Bombardier 5000/6000 Limitations

Question 1

Max taxi/ramp weight
(6000)

Answer 1

99,750 lb

Question 2

Max takeoff weight

Answer 2

99,500

Question 3

Max Landing weight

Answer 3

78,600 lb

Question 4

Max zero fuel weight

Answer 4

26,308 lb

Question 5

Min flight weight

Answer 5

21,863 lb

Question 6

Min operating empty weight

Answer 6

20,412 lb

Question 7

Buoyancy limitation, when taking off or landing on runways near bodies of water

Answer 7

OUTFLOW VLV 2 closed
and
One pac off

Question 8

Max airport pressure altitude for takeoff and landing

Answer 8

10,000’

Question 9

Max operating altitude

Answer 9

51,000’

Question 10

Max ambient air temp for takeoff and landing

Answer 10

+50°C

Question 11

Min ambient air temp for takeoff and landing

Answer 11

-40°C

Question 12

Cowl anti-ice during takeoff limit

Answer 12

Must not be in AUTO.
OFF or ON only

Question 13

Limit for cowl anti-ice on during flight

Answer 13

TAT is 10°C or less in visible moisture (snow, rain, fog, visibility <1 mile)

Question 14

Limit for cowl anti-ice while on the ground

Answer 14

SAT is 10°C or less with contaminated surfaces (snow, ice, standing water or slush)

Question 15

Define inflight icing conditions

Answer 15

TAT 10°C or less with visible moisture, except when SAT is -40°C or below

Question 16

Minimum engine speed, while in icing conditions

Answer 16

76% N2

Question 17

Maximum runway slope for takeoff and landing

Answer 17

+2% uphill
-2% downhill

Question 18

Maximum tail wind component approved for takeoff and landing

Answer 18

10 kts

Question 19

Minimum flight crew

Answer 19

One pilot and one copilot

Question 20

Maximum number of passengers

Answer 20

19

Question 21

Maximum number of occupants for operation

Answer 21

22

Question 22

Prohibited runway conditions for operations

Answer 22

Unprepared surfaces
(i.e. gravel, grass, etc.)

Question 23

Limitation for operating display units with flight compartment temperatures in excess of 40°

Answer 23

Operations greater than 30 minutes are prohibited

Question 24

Maximum limit for runway threshold, glidepath, angles

Answer 24

Approach angles greater than 5.5° are prohibited.

Question 25

Maximum ITT for start on the ground

Answer 25

700°C

Question 26

Maximum engine ITT for start in flight

Answer 26

850°C

Question 27

Minimum N2 speed during idle

Answer 27

58%

Question 28

Max N2 speed for takeoff

Answer 28

99.6%

Question 29

Max fan speed for takeoff

Answer 29

102.0%

Question 30

Max ITT for takeoff

Answer 30

900°C (5 min AIO)

Question 31

Max continuous N2

Answer 31

98.9%

Question 32

Max continuous fan speed

Answer 32

102.0%

Question 33

Max continuous ITT

Answer 33

860°C

Question 34

Max transient N2 speed

Answer 34

99.8% (20 seconds)

Question 35

Max transient fan speed

Answer 35

102.0% (20 seconds)

Question 36

Max transient ITT

Answer 36

905°C (20 seconds)

Question 37

Time limit for takeoff thrust all engines operating

Answer 37

5 min

Question 38

Time limit for takeoff, thrust, one engine inoperative

Answer 38

10 min

Question 39

Maximum tailwind for engine starts

Answer 39

20 kts

Question 40

Maximum crosswind for engine starts

Answer 40

35 kts

Question 41

Minimum crank time for engine start with N1 rotation due to tailwind

Answer 41

30 seconds with an immediate AUTO start.

Question 42

Thrust limit for taxing when winds exceed 20 kts

Answer 42

Minimum only

Question 43

Limitation for Crosswinds during takeoff that exceed 20 kts

Answer 43

Do not exceed 66% N1 below 30 KIAS, then TO thrust.

Question 44

Maximum crosswind component during start

Answer 44

35 kts

Question 45

Max N2 RPM for engine starter engagement

Answer 45

42%

Question 46

Engine start limits

Answer 46

3 min ON, 15 sec OFF, 3 min ON, 15 sec OFF, 3 min ON, 15 min OFF

Question 47

Maximum wing fuel imbalance during flight

Answer 47

1100 lb

Question 48

Maximum wing fuel imbalance during takeoff and landing

Answer 48

600 lb (1100-600 lb depending on remaining fuel)

Question 49

Usable fuel in each main wing tank

Answer 49

15,050 lb

Question 50

Usable fuel in auxiliary tank

Answer 50

12,700 lb

Question 51

Usable fuel in aft tank

Answer 51

2,300 lb

Question 52

Minimum flight planned cruise altitude for center tank fuel to be usable

Answer 52

30,000'

Question 53

Limit to consider aft tank fuel usable

Answer 53

5500 lb wing fuel, planned cruise > FL300 500 lb min in Aft tank

Question 54

Minimum fuel for a go-around

Answer 54

600 lb Wings level, max 10° nose up.

Question 55

Minimum engine fuel temperature for takeoff

Answer 55

5°C

Question 56

Minimum oil temperature for starting

Answer 56

-40°C

Question 57

Minimum oil temperature before accelerating above idol

Answer 57

20°C

Question 58

Maximum permissible oil temperature

Answer 58

160°C

Question 59

Maximum oil consumption rate per engine

Answer 59

.21 US quarts per hour

Question 60

Auxiliary power unit type

Answer 60

RE 220

Question 61

Maximum APU rpm

Answer 61

106%

Question 62

Maximum operating altitude of the APU

Answer 62

45,000'

Question 63

Maximum number of APU starts

Answer 63

3 per hour

Question 64

Maximum altitude for starting the APU

Answer 64

37,000'

Question 65

Maximum altitude for APU bleed air extraction

Answer 65

30,000'

Question 66

Maximum OAT for APU bleeder extraction for air conditioning

Answer 66

45°C

Question 67

Maximum slats extended speed

Answer 67

225 kts

Question 68

Maximum speed for flaps 16°

Answer 68

210 kts

Question 69

Maximum speed for flaps 6°

Answer 69

210 kts

Question 70

Maximum speed for flaps 30°

Answer 70

185 kts

Question 71

Landing gear operating speed

Answer 71

200 kts

Question 72

Landing gear extended speed

Answer 72

250 kts/0.7M

Question 73

Maximum altitude for landing gear extended

Answer 73

20,000'

Question 74

Tire limit speed

Answer 74

183 kts

Question 75

Max turbulence penetration speed

Answer 75

300 kts/0.80M

Question 76

Maneuvering limit load factors - slats/flaps retracted

Answer 76

-1.0 G to +2.05 G

Question 77

Maneuvering limit load factors - slats/flaps extended

Answer 77

0.0 G to +2.0 G

Question 78

Cooling pack discharge temperature range during manual mode operations

Answer 78

5°C to 60°C

Question 79

Pack limit during manual mode operations

Answer 79

One pack must be selected off

Question 80

Maximum relieve differential pressure on cabin

Answer 80

10.73 psi

Question 81

Maximum negative relief differential pressure on cabin

Answer 81

-.5 psi

Question 82

Maximum cabin differential pressure during taxi and takeoff

Answer 82

0.1 psi

Question 83

Maximum cabin differential pressure during touchdown limit

Answer 83

1.0 psi

Question 84

Altitude limit for use of AUX PRESS

Answer 84

41,000'

Question 85

Max altitude for EMER DEPRESS

Answer 85

15,000'

Question 86

Maximum altitude with a yard damper disengaged 

Answer 86

41,000'

Question 87

Minimum speed to set autothrottles on takeoff

Answer 87

60 KIAS

Question 88

Minimum altitude for auto pilot engagement after takeoff

Answer 88

400' AGL

Question 89

Minimum altitude for the autopilot during a Cat I ILS or LPV

Answer 89

80' AGL

Question 90

Minimum altitude for auto pilot during a non-precision approach

Answer 90

400' AGL

Question 91

Minimum altitude for auto pilot during a non-precision approach with vertical path reference

Answer 91

160' AGL

Question 92

APU generator load limit

Answer 92

40 kVA

Question 93

Maximum altitude for slats/flaps extended

Answer 93

18,000'

Question 94

Minimum altitude for flight spoilers

Answer 94

300' AGL

Question 95

Limitations on the use of MAX spoilers

Answer 95

Prohibited, except during emergency conditions, or as required by AFM procedures