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Bell 206 B2 > Type Exam #1 > Flashcards

Type Exam #1 Flashcards

1
Q

What are the max internal and external gross weight limits?

A

3200lbs

3350lbs

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2
Q

What is the VNE between 85% and 100% torque power range?

A

92 MPH

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3
Q

What is the VNE when gross weight is 3000lbs?

A

150MPH

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4
Q

What is the VNE when gross weight is above 3000lbs

A

140MPH

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5
Q

What is max operating altitude for gross weights of 3000lbs and below?

A

20 000 feet pressure altitude

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6
Q

Min and max rotor RPM (Nr) with power off?

A

90% and 107%

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7
Q

Min rotor RPM for gross weights above 3000lbs is ________ and can droop down to ________ for max of _______ seconds

A

97%
95%
5 seconds

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8
Q

Which engine is in Bell 206B2?

A

Allison 250-C20

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9
Q

Max Power Turbine N2 RPM is ________ and min is _________ when gross weights above 3000lbs?

A

100%

97%

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10
Q

N2 transient over speed limit is _____ for max of ______ seconds

A

105%

15 seconds

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11
Q

The max Gas producer (N1) RPM is ________ and transient limit is _______ for max of _________ seconds?

A

104%
105%
15 seconds

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12
Q

Max allowable engine oil temp?

A

107 C

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13
Q

Max takeoff torque is _______ for a max of _______ minutes?

A

100%

5 minutes

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14
Q

Max continuous torque is _________ with max TOT of _________?

A

85%

737 C

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15
Q

Max TOT limit for take off?

A

793 C for 5 minutes

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16
Q

What are transient TOT limits?

A

793 C to 843 C for 6 seconds

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17
Q

What are Max starting and shut down TOT limits?

A

793 C to 927 C for 10 seconds

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18
Q

Anti icing must be on for flight in visible moisture when temp is below _______?

A

4.4 C

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19
Q

Max transmission oil pressure is ________ and max transmission oil temp is ________?

A

70 PSI

110 C

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20
Q

Above 8000 feet what are the min and max N2 limits?

A

97%

100%

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21
Q

Min front seat weight?

A

150lbs

22
Q

The C of G longitudinal limits from station are?

A

106 inches to 114.2 inches

23
Q

What are the later C of G limits?

A

3 inches left

4 inches right

24
Q

When staring when should fuel be introduced N1?

A

15%

25
Q

If main rotor is not turning by ______ N1 start should be aborted.

A

25%

26
Q

On start up the starter should be released at _______ N1?

A

58%

27
Q

When should the generator be turned on? (N1)

A

100%

28
Q

If engine has been shut down for more than 15 min engine must stabilize at ground idle speed for ________ before increasing power?

A

1 minute

29
Q

Before takeoff the generator load should be below ______?

A

70%

30
Q

On shutdown how long should engine stabilize at idle speed before the throttle is closed?

A

2 minutes

31
Q

When both fuel pumps become inoperative the unusable fuel becomes________ gallons?

A

10 gallons

32
Q

If one or both boost pumps become inoperative descend below?

A

6000 feet pressure altitude

33
Q

What is the desired airspeed in autorotation?

A

58 to 69 MPH

34
Q

During hydraulic system failure the airspeed should be reduced to ______ ?

A

70 to 80 MPH

35
Q

Area B in critical wind azimuth chart is from ______ to _______ degrees?

A

50 to 210 degrees

36
Q

C of G will ______ as fuel is consumed?

A

Move fwd

37
Q

Baggage compartment has load limit of ______ lbs with max of _______ lbs per square foot?

A

250 lbs and 86 lbs

38
Q

With single bladder fuel cell total capacity is ______ US Gallons and the useable fuel capacity is ______ US gallons?

A

77.06 and 76 US gallons

39
Q

Engine oil capacity?

A

5.5 US Quarts

40
Q

Max tie down load applied to blade tips shall not exceed_______ ?

A

100 lbs

41
Q

With Range extender fuel system installed the min cockpit weight becomes ________ lbs ?

A

200 lbs

42
Q

With range extender fuel system installed the baggage compartment is restricted to ________ lbs when Aircraft is loaded with 3 rear pax?

A

110 lbs

43
Q

What is max capacity with range extender full (US Gallons)

A

96.7 US Gallons

44
Q

When external cargo hook is installed what is the VNE when flying a sling load above 3000 lbs gross weight?

A

91 MPH

45
Q

External cargo hook model 206-706-335 has max load of ______ lbs?

A

1500 lbs

46
Q

With particle separator engine air induction system the deflector baffled shall be removed at _____ f OAT and above?

A

80 degrees f

47
Q

When engine re-ignition system is installed it should not be activated above _______ ft?

A

12 000 feet

48
Q

What is the VNE with one or both aft cabin doors of up 3000 feet?

A

100 MPH

49
Q

What is the VNE with one or both forward doors off all or any combination of fwd and aft doors off?

A

80 MPH

50
Q

With fwd or aft doors removed the VNE decreases _______

A

1 MPH per 1000 feet above 3000 feet

Bell 206 B2 (1 decks)

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