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B350 Study Materials > Specifications And Limitations > Flashcards

Specifications And Limitations Flashcards

1
Q

Aircraft Length

A

46’ 8”

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2
Q

Aircraft Wingspan

A

57’ 11”

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3
Q

Aircraft Height

A

14’ 4”

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4
Q

Max Occupancy

A

17 including crew

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5
Q

Engine Type and SHP

A

PT6A-60A 1050 SHP

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6
Q

Max Ramp Weight

A

15,100 lbs

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7
Q

Max Takeoff Weight

A

15,000 lbs

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8
Q

Max Landing Weight

A

15,000 lbs

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9
Q

Max ZFW

A

12,500 lbs

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10
Q

Max Weight in Baggage Area

A

510 lbs with folding seats

550 lbs without folding seats

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11
Q

Vxse and Vyse

A

125 KIAS

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12
Q

Vmca

A

94 KIAS flaps UP

93 KIAS flaps Approach

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13
Q

Emergency Descent Speed

A

184 KIAS

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14
Q

Best Glide Speed

A

135 KIAS

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15
Q

Va

A

184 KIAS

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16
Q

Vfe Approach

A

202 KIAS

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17
Q

Vfe Full

A

158 KIAS

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18
Q

Vle

A

184 KIAS

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19
Q

Vlo Extension

A

184 KIAS

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20
Q

Vlo Retraction

A

166 KIAS

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21
Q

Vmo

A

263 KIAS, .58 mach

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22
Q

Max Demonstrated Crosswind

A

20 KIAS

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23
Q

Vx

A

125 KIAS

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24
Q

Vy

A

140 KIAS

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25
Q

Turbulent Air Penetration Speed

A

170 KIAS

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26
Q

Vsse

A

110 KIAS

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27
Q

Turning Radius

A

41’ 7”

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28
Q

Hydraulic Fluid Type

A

MIL-5606

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29
Q

Battery

A

24 volt 34 or 36 amp NiCad

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30
Q

Main Tires

A

10 ply 80-92 psi

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31
Q

Nose Tire

A

8 ply 55-60 psi

32
Q

Vso

A

81 IAS

33
Q

Vs

A

96 IAS

34
Q

Max Starting ITT

A

1000 C for 5 seconds

35
Q

Max Idle ITT

A

750 C

36
Q

Max Takeoff ITT

A

820 C

37
Q

Max Continuous ITT

A

820 C

38
Q

Max Cruise Climb ITT

A

785 C

39
Q

Max Cruise ITT

A

820 C

40
Q

Max Reverse ITT

A

760 C

41
Q

Max Transient ITT

A

850 C for 20 sec

42
Q

Transient Torque Limit

A

156% for 20 seconds

43
Q

Min N1 at IDLE

A

62%

44
Q

Max N1

A

104%

45
Q

Prop RPM at IDLE

A

1050 rpm

46
Q

Max Prop RPM

A

1700 rpm, excursions up to 1735 rpm are acceptable for 7 min

47
Q

Max Reverse RPM

A

1650 rpm

48
Q

Max Transient Prop RPM

A

1870 rpm

49
Q

Overspeed Governor RPM

A

1768 rpm

50
Q

Overspeed Governor RPM

A

1768 rpm

51
Q

Overspeed Governor RPM

A

1768 rpm

52
Q

Max Starting Oil Press

A

200 psi

53
Q

Min oil pressure at IDLE

A

60 psi

54
Q

Normal Oil Pressure Range

A

90-135 psi

55
Q

Transient Oil Pressure

A

200 psi

56
Q

Min Oil TEMP for starting

A

-40 C

57
Q

Min recommended oil temp for takeoff

A

55 C

58
Q

Normal oil temp range

A

0-110 C…temps between 99-110 C are limited to 10 min

59
Q

External power limits

A

28.0-28.4 volts

1000 amps momentarily, 300 amps continuous

60
Q

Generator Limits

A

SL - 34,000 feet = 100% load

Above 34,000 feet = 95%

61
Q

Max Generator Load 62-70% N1

A

75%

62
Q

Max Generator Load 70-100% N1

A

100%

63
Q

Starter limits

A

30 seconds ON, 5 min OFF, 30 seconds ON, 5 min off, 30 seconds ON, 30 min OFF

64
Q

Limitations using aviation gasoline

A

150 hours
Prohibited if either standby fuel pump is inop
Crossfeed capability is required above 20,000 feet

65
Q

Usable Fuel (without saddle tanks)

A

3611 pounds total
1273 pounds in each main
533 pounds in each aux tank

66
Q

Max fuel imbalance

A

300 pounds

67
Q

Fuel gages in yellow arc

A

Do not take off if less than 265 pounds in each wing system

68
Q

Aux tank fueling

A

Do not put any fuel in the aux tanks unless the mains are full

69
Q

Prop manufacturer & diameter

A

Hartzell, 105”

70
Q

Prop overspeed limits

A

Flight may be continued with an overspeed up to 1768 rpm as long as torque is limited to 96%

71
Q

Max cabin pressure differential

A

0 - 6.6 psi

72
Q

Pneumatic pressure gage range

A

12 - 20 psi, redline is 20 psi

73
Q

Prop de-ice ammeter range

A

26 - 32 amps

74
Q

Flight Load Limits

A

Flaps UP = +3.1, -1.24 g

Flaps DOWN = +2.0. -0.0 g

75
Q

Max Operating Altitude

A

35,000 feet

76
Q

Max Operating Altitude with YD inop

A

Above 5,000 feet without strakes

Above 19,000 feet with Raisbeck STC SA5151NM

B350 Study Materials (3 decks)

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