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CL350 > Limitations > Flashcards

Limitations Flashcards

1
Q

MTOM?

A

40.600 lbs

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2
Q

MLM?

A

34.150 lbs

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3
Q

MRM?

A

40.750 lbs

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3
Q

MZFM?

A

28.200 lbs

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4
Q

MFM?

A

24.800 lbs

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5
Q

With what configuration is holding in icing-conditions prohibited?

A

With Flaps extended

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6
Q

VMOs/MMO?

A

0-8.000 ft - 300 KIAS
8.001-29.475 ft - 320 KIAS
Above 29.475 ft - 0.83 Mi

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7
Q

VFEs?

A

F10 - 210 KIAS
F20 - 210 KIAS
F30 - 175 KIAS

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8
Q

VLOs/VLE?

A

VLOret - 200 KIAS
VLOext - 250 KIAS
VLE - 250 KIAS/0.70 Mi

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9
Q

VMCA F10/F20
VMCG F10/F20
Minimum V1

A

110/109 KIAS
115/114 KIAS
119 KIAS

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10
Q

VRA?

A

265 KIAS/0.75 Mi (whichever is lower)

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11
Q

Minimum Clean Speeds below FL100?

A

Below 34.000 lbs - 170 KIAS

Above 34.000 lbs - 180 KIAS

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12
Q

Minimum Clean Speed between FL100 and FL300?

A

200 KIAS

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13
Q

Minimum Clean Speed above FL300?

A

0.75 Mi

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14
Q

Maximum Tire Speed?

A

182 ground speed

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15
Q

Maximum Crosswind Components?

A 
T/O on a dry or wet runway - 28 kts
LDG on dry or wet runway - 24 kts
FC 0.36-0.39 (medium-good) - 20 kts
FC 0.30-0.35 (medium) - 15 kts
FC 0.26-0.29 (medium-poor) - 10 kts
LVTO RVR 250-400 m - 10 kts
LVTO RVR 125-250 m - 5 kts
T/O or LDG with NWS inoperative - 15 kts
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16
Q

Maximum Tailwind Component for T/O or LDG?

A

10 kts

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17
Q

Maximum Wind/Gust-speed for parking/ground movement?

A

45 kts

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18
Q

OEI Speed and maximum distance from adequate aerodrome?

A

383 KIAS

779 NM

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19
Q

Maximum Runway Slope?

A

+/- 2%

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20
Q

Maximum Certified Altitude?

A

45.000 ft

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21
Q

Maximum Altitude with Gear and/or Flaps Extended?

A

18.000 ft

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22
Q

Maximum Altitude for T/O and LDG?

A

10.000 ft

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23
Q

G-limits:

  • Flaps 0
  • Flaps >0
A
  1. 6/-1.0 g

2. 0/-0.0 g

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24
Q

Temperature Limit at MSL and below?

A

-40C to +50C

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25
Q

Temperature Limit FL010 to FL135?

A

-40C to ISA+35

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26
Q

Temperature Limit FL135 to FL350?

A

Decreasing linearly to -70C to ISA+35

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27
Q

Temperature Limit FL350 to FL410?

A

-70C to ISA+35

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28
Q

Temperature Limit FL410 to FL450?

A

Decreasing linearly to -75C to ISA+35

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29
Q

WING A/I and Type II, III and IV application - what to consider for T/O?

A

WING A/I ON just prior setting Takeoff Thrust

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30
Q

Which maneuvers are prohibited?

A

Aerobatics and Spins

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31
Q

What has to be considered when using air condition on ground?

A

Do not select TRIM AIR ONLY

If electrical power (BATT/EXT) is used for more than 30 minutes at +40C (acc. OM-B +30C) or above the pack must be running (ENG/APU On with AIR SOURCE on NORM or PACK ONLY)

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32
Q

Altitude Limitations for the use of Oxygen Masks?

A

Passenger Oxygen Masks not recommended for prolonged use above 25.000 ft;
Crew and Passenger Oxygen Masks not approved above FL400

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33
Q

Maximum Differential Pressures:

  • Positive
  • Negative
  • Landing
  • Ground (Taxi etc.)
A
  • Maximum Positive 9.4 psi
  • Maximum Negative -0.5 psi
  • Maximum Landing 1.0 psi
  • Maximum Ground (Taxi etc.) 0.1 psi
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34
Q

Minimum Autopilot Altitudes:

  • CLB/CRS/DSC
  • NPA/VIS Approach
  • PA Approach below 3.5 deg
  • PA Approach 3.5-4.49 deg
A
  • 700 ft
  • 200 ft
  • 80 ft
  • 160 ft
35
Q

Maximum Approach Glidepath Angle?

A

4.49 deg.

36
Q

Maximum Altitude without YD?

A

31.000 ft

37
Q

Altitude for automatic 1/2 BANK engagement?

A

31.600 ft

38
Q

Performance-, Approach- and Firecategory?

A

A, C, 4

39
Q

Minimum Runway Width; to what surface is the operation restricted?

A

30 m (Code 3B); limited to paved surfaces

40
Q

Do not use FMS for navigation unless receiving data from:

A

One VOR/DME
One IRS
Two DME
Two GNSS

41
Q

RNP/RNAV and Datalink capabilities?

A

RNP 1/4/10, RNAV 1/5/10

FANS 1/A, Link2000+, ADS-B/C

42
Q

Which areas must be completely free of any deposits?

A
  • Wings
  • Control Surfaces
  • Horizontal Stabilizer
  • Vertical Stabilizer
  • Upper Side of Fuselage
  • Engine Inlets
43
Q

Which deposits are allowed if CWO according to FCOM 1 are followed?

A
  • Light Frost on Upper Side of Fuselage

- Up to 3 mm Frost on Wing’s Underside due to cold soaked fuel

44
Q

When must ENG A/I be ON on ground and inflight?

A

Ground:
OAT +10C and below (visible moisture, contaminated surface)

Flight:
TAT +10C to SAT -40C (visible moisture, icing conditions, ICE DETECTED CAS)

45
Q

When must WING A/I be ON on ground and inflight?

A

Ground:
OAT +5C and below (visible moisture, contaminated surface)

Flight:
TAT +10C to SAT -40C (visible moisture, icing conditions if less than 210 KIAS, ICE DETECTED CAS)

46
Q

How do you know that SLD exist and what are the actions?

A

Ice accretion on Side Windows; ENG/WING A/I ON, leave icing conditions ASAP.

47
Q

Approved Types of Operation for the CL350?

A

FAR25, two pilots, VFR, IFR, day, night, known icing (no FZRA, FZDZ), ditching with the relevant equipment on board, MNPS, RVSM, CAT I ILS (max. 4.49 deg.), LVTO 125 m

48
Q

What to consider when using:

  • STBY INST
  • STBY Compass
A
  • Do not use deviaiton bar when flying a LOC B/C Approach

- L/R WSHLD/WINDOW OFF while reading the Compass

49
Q

Maximum GEN amps?

A

Two or three GEN - 400 amp (i.e. normal operation in flight)
One GEN on Ground - 400 amp (i.e. APU operation)
One GEN in Flight - 500 amp (single GEN operation)
Transient for 5 min. - 600 amp

50
Q

Minimum BATT temperature for T/O?

A

-20C

51
Q

Spoiler Limitations?

A
  • Do not select EMER unless required by procedure or in case of emergency
  • Do not extend below 500 ft AGL
  • Do not extend below Vapp +8 KIAS
52
Q

Approved Fuels?

A
  • JET A, JET A1, JET B, JP4, JP5, JP8

- Mixing is permitted

53
Q

Fuel Temperature Limitations for:

  • Jet A
  • Jet A1/JP5/JP8
  • Jet B/JP4
A
  • 30C to +50C (JET A)
  • 35C to +50C (JET A1, JP5, JP8)
  • 40C to +50C (JET B, JP4)
54
Q

Altitude Limitations for:

  • Russian TS1
  • Jet B/JP4
A
  • Russian TS1 maximum 37.000 ft if fuel temp. is above +30C

- JET B/JP4 maximum 16.000 ft

55
Q

Which restriction applies if the fuel temp. is above +45C?

A

Minimum 2.800 lbs fuel required.

Minimum 1.000 lbs per side required if engines run more than 30 minutes.

56
Q

Are you allowed to add unblended Prist?

A

No

57
Q

Maximum Pressure for Re- and Defueling?

A

+55 psi, -8 psi

58
Q

Restriction for FUEL XFERs during T/O?

A

GRAVITY XFLOW and XFER must be OFF for T/O

59
Q

Maximum Fuel Capacity per Tank for:

  • Gravity Refueling
  • Pressure Refueling
  • Minimum G/A fuel
A
  • Gravity 6.500 lbs
  • Pressure 7.075 lbs
  • Minimum 500 lbs per tank
60
Q

Maximum Fuel Imbalances:

  • Below 4.700 lbs
  • 4.700-10.000 lbs
  • 10.000-13.700 lbs
  • Above 13.700 lbs
A
  • 600 lbs
  • 450 lbs
  • 315 lbs
  • 250 lbs
61
Q

Minimum Oil Temperatures for:

  • Starting
  • Above Idle (up to excl. CLB)
  • T/O
  • T/O without icing inhibitor (not applicable for JET A1)
A
  • -40C
  • +5C
  • +15C
  • +27C
62
Q

Thrust Time Limits for:

  • T/O
  • APR Auto/Manual
A
  • 5 minutes

- 10/5 minutes

63
Q

Thrust Reverser Limitations?

A
  • Use only on paved surfaces
  • No Touch and Go’s
  • No Powerback
  • Do not attempt to deploy in flight
  • No REV above idle below 40 KIAS
  • Maximum REV Thrust is automatically reduced below 85 KIAS
64
Q

Engine and APU Consecutive Start Limitations?

A

Engine:
3 consecutive starts - each followed by 30 seconds cranking.
15 minutes cooling period.

APU:
3 consecutive starts - each followed by 1 minute cooling period.
20 minutes cooling period.
2 more consecutive starts with 1 minutes cooling period.
40 minutes cooling period.

Maximum 6 good starts with 10 minutes intervals - then 60 minutes cooling period.

65
Q

Engine cranking limits?

A

Maximum 5 minutes followed by 15 minutes cooling

66
Q

Engine and APU model?

A
  • AS907-2-1 (HTF7350)

- Honeywell 36-150BD

67
Q

APU Altitude Limitations for:

  • Operation
  • Generator
  • Bleed for ECS and ENG Start
A
  • 37.000 ft
  • 30.000 ft
  • 20.000 ft
68
Q

APU Altitude Limitations for:

  • Ground Start
  • Air Start
A
  • 14.000 ft

- 30.000 ft

69
Q

Minimum and Maximum Temperature for Engine Starting?

A

-40C to +50C

Every 1.000 ft maximum temperature decreases by 2C

70
Q

APU ON or OFF during de/anti-Icing?

A

OFF

71
Q

When to abort the APU Start?

A

If after 30 seconds RPM is not >30%

72
Q

What is prohibited on ground above 9.000 ft - and why?

A

Starting the LH ENG with the APU.

Ducting from APU to LH ENG is too long to create enough pressure.

73
Q

Maximum Airspeed for APU Air Start?

A

285 KIAS

74
Q

If the first APU Air Start is unsuccessful:

A

No further attempt before landing

75
Q

Maximum APU EGT for:

  • Starting
  • Normal Operation
A
  • 973C

- 718C

76
Q

Maximum APU RPM?

A

108%

77
Q

Are you allowed to use the secondary flightplan?

A

No

78
Q

CWO have to be followed according to _______.

A

FCOM 1

79
Q

The effect of landing gear retraction on the CG position is __________.

A

Negligible

80
Q

Determined Maximum Distance from an Adequate Aerodrome?

A

120 minutes

81
Q

What is prohibited to use during QFE Operation?

A
  • SVS

- VNAV

82
Q

What is prohibited while using TAWS and TCAS?

A

Do not use TAWS for navigation.

Do not maneuver based on information presented on the TFC map.

83
Q

Approximate dimensions of the CL350?

A

22 m x 22 m x 7 m

84
Q

Minimum Temperature to start the APU?

A

-40C

85
Q

Minimum Cabin Temperature for the O2 Mask test?

A

+15C

CL350 (4 decks)

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