Automatic Flight Control System (AFCS):

On precision approaches, the autopilot must be disengaged at or above a minimum altitude of?

A

200 ft AGL

95
Q 
Power Plant Limitations:
Max Reverse...
Max TRQ?
Max ITT?
Max Nl % rpm?
Max Nh % rpm?
Max Np rpm?
Oil PSID?
Oil temp?
A 
Max TRQ - 35
Max ITT - 880º
Max Nl % rpm - 100
Max Nh % rpm - 100
Max Np rpm - 1020
Oil PSID - 61 to 72
Oil temp - 0º to 107º C
96
Q

Engine Airborne Ops Limitations:

Min SAT for engine relight?

A

-40º C

97
Q

Electrical System:
Battery…
Max loadmeter reading for takeoff?

A

0.1

100
Q

Cargo Compartment Limitation?

A

Unless the FWD and AFT cargo compartments are empty, the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.

101
Q

Avionics:
To ensure uninterrupted operation of PFD, MFD, and the ED, electrical power must be cycled on all displays once every _____?

A

24 hours (flying day)

103
Q

Republic Imposed Limitations:

On ground, operation of landing (APPROACH and FLARE) lights is limited to _____?

A

5 minutes

Does not preclude continuous operation of TAXI light.

104
Q

Maximum tire speed

A

182 kts

105
Q

Route Limitations:
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.
Takeoff alternates for DHC-8-402 must be within?

A

250 nm of departure airport.

105
Q 
Center of Gravity:
Serial Numbers 4187 and above:
Forward Limit (up to 53,000 lbs) - ?
Forward Limit (53,000-65,200 lbs) - ?
Aft Limit - ?
A 
Forward Limit (up to 53,000 lbs) - 13.8% MAC
Forward Limit (53,000-65,200 lbs) - 13.8 through 17.7% MAC
Aft Limit - 36.0% MAC
106
Q

Max altitude for gear and flap extension?

A

15,000 feet

107
Q

Temp limits of packs in MANUAL mode

A

3 - 71c

37 - 160f

108
Q

Rudder travel limit with flaps 0

A

12 degrees

109
Q

Rudder travel limit with flaps greater than 0

A

18 degrees

110
Q

Limits for taxiing on contaminated surfaces

A

Max speed of 10kts

Dry snow - 4 inches
Wet snow - .75 inches
Slush - .5 inches
Water - .25 inches

111
Q

Plowed minimum width for taxi and takeoff/landing

A

Taxi - 50ft

Takeoff/Landing - 75ft

These are allowed at captain’s discretion

70.10 pg 16

112
Q

Aft cargo limit for High Gross model

A

3765 lbs

113
Q

Oxygen:

At 70º F, the min Crew Oxygen and Portable Oxygen psi for dispatch is?

A

Portable O2 - 1600 psi
3 Crew - 1450 psi
2 Crew - 1050 psi

114
Q

Avionics:
With Integrated Standby Instrument installed the airplane must not be operated further than ___ hour flying time from a suitable airport for landing.

A

1 hour flying time

114
Q 
Center of Gravity:
Serial Numbers below 4187:
Forward Limit (up to 53,000 lbs) - ?
Forward Limit (53,000-64,000 lbs) - ?
Aft Limit - ?
A 
Forward Limit (up to 53,000 lbs) - 13.8% MAC
Forward Limit (53,000-64,000 lbs) - 13.8 through 17.4% MAC
Aft Limit - 36.0% MAC
114
Q

Max altitude for gear and flap extension?

A

15,000 feet

114
Q

Temp limits of packs in AUTO mode?

A

15 - 27c

59 - 81f

114
Q

Forward cargo compartment (F1) weight limit:

A

910 lbs

This is for both aircraft types

114
Q

Aft cargo limit for Enhanced Model

A

2545 lbs

Dash-8 (3 decks)

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