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C208 FCOM > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the preferred oil level?

A

2 and 3 units down from full

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2
Q

What are the Va weights and respective speeds?

A

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

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3
Q

Reduction of VFE speeds on C208B and EX

A

25 knots on C208B and as placarded on EX

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4
Q

Load factor limits at MTOW

A

+3.36 g
-1.34 g

Flap down

+2.0 g

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5
Q

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

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

C208B and EX torque limitations

  1. Maximum rated
  2. Transient
A
  1. 1865/2397 ft-lbs

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

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7
Q

Prop RPM limitations C208B and EX

  1. Maximum transient
  2. Maximum reverse
A
  1. 2090 RPM (emerg. condition, to complete flight and at all engine ratings)
  2. 1825 RPM
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8
Q

Ng limitations C208B and EX

  1. Take-off, climb, cruise, reverse
  2. Idle
  3. Transient
A
  1. 101.6%/103.7%
  2. 52% minimum, 55% minimum
  3. 102.6% (2 secs.), 105.4% (20 secs.)
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9
Q

C208B oil pres. limitations

  1. Take-off, climb, cruise, reverse
  2. Idle
A
  1. 85-105 psi

2. 40 psi minimum

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10
Q

C208B EX oil pres. limitations

  1. Take-off, climb, cruise, reverse
  2. Idle
  3. Starting
A
  1. 85-105 psi
  2. 40 psi min
  3. 200 psi max
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11
Q

C208B oil temp limitations

  1. Take-off
  2. Climb, cruise, reverse
  3. Idle
  4. Transient
  5. Starting
A
  1. 10-99°
  2. 0-99°
  3. -40-99°
  4. 99-104° (10 mins)
  5. -40° minimum
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12
Q

C208 EX oil temp limitations

  1. Take-off, climb, cruise, reverse
  2. Idle
  3. Starting
  4. Transient
A
  1. 32-99°
  2. -40-99°
  3. -40° minimum
  4. 104° (10 minutes)
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13
Q

Normal oil pressure and temp above 72% Ng

A

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

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14
Q

Starter cycle limitations C208B and EX

A

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

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15
Q

Maximum oil consumption rate

A

0.1 qt per hour

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16
Q

Fuel useable capacity

A

332 US GALLONS / 1256 L approx 2228 lbs

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17
Q

With low fuel reserves max balance ball deflection?

A

1/4 deflection

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18
Q

Max side lisp duration and maximum inflight fuel imbalance

A

3 minutes and 200 lbs

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19
Q

Company aircraft altitude limitation

A

20,000 feet

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20
Q

Use of AVGAS in 208B

A
  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
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21
Q

Autopilot

  1. Max engagement speed
  2. Minimum engagement speed
  3. Max electric trim operating speed
A
  1. 175 KIAS
  2. 80 KIAS
  3. 175 KIAS
22
Q

Autopilot

  1. Minimum altitude on approach
  2. Minimum altitude on all other operations
A
  1. 200 feet AGL

2. 800 feet AGL

23
Q

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

24
Q

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

25
Q

ILS approaches are limited to CAT1

26
Q

Raw data ILS approaches are prohibited below 400 feet AGL

27
Q

IDENTIFY , CONFIRM , SELECT

28
Q

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

29
Q

Best rate of climb speed C208 EX

30
Q

Decision points and respective distances

A 
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
31
Q

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

32
Q

Hung start

A

Ng stagnate at 35-40%

33
Q

Aborted start reasons

A
  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%
34
Q

Aborted start sequences

A
  1. Starter switch off
  2. FCL cut off
  3. If ITT excessive or requires assistance to reduce thence motor
35
Q

Minimum Ng for aircon in B

36
Q

Intertidal sep torque change on ground

37
Q

Bus volts drop on stby per

38
Q

Generator load on ground

A

30 but no more than 60 amps

39
Q

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

40
Q

How to rebalance fuel

A

1/2 ball down towards tank with least fuel

41
Q

Avionics switch off below what NG

42
Q

Stable approach by 300 feet agl

43
Q

Circling approach procedure

A

140 initial
Prop max
Flap 10

Final segment 120 Kias
Flap 20

Circling segment 100 Kias for level

44
Q

Missed approach

A 
Power max allowed
Set attitude 
Wing flaps 20
80 Kias 
Wing flaps retract 
Climb checklist complete
45
Q

Normal circuit entry and landing

A 
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

46
Q

TORR FACTORING

47
Q

All aircraft stores to be carried in Pod D

48
Q

Max passengers

A

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

49
Q

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

50
Q

Separator use in flight

A

Visible moisture at or below 5 degrees Celsius

51
Q

Ignition switch on 6 situations

A

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

52
Q

ASETPA SAFETY DIST

A

Glide 15 mins at TAS

GLIDE TO 1000’ AGL

C208 FCOM (1 decks)

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