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Challenger 350 > 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 moisture(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

Maximum Approach Glide Path Angle

A

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

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

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6
Q

Max Ramp Weight

A

40,750 lbs

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7
Q

Max Takeoff Weight

A

40,600 lbs

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8
Q

Minimum Takeoff Weight

A

25,000

due to Vmcg

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9
Q

Max Zero Fuel Weight

A

28,200 lbs

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10
Q

Max Landing Weight

A

34,150

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11
Q

Minimum Flight Weight

A

24,800

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12
Q

Vmo (up to 8000’)

A

300 KIAS

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13
Q

Vmo (above 8000’)

A

320 KIAS

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14
Q

Mmo (above 29,475’)

A

.83 mach

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15
Q

Vra (rough air penetration)

A

265 KIAS/.75m

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16
Q

Vlo ret (max landing gear retraction)

A

200 KIAS

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17
Q

Vlo ext (max landing gear extension)

A

250 KIAS

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18
Q

Vle (max landing gear extended)

A

250 KIAS

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19
Q

Vfe (max flaps extended speed)

A

Flaps 10……………210 KIAS

Flaps 20…………..210 KIAS

Flaps 30…………..175 KIAS

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20
Q

Max tire ground speed

A

182 KTS

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21
Q

Max takeoff and landing pressure altitude

A

10,000’

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22
Q

Max tailwind component for takeoff and landing

A

10 KTS

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23
Q

Maximum Runway Slope for Takeoff and Landing

A

+2% uphill

-2% downhill

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24
Q

Max Crosswind for Takeoff

A

28 knots

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25
Q

Max Crosswind for Landing

A

24 knots

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26
Q

Cold Weather Operations-Frost limitations

A

Takeoff is prohibited with frost, ice snow or sluch 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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27
Q

Maximum Pressure Altitude

A

45,000’

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28
Q

Maneuvering Load Factors

A

Flaps up……………………+2.6g to -1.0g

Flaps extended………..+2.0g to 0.0 g

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29
Q

Operations with Type II, III, & 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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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)

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30
Q

MIN OPERATING TEMPERATURE

A

-4OC at pressure ALT below 14,000’

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31
Q

Air Conditioning

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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32
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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33
Q

Max Altitude with YAW DAMP off

A

31,000’

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34
Q

Minimum Autopilot Use Heights

A

Climb, En Route or Descent……………………..700’ AGL

Precision Approach:
glidepath 3.5 degrees or less……………………80’

Visual or non-precision Approach……………..200’ AGL

35
Q

Use of FMS V-speed data

A

prohibited for temperatures above ISA +33C

36
Q

Minimum Autopilot Use Heights

A

Climb, En Route or Descent……………………..700’ AGL

Precision Approach:

glidepath 3.5 degrees or less……………………80’ AGL

glidepath 3.5 to 4.5 degrees……………………..160’ AGL

Visual or non-precision Approach……………..200’ AGL

37
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.

38
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
39
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
40
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)

41
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.

42
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)

43
Q

VNAV Guidance limitation

A

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

44
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)

45
Q

RNP LPV operations required equipment

A

Dual PFD

Dual GNSS with SBAS

Dual FMC

46
Q

Standby Instrument Localizer

A

prohibited to use standby instrument localizer guidance during localizer backcourse approaches

47
Q

Standby Compass use

A

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

48
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.

49
Q

Max altitude for flap extension

50
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

52
Q

Minimum 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.

52
Q

Max Altitude for gear extension

53
Q

Minimum airspeed for Spoiler Extension

A

Vapp + 8 knots

54
Q

Max single-point refueling pressure

A

55 psig

defuel limited to -8 psig

55
Q

Max fuel load-SPPR

A

14,150 lbs

*7075 lbs per wing tank

56
Q

Fuel transfer systems

A

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

57
Q

Max fuel load-Gravity Refuel

A

13,000 lbs

*6,500 lbs per wing tank

58
Q

Min fuel for go around

A

500 lbs per side

59
Q

Maximum Fuel Imbalance

A

Total fuel >13,700………………….250 lbs max

Total fuel 10,000- 13,700……….315 lbs max

Total fuel 10,000-4700……………450 lbs max

Total fuel <4700 ………………………600 lbs max

60
Q

Min Bulk Fuel temp, Jet A

61
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.
62
Q

MAX ITT-GROUND START

63
Q

MAX ITT- AIR START

64
Q

MAX ITT REVERSE

65
Q

MAX ITT-CONTINUOUS

66
Q

MAX ITT-TAKEOFF

A

955

*normal takeoff pover limited to 5 minutes

67
Q

MAX ITT APR

A

955

*APR power(OEI) is limited to 10 minutes

68
Q

MAX OIL TEMP

69
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.
70
Q

MIN OIL PRESS

71
Q

MAX N2

72
Q

MAX N1

73
Q

MIN N2 -IDLE

74
Q

ENGINE CRANKING

A

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

75
Q

ENGINE STARTER LIMITS

A

Three consecutive engines start cycles may be conducted, followed by 15 minutes cooling period before more starts may be attempted.

Engine must be motored for 30 seconds after an aborted Start.

76
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.

77
Q

MAX ALT APU OPERATION

78
Q

MAX ALT APU GEN OPERATION

79
Q

MAX ALT APU BLEED AIR

A

20,000’

*Do not use the APU to start the left engine on the ground above 9,000’.

80
Q

MAX ALT APU START

81
Q

MAX APU STARTS

A

3 attempts, each with 1 minute cooling period, then 20 minutes cooling. 2 more attempts may then be made followed by at least 40 minutes cooling.

6 successive starts may be made at 10 minute intervals, then one hour off for cooling.

82
Q

MAX SPEED APU START

83
Q

MAX APU RPM

84
Q

MAX APU EGT-START

85
Q

MAX APU EGT- NORMAL OPS

86
Q

Max crosswind contaminated runway

A

10 KTS for take off and landing

Challenger 350 (6 decks)

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