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Lorne - 350 study > CL350 AFM Limitations (NICE TO KNOW) > Flashcards

CL350 AFM Limitations (NICE TO KNOW) Flashcards

Learn aircraft limitaions

1
Q

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

What is needed, 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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2
Q

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

A

TAT +10° or below:

Engine - On

*Unless SAT is -40C or below.

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

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3
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

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4
Q

Min Takeoff Weight

A

25,000 lbs

due to Vmcg

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5
Q

Max Zero Fuel Weight

A

28,200 lbs

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6
Q

Min Flight Weight

A

24,800 lbs

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7
Q

Vmo (up to 8000’)

A

300 KIAS

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8
Q

Vmo (above 8000’)

A

320 KIAS

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9
Q

Mmo (above 29,475’)

A

.83 mach

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10
Q

Max Tire Groundspeed

A

182 kts

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11
Q

Max Takeoff and Landing Pressure Altitude

A

10,000’

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12
Q

Max Runway Slope for Takeoff and Landing

A

+2% uphill

-2% downhill

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13
Q

Cold Weather Operations - 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.

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14
Q

Maneuvering Load Factors

A

Flaps up = +2.6g to -1.0g

Flaps extended = +2.0g to 0.0 g

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15
Q

Min Operating Temperature

A

-4OC at pressure ALT below 14,000’

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16
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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17
Q

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

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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18
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
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19
Q

RNP Operations

Required CDI Scales (In NM)

A 
RNP APCH = 0.3nm
Basic RNP = 1.0nm
RNP-2 = 2.0nm
RN-4 = 4.0nm
RNP-10 = 4.0nm
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20
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)
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21
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.

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22
Q

VNAV Guidance Limitation

A

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

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23
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)
24
Q

RNP LPV Operations

Required Equipment

A

Dual PFD
Dual GNSS with SBAS
Dual FMC

25
Q

Standby Instrument Localizer (prohibited use)

A

Prohibited to use standby instrument localizer guidance during localizer backcourse approaches

26
Q

Standby Compass Use Requirement

A

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

27
Q

After initial IRS Alignment, what should you not do:

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

28
Q

Max Flap Extension Altitude

A

18,000’

29
Q

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):

A

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

30
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)

31
Q

Max Altitude for gear extension

A

18,000’

32
Q

Min airspeed for Flight Spoiler Extension

A

Vref +8 knots

33
Q

Max single-point refueling pressure

A

55 psig

Defuel limited to -8 psig

34
Q

Fuel transfer systems configuration (takeoff)

A

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

35
Q

Min Go Around Fuel

A

1000 lbs

(500 lbs per side)

*Collector tanks hold 500lbs each.

36
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

37
Q

Min Bulk Fuel temp, Jet A

A

-30C

38
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.

39
Q

Max Engine ITT

Ground Start

A

650°

40
Q

Max ITT

Air Start

A

800°

41
Q

Max ITT

Max Reverse

A

955°

42
Q

Max ITT

Max Continuous

A

950°

43
Q

Max ITT

Takeoff

A

955°

*normal takeoff power limited to 5 minutes

44
Q

Max ITT

APR

A

955°

APR power (OEI) is limited to 10 minutes

*use it as necessary during an emergency

45
Q

Min Oil Temp

Engine Ground Start

A
  • 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.

46
Q

Max N2

Takeoff & Max Continuous

A

98.0%

47
Q

Max N1

A
  1. 8% APR & Takeoff
  2. 5% Max Continuous

70.7 Max Reverse
(Auto reduced <85kts)

48
Q

Min N2 - Idle

A

46.0%

49
Q

Max Engine Cranking time(not starting)

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

50
Q

Thrust Reverser Operation where, and what not to do

5 things

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.
51
Q

Max APU RPM

A

108%

52
Q

Max APU EGT

Start

A

973°

53
Q

Max APU EGT

Normal Ops

A

718°

54
Q

Min Altitude for Spoiler Extension

A

500’ AGL

Flight spoilers must not be extended below 500’ AGL

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

55
Q

Fuel Quantities:
45 min IFR Reserve
Release
Hot Spare

A

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

Lorne - 350 study (5 decks)

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