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Q400 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max. Take-off (MTOP) (1) Max N(L) % rpm

A

100%

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2
Q

Autopilot approaches have been demonstrated in crosswind components up to ___. This is not considered limiting.

A

18 knots.

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3
Q

Transient (20 seconds maximum) Max. Torque %

A

135 %

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4
Q

Maximum cabin pressure differential limit

A

5.95 psi

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5
Q

APU must not be operated during…

A

gravity refueling

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6
Q

Serial numbers: 4187 and above Ramp Weight

A

65,400 lbs

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7
Q

Oil pressure minimum

A

44 psi

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8
Q

Maximum Oil Temperature at ground idle

A

107 C

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9
Q

Powerplant Start Cranking Limits

A

START MAX TIME ON FOLLOWED BY 1 70 seconds 2 minutes off 2 70 seconds 2 minutes off 3 70 seconds 30 minutes off

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10
Q

Max. Reverse Max. N(L) % rpm

A

100%

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11
Q

Maneuvering Limit Load Factors Flap retracted

A

+ 2.5 g - 1. 0 g

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12
Q

Route Limitation

A

The route must be within one hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative. Take-off alternates for the DHC-8-402 must be within 250 nm of the departure airport.

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13
Q

Minimum SAT for engine relight is

A

-40C

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14
Q

When using previously store flight plans and waypoints, the waypoints must

A

be verified for accuracy, by reference to current publication, prior to their use.

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15
Q

For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground static operation is as follows

A

WIND SPEED MAXIMUM POWER SETTING (GROUND STATIC) 9 to 20 kts Power levers angle at 60 degrees (approximately midway between FLIGHT IDLE and Take-off power detent) 21 to 35 kts FLIGHT IDLE 36 to 50 kts DISC (gusts to 55kts)

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16
Q

APU Starter Cranking Limits

A

START MAX TIME ON… FOLLOWED BY… 1 60 secs 2 mins off 2 60 secs 2 mins off 3 60 secs 30 mins off NOTE: If the APU does not start in the third attempt, maintenance action is required.

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17
Q

Maximum torque

A

100%

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18
Q

Transient (20 seconds maximum) Max. N(H) % rpm

A

101.2%

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19
Q

Max Continuous (MCP) Max. N(L) % rpm

A

100%

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20
Q

Maximum fuel imbalance between the main fuel tanks

A

600 lb.

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21
Q

Transient (20 seconds maximum) Max N(L) % rpm

A

102.3%

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22
Q

Maneuvering Speed (Va)

A

204 KIAS

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23
Q

Max. reverse Max. torque %

A

35%

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24
Q

Powerplant: Maximum Altitude for Airstart

A

20,000 ft

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25
Q

Landing Gear Extended Speed (Vle)

A

215 KIAS

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26
Q

Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff

A

0.1

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27
Q

Transient (20 seconds maximum) Max. N(P) rpm

A

1173 rpm

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28
Q

Instrument approaches must be conducted in the approach mode and for

A

GSP approaches, RAIM must be available at the final approach fix.

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29
Q

Normal Take-off (NTOP) Max ITT C

A

The Normal Take-off ITT limit for a given ambient air temperature is given in “Variation of ITT with Ambient Air Temperature for NTOP” below.

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30
Q

Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway

A

32 knots

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31
Q

Vmo 20,000 ft

A

275 KIAS

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32
Q

Max. Reverse Max N(H) % rpm

A

100%

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33
Q

Maximum tire speed

A

182 kts groundspeed

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34
Q

Minimum N(H)

A

64.2%

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35
Q

All flaps 35 landings will be done with a maximum flap setting of…

A

15 during the approach to the final segment

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36
Q

Powerplant: Automatic Take-Off Power Uptrim

A

10% torque (nominal)

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37
Q

Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15

A

10 kts

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38
Q

Starting Max ITT C

A

920 C 20 seconds maximum

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39
Q

Flight Compartment Communication Limit

A

HOT MIC select switches on the pilot and co-pilot ARCDU must be OFF and the INT/RAD switch on the observers Audio Control Panel must be centered, when using the cockpit speakers.

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40
Q

Maximum altitude for extending or extended landing gear or wing flap is

A

15,000 ft

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41
Q

Minimum oil temperature above ground idle

A

0 C (55 C for take-off in icing conditions)

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42
Q

Max Continuous (MCP) Oil Press PSID

A

61 to 72

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43
Q

DC Gen, AC Gen, TRU Maximum load air/ground

A

1.0

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44
Q

To ensure uninterrupted operating of the pilot’s and co-pilot’s PFD, MFD and the ED, electrical power must be cycled on all displays…

A

once every 24 hours (flying day)

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45
Q

Max continuous oil temperature above ground idle

A

107 C

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46
Q

Fuel Heater limit

A

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

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47
Q

Flight in conditions of _______ ________ _______ with autopilot engaged is _________.

A

severe atmospheric turbulence prohibited

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48
Q

Powerplant: With Bypass Doors Open, take-off, landing and setting MTOP and MCP are limited to a maximum ambient temperature limitation of

A

ISA +25 C

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49
Q

The aircraft must have approved navigation equipment appropriate to the

A

route of flight installed and operating so as to provide an alternate means of navigation.

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50
Q

Usable fuel tank capacities per tank

A

5,862 lb per tank

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51
Q

Flight Compartment Door Limit

A

The flight compartment door must be closed and locked at all times during flight except to provide access egress as required per the FOM and SOP400.

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52
Q

Max. Take-off (MTOP) (1) Max ITT C

A

880 C

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53
Q

Transient minimum oil pressure

A

44 to 61 psi

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54
Q

Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight

A

64,500 lbs

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55
Q

Normal cabin pressure differential limit

A

5.46 +/- 0.1 psi

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56
Q

Max. Take-off (MTOP) (1) Oil press PSID

A

61 to 72

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57
Q

Serial numbers: 4187 and above Maximum Zero Fuel Weight

A

58,000 lbs

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58
Q

Minimum Runway Width

A

100 feet

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59
Q

Maximum crosswind component Runway with standing water, slush or wet snow

A

14 kts

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60
Q

Transient (20 seconds maximum) Oil Temp C

A

125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)

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61
Q

Rough Air Speed

A

210 KIAS

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62
Q

P-RNAV operations may

A

only be conducted with the FMS in terminal mode.

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63
Q

Flap Extended Speed (Vfe) Flap 35

A

158 KIAS

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64
Q

Powerplant Ambient temperature limitations

A

-54 C to +50 C or ISA +35 C, whichever is lower

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65
Q

Normal operating range (oil pressure)

A

61 to 72 psi

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66
Q

Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power

A

65 C

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67
Q

Oxygen Limit

A

At 70F the minimum Crew oxygen and Portable oxygen pressure for dispatch is as follows: Portable oxygen 1600 psi 3 Crew 1450 psi 2 Crew 1050 psi

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68
Q

Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off

A

55 C

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69
Q

Transient (20 seconds maximum) Oil Press PSID

A

44 to 61 72 to 100

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70
Q

Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight

A

57,000 lbs

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71
Q

Max. Reverse Max. ITT C

A

880 C

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72
Q

Instrument approaches must be accomplished in accordance with instrument approach procedures that

A

are retrieved from the FMS database.

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73
Q

An autopilot approach must be continued past the ______ _______ ___ or ____ feet AGL, whichever is lower, with an _______ ______.

A

final approach fix 1000 inoperative engine

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74
Q

When altitudes are manually entered before or after the

A

temperature compensation function is activated, it may produce VNAV paths with climb segments, and result in a VNAV disconnect.

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75
Q

Normal Take-off (NTOP) Oil Temp C

A

0 to 107 C

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76
Q

Max Take-off (MTOP) (1) Max Torque %

A

106%

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77
Q

Vmo 10,000 ft

A

282 KIAS

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78
Q

Navigation by means of Pilot-defined,

A

non published approaches under instrument meteorological conditions is prohibited.

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79
Q

Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):

A

13.8% MAC

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80
Q

Max. Reverse Oil Temp C

A

0 to 107 C

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81
Q

Serial numbers: 4187 and above Maximum Take-off Weight

A

65,200 lbs

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82
Q

Flap Extended Speed (Vfe) Flap 5

A

200 KIAS

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83
Q

Minimum oil temperature for start up

A

-40 C

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84
Q

Landing Gear Operating Speed (Vlo)

A

200 KIAS

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85
Q

Maximum cabin pressure differential limit during taxiing, take-off and landing

A

0.5 psi

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86
Q

Wheel Brake Cooling Limits

A

Brake cooling times must be observed between a landing or a low-energy rejected take-off and a subsequent takeoff, to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected.

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87
Q

Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight

A

61,750 lbs

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88
Q

Take-off Power Setting Limitation

A

Setting take-off power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than 8 kts.

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89
Q

Transient (20 seconds maximum) Max ITT C

A

920 C

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90
Q

Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35

A

20 kts

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91
Q

Max Continuous (MCP) Max Torque %

A

100%

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92
Q

Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):

A

13.8% MAC

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93
Q

APU ambient temperature (lower)

A

-35 C

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94
Q

Starting Oil Temp C

A

-40 C min.

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95
Q

Flap Extended Speed (Vfe) Flap 10

A

181 KIAS

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96
Q

Normal Take-off (NTOP) Oil Press PSID

A

61 to 72

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97
Q

Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind

A

50 kts

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98
Q

Airplane minimum operating ambient temperature limit

A

-54 C

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99
Q

APU must be shutdown…

A

prior to take-off

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100
Q

Maximum operating altitude

A

25,000 ft

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101
Q

Taxi Limitations

A

Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.

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102
Q

Max. Reverse Oil Press PSID

A

61 to 72

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103
Q

Powerplant Manufacturer and Model

A

Pratt & Whitney, PW 150A

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104
Q

Fuel display parameter is advisory only and

A

must not be used as the primary means for computing fuel load and range.

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105
Q

FMS based ILS and MLS approaches

A

are prohibited.

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106
Q

Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff

A

-20C

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107
Q

Starting Oil Press PSID

A

100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)

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108
Q

For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground maneuvering is as follows

A

WIND SPEED MAX POWER SETTING (GROUND) 9 to 20 kts FLIGHT IDLE (power levers may be momentarily increased above flight idle) 21 to 35 kts FLIGHT IDLE 36 to 50 kts FLIGHT IDLE (must be at DISC with airplane static)

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109
Q

Normal Take-off (NTOP) Max Torque %

A

90.3% (NTOP torque indication will be 90% or 91%)

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110
Q

Use of ___ without associated ___ is prohibited in ___ mode.

A

VOR DME APP

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111
Q

Autopilot must be ________ in _______ icing.

A

disengaged severe

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112
Q

Maneuvering Limit Load Factors Flap extended

A

+ 2.0 g 0.0 g

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113
Q

Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)

A

18 kts

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114
Q

Propeller Manufacturer and Model

A

Dowty Aerospace R408

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115
Q

Max. Take-off (MTOP) (1) Max N(H) % rpm

A

100%

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116
Q

APP mode, autopilot engaged approaches, is approved for:

A

a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35

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117
Q

During autopilot operation, the pilot must be ________ at the controls with _______ ________.

A

seated harness secured

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118
Q

Serial numbers: 4187 and above Maximum Landing Weight

A

62,000 lbs

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119
Q

Alternate Gear Extension Speed

A

185 KIAS

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120
Q

Max. Take-off (MTOP) (1) Max N(P) rpm

A

1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)

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121
Q

Max Continuous (MCP) Oil Temp C

A

0 to 107 C

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122
Q

In-flight operating of the ______ levers aft of the _____ ____ gate is prohibited.

A

POWER FLIGHT IDLE

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123
Q

Normal Take-off (NTOP) Max. N(P) rpm

A

1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm

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124
Q

VNAV vertical path angles greater than

A

6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.

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125
Q

Minimum oil temperature above FLT IDLE

A

0 C

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126
Q

Republic Airlines Imposed Light Limitations

A

On the ground, operating of landing (APPROACH and FLARE) lights is limited to 5 minutes (This does no preclude continuous operation of the TAXI light).

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127
Q

Aircraft Approach Category

A

Category C

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128
Q

Minimum oil temperature at ground idle

A

-40 C

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129
Q

Normal Take-off (NTOP) Max. N(H) % rpm

A

The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in “Variation of N(H) and N(L) with Ambient Air Temperature for NTOP”.

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130
Q

The FMS may only be used for

A

navigation guidance if the reference coordinated data system for the intended route is referenced to in WGS-84 and NAD-83.

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131
Q

Maximum runway slopes approved for take-off and landing

A

+ 2% (uphill) - 2% (downhill)

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132
Q

Vmo 18,000 ft

A

286 KIAS

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133
Q

Kinds of Operation

A
  1. Day and night VFR 2. IFR 3. Icing Conditions
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134
Q

On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.

A

200

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135
Q

Maximum oil temp PLA between Disc and FLT IDLE

A

125 C

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136
Q

The use of _____ ____ _____ FUELS is prohibited

A

WIDE CUT TYPE

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137
Q

Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:

A

36.0% MAC

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138
Q

Airplane maximum operating ambient temperature limit

A

50 C or ISA +35 C whichever is lower

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139
Q

The UNS-1E is approved for

A

VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.

140
Q

APU ambient temperature (upper)

A

+50 C or ISA +35 C, whichever is lower

141
Q

Serial Numbers: 4187 and above Aft limit:

A

36.0% MAC

142
Q

Normal Take-off (NTOP) Max. N(L) % rpm

A

The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in “Variation of N(H) and N(L) with Ambient Air Temperature for NTOP”.

143
Q

Flight above 73 degrees north latitude or below 60 degrees latitude using the

A

FMS may be conducted only when magnetic variation is input manually into the system or an alternate true heading source is used and no manual variation has been input.

144
Q

With APU inlet louvres installed, APU operation is limited to

A

+21 C maximum ambient temperature

145
Q

Vmo 0 to 8,000

A

245 KIAS

146
Q

FMS Approach Navigation is prohibited with the ___ ___ ___ ___. IFR enroute and terminal navigation is prohibited with the ___ ___ ___ ____ expired unless the Pilot….

A

FMS Data Base expired FMS Data Base expired verifies the waypoints for accuracy by reference to current publications.

147
Q

NOTE: Ground operations in winds greater than 50 kts must be recorded and…

A

the maximum wind speed provided to maintenance within 24 hours (flying day)

148
Q

Maximum cabin altitude (pressurized flight)

A

8,000 ft

149
Q

Max. Take-off (MTOP) (1) Oil temp C

A

0 C to 107 C

150
Q

APU must not be operated unattended…

A

…with passengers onboard …during pressure refueling

151
Q

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

A

200 ft. AGL.

152
Q

Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):

A

13.8% thru 17.7% MAC

153
Q

Max Continuous (MCP) Max N(H) % rpm

A

100%

154
Q

On RNAV approaches where vertical guidance (VNAV Mode) is used, the Company must bug

A

MDA plus fifty (50) feet. This is referred to as a Derived Descent Altitude (DDA) and allows for dip during a missed approach without descending below the charted LNAV MDA.

155
Q

Max. Reverse Max N(P) rpm

A

1020 rpm

156
Q

AFCS is approved for autopilot approaches to ___ _ _____ ____.

A

CAT I limits only.

157
Q

APU is approved for what kind of operation?

A

GROUND OPERATIONS ONLY

158
Q

Max Continuous (MCP) Max N(P) rpm

A

1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm

159
Q

Maximum operation altitude for take-off and landing

A

10,000 ft

160
Q

Auxiliary Fuel Pumps limitation

A

Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.

161
Q

Whenever navigation is predicated on the FMS,

A

the Operator’s Manual, Report no. 2423sv801 (or equivalent at current revision) must be available to the Flight Crew.

162
Q

With Integrated Standby Instrument installed the airplane must not be operated further than

A

1 hour flying time from a suitable airport for landing

163
Q

Cargo Compartment Limit

A

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

164
Q

Flap Extended Speed (Vfe) Flap 15

A

172 KIAS

165
Q

After take-off or go-around, the minimum height for autopilot engagement is

A

1,000 ft. AGL.

166
Q

SCN 802.2, SCN 802.8: Manually entered altitudes will not have an altitude correction applied when

A

temperature compensation function is activated. All manually entered altitudes must be adjusted with the appropriate temperature correction before they are entered into the FMS, even if the temperature compensation function is not active.

167
Q

Ice Protection Limit

A

Engine intake bypass doors must be open for engine operating in icing conditions. When ice is detected the AIRFRAME MODE SELECT selector must be positioned at FAST.

168
Q

Vmo 25,000 ft

A

248 KIAS

169
Q

Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight

A

64,700 lbs

170
Q

Maximum Oil Temperature above ground idle

A

107 C

171
Q

Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):

A

13.8% thru 17.4% MAC

172
Q

Max Continuous (MCP) Max ITT C

A

880 C

173
Q

Icing conditions exist when:

A

the SAT on the ground and for take-off 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.

174
Q

100%

A

Max. Take-off (MTOP) (1) Max N(L) % rpm

175
Q

18 knots.

A

Autopilot approaches have been demonstrated in crosswind components up to ___. This is not considered limiting.

176
Q

135 %

A

Transient (20 seconds maximum) Max. Torque %

177
Q

5.95 psi

A

Maximum cabin pressure differential limit

178
Q

gravity refueling

A

APU must not be operated during…

179
Q

65,400 lbs

A

Serial numbers: 4187 and above Ramp Weight

180
Q

44 psi

A

Oil pressure minimum

181
Q

107 C

A

Maximum Oil Temperature at ground idle

182
Q

START MAX TIME ON FOLLOWED BY 1 70 seconds 2 minutes off 2 70 seconds 2 minutes off 3 70 seconds 30 minutes off

A

Powerplant Start Cranking Limits

183
Q

100%

A

Max. Reverse Max. N(L) % rpm

184
Q

+ 2.5 g - 1. 0 g

A

Maneuvering Limit Load Factors Flap retracted

185
Q

The route must be within one hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative. Take-off alternates for the DHC-8-402 must be within 250 nm of the departure airport.

A

Route Limitation

186
Q

-40C

A

Minimum SAT for engine relight is

187
Q

be verified for accuracy, by reference to current publication, prior to their use.

A

When using previously store flight plans and waypoints, the waypoints must

188
Q

WIND SPEED MAXIMUM POWER SETTING (GROUND STATIC) 9 to 20 kts Power levers angle at 60 degrees (approximately midway between FLIGHT IDLE and Take-off power detent) 21 to 35 kts FLIGHT IDLE 36 to 50 kts DISC (gusts to 55kts)

A

For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground static operation is as follows

189
Q

START MAX TIME ON… FOLLOWED BY… 1 60 secs 2 mins off 2 60 secs 2 mins off 3 60 secs 30 mins off NOTE: If the APU does not start in the third attempt, maintenance action is required.

A

APU Starter Cranking Limits

190
Q

100%

A

Maximum torque

191
Q

101.2%

A

Transient (20 seconds maximum) Max. N(H) % rpm

192
Q

100%

A

Max Continuous (MCP) Max. N(L) % rpm

193
Q

600 lb.

A

Maximum fuel imbalance between the main fuel tanks

194
Q

102.3%

A

Transient (20 seconds maximum) Max N(L) % rpm

195
Q

204 KIAS

A

Maneuvering Speed (Va)

196
Q

35%

A

Max. reverse Max. torque %

197
Q

20,000 ft

A

Powerplant: Maximum Altitude for Airstart

198
Q

215 KIAS

A

Landing Gear Extended Speed (Vle)

199
Q

0.1

A

Standby, Auxiliary, and Main Battery Maximum loadmeter reading for takeoff

200
Q

1173 rpm

A

Transient (20 seconds maximum) Max. N(P) rpm

201
Q

GSP approaches, RAIM must be available at the final approach fix.

A

Instrument approaches must be conducted in the approach mode and for

202
Q

The Normal Take-off ITT limit for a given ambient air temperature is given in “Variation of ITT with Ambient Air Temperature for NTOP” below.

A

Normal Take-off (NTOP) Max ITT C

203
Q

32 knots

A

Maximum crosswind component approved for take-off and landing, on a hard, dry or wet runway

204
Q

275 KIAS

A

Vmo 20,000 ft

205
Q

100%

A

Max. Reverse Max N(H) % rpm

206
Q

182 kts groundspeed

A

Maximum tire speed

207
Q

64.2%

A

Minimum N(H)

208
Q

15 during the approach to the final segment

A

All flaps 35 landings will be done with a maximum flap setting of…

209
Q

10% torque (nominal)

A

Powerplant: Automatic Take-Off Power Uptrim

210
Q

10 kts

A

Maximum tailwind component approved for takeoff with flaps 5 or landing with flaps 10 or 15

211
Q

920 C 20 seconds maximum

A

Starting Max ITT C

212
Q

HOT MIC select switches on the pilot and co-pilot ARCDU must be OFF and the INT/RAD switch on the observers Audio Control Panel must be centered, when using the cockpit speakers.

A

Flight Compartment Communication Limit

213
Q

15,000 ft

A

Maximum altitude for extending or extended landing gear or wing flap is

214
Q

0 C (55 C for take-off in icing conditions)

A

Minimum oil temperature above ground idle

215
Q

61 to 72

A

Max Continuous (MCP) Oil Press PSID

216
Q

1.0

A

Standby, Auxiliary, and Main Battery Maximum load air/ground

217
Q

once every 24 hours (flying day)

A

To ensure uninterrupted operating of the pilot’s and co-pilot’s PFD, MFD and the ED, electrical power must be cycled on all displays…

218
Q

107 C

A

Max continuous oil temperature above ground idle

219
Q

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

A

Fuel Heater limit

220
Q

severe atmospheric turbulence prohibited

A

Flight in conditions of _______ ________ _______ with autopilot engaged is _________.

221
Q

ISA +25 C

A

Powerplant: With Bypass Doors Open, take-off, landing and setting MTOP and MCP are limited to a maximum ambient temperature limitation of

222
Q

route of flight installed and operating so as to provide an alternate means of navigation.

A

The aircraft must have approved navigation equipment appropriate to the

223
Q

5,862 lb per tank

A

Usable fuel tank capacities per tank

224
Q

The flight compartment door must be closed and locked at all times during flight except to provide access egress as required per the FOM and SOP400.

A

Flight Compartment Door Limit

225
Q

880 C

A

Max. Take-off (MTOP) (1) Max ITT C

226
Q

44 to 61 psi

A

Transient minimum oil pressure

227
Q

64,500 lbs

A

Serial numbers: 4168, 4181, 4182, 4186 Maximum Take-off Weight

228
Q

5.46 +/- 0.1 psi

A

Normal cabin pressure differential limit

229
Q

61 to 72

A

Max. Take-off (MTOP) (1) Oil press PSID

230
Q

58,000 lbs

A

Serial numbers: 4187 and above Maximum Zero Fuel Weight

231
Q

100 feet

A

Minimum Runway Width

232
Q

14 kts

A

Maximum crosswind component Runway with standing water, slush or wet snow

233
Q

125 C Max. (5 seconds maximum for torque values above flight idle and less than 55%)

A

Transient (20 seconds maximum) Oil Temp C

234
Q

210 KIAS

A

Rough Air Speed

235
Q

only be conducted with the FMS in terminal mode.

A

P-RNAV operations may

236
Q

158 KIAS

A

Flap Extended Speed (Vfe) Flap 35

237
Q

-54 C to +50 C or ISA +35 C, whichever is lower

A

Powerplant Ambient temperature limitations

238
Q

61 to 72 psi

A

Normal operating range (oil pressure)

239
Q

65 C

A

Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power

240
Q

At 70F the minimum Crew oxygen and Portable oxygen pressure for dispatch is as follows: Portable oxygen 1600 psi 3 Crew 1450 psi 2 Crew 1050 psi

A

Oxygen Limit

241
Q

55 C

A

Minimum oil temperature required to ensure engine air inlet ice protection, prior to take-off

242
Q

44 to 61 72 to 100

A

Transient (20 seconds maximum) Oil Press PSID

243
Q

57,000 lbs

A

Serial numbers: 4168, 4181, 4182, 4186 Maximum Zero Fuel Weight

244
Q

880 C

A

Max. Reverse Max. ITT C

245
Q

are retrieved from the FMS database.

A

Instrument approaches must be accomplished in accordance with instrument approach procedures that

246
Q

final approach fix 1000 inoperative engine

A

An autopilot approach must be continued past the ______ _______ ___ or ____ feet AGL, whichever is lower, with an _______ ______.

247
Q

temperature compensation function is activated, it may produce VNAV paths with climb segments, and result in a VNAV disconnect.

A

When altitudes are manually entered before or after the

248
Q

0 to 107 C

A

Normal Take-off (NTOP) Oil Temp C

249
Q

106%

A

Max Take-off (MTOP) (1) Max Torque %

250
Q

282 KIAS

A

Vmo 10,000 ft

251
Q

non published approaches under instrument meteorological conditions is prohibited.

A

Navigation by means of Pilot-defined,

252
Q

13.8% MAC

A

Serial number: 4187 and above Forward limit (all weights up to 53,000 lbs.):

253
Q

0 to 107 C

A

Max. Reverse Oil Temp C

254
Q

65,200 lbs

A

Serial numbers: 4187 and above Maximum Take-off Weight

255
Q

200 KIAS

A

Flap Extended Speed (Vfe) Flap 5

256
Q

-40 C

A

Minimum oil temperature for start up

257
Q

200 KIAS

A

Landing Gear Operating Speed (Vlo)

258
Q

0.5 psi

A

Maximum cabin pressure differential limit during taxiing, take-off and landing

259
Q

Brake cooling times must be observed between a landing or a low-energy rejected take-off and a subsequent takeoff, to ensure that sufficient brake energy is available to bring the airplane to a complete stop if the subsequent takeoff is rejected.

A

Wheel Brake Cooling Limits

260
Q

61,750 lbs

A

Serial numbers: 4168, 4181, 4182, 4186 Maximum Landing Weight

261
Q

Setting take-off power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than 8 kts.

A

Take-off Power Setting Limitation

262
Q

920 C

A

Transient (20 seconds maximum) Max ITT C

263
Q

20 kts

A

Maximum tailwind component approved for take-off with flaps 10 or 15 or landing with flaps 35

264
Q

100%

A

Max Continuous (MCP) Max Torque %

265
Q

13.8% MAC

A

Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (all weights up to 53,000 lbs.):

266
Q

-35 C

A

APU ambient temperature (lower)

267
Q

-40 C min.

A

Starting Oil Temp C

268
Q

181 KIAS

A

Flap Extended Speed (Vfe) Flap 10

269
Q

61 to 72

A

Normal Take-off (NTOP) Oil Press PSID

270
Q

50 kts

A

Maximum wind speed for ground operation, with nose of the airplane more than 30 degrees out of the wind

271
Q

-54 C

A

Airplane minimum operating ambient temperature limit

272
Q

prior to take-off

A

APU must be shutdown…

273
Q

25,000 ft

A

Maximum operating altitude

274
Q

Single Engine Taxi is not authorized. Reverse Taxi is no authorized. Note: Exiting the runway after a single engine landing is acceptable.

A

Taxi Limitations

275
Q

61 to 72

A

Max. Reverse Oil Press PSID

276
Q

Pratt & Whitney, PW 150A

A

Powerplant Manufacturer and Model

277
Q

must not be used as the primary means for computing fuel load and range.

A

Fuel display parameter is advisory only and

278
Q

are prohibited.

A

FMS based ILS and MLS approaches

279
Q

-20C

A

Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff

280
Q

100 max. 165 (Maximum oil pressure at discing with OAT below 0 C)

A

Starting Oil Press PSID

281
Q

WIND SPEED MAX POWER SETTING (GROUND) 9 to 20 kts FLIGHT IDLE (power levers may be momentarily increased above flight idle) 21 to 35 kts FLIGHT IDLE 36 to 50 kts FLIGHT IDLE (must be at DISC with airplane static)

A

For wind speed greater than 8 kts, with the nose of the airplane more than 30 degrees out of wind, the maximum power for ground maneuvering is as follows

282
Q

90.3% (NTOP torque indication will be 90% or 91%)

A

Normal Take-off (NTOP) Max Torque %

283
Q

VOR DME APP

A

Use of ___ without associated ___ is prohibited in ___ mode.

284
Q

disengaged severe

A

Autopilot must be ________ in _______ icing.

285
Q

+ 2.0 g 0.0 g

A

Maneuvering Limit Load Factors Flap extended

286
Q

18 kts

A

Maximum crosswind component Runway with dry loose snow (4.0 inches for take-off, 5.1 inches for landing)

287
Q

Dowty Aerospace R408

A

Propeller Manufacturer and Model

288
Q

100%

A

Max. Take-off (MTOP) (1) Max N(H) % rpm

289
Q

a. Flap 0 (minimum altitude: 1,000 AGL) b. Flap 5, 10, 15 and 35

A

APP mode, autopilot engaged approaches, is approved for:

290
Q

seated harness secured

A

During autopilot operation, the pilot must be ________ at the controls with _______ ________.

291
Q

62,000 lbs

A

Serial numbers: 4187 and above Maximum Landing Weight

292
Q

185 KIAS

A

Alternate Gear Extension Speed

293
Q

1020 (maximum allowable continuous N(P) overspeed is 1071 rpm.)

A

Max. Take-off (MTOP) (1) Max N(P) rpm

294
Q

0 to 107 C

A

Max Continuous (MCP) Oil Temp C

295
Q

POWER FLIGHT IDLE

A

In-flight operating of the ______ levers aft of the _____ ____ gate is prohibited.

296
Q

1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm

A

Normal Take-off (NTOP) Max. N(P) rpm

297
Q

6 degrees in enroute and terminal mode and greater than 4 degrees in approach mode are prohibited.

A

VNAV vertical path angles greater than

298
Q

0 C

A

Minimum oil temperature above FLT IDLE

299
Q

On the ground, operating of landing (APPROACH and FLARE) lights is limited to 5 minutes (This does no preclude continuous operation of the TAXI light).

A

Republic Airlines Imposed Light Limitations

300
Q

Category C

A

Aircraft Approach Category

301
Q

-40 C

A

Minimum oil temperature at ground idle

302
Q

The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in “Variation of N(H) and N(L) with Ambient Air Temperature for NTOP”.

A

Normal Take-off (NTOP) Max. N(H) % rpm

303
Q

navigation guidance if the reference coordinated data system for the intended route is referenced to in WGS-84 and NAD-83.

A

The FMS may only be used for

304
Q

+ 2% (uphill) - 2% (downhill)

A

Maximum runway slopes approved for take-off and landing

305
Q

286 KIAS

A

Vmo 18,000 ft

306
Q
  1. Day and night VFR 2. IFR 3. Icing Conditions
A

Kinds of Operation

307
Q

200

A

On precision approaches, the autopilot must be disengaged at or above a min altitude of _____ feet AGL.

308
Q

125 C

A

Maximum oil temp PLA between Disc and FLT IDLE

309
Q

WIDE CUT TYPE

A

The use of _____ ____ _____ FUELS is prohibited

310
Q

36.0% MAC

A

Serial Numbers: 4168, 4181, 4182, 4186 Aft limit:

311
Q

50 C or ISA +35 C whichever is lower

A

Airplane maximum operating ambient temperature limit

312
Q

VFR/IFR enroute, terminal, and approach LNAV and VNAV operations.

A

The UNS-1E is approved for

313
Q

+50 C or ISA +35 C, whichever is lower

A

APU ambient temperature (upper)

314
Q

36.0% MAC

A

Serial Numbers: 4187 and above Aft limit:

315
Q

The Normal Take-off N(H) and N(L) limit for a given ambient air temperature is given in “Variation of N(H) and N(L) with Ambient Air Temperature for NTOP”.

A

Normal Take-off (NTOP) Max. N(L) % rpm

316
Q

FMS may be conducted only when magnetic variation is input manually into the system or an alternate true heading source is used and no manual variation has been input.

A

Flight above 73 degrees north latitude or below 60 degrees latitude using the

317
Q

+21 C maximum ambient temperature

A

With APU inlet louvres installed, APU operation is limited to

318
Q

245 KIAS

A

Vmo 0 to 8,000

319
Q

FMS Data Base expired FMS Data Base expired verifies the waypoints for accuracy by reference to current publications.

A

FMS Approach Navigation is prohibited with the ___ ___ ___ ___. IFR enroute and terminal navigation is prohibited with the ___ ___ ___ ____ expired unless the Pilot….

320
Q

the maximum wind speed provided to maintenance within 24 hours (flying day)

A

NOTE: Ground operations in winds greater than 50 kts must be recorded and…

321
Q

8,000 ft

A

Maximum cabin altitude (pressurized flight)

322
Q

0 C to 107 C

A

Max. Take-off (MTOP) (1) Oil temp C

323
Q

…with passengers onboard …during pressure refueling

A

APU must not be operated unattended…

324
Q

200 ft. AGL.

A

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

325
Q

13.8% thru 17.7% MAC

A

Serial Numbers: 4187 and above Forward limit (53,000 lbs. thru 64,500 lbs.):

326
Q

100%

A

Max Continuous (MCP) Max N(H) % rpm

327
Q

MDA plus fifty (50) feet. This is referred to as a Derived Descent Altitude (DDA) and allows for dip during a missed approach without descending below the charted LNAV MDA.

A

On RNAV approaches where vertical guidance (VNAV Mode) is used, the Company must bug

328
Q

1020 rpm

A

Max. Reverse Max N(P) rpm

329
Q

CAT I limits only.

A

AFCS is approved for autopilot approaches to ___ _ _____ ____.

330
Q

GROUND OPERATIONS ONLY

A

APU is approved for what kind of operation?

331
Q

1020 rpm Maximum allowable continuous N(P) overspeed is 1071 rpm

A

Max Continuous (MCP) Max N(P) rpm

332
Q

10,000 ft

A

Maximum operation altitude for take-off and landing

333
Q

Tank 1 or take 2 auxiliary fuel pumps must be on for take-off and landing.

A

Auxiliary Fuel Pumps limitation

334
Q

the Operator’s Manual, Report no. 2423sv801 (or equivalent at current revision) must be available to the Flight Crew.

A

Whenever navigation is predicated on the FMS,

335
Q

1 hour flying time from a suitable airport for landing

A

With Integrated Standby Instrument installed the airplane must not be operated further than

336
Q

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

A

Cargo Compartment Limit

337
Q

172 KIAS

A

Flap Extended Speed (Vfe) Flap 15

338
Q

1,000 ft. AGL.

A

After take-off or go-around, the minimum height for autopilot engagement is

339
Q

temperature compensation function is activated. All manually entered altitudes must be adjusted with the appropriate temperature correction before they are entered into the FMS, even if the temperature compensation function is not active.

A

SCN 802.2, SCN 802.8: Manually entered altitudes will not have an altitude correction applied when

340
Q

Engine intake bypass doors must be open for engine operating in icing conditions. When ice is detected the AIRFRAME MODE SELECT selector must be positioned at FAST.

A

Ice Protection Limit

341
Q

248 KIAS

A

Vmo 25,000 ft

342
Q

64,700 lbs

A

Serial numbers: 4168, 4181, 4182, 4186 Ramp Weight

343
Q

107 C

A

Maximum Oil Temperature above ground idle

344
Q

13.8% thru 17.4% MAC

A

Serial Numbers: 4168, 4181, 4182, 4186 Forward limit (53,000 lbs. thru 64,500.):

345
Q

880 C

A

Max Continuous (MCP) Max ITT C

346
Q

the SAT on the ground and for take-off 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.

A

Icing conditions exist when:

Q400 (19 decks)

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