CL350 AFM Limitations (NICE TO KNOW)

Question 1

During Ground Operations, when is Ice and Rain Protection needed?

What is needed, when visible moisture is present or operating on contaminated surfaces

Answer 1

OAT +10° or below:

L and R Engine - On
Wing - Off

AOM 9.16

Question 2

At what point is Ice and Rain Protection required during Flight Operatons:
When visible moisture is present

Answer 2

TAT +10° or below:

Engine - On

*Unless SAT is -40C or below.

If ICE DETECTED displayed and <210kts WING must be selected ON

Question 3

Max Approach Glide Path Angle

Answer 3

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

Question 4

Min Takeoff Weight

Answer 4

25,000 lbs

due to Vmcg

Question 5

Max Zero Fuel Weight

Answer 5

28,200 lbs

Question 6

Min Flight Weight

Answer 6

24,800 lbs

Question 7

Vmo (up to 8000’)

Answer 7

300 KIAS

Question 8

Vmo (above 8000’)

Answer 8

320 KIAS

Question 9

Mmo (above 29,475’)

Answer 9

.83 mach

Question 10

Max Tire Groundspeed

Answer 10

182 kts

Question 11

Max Takeoff and Landing Pressure Altitude

Answer 11

10,000’

Question 12

Max Runway Slope for Takeoff and Landing

Answer 12

+2% uphill

-2% downhill

Question 13

Cold Weather Operations - Frost limitations

Answer 13

*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.

Question 14

Maneuvering Load Factors

Answer 14

Flaps up = +2.6g to -1.0g

Flaps extended = +2.0g to 0.0 g

Question 15

Min Operating Temperature

Answer 15

-4OC at pressure ALT below 14,000’

Question 16

ECS (Air Conditioning) limitations during ground ops

Answer 16

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.

Question 17

Crew &
Pax Oxygen Masks (prolonged use)
(max cabin altitude)

Answer 17

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.

Question 18

Minimum FMS sources for Navigation

Answer 18

FMS navigation prohibited when not receiving:

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

Question 19

RNP Operations
RNP APCH =
Basic RNP =
RNP-2 =
RN-4 =
RNP-10 =

Required CDI Scales (In NM)

Answer 19

RNP APCH = .1nm
Basic RNP = 1.0nm
RNP-2 = 2.0nm
RN-4 = 4.0nm
RNP-10 = 4.0nm

Question 20

FMS messages which must not be annunciated for RNAV operations (5)

Answer 20

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)

Question 21

Max RNP Leg Lengths
BASIC RNP-1
RNP-2
RNP4 or RNP-10

Answer 21

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.

Question 22

VNAV Guidance Limitation (Altimeter Setting)

Answer 22

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

Question 23

RNP operations down to LPV minimums are prohibited when these messages are displayed: (5)

Answer 23

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)

Question 24

RNP LPV Operations

Required Equipment

Answer 24

Dual PFD
Dual GNSS with SBAS
Dual FMC

Question 25

Standby Instrument Localizer (prohibited use)

Answer 25

Prohibited to use standby instrument localizer guidance during localizer backcourse approaches

Question 26

Standby Compass Use Requirement

Answer 26

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

Question 27

After initial IRS Alignment, what should you not do:

Answer 27

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 aricraft and IRSs must be completed. Failure to do so may lead to a total IRU loss during subsequent flight legs.

Question 28

Max Flap Extension Altitude

Answer 28

18,000'

Question 29

Max Generator Load: In flight 2, or 3 generators operating: On the ground, with one generator operating: In flight, with one generator operating: Transient (5 minutes):

Answer 29

Continuous: In flight, 2 or 3 generators operating: 400A On ground, one generator operating 400A In flight, one generator operating: 500A Transient (5 minutes): 600A Do not takeoff with Battery temperature below -20C

Question 30

Max Operating OAT

Answer 30

+50C at sea level Max temp reduces as pressure altitude increases. Max Temp is +34C at 8,000'. (see chart)

Question 31

Max Altitude for gear extension

Answer 31

18,000'

Question 32

Min airspeed for Flight Spoiler Extension

Answer 32

Vref +8 knots

Question 33

Max single-point refueling pressure

Answer 33

55 psig Defuel limited to -8 psig

Question 34

Fuel transfer systems configuration (takeoff)

Answer 34

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

Question 35

Min Go Around Fuel

Answer 35

1000 lbs (500 lbs per side) *Collector tanks hold 500lbs each.

Question 36

Max Fuel Imbalance

Answer 36

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

Question 37

Min Bulk Fuel temp, Jet A

Answer 37

-30C

Question 38

Max Bulk Fuel Temp for Takeoff

Answer 38

+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.

Question 39

Max Engine ITT | Ground Start

Answer 39

650°

Question 40

Max ITT | Air Start

Answer 40

800°

Question 41

Max ITT | Max Reverse

Answer 41

955°

Question 42

Max ITT | Max Continuous

Answer 42

950°

Question 43

Max ITT | Takeoff

Answer 43

955° *normal takeoff power limited to 5 minutes

Question 44

Max ITT | APR

Answer 44

955° APR power (OEI) is limited to 10 minutes *use it as necessary during an emergency

Question 45

Min Oil Temp | Engine Ground Start

Answer 45

- "-"40C * min oil temp of +5C required to operate engines above ground idle. Between +5C and +14C engines may be operated up to but not including CLB power.

Question 46

Max N2 | Takeoff & Max Continuous

Answer 46

98.0%

Question 47

Max N1

Answer 47

APR Takeoff 96.8% Max Continuous 96.5% Max Reverse 70.7% (Auto reduced <85kts)

Question 48

Min N2 - Idle

Answer 48

46.0%

Question 49

Max Engine Cranking time(not starting)

Answer 49

The engine may be motored for up to 5 minutes, followed by a cooling period of 15 minutes. *This is different than a start

Question 50

Thrust Reverser Operation where, and what not to do | 5 things

Answer 50

``` 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. ```

Question 51

Max APU RPM %

Answer 51

108%

Question 52

Max APU EGT | Start

Answer 52

973°

Question 53

Max APU EGT | Normal Ops

Answer 53

718°

Question 54

Min Altitude for Spoiler Extension

Answer 54

500' AGL Flight spoilers must not be extended below 500' AGL Do not select EMER except during emergency conditions or when required by procedure.

Question 55

Fuel Quantities: 45 min IFR Reserve Release Hot Spare

Answer 55

1850 lbs = 45 min IFR Reserve 3060 lbs = Release 5000 lbs= Hot Spare