Exam

Question 1

The 206LR rotor disk diameter is approximately:

Answer 1

37 feet

Question 2

The engine in FBKS is an:

Answer 2

Allison 250 C20R

Question 3

The capacity of FBKS’s fuel tank is ___ US gal or approximately ___ pounds

Answer 3

110 US gal, 748 pounds

Question 4

Minimum front seat total weight limit for FBKS is:

Answer 4

170 lbs

Question 5

Maximum internal gross weight for the 206LR is:

Answer 5

4000 lbs

Question 6

Maximum external gross weight for the 206LR is:

Answer 6

4000 lbs

Question 7

Vne in the take off torque range is:

Answer 7

92 mph

Question 8

Vne with external loads is:

Answer 8

100 mph

Question 9

Vne with any combination of door(s) off is:

Answer 9

100 mph

Question 10

Vne for FBKS with the pilot bubble window installed is:

Answer 10

110 mph

Question 11

Maximum continuous torque is limited to:

Answer 11

88%

Question 12

Maximum takeoff torque is limited to:

Answer 12

100% for 5 minutes

Question 13

Maximum transient torque is ___ and ___ be used intentionally.

Answer 13

105% for 5 seconds, may not

Question 14

Maximum continuous TOT is:

Answer 14

752 degrees C

Question 15

Maximum take-off TOT is:

Answer 15

810 degrees C for 5 minutes

Question 16

Maximum TOT during starting and shutdown is:

Answer 16

810 - 927 degrees C for 10 seconds

Question 17

Maximum transient N2 RPM is:

Answer 17

105% for 15 seconds

Question 18

Maximum load on the load meter is:

Answer 18

83%

Question 19

During the start procedure, do not open the throttle at N1 speeds below:

Answer 19

12%

Question 20

What are some points in regards to the 71-88% N2 speed avoidance range:

Answer 20

• Transient operation through this range is permitted
• Continuous operation in this range must be avoided regardless of torque setting
• Allowing the N1 to linger at or around 70% may place the N2 into the speed avoidance range

Question 21

True or False?
The CAUTION LT circuit breaker need not be pulled on FBKS as it is equipped with a WRN HORN MUTE button?

Answer 21

True

Question 22

True or False?
The fuel system on a 206L is exactly the same as on a 206B?

Answer 22

False

Question 23

What are some points in regards to the 206L fuel system?

Answer 23

• Fuel is transferred from the forward cells to the aft cell by an ejector pump that will function with one or both boost pumps operating
• The FUEL LOW light and fuel gauge are separate systems and whichever indicates the lowest fuel quantity should be trusted
• Up to 155 lbs of fuel can remain unavailable to the engine if both boost pumps fail

Question 24

True or False?
The pilot can ensure that both boost pumps are turned off by turning the battery switch off when the helicopter is parked?

Answer 24

False

Question 25

True or false? The left hand boost pump is wired directly to the battery and, if the LEFT FUEL BOOST circuit breaker is left in and the FUEL VALVE switch is left on, will continue to run with the BAT switch left in the off position?

Answer 25

True

Question 26

True or false? In addition to a circuit breaker in the overhead panel for the left boost pump, there is a circuit breaker located in the battery compartment on the starboard side?

Answer 26

True

Question 27

The FUEL LOW light illuminates in flight with approximately 230 lbs of fuel indicated on the fuel gauge. you elect to:

Answer 27

Land as soon as practical. Despite what the fuel gauge indicates, you only have about 60-70 lbs of fuel available to the engine.

Question 28

The FUEL FILTER light illuminates in flight. This means the ___ is in impending bypass and you elect to ___.

Answer 28

Airframe fuel filter, land as soon as possible

Question 29

When armed, the auto-relight system in FBKS will activate when

Answer 29

N2 falls below 96%

Question 30

True or false? If, during the pre-flight check (engine not operating), the auto-relight activates with the switch in the ARM position, the system is serviceable?

Answer 30

False

Question 31

In autorotation, what airspeed/rotor RPM combination give the best glide?

Answer 31

80 mph/90%

Question 32

What is the procedure to perform a power check on the 206L?

Answer 32

Perform at 0 airspeed with all sources of bleed air off. Record OAT, pressure altitude, torque, TOT, N1

Question 33

The power check charts to be used for FBKS are those found in:

Answer 33

Section 5 of the Soloy C20R supplement

Question 34

What items make up the 'snow kit' on the 206L and are required when operating in falling and/or blowing snow?

Answer 34

Snow deflectors and auto-relight

Question 35

On FBKS, the longline release button is located on the ___ and the cargo hook release is located on the ___. The manual release for the cargo hook is located ___. The longline and cargo hook systems are ___ armed.

Answer 35

Collective, cyclic, between the pilot and co-pilot seats, always

Question 36

Which of the Flight Manual sections and charts are most appropriate for performance calculations for FBKS?

Answer 36

- Section 5 performance charts of the basic flight manual, adjusted for a +7% engine in accordance with the existing Section 9 Charts - For operations up to 10 000' pressure altitude, charts found in Bell's Water-Alcohol Power Augmentation supplement (FMS1) may also be used

Question 37

True or false? In FBKS, take-off, hover and landing are prohibited with the Paravion cabin heater operating?

Answer 37

True

Question 38

Maximum inflation airspeed for the emergency pop-out floats on FBKS is:

Answer 38

60 mph

Question 39

True or false? For flight over land, or for flight over water at altitudes exceeding 500' and at airspeeds of 60 mph and above, the FLOAT MANUAL ARM switch should be in the OFF (guard closed) position?

Answer 39

True

Question 40

True or false? Regardless of the position of the FLOAT MANUAL ARM switch, the FLOAT INFLATION trigger switch will deploy the pop-out floats?

Answer 40

False

Question 41

True or false? Failure the comply with the Pre-flight Float System Check as written in the appropriate flight manual supplement can result in an inadvertent deployment of the pop-out floats, or can result in a faulty float deployment system going undetected?

Answer 41

True

Question 42

What are some points in regards to the unique seating configuration of the 206L?

Answer 42

- When both crew seats are occupied, only one mid passenger is permitted unless there are two aft passengers. - The aircraft will be loaded dangerously beyond its forward C of G limit if both forward seats and both mid seats are occupied without any aft seats occupied. - Passengers must be briefed to remain in their assigned seats and in particular aft seat passengers must not be permitted to transfer into the mid seats during flight.