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
Props (N2 RPM) limits
``` 1050. Minimum idle 1450-1700. Normal Op range 1650. Max Reverse 1700. Max 1870. Transient 400-1050. Avoid during ground op ```
25
Weight Limits
300. 350. ``` 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
Rudder boost
Must be operative for all flights
27
Yaw damp system
18500 (300). 19000 (350) Max alt inop (Dual strakes) | Greater than or above must be on except for takeoff and landing Check REL
28
Brake Deice limitations
Don't use: 1 Above. 15 degrees C 2 More than 10 min w/wheels retracted
29
Fuel system limits
``` 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
Gear cycle limits
1. 6 cycles at one cycle every 5 min | 2. 15 minutes rest after 6 cycles
31
Starter limitations
30 seconds on 5 min off 30 seconds on 5 min off 30 seconds on 30 min
32
Prop deice ammeter limits
26-32 amps normal range
33
Cabin altimeter and differential limits
0. - 6.6 PSI