300/350 Limits Flashcards

0
Q

Vmca flaps down

A
  1. 350

86. 98

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1
Q

Min for reverse

A
  1. 350

40. 40

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2
Q

Vmca. flaps up

A
  1. 350

92. 101

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3
Q

V SSE

A
  1. 350

115. 135

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4
Q

V yse

A
  1. 350

122. 135

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5
Q

Vx

A
  1. 350

122 135

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6
Q

Maximum Glide Range

A
  1. 350

134 135

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7
Q

Vy

A
  1. 350

137. 135

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8
Q

Minimum in sustained Icing flight

A
  1. 350

140. 140

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9
Q

VLO. (Retraction)

A
  1. 350

163. 164

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10
Q

Vb. (Turbulence penetration)

A
  1. 350

170. 170

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11
Q

Va (flaps up)

A
  1. 350

181. 182

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12
Q

Vlo. Extension

A
  1. 350

181. 182

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13
Q

Vfe (approach)

A
  1. 350

200. 202

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14
Q

Max Windshield Deicing

A
  1. 350

226. 226

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15
Q

Vmo (below 24000 ft)

A
  1. 350

259. 245

16
Q

Mmo

A
  1. 350

.58. .58

17
Q

Torque Limits

A

0-100 Norm op range

  1. Max transient (20 sec)
  2. Max TQ Abv 1700
  3. Transient 7 minutes (350)
18
Q

Turbine Tach (N1) speed limits

A
  1. Min low idle
  2. Max
  3. Max transient
19
Q

ITT Limits

A
  1. Max low idle
  2. Max reverse
  3. Rec Cruise climb
  4. Max Cruise
  5. Transient. (20 sec)
  6. Max transient starting
20
Q

Oil temp limits

A
-40 to. 110.    Starting, low idle
    0 to.  99     Normal
    110.           Maximum
 99. To. 110.  Max transient (10 min)
    55.             Rec for fuel heater op
21
Q

Oil PSI limits

A
  1. Minimum low idle
    60-90. Caution range
    90-136. Normal operating
    200 Max starting
22
Q

Pneumatic pressure limits

A

12-20 psi. Normal Op range

20 psi. Max

23
Q

DC Power limits

A

75 Pct. Max (62 - 70 n1)
100 Pct. Max (< 34000)
95 Pct. Max (> 34000)
27.5-29. Norm VDC

24
Q

Props (N2 RPM) limits

A
1050.          Minimum idle
1450-1700. Normal Op range
1650.          Max Reverse
1700.          Max
1870.          Transient
400-1050.   Avoid during ground op
25
Q

Weight Limits

A
15100   16600.  Max ramp weight
15000.  16400.  Max TO weight
14000.  15675.  Max Land weight
11500.  13000.  Max zero fuel
550 lbs Max baggage compmnt wt. 
one person Max on airstair door
26
Q

Rudder boost

A

Must be operative for all flights

27
Q

Yaw damp system

A

18500 (300). 19000 (350) Max alt inop (Dual strakes)

Greater than or above must be on except for takeoff and landing
Check REL

28
Q

Brake Deice limitations

A

Don’t use:
1 Above. 15 degrees C
2 More than 10 min w/wheels
retracted

29
Q

Fuel system limits

A
300 lbs maximum imbalance
265 lbs Min each main for takeoff
10 hrs Max with fuel pressure light
539 (300)   775 (ER) gal Max usable
Fuel quantity.
If fuel in Aux.'s mains must be full 
(Main and aux full before filling
30
Q

Gear cycle limits

A
  1. 6 cycles at one cycle every 5 min

2. 15 minutes rest after 6 cycles

31
Q

Starter limitations

A

30 seconds on 5 min off
30 seconds on 5 min off
30 seconds on 30 min

32
Q

Prop deice ammeter limits

A

26-32 amps normal range

33
Q

Cabin altimeter and differential limits

A
    • 6.6 PSI