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CL650 AOM > Chapter 9 of AOM > Flashcards

Chapter 9 of AOM Flashcards

1
Q

9.2.1

45 min fuel requirement per Netjets

A

2019 lbs

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2
Q

9.2.1

Minimum Release Fuel

A

4000 lbs

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3
Q

9.2.1

Hot Spare Required Fuel

A

8500 lbs

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4
Q

9.2.1

Emergency release fuel

A

1500 lbs

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5
Q

9.2.2

Minimum dry runway length for release

A

4500 feet

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6
Q

9.2.2

Minimum runway width for release

A

75 feet

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7
Q

9.2.2

Max runway slope for release

A

(+-) 2%

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8
Q

9.2.2

Chief Pilot/ACP Approval required if runway length is less than: (dry/wet)

A

Dry: Less than 5000 feet Wet: Less than 5800 feet

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9
Q

9.2.2

What is the foot note (1) with regards to minimum length required for release

A

Upon arrival, land if LPA calculated length is less than the landing distance available

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10
Q

9.2.3 (Red Letter)

Max crosswind for Dry and Wet Runway

A

24 knots

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11
Q

9.2.3 (Red Letter)

Max Crosswind Fair/Medium Contaminated runway conditions

A

15 knots

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12
Q

9.2.3 (Red Letter)

Max crosswind for poor runway conditions

A

10 knots

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13
Q

9.2.4 (Red Letter)

Max tailwind

A

10 knots

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14
Q

9.2.5

What is the maximum Mach number in RVSM

A

.83 Mach

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15
Q

9.3.3 (Red Letter)

Max Certified Ramp and Taxi weight

A

48,300 lbs

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16
Q

9.3.3 (Red Letter)

Max Certified Takeoff weight

A

48,200 lbs

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17
Q

9.3.3 (Red Letter)

Max Certified Landing weight

A

38,000 lbs

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18
Q

9.3.3

Max Certified Zero fuel weight

A

32,000 lbs

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19
Q

9.3.4

Max weight in the baggage compartment

A

900 lbs

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20
Q

9.4 (Red Letter)

Max Certified Altitude for Operations

A

41,000 feet

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21
Q

9.4

Max Certified Pressure Altitude for Takeoff and Landing

A

10,000 feet

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22
Q

9.4 (Red Letter)

Max Certified altitude for Flaps Extended (Odd number?)

A

15,500 feet

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23
Q

9.4

Max Certified altitude for landing gear extended

A

20,000 feet

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24
Q

9.4

Minimum Certified altitude for use of Flight Spoilers

A

300 feet

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25
Q

9.5

Minimum temperature for takeoff

A

-40 degrees C

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26
Q

9.5

Maximum temperature for takeoff and landing

A

ISA +35

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27
Q

9.5

What does the AOM ask you to refer to with respect to Altitude and temperature operations

A

Refer to the AFM

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28
Q

9.6 Vfe (Red Letter)

Max airspeed for flaps 20

A

231 knots

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29
Q

9.6 Vfe (Red Letter)

Max speed for flaps 30

A

197 knots

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30
Q

9.6 Vfe (Red Letter)

Max speed for flaps 45

A

189 knots

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31
Q

9.6 Vle (Red Letter)

Max landing gear extended speed (knots/mach)

A

250/.7

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32
Q

9.6 Vlo (Red Letter)

Max landing gear operating speed (knots/mach)

A

197/.6

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33
Q

9.6

Max tire speed

A

182 knots

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34
Q

9.6 Vturb (Red Letter)

Max Turbulent air penetration speed (knots/mach)

A

280/.75

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35
Q

9.7

Max press differential

A

9.2 psi

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36
Q

9.7

Max negative relief

A

-0.5 psi

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37
Q

9.7 (Red Letter)

Max Press Differential for taxi and takeoff

A

0.2 psi

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38
Q

9.7 (Red Letter)

Max Press Differential for Landing

A

0.2 psi

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39
Q

9.8

With respect to Oxygen duration for over water ops what does the AOM ask you to refer to?

A

Oxygen Duration tables in FCOM Supplemnts

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40
Q

9.8

Max number of pax including lap children

A

14 due to number of installed oxygen masks

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41
Q

9.9.1

What are the time restrictions for starting the APU using the aircraft batteries on the ground or in-flight

A

Three 30-second start attempts of continuous cranking, followed by a 20 minutes of cooling time. Followed by two further 30-second attempts. If not successful do not attempt additional starts for at least 35 minutes

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42
Q

9.9.1

What are the time limits for starting the APU with a ground power unit (GPU)

A

Two 15 seconds start attempts of continuous cranking, followed 20-minutes of cooling time. Two further 15-second attempts of continuous cranking If not successful do not attempt additional starts for at least 35 minutes

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43
Q

9.9.1 (Red Letter)

How many APU start attempts in an hour

A

3

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44
Q

9.9.1 (Red Letter)

What is the Max altitude for starting the APU

A

20,000 feet

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45
Q

9.9.1

Minimum Temperature for starting the APU

A

-40 degrees C

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46
Q

9.9.1

Maximum Temperature for the APU during start

A

974 degrees C

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47
Q

9.9.1 (Red Letter)

Maximum operating altitude for the APU Bonus: does this include bleed air?

A

20,000 feet No. 15,000

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48
Q

9.9.1

Can you use the APU for single engine in-flight restart

A

APU use prohibited

49
Q

9.9.1 (Red Letter)

Maximum altitude for bleed air use

A

15,000 feet

50
Q

9.10

Do not use the Autopilot for what three things

A

Takeoff

Landing

Any approach with a glidepath angle greater than 40

51
Q

9.10. Autoflight

What are the Autopilot Minimum Altitude (AGL):

After takeoff

Cat I ILS or LPV (GS less than 5.30)

IPA to MDA

A

320 ft

80 ft

320 ft

52
Q

9.11.1 Electiral (Batteries)

Minimum votage for engine start or APU start

53
Q

9.11.2 AC Generator Load Limits

What is the Generator load limit from

0 to 20,000 feet (Main / APU)

20,001 to 35,000 feet (Main / APU)

Above 35,000 feet

A

Main 30 / APU 30

Main 30 / APU 0

Main 25

54
Q

9.11.3 DC TRU Load Limits

Maximum Continuous

55
Q

9.12 External Lights

What are the limitation on RECOG TAXI LTS

A

Do not illuminate while the aircraft is not moving

56
Q

9.12 External Lights

What is the limitation on the Landing Lights

A

Do not illuminate on the ground, except for takeoff or landing

57
Q

9.14 Fuel

What is the fuel quantity in lbs for the left or right main tanks

A

4,860 lbs each

58
Q

9.14 Fuel

What is the fuel capacity of the Auxiliary tank

59
Q

9.14 Fuel

What is the fuel capacity of the tail tank

60
Q

9.14 Fuel

What is the total fuel capacity (Pressure fueling) of all the tanks (Red Letter)

A

20,000 lbs

61
Q

9.14 Fuel

What is the total fuel capacity if Gravity fueling (aircraft level)

A

Reduce pressure fueling weight by 7%

62
Q

9.14 Fuel

Fuel imbalance (Red Letter)

What is the max fuel imbalance during Taxi, Takeoff and Landing

63
Q

9.14 Fuel

Fuel imbalance (Red Letter)

What is the max imbalance during flight

64
Q

9.14 Fuel

What is the Minimum fuel1 per tank for go-arounds

A

500 lbs

1 Bank and pitch must be limited to wings level and 100 nose up

65
Q

9.14.1 Auxiliary Tank Fuel Load Restrictions

What are the restrictions for the Aux tank

A

See AOM page 9-7

66
Q

9.14.2 Fuel Temperature Limitation

Do not takeoff if engine fuel temperature is below what temperature

BONUS: Where do you find this temperature reading

A

Below 5o

On the EICAS synoptic “Summary” page

67
Q

9.14.2 Fuel Temperature Limitations

What temperature must Bulk fuel stay above

A

Must remain above it applicable freezing point

68
Q

9.14.3 Fuel Jettison

What are the 2 limits for fuel jettison

A
  1. Flap must be 0
  2. Do not jettison in known lightning conditions
69
Q

9.14.4 Fuel transfer

Can you takeoff with fuel transfer on

A

No. Must be off during takeoff

70
Q

9.14.4 Fuel Transfer

During normal Operation can you use the tail tank transfer system as a center of gravity conrol device

A

No. During normal operations it must remain in the automatic mode

71
Q

9.14.4 Fuel Transfer

During manual transfer operations how do you determin Aux Tank Quantity when the Tail Tank contains greater than (1) 1200 lbs (2) less than 1200 lbs (Table 9.16 : Page 9-8 of the AOM)

A
  1. 2.75 x tail tank qty
  2. 2.2 x tail tank qty
72
Q

9.14.4 Fuel Transfer

Can you manually transfer tail tank fuel with more than 7000 lbs of fuel in the Aux tank

A

No, do not do this…

73
Q

9.14.4 Fuel Transfer

What is the Caution associated with manual tail tank fuel transfer

A

Continuously monitor aux tanks quantity for overfill

74
Q

9.16.1 Ice and Rain Protection

What are the 3 things for icing conditions exist on the ground when

A
  1. SAT is 10o or below
  2. Visible moisture (rain, snow or vis less than 1 sm) is present
  3. Operating on contaminated surfaces
75
Q

9.16.1 Ice and Rain Protection

What are the 3 things for Icing conditons to exist in flight

A
  1. EICAS mssage ICE is displayed
  2. TAT is 10o C or below
  3. Visiable moistrue (rain, snow or vis lest than 1 sm) is present

Except when SAT is -40o C or below

76
Q

9.16.1 Ice and Rain Protection

What is the restriction pertaining to flight in freezing rain

A

Prohibited

77
Q

9.16.2/3 Engine/Wing (Red Letter)

In accordance with Chp 4 para 6.4 operate COWL’s on when the temp on the ground is…

A

OAT 10o C or below

78
Q

9.16.2/3 Engine/Wing (Red Letter)

In accordance with Chp 4 para 6.4 operate COWL’s on and Wings Norm2 when the temp on the ground is…

A

OAT 5o C1 or below just prior to takeoff

1 Anytime temp is 5o C or below, even when all of the conditions above are not present, operate WING anti-ice during taxi. Turn off prior to takeoff.

2 If anti-ice fluid was applied select NORM prior to takeoff

79
Q

9.16.2/3 Engine/Wing (Red Letter)

In accordance with Chp 4 para 6.4 operate COWL’s on, Wings Norm when the temp inflight and below 22,000 feet is…

A

TAT 10o or below3

3 Unless SAT is -40o C or below

80
Q

9.16.2/3 Engine/Wing (Red Letter)

In accordance with Chp 4 para 6.4 operate COWL’s on, Wings Norm when the temp inflight and above 22,000 feet is…

A

TAT 10oC or below3 and ice detector has failed

3 Unless SAT is -40o C or below

81
Q

9.16.4 Probes

What is the limitation on the ground with regards to Probe heat

A

Limited to 2 min when the temp is 15o C or greater

82
Q

9.17.1 Display Unit Operating Temperature

What is the restrictions on Display Units when on the ground and the temperature exceeds 40o C

A

Do not power on for more than 30 min unless one air conditioning pack is operating and pax door is closed

83
Q

9.18.3 Brakes

What is the min turn time with regards to breaks not including RTO’s

A

15 min

Refer to AFM for RTO brake cooling times

84
Q

9.19.3 Synthetic Vision System (SVS)

Can you use SVS for navigation

85
Q

9.19.3 Sysnthetic Vision System (SVS)

When operating outside WGS-84 and NAD-83 what must you do with SVS

A

Deselect SVS prior to FAF

86
Q

9.16.3 Synthetic Vision System (SVS)

When must you de-select SVS

A

When conducting an approach to a runway not in the FMS flight plan (e.g., side-step maneuver)

87
Q

9.19.1 Electronic Flight Instrument System (EFIS)

When must you not use MAP PLAN display for navigation

A

When operating north of 70N or south of 70S

88
Q

9.19.1 Electronic Flight Instrument System (EFIS)

OBSTACLE symbols on MFW MAP are to be used for…

A

Situational Awareness only

89
Q

9.19.4 Integrated Flight Imformation System (IFIS)

Can you use IFIS Charts databases when not current

A

Use is Prohibited

90
Q

9.19.4 Integrated Flight Information System (IFIS)

Can Geopolitical boundaries, Controlled and Special Use airspace on the MFD MAP be used for navigation

A

Use is Prohibited

91
Q

9.19.4 Integrated Flight Information Systems (IFIS)

Can the aircraft sysmble on any charts (apprach or taxi) be used for navigation or precision maneuvers on the ground

A

Use is Prohibited

92
Q

9.19.5 Terrain Awareness System (TAWS)

What three countries does the TAWS database accunt for known man-made obstrucions

A

Canada

US

Mexico

93
Q

9.19.5 Terrain Awareness Warning System (TAWS)

If landing at an airport not contained in the TAWS database what must be done with the TAWS

A

Select TAWS TERRAIN OFF

94
Q

9.19.5 Terrain Awareness Warning System (TAWS)

If QFE operations with no GPS sensors available what must be done with TAWS

A

Select TAWS TERRAIN OFF

95
Q

9.19.5 Terrain Awareness Warning System (TAWS)

Can you navigate based on the terrain awareness display

96
Q

9.19.6 RNAV and RNP Operations

The aircraft is equipped with the Rockwell Collins Pro Line 21 Avionics System. What Table in the AOM can you find authorized IFR Operations

A

Table 9.17

97
Q

9.19.7 FMS

Can you use the FMS as the primary source of navigation during Dead Reckoning operations

98
Q

North of 73o and Candadian Northern airspace flights can the FMS be used as the primary source of navigation

99
Q

9.19.7 FMS

In flight can you use the FPLAN RECALL or laod a route from PILOT ROUTE within the FMS

100
Q

9.19.7 FMS

Is tuning NAVAID using identifier only on the FMS authorized

101
Q

9.19.7 FMS

To retrieve approaches from the FMS does the database have to be current

102
Q

9.19.7 FMS

To use the FMS for terminal operations and en route must the database be current or pilot-verified

103
Q

9.19.7 FMS

To conduct dual FMS approaches must the flight plans be identical

104
Q

9.19.7 FMS

To continue an approach past the FAF using the FMS what must be displayed on the PFD

105
Q

9.19.7 FMS

For approach guidance while conducting appraches using WGS-84 or NAD-83 coordinates reference data the FMS must use input from were

106
Q

9.19.7 FMS

If two air data computers are available is FMS thrust data primay

107
Q

9.19.7 FMS

If two flight management computers are available is FMS V speed informations primary

108
Q

9.19.7 FMS

RNP operations require verification of PFD CDI scale annuciation, what table in the AOM can you reference

A

Table 9.18: RNP Scale Limits

109
Q

9.19.7 FMS

If the FMS message LOSS OF INTEGRITY is displayed can you continue RNP operations

A

No, Prohibited

110
Q

9.19.7 FMS

If the GNSS-FMS DISAGREE message is displayed on the FMS can you continue RNP operations

A

No, Prohibited

111
Q

9.19.7 FMS

If NO APPR is displayed on the FMS can you continue RNP operations

A

No, Prohibited

112
Q

9.19.7 FMS

If the message UNABLE RNP is displayed can you continue RNP operations

A

No, Prohibited

113
Q

9.19.7 FMS

Is the FMS fuel and range information advisory information or Primary infromation

A

Advisory only

114
Q

9.19.7 FMS

Can operations be predicated upon Required Time of Arrival (RTA) or fuel remaining calculations

115
Q

9.19.8 VNAV

Using QFE barometric altitudes can you use VNAV

116
Q

9.19.8 VNAV

After go-around can I use VNAV

A

No, not until completion of the missed approach procedure

117
Q

9.19.8 VNAV

During climb can I use VFLC (FLC with VNAV) when the airspeed reference is displayed as Mach

A

No, do not use VFLC

118
Q

9.19.9 Approach

CL650 AOM (6 decks)

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