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Challenger 350 Study v1.0 Frank > CL350 AFM Limitations (NICE TO KNOW) > Flashcards

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 +10C or below when operating of ramps taxiways and runways with snow, ice, standing water, or slush present.

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2
Q

Engine Anti-Ice Flight Operatons

A

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

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

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3
Q

Wing Anti-Ice Ground Operations

A

Must be on for takeoff when OAT is +5C or below 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.

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4
Q

Wing Anti-Ice Flight Operations

A

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

WING A/I must be on when:

  • ICE DETECT CAS message is on, or
  • in icing conditions but airspeed is < 210 KIAS
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5
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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6
Q

Min Takeoff Weight

A

25,000 lbs

due to Vmcg

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7
Q

Max Zero Fuel Weight

A

28,200 lbs

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8
Q

Min Flight Weight

A

24,800 lbs

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9
Q

Vmo (up to 8000’)

A

300 KIAS

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10
Q

Vmo (above 8000’)

A

320 KIAS

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11
Q

Mmo (above 29,475’)

A

.83 mach

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12
Q

Max Tire Groundspeed

A

182 kts

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13
Q

Max Takeoff and Landing Pressure Altitude

A

10,000’

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14
Q

Max Runway Slope for Takeoff and Landing

A

+2% uphill

-2% downhill

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15
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; or
b) the upper surface of the fuselage.

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16
Q

Maneuvering Load Factors

A

Flaps up = +2.6g to -1.0g

Flaps extended = +2.0g to 0.0 g

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17
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.

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18
Q

Min Operating Temperature

A

-4OC at pressure ALT below 14,000’

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19
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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20
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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21
Q

Use of FMS V-speed data

A

Prohibited for temperatures above ISA +33C

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22
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.

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23
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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24
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
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25
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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26
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.

27
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)
28
Q

VNAV Guidance Limitation

A

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

29
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)
30
Q

RNP LPV Operations

Required Equipment

A

Dual PFD
Dual GNSS with SBAS
Dual FMC

31
Q

Standby Instrument Localizer

A

Prohibited to use standby instrument localizer guidance during localizer backcourse approaches

32
Q

Standby Compass Use Requirement

A

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

33
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 aricraft and IRSs must be completed. Failure to do so may lead to a total IRU loss during subsequent flight legs.

34
Q

Max Flap Extension Altitude

A

18,000’

35
Q

Max Generator amps

A

Continuous:

2 or 3 generators operating: 400 amps

One generator operating on ground: 400 amps

One generator operating in flight: 500 amps

Transient( 5 minutes): 600 amps

Do not takeoff with Battery temperature below -20C

36
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)

37
Q

Max Altitude for gear extension

A

18,000’

38
Q

Min airspeed for Spoiler Extension

A

Vapp + 8 knots

39
Q

Max single-point refueling pressure

A

55 psig

Defuel limited to -8 psig

40
Q

Fuel transfer systems

A

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

41
Q

Min Go Around Fuel

A

1000 lbs

(500 lbs per side)

*Collector tanks hold 500lbs each.

42
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

43
Q

Min Bulk Fuel temp, Jet A

A

-30C

44
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.

45
Q

Max ITT

Ground start

A

650°

46
Q

Max ITT

air start

A

800°

47
Q

Max ITT

Reverse

A

955°

48
Q

Max ITT

Continuous

A

950°

49
Q

Max ITT

Takeoff

A

955°

*normal takeoff power limited to 5 minutes

50
Q

Max ITT

APR

A

955°

APR power (OEI) is limited to 10 minutes

*use it as necessary during an emergency

51
Q

Max Oil Temp

A

138°

52
Q

Min Oil Temp

Engine start

A
  • 40C
  • min oil temp of +5C required to operate engines above idle. Between +5C and +14C engines may be operated up to but not including CLB power.
53
Q

Min Oil Pressure

A

28 PSI

54
Q

Max N2

A

98.0%

55
Q

Max N1

A

96.8%

56
Q

Min N2 Idle

A

46.0%

57
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

58
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.
59
Q

Max APU RPM

A

108%

60
Q

Max APU EGT

Start

A

973°

61
Q

Max APU EGT

Normal Ops

A

718°

62
Q

Min Altitude for Spoiler Extension

A

500’ AGL

Flight spoilers must not be extended below 500’ AGL

note: do not select EMER except during emergency conditions or as required by procedure.

63
Q

Fuel Quantities:
45 min IFR Reserve
Release
Hot Spare

A

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

Challenger 350 Study v1.0 Frank (7 decks)

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