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Challenger 350 Flashcards rev0124 > CL350 AFM/AOM Limitations (NICE TO KNOW) Rev0124 > Flashcards

CL350 AFM/AOM Limitations (NICE TO KNOW) Rev0124 Flashcards

Learn aircraft limitaions

1
Q

AOM Required Fuel Quantities:
1. 45-min IFR Reserve
2. Hot Spare
3. Inclement Wx

A
  1. 45-min IFR Reserve: 1850 lbs
  2. Hot Spare: 6000 lbs
  3. Inclement Wx: 6000
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2
Q

Ice and Rain Protection
Ground Operations

When visible moisture is present or operating on contaminated surfaces

A

OAT +10° or below:

L and R Engine - On
Wing - Off

AOM 9.16

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3
Q

Runway Requirements
Minimum Runway Width

A

70ft

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4
Q

Max Runway Slope for Takeoff and Landing

A

+2% uphill

-2% downhill

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5
Q

Runway Requirements
Ops Review Required if contaminated lngth is less than?

A

5500’

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6
Q

Specific Airport Restrictions

A

Roadtown, BVI (TUPJ)
Length 3957’ / Width 98’
Day Only
Dry Dpeartures Only

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7
Q

RVSM Airspace
Operational Systems Requirements

A

Autopilot (1)
Altitude Alerting Device (1)
ATC Altitude Reporting Transponder (1)
Air Data Computer (2)
Pitot Probe Heaters (2) on probes linked to ADC in use

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8
Q

Takeoff Weight
Maximum Takeoff Weight is limited by the most restrictive of the following:

A
  • Max certified Takeoff Weight
  • Max Runway-limited Takeoff Weight
  • Tired Speed and Brake Energy Limit Weights
  • Maximum Takeoff Weight (Climb Limited)
  • Obstacle Clearance, En Route and Landing Weight Limitations
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9
Q

Landing Weight
The maximum landing weight is limited by the most restrictive of the following:

A

Max certified landing weight
Max landing weight (Runway length plus obstacle)
Max Landing weight (climb limit or brake energy limits)

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10
Q

Max Zero Fuel Weight

A

28,200 lbs

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11
Q

Baggage Compartment Placards

A

Weight limits are placarded above each compartment

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12
Q

Max Takeoff and Landing Pressure Altitude

A

10,000’

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13
Q

Max Flap Extension Altitude

A

18,000’

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14
Q

Max Altitude for Gear Extension

A

18,000’

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15
Q

Min Takeoff Weight

A

25,000 lbs

(due to Vmcg)

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16
Q

Min Flight Weight

A

24,800 lbs

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17
Q

Vmo (above 8000’)

A

320 KIAS

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18
Q

Mmo
(above 29,475’)

A

.83 mach

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19
Q

Vmo (up to 8000’)

A

300 KIAS

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20
Q

Max Tire Groundspeed

A

182 kts

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21
Q

Minimum Control Speed
Vmcg (Flaps 10/20)

A

Vmcg Flaps 10: 115 kts
Vmcg Flaps 20: 114 kts

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22
Q

Minimum Control Speed
Vmca (Flaps 10/20 takeoff)

A

Vmca Flaps 10 (takeoff): 110 kts
Vmca Flaps 20 (takeoff): 109 kts

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23
Q

ECS (Air Conditioning) limitations during ground ops

A

Do not select the AIR SOURCE switch TRIM AIR ONLY while the aircraft is on the ground.

PACK must be operating when electrical power is on for more than 30 minutes and the OAT is above +40C.

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24
Q

Pressuriaztion (psi)
Max Differential

A

9.4 (S/N 20886 and before)
10.1 (S/N 20887 and later)

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25
Q

Pressuriaztion (psi)
Max Negative

A

-.5PSI

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26
Q

OXYGEN QUANTITY LOW

A

<700L O2 Remains

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27
Q

Crew and Pax Oxygen Masks

A

Crew and Pax oxygen masks are not approved for use above 40,000’ cabin altitude.

Prolonged operation of Pax masks above 25,000’ cabin altitude is not recommended.

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28
Q

APU Limits:
Max Pressure Altitude to start left engine

A

9000’ (pressure altitude)

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29
Q

APU Operating Restrictions (4)

A

Do not operate the APU under the following conditions:
* During ground de/anti-icing procedures
* Above 37,000’
* Do not use generator above 30,000’
* Do not use bleed air above 20,000’

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30
Q

Autopilot Limitations:
Glidepath Angle Limits

A

If glidepath angle is more than 3.5degrees, disengage autopilot by 160’

*Normal precision approach glidepath: 80’

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31
Q

Autopilot Limitations:
5G Limitations

A

For 5G non-tolerant aircraft operating in the contiguous US airspace, autopilot operation on approach below 1000’ is prohibited

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32
Q

Max Generator Load

A

Continuous:
In flight, with 2 or 3 generators operating: 400A

On ground, one generator operating 400A
*Caution using hydraulics with only APU Gen operating

In flight, one generator operating: 500A

Transient (5 minutes): 600A

Do not takeoff with Battery temperature below -20C

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33
Q

Electrical Load Limitations:
1 Generator operating

A

500A

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34
Q

Electrical Load Limitations:
Transient (5min)

A

600A

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35
Q

Min airspeed and altitude for Flight Spoiler Extension

A

Vapp +8
Min 500’ AGL

Straight-In Approach (Vref min)
Vapp = Vref+8

Circling Approach (ref+10min)
Vapp = Vref+10+8

Do not select EMER except during emergency conditions or when required by procedure.

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36
Q

Max Fuel Quantity:
Pressure Refueling
Gravity Refueling

A

14,150lbs Pressure Refueling
13,000lbs Gravity Refueling

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37
Q

Max Fuel Imbalance

A

Total fuel >13,700 = 250 lbs max
Total fuel 10,000-13,700 = 315 lbs max
Total fuel 10,000-4,700 = 450 lbs max
Total fuel <4,700 = 600 lbs max

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38
Q

Min Go Around Fuel

A

500 lbs per side
(1000 lbs total)

*Collector tanks hold 500lbs each.

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39
Q

Max Fuel Imbalance During Gravity Refueling

A

250lbs

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40
Q

Max single-point refueling pressure

A

55 psig

Defuel limited to -8 psig

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41
Q

Max Bulk Fuel Temp for Takeoff

A

+50C

With wing bulk fuel temp at +45C or above min fuel load for takeoff is 2,800 lbs

With <1,000 lbs of fuel per side do not operate engines for more than 30 minutes.

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42
Q

Min Bulk Fuel temp, Jet A

A

-30C

43
Q

Cockpit Speaker Mute System

A
  • When cockpit speakers are muted, both pilots must use headsets
  • When one pilot removes headset, select COCKPIT SPEAKER MUTE - OFF
44
Q

Ice and Rain Protection

Frost limitations

A

*NetJets adheres to the clean wing concept.

Takeoff is prohibited with frost, ice snow or slush adhering to any critical surface (wings, horizontal stabilizer, control surfaces, engine inlets, and upper surface of the fuselage).

Takeoff is permitted with frost adhering to:
a) the underside of the wing when caused by cold soaked fuel; or
b) the upper surface of the fuselage.

45
Q

Ice and Rain Protection

Anti Ice System Required Use
During Flight Operations

A
  1. When visible moisture is present or operating on contaminated surfaces

And:
2. TAT +10° or below:

Then:
L and R Engine - On
Wing - Optional

2a. If ICE DETECTED and ≤210kts WING must also be selected ON

*Anti Ice Systems Min Usage Temp
SAT -40C or colder

46
Q

Ice & Rain Protection

Takeoff procedure after deice operations with Type II, III, and IV Anti-icing Fluids

A

The wing anti-ice system must only be selected ON, if required, just prior to thrust increase for takeoff.

47
Q

Anti-Ice Operation:
On Ground with OAT 5C or Below, Just Prior to Takeoff

A

OAT 5C or below:
* L&R ENG - ON
* Wing - ON*

*If type II, III, or IV fluid has been applied, select ON just prior to

48
Q

Icing System Operation Limitations:
Min Temperature - L&R Wing/ENG

A

SAT -40C

49
Q

Required Anti ice if ICE DETECTED EICAS message is displayed or in icing conditions with airspeed below 210kts

A

WING must be selected ON

50
Q

Min Operating Temperature

A

-4OC at pressure ALT below 14,000’

51
Q

Anti-Ice Operation:
In Flight, TAT 10C or Below to SAT <-40C

A

TAT 10C or below:
* L&R ENG - ON
* Wing - ON*

if SAT is -40C, Anti-ice systems - OFF

52
Q

Anti-Ice Operation:
On Ground with OAT 5C or Below, Just Prior to Takeoff

A

OAT 5C or below:
* L&R ENG - ON
* Wing - ON*

*If type II, III, or IV fluid has been applied, select ON just prior to

53
Q

Max Approach Glide Path Angle

A

Operations with a glidepath angle greater than 4.5 degrees or greater is prohibited.*

*Glidepath angle further limited at airport elevations above 5,000’ MSL. see chart , figure 02-01-1

54
Q

Configuration for holding while in icing conditions

A

Flaps 0
(No Flaps Extended)

55
Q

If a rejected takeoff is performed, or a quick turn is expected, what limitations might be exceeded?

A

Brake Energy
(Review Charts)

56
Q

Maneuvering Load Factors

A

Flaps up = +2.6g to -1.0g
Flaps extended = +2.0g to 0.0 g

57
Q

Use of FMS V-speed data

A

Prohibited for temperatures above ISA +33C

58
Q

Max Latitudes for FMS navigation

A

Prohibited south of 60 degrees South latitude.

Prohibited North of 73 degrees north latitude and for Canadian Northern Domestic Airspace.

59
Q

Minimum FMS sources for Navigation

A

FMS navigation prohibited when not receiving:

One GNSS; or
Two DME’s; or
One VOR/ DME; or
One IRS

60
Q

RNP Operations
Required CDI Scales

A

RNP APCH = 0.3nm
Basic RNP = 1.0nm
RNP-2 = 2.0nm
RN-4 = 4.0nm
RNP-10 = 4.0nm

61
Q

Max RNP Leg Lengths

A

When conducting RNP navigation operations the length of each individual flight plan leg or between the aircraft and the TO waypoint must not exceed:

BASIC RNP-1……………50nm
RNP-2………………………400nm
RNP4 or RNP-10………500nm (Oceanic)

note: pilot defined waypoints must not be used to create individual legs shorter than the limiting length.

62
Q

FMS messages which must not be annunciated for RNP operations

A

NO APPR (FMS A1 ON PFD)
LOI (FMS A1 ON PFD)
LOSS ON INTEGRITY (on CDU)
GNSS NOT AVAILABLE (on CDU)
GNSS-FMS DISAGREE (on CDU)

63
Q

FMS Limitations:
SmartPerf Restrictions

A

*Primary means of calculating PDCS is iPreFlight Genesis
* Both Flight Management Computers must be operating
* Performance data, ETE/ETA and Fuel Remaining information are advisory only
* SmartPerf not approved for operations at airports above 8000’ pressure altitude
* When comparing FMS and PDCS derived data, do not mix performance information
* When calcualating ALD on contaminated runways use QRH or PDCS correction factors

64
Q

FMS Limitations:
Latitude Navigation Limitation

A

Do not use the FMS for the following:
* Navigation at latitudes South of 60deg South
* Navigation at latitudes North of 73 and for Canadian Northern Domestic Airspace

65
Q

VNAV Guidance Limitation

A

VNAV vertical guidance is prohibited when the barometric altitude is corrected to the landing field elevation (QFE).

66
Q

RNP operations down to LPV minimums are prohibited when these messages are displayed:

A

Red boxed “VNV” (vertical deviation scale on PFD)
NO APPR (on PFD)
EFIS MISCOMPARE (CAS messge)
EFIS COMP INOP (CAS message)
LPV NOT AVAIL (on CDU)

67
Q

FMS messages which prohibit RNAV operations

A

FMS DR (PFD, MFD or CDU)
IRS ONLY (PFD, MFD or CDU)
VOR/DME ONLY (CDU) OR V/D ONLY (PFD)
VOR/DME DIST>40.0 NM ( CDU)
CHK POS (PFD OR CDU)

68
Q

RNP LPV Operations
Required Equipment

A

Dual PFD
Dual GNSS with SBAS
Dual FMC

69
Q

FMS Limitations:
SmartPerf Restrictions

A

*Primary means of calculating PDCS is iPreFlight Genesis
* Both Flight Management Computers must be operating
* Performance data, ETE/ETA and Fuel Remaining information are advisory only
* SmartPerf not approved for operations at airports above 8000’ pressure altitude
* When comparing FMS and PDCS derived data, do not mix performance information
* When calcualating ALD on contaminated runways use QRH or PDCS correction factors

70
Q

FMS Limitations:
NAV RADIO SELF TEST

A

Do not initiate NAV RADIO SELF TEST from either NAV radio tuning page on the FMS CDU or MFD nav radio during flight

71
Q

FMS Limitations:
Use of RNAV flight procedures

A

MUST be retrieved from current database
(Cannot be built by user)

72
Q

FMS Limitations:
En route & Terminals Ops

A

Current database required or Pilot-verified waypoints

73
Q

FMS Limitations:
Tuning Localizer

A

Do not tune a localizer on the TUNE page using the identifier only

74
Q

FMS Limitations:
CPDLC INSERT MOD Limitation

A

Do not use CPDLC INSERT MOD when within 2 minutes of a TO waypoint

75
Q

FMS Limitations:
NAV RADIO SELF TEST

A

Do not initiate NAV RADIO SELF TEST from either NAV radio tuning page on the FMS CDU or MFD nav radio during flight

76
Q

Standby Instrument Localizer

A

Prohibited to use standby instrument localizer guidance during localizer backcourse approaches

77
Q

FMS Limitations:
FPLN WIND Limitation

A

Do not select FPLN WIND update from the ROUTE MENU

78
Q

FMS Limitations:
In Flight Limits

A

Do not accomplish the following in flight:

  • Load pilot routes from the PILOT ROUTE LIST
  • Upload flight plansfrom ROUTE MENU (FPLN RECALL)
79
Q

FMS Limitations:
FPLN UPLINK

A

Do not use in flight. Must be completed or canceled before taxiing

80
Q

FMS Limitations:
CPDLC FLight Plan Updates

A

Ensure flight plan is loaded in FMS before updating a flight plan through CPDLC

81
Q

FMS Limitations:
Single FMS Restriction

A

Single FMS restricted to no more than two MFD MAP or HSI displays

82
Q

FMS Limitations:
CPDLC Autoload Restriction

A

Do not use CPDLC autoload for any clearance containing RTA constraints

83
Q

Standby Compass Use Requirement

A

L and R WHSLD/WINDOW switches must be temporarily selected OFF while the standby compass is being used.

84
Q

IRS Alignment

A

Following a successful initial alignment, do not manually re-enter the position in the FMS CDU either immediately before, or immediately after aircraft motion.
If this has occurred, a complete normal shutdown and restart of the aircraft and IRSs must be completed. Failure to do so may lead to a total IRU loss during subsequent flight legs.

85
Q

Max Operating OAT

A

+50C at sea level

Max temp reduces as pressure altitude increases

Max Temp is +34C at 8,000’ (see chart)

86
Q

Fuel transfer systems

A

Power and Gravity transfer valves shall be selected off for takeoff.

87
Q

Max ITT
Ground Start

A

650°

88
Q

Max ITT
Air Start

A

800°

89
Q

Max ITT
Max Reverse

A

955°

90
Q

Max ITT
Max Continuous

A

950°

91
Q

Max ITT
Takeoff

A

955°

*normal takeoff power limited to 5 minutes

92
Q

Max ITT
APR

A

955°

APR power (OEI) is limited to 10 minutes

*use it as necessary during an emergency

93
Q

Max Oil Temp

A

138°

94
Q

Min Oil Temp:
1. Engine Ground Start
2. Engines Above Idle
3. Takeoff Power

A

Min Oil Temp:

  1. Engine Ground Start -40C
  2. Engines Above Idle +5C
  3. Takeoff Power +14C
    *Between +5C and +14C engines may be operated up to but not including CLB power.
95
Q

Min Oil Pressure - Idle

A

28 PSI

96
Q

Max N2
Takeoff & Max Continuous

A

98.0%

97
Q

Max N1

  1. APR & Takeoff
  2. Max Continuous
  3. Max Reverse
A
  1. APR & Takeoff 96. 8%
  2. Max Continuous 96. 5%
  3. Max Reverse 70.7%
    (Auto reduced @ <85kts)
98
Q

Min N2 - Idle

A

46.0%

99
Q

Engine Cranking

A

The engine may be motored for up to 5 minutes, followed by a cooling period of 15 minutes.

*This is different than a start

100
Q

Thrust Reverser Operation

A

Paved surfaces only

Do not attempt to:

Deploy in flight
Back up the aircraft
Use for touch and go landings
Use above idle thrust below 40 KIAS.

101
Q

Max APU RPM

A

108%

102
Q

Max APU EGT
Start

A

973°

103
Q

Max APU EGT
Normal Ops

A

718°

104
Q

Overspeed Inspection Requirements

A

A visual inspection of the aircraft is not required when an overspeed event occurs under the following conditions:

  • Level flight
  • No turbulence
  • Landing gear and flaps retracted
  • Did not exceed the following: Vmo+15kts, or Mmo+.03

Challenger 350 Flashcards rev0124 (8 decks)

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