Limitations

Question 1

What is the preferred oil level?

Answer 1

2 and 3 units down from full

Question 2

What are the Va weights and respective speeds?

Answer 2

4110kg - 143 KIAS
3208kg - 137 KIAS
2835kg - 125 KIAS
2268kg - 112 KIAS

Question 3

Reduction of VFE speeds on C208B and EX

Answer 3

25 knots on C208B and as placarded on EX

Question 4

Load factor limits at MTOW

Answer 4

+3.36 g
-1.34 g

Flap down

+2.0 g

Question 5

C208B and EX max ITT ( normal and Hardy’s) for

1. Start
2. Take-off
3. Climb
4. Cruise
5. Transient
6. Idle

Answer 5

1. 1090°
2. 805°, 850° EX
3. 765°/760°, 825° EX/800° EX
4. 740°/740°, 805° EX/780° EX
5. 850° (2 secs.), 905° (20 secs.)
6. 685°, 700°

Question 6

C208B and EX torque limitations

1. Maximum rated
2. Transient

Answer 6

1. 1865/2397 ft-lbs

2. 2400/2600 ft-lbs (20 secs.)

Question 7

Prop RPM limitations C208B and EX

1. Maximum transient
2. Maximum reverse

Answer 7

1. 2090 RPM (emerg. condition, to complete flight and at all engine ratings)
2. 1825 RPM

Question 8

Ng limitations C208B and EX

1. Take-off, climb, cruise, reverse
2. Idle
3. Transient

Answer 8

1. 101.6%/103.7%
2. 52% minimum, 55% minimum
3. 102.6% (2 secs.), 105.4% (20 secs.)

Question 9

C208B oil pres. limitations

1. Take-off, climb, cruise, reverse
2. Idle

Answer 9

1. 85-105 psi

2. 40 psi minimum

Question 10

C208B EX oil pres. limitations

1. Take-off, climb, cruise, reverse
2. Idle
3. Starting

Answer 10

1. 85-105 psi
2. 40 psi min
3. 200 psi max

Question 11

C208B oil temp limitations

1. Take-off
2. Climb, cruise, reverse
3. Idle
4. Transient
5. Starting

Answer 11

1. 10-99°
2. 0-99°
3. -40-99°
4. 99-104° (10 mins)
5. -40° minimum

Question 12

C208 EX oil temp limitations

1. Take-off, climb, cruise, reverse
2. Idle
3. Starting
4. Transient

Answer 12

1. 32-99°
2. -40-99°
3. -40° minimum
4. 104° (10 minutes)

Question 13

Normal oil pressure and temp above 72% Ng

Answer 13

85-105psi
60-70°

Oil pres below 85/80 tolerate for completion of flight at reduced power if possible. 40 psi or less is unsafe , engine shut down or landing using minimum power to maintain flight

Question 14

Starter cycle limitations C208B and EX

Answer 14

BATTERY

30 secs on 60 secs off
30 secs on 60 secs off
30 secs on 30 mins off

EXT POWER

20 secs on 120 secs off
20 secs on 120 secs off
20 secs on 60 mins off

Question 15

Maximum oil consumption rate

Answer 15

0.1 qt per hour

Question 16

Fuel useable capacity

Answer 16

332 US GALLONS / 1256 L approx 2228 lbs

Question 17

With low fuel reserves max balance ball deflection?

Answer 17

1/4 deflection

Question 18

Max side lisp duration and maximum inflight fuel imbalance

Answer 18

3 minutes and 200 lbs

Question 19

Company aircraft altitude limitation

Answer 19

20,000 feet

Question 20

Use of AVGAS in 208B

Answer 20

1. Emerg. Use only
2. 150 hours maximum
3. 29 degrees maximum take off temp
4. 9000 max alt.
5. Fuel boost pump on all operations

Question 21

Autopilot

1. Max engagement speed
2. Minimum engagement speed
3. Max electric trim operating speed

Answer 21

1. 175 KIAS
2. 80 KIAS
3. 175 KIAS

Question 22

Autopilot

1. Minimum altitude on approach
2. Minimum altitude on all other operations

Answer 22

1. 200 feet AGL

2. 800 feet AGL

Question 23

A/P not permitted on MAP procedure until an established rate of climb is reached for that procedure.

Answer 23

As front

Question 24

Use of autopilot is not permitted when audio panel is inop.

Answer 24

As above

Question 25

ILS approaches are limited to CAT1

Answer 25

As above

Question 26

Raw data ILS approaches are prohibited below 400 feet AGL

Answer 26

As above

Question 27

IDENTIFY , CONFIRM , SELECT

Answer 27

As above

Question 28

If engine oil drops below 15 PSI the engine should be feathered

Answer 28

As above

Question 29

Best rate of climb speed C208 EX

Answer 29

108 KIAS

Question 30

Decision points and respective distances

Answer 30

``` Less than 800m - 40 KIAS OR 1/3 TODA 800m - 1200m - Vlift off - 10 KIAS 1200 - 1500m - Vlift off 1500m - 2000m - 50’ AGL < 2000m - 200’ AGL ```

Question 31

If Ng is observed slower than normal. Abort start, possible weak battery

Answer 31

As above

Question 32

Hung start

Answer 32

Ng stagnate at 35-40%

Question 33

Aborted start reasons

Answer 33

1. No light off within 10 seconds 2. Poor cranking power (Ng stagnate at 35-40%) 3. Starter accelerates Ng rapidly above 20% (gear train decouple) 4. Rapid acceleration beyond 35% (start on secondary nozzles) 5. Rapid ITT increase toward 1090° 6. Compressor stall 7. Starter on after 46%

Question 34

Aborted start sequences

Answer 34

1. Starter switch off 2. FCL cut off 3. If ITT excessive or requires assistance to reduce thence motor

Question 35

Minimum Ng for aircon in B

Answer 35

54%

Question 36

Intertidal sep torque change on ground

Answer 36

25 lbs

Question 37

Bus volts drop on stby per

Answer 37

1 volt

Question 38

Generator load on ground

Answer 38

30 but no more than 60 amps

Question 39

If TRIM warning light does not stay on then the autopilot did not pass the preflight test

Answer 39

As above

Question 40

How to rebalance fuel

Answer 40

1/2 ball down towards tank with least fuel

Question 41

Avionics switch off below what NG

Answer 41

5%

Question 42

Stable approach by 300 feet agl

Answer 42

Stable

Question 43

Circling approach procedure

Answer 43

140 initial Prop max Flap 10 Final segment 120 Kias Flap 20 Circling segment 100 Kias for level

Question 44

Missed approach

Answer 44

``` Power max allowed Set attitude Wing flaps 20 80 Kias Wing flaps retract Climb checklist complete ```

Question 45

Normal circuit entry and landing

Answer 45

``` Downwind Flaps 10 Prop max Torque 800-1100 Speed 120 Kias ``` Base Torque 500ft Flaps 20 Speed 110 Final Torque 500 ft Flaps 30 Speed 85

Question 46

TORR FACTORING

Answer 46

1.25%

Question 47

All aircraft stores to be carried in Pod D

Answer 47

As above

Question 48

Max passengers

Answer 48

13 day IFR and night VFR charter or 9 if TAW b US 13 day VFR 9 RPT single pilot 12 IFR TWO PILOTS RPT CAN HAVE TWO INFANTS OR TWO CHILDREN ON TOP OF 9 adult pax

Question 49

Trim sheet to show TOW, Landing W, zero fuel weight and to be signed

Answer 49

As above

Question 50

Separator use in flight

Answer 50

Visible moisture at or below 5 degrees Celsius

Question 51

Ignition switch on 6 situations

Answer 51

Emergency air start Without starter assist Operation on slush or water runways Flight in heavy precip Inadvertent icing encounters until internal sep has been in use for 5 minutes As part of initial response to any engine or fuel system malfunction During low vis take off 5000m less or at night until above turn back altitude

Question 52

ASETPA SAFETY DIST

Answer 52

Glide 15 mins at TAS | GLIDE TO 1000’ AGL