CL350 AFM Limitations (NICE TO KNOW) Flashcards

memorize aricraft limitaions

1
Q

Engine Anti-Ice Ground Operation

A

Must be on when OAT on the ground and for takeoff is ≤ +10°C or when operating on ramps taxiways and runways with snow, ice, standing water, or slush present.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Engine Anti-Ice Flight Operatons

A

Must be on in visible moisture when TAT is ≤ +10°C except when SAT is -40°C or below.

*Must be on when ICE DETECT CAS message is on or in icing conditions

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Wing Anti-Ice Ground Operations

A

Must be on for takeoff when OAT is ≤ +5°C in visible moisturee (fog, rain, etc with vis < 1 mile) and/or when operating on ramps, taxiways, and runways when surface snow, ice, standing water, or slush is present.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Wing Anti-Ice Flight Operations

A

Icing conditions exist in flight at a TAT of ≤ +10°C and visible moisture in any form is encountered, except when SAT is ≤ -40°C.

WING A/I must be on when: - ICE DETECT CAS message is on, or - in icing conditions and airspeed is ≤ 210 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max Approach Glide Path Angle

A

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

*Glidepath angle further limited at airport elevations above 5,000’ MSL.

See Bombardier AFM , figure 02-01-1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Min Takeoff Weight

A

25,000 lbs (due to Vmcg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Max Runway Slope for Takeoff and Landing

A

+/-2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Cold Weather Operations-Frost limitations

A

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
b) the upper surface of the fuselage.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

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.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Min Operating Temperature

A

-4O°C at pressure ALT below 14,000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
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 ≥ +40°C.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Use of FMS V-speed data

A

Prohibited for temperatures above ISA +33C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
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.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Minimum FMS sources for Navigation

A

FMS navigation prohibited unless receiving:

One GNSS

or

Two DME’s

or

One VOR/ DME

or

One IRS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

RNP Operation CDI Scales

A

RNP APCH = 0.3nm

Basic RNP = 1.0nm

RNP-2 = 2.0nm

RNP-4 = 4.0nm

RNP-10 = 4.0nm

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

FMS messages which must not be annunciated for 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)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
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………………………100nm RNP4 or RNP-10………500nm

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

FMS messages which must not be annunciated for RNP operations

A

NO APPR (FMS A1 ON PFD)

LOI (FMS A1 ON PFD)

LOSS OF INTEGRITY (on CDU)

GNSS NOT AVAILABLE (on CDU)

GNSS-FMS DISAGREE (on CDU)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

VNAV Guidance Limitation

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
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)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

RNP LPV Operations Required Equipment

A

Dual PFD

Dual GNSS with SBAS

Dual FMC

22
Q

Standby Instrument Localizer

A

Prohibited to use standby instrument localizer guidance during localizer backcourse approaches

23
Q

Standby Compass Use Requirement

A

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

24
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 movement. If this has occurred, a complete normal shutdown and restart of the aricraft and IRSs must be completed. Failure to do so may lead to a total IRU loss during subsequent flight legs.

25
Q

Max Operating OAT

A

+50°C at sea level

Max temp reduces as pressure altitude increases.

Max Temp is +34°C at 8,000’.

See Bombardier AFM Figure 02-03-2

26
Q

Max Altitude for gear extension

A

18,000 ft

27
Q

Max single-point refueling pressure

A

55 psig

Defuel limited to -8 psig

28
Q

Fuel transfer systems

A

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

29
Q

Min Go Around Fuel

A

1000 lbs (500 lbs per side)

*Collector tanks hold 500 lbs each.

30
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

31
Q

Min Bulk Fuel temp, Jet A

A

-30°C

32
Q

Max Bulk Fuel Temp for Takeoff

A

+50°C

With wing bulk fuel temp at +45°C 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.

33
Q

Max ITT Ground start

A

650°C

34
Q

Max ITT air start

A

800°C

35
Q

Max ITT Reverse

A

955°C

36
Q

Max ITT Continuous

A

950°c

37
Q

Max ITT Takeoff

A

955°C

*Normal takeoff power limited to 5 minutes

38
Q

Max ITT APR

A

955°C

APR power (OEI) is limited to 10 minutes

*use as necessary during an emergency

39
Q

Max Oil Temp

A

138°C

40
Q

Min Oil Temp Engine start

A

-40°C

*min oil temp of +5°C required to operate engines above idle.

Between +5°C and +14°C engines may be operated up to but not including CLB power.

41
Q

Min Oil Pressure

A

28 PSI

42
Q

Max N2

A

98.0 %

43
Q

Max N1

A

96.8 %

44
Q

Min N2 Idle

A

46.0 %

45
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

46
Q

Thrust Reverser Operation

A

Paved surfaces only

Do not attempt to deploy in flight

Do not use to back up the aircraft

Do not use for touch and go landings

Do not use above idle thrust below 40 KIAS.

47
Q

Max APU RPM

A

108 %

48
Q

Max APU EGT Start

A

973°C

49
Q

Max APU EGT Normal Ops

A

718°C

50
Q

Fuel Quantities:

45 min IFR

Reserve Release

Hot Spare

A

1850 lbs = 45 min IFR Reserve

3060 lbs = Release

5000 lbs= Hot Spare