1. NASCC VT-31 GOUGE

2. V SPEEDS

3. Min safe one engine inoperative
Airspeed Limitations
Condition V
Airspeed (KIAS)
Max dive/level flight
VMO
227
Min safe one engine inoperative
VSSE 91
Minimum controllable
VMCA 86
Maneuvering VA
153
Max gear extended
VLE
155
Max gear retraction
VLR
145
Max 35% (Approach) Flaps
VFE
174
Max Full Flaps
VFE
140

4. Vmca Minimum controllable airspeed
86 KIAS

6. Vmcg Minimum controllable groundspeed
63 KIAS

7. VSSE Minimum safe 1 engine inop
91 KIAS

8. VX / VXSE Best angle of Climb
102 KIAS

9. VY
108 KIAS

10. VYSE
110 KIAS

11. VFE Max flap extension/extended (full)
140 KIAS

12. VFE Max flap extension/extended (appr)
174 KIAS

13. VLR Max landing gear retraction
145 KIAS

14. VLE Max landing gear extension
155 KIAS

15. Max endurance glide
102 KIAS

16. Max range glide
130 KIAS

17. VA Maneuvering speed
153 KIAS

18. VMO/VNE Max dive/level flight
227 KIAS

19. ELECTRICAL SYSTEM

20. DC generator voltage
28.25±.8 V

21. AC inverter voltage
114±7/26 V

22. AC inverter frequency
400±6 Hz

23. Min volts for APU charge

24. Min volts for APU start
20V

25. Min battery voltage for Batt start

26. Starter cycle limits
(40 sec, 1 min) x2, then 30 min

27. Interstage Turbine Temperature (ITT)

28. ITT Normal operating range
400 – 790 °C

29. ITT Max allowable
790 °C

30. ITT Max continuous
790 °C

31. ITT Max reverse
790 °C

32. ITT Max acceleration (up to 2 sec)

33. ITT Max low idle
685 °C

34. ITT Max cruising
740 °C

35. ITT Cruise climb
765 °C

36. ITT Max start
925 °C cutoff
1090 °C (2 sec)

37. Torque

38. Torque Normal operating range
400 – 1315 ft-lb

39. Max 1900RPM
1520 ft-lb

40. Max 2200RPM
1315 ft-lb

41. Torque Max acceleration
2100 ft-lb (2 sec)

42. Turbine tachometer (N1)

43. N1 Normal operating range
50% – 101.5%

44. N1 Low idle range
50% - 53%

45. N1 High Idle Range
64% - 67%

46. N1 Max reverse
86%

47. N1 Max acceleration (2 sec)
102.6%

48. N1 Max continuous
101.5%

49. Propeller tachometer (N2)

50. N2 Normal operating range
1800 – 2200 RPM

51. N2 Max reverse
2100 RPM

52. Max N2 during accel (2 sec)
2420 RPM

53. Oil Temperature

54. Normal oil temp operating range
10 – 99 °C

55. Max oil temp
99 °C

56. Oil Pressure

57. Normal oil press operating range @ 72% N1
85 – 100 psi

58. Max oil pressure
100 psi

59. Min oil pressure
40 psi

60. Prohibited maneuvers
Intentional Spins
Aerobatics

61. General

62. Max ramp weight
9,710 lbs

63. Max takeoff weight
9,650 lbs

64. Max landing weight
9,168 lbs

65. Pneumatic pressure norm operating range
16 ± 4 psi

66. Aircraft ceiling
31,000 ft

67. Max sink rate on landing
600 FPM

68. Min O2 required during local/XC flight
1,000/1,500 psi

69. Blade angle for beta
15/-5 deg

70. Blade angle for reverse
-5/-11 deg

71. Blade angle in feather
87 deg

72. Prop deicer ammeter normal operation
amp

73. Max crosswind
20 kts

74. Max cabin pressure differential
4.7 psid

75. Gyro suction norm operating range
5.1 ± .8 Hg

76. Nosewheel travel left/right of center
12L/14R deg

77. Nosewheel travel with brake assist
48 deg

78. Left squat switch (HHHAP)
H – AOA Heat
H – Heat left engine lip boot
H – Electric heat from GRD MAX - normal
A – Ambient air solenoid opens w/ airborne
P – Pressurization controls
1. Preset, 2. Dump, 3. Door

79. Right squat switch (GFISH)
G – Landing Gear circuit inop, downlock hook
F – Flight hour meter
I – AOA Indexer lights
S – Deactivates Stall warning
H – Heat right engine lip boot

80. Memory Items (Boldface)

81. Fuel Leak Emergency Shutdown Checklist - Execute
† Condition Lever – Fuel Cutoff
Emergency Shutdown Checklist - Execute

82. Engine Failure After Takeoff
1) Power – As Required
2) Gear – UP
3) Airspeed – As Required (VXSE or VYSE)
4) Emergency Shutdown Checklist – Execute

83. Emergency Engine Shutdown on Deck
Condition levers – FUEL CUTOFF
Firewall valves – CLOSED
Boost pumps – OFF
Fire extinguisher – As Required
Gang bar – OFF
Evacuate aircraft

84. Generator Failure 1) Generator-OFF, Reset Momentarily, Then ON.
If generator will not reset:
2) Generator – OFF
3) Current Limiter (Battery Ammeter) – Checked

85. Brake Fire Firefighting assistance – Request Stop aircraft
Emergency Shutdown on Deck Checklist - Execute

86. Jammed Power Lever † 1) Condition Lever – Fuel Cutoff
2) Emergency Shutdown Checklist - Execute

87. Windmilling Airstart † Power Lever (failed engine) – Idle
† Prop lever (failed engine) – Full Forward
† Condition Lever – Fuel Cutoff
Firewall Valve – Open
Autoignition – Arm
Condition lever – Low Idle
Power – As Required

88. Prop Primary Gov Failure/Malfunction
Attempt to adjust prop rpm to normal operating range
† Power lever – Idle
† Prop lever – Feather
Alt Feathering Checklist – As Required

89. Smoke and Fume Elimination
O2 Mask-MIC switch 100% - As required
Pressurization - Dump

90. Smoke/Fire of Unknown Origin
1) Crew – Alerted 2) Cabin Temperature Mode – OFF 3) Vent Blower – AUTO 4) Oxygen Masks/MIC switches (100%) – As Required

91. Explosive Decompression
O2 Mask-MIC switch 100% - As required
Descend – As Required

92. Emergency Engine Shutdown Checklist
† Power Lever – Idle
† Propeller – Feather
† Condition Lever – Fuel Cutoff
If fire or fuel leak
† Firewall valve – closed
† Fire extinguisher – As Required
† Bleed Air – Closed
Dead engine checklist – As Required

93. Aborting Takeoff Checklist
Announce - Abort
Power levers – Idle
Reverse – As required
Brakes – As required
Immediately prior to departing runway
Condition levers – Fuel Cutoff
as soon as practical
Firewall Valves – Closed
Boost pumps – Off
Fire extinguishers – As Required
Gang bar – Off
Evacuate aircraft

94. Emergency Descent Power Levers – Idle Propellers – Full Forward
Flaps – As Required
Landing Gear – As Required
Airspeed – As Required
Windshield heat – As Required

95. Single Engine waveoff Power – Max allowable (estab pos ROC - VXSE min)
Flaps – Approach (unless already up)
Gear – Up
Flaps – Up
Prop – 1900 RPM

96. Abnormal Start Condition lever – Fuel Cutoff (note max ITT)
Starter - Off

97. Low Alt Windshear Power – Max allowable
Attitude – Set/hold 15 deg nose up
Gear – Up
Flaps – Maintain current setting

98. Spin Recovery Power levers – Idle Full opposite rudder
Yoke rapidly forward
Neutralize controls
Recover

99. Things that aren’t boldface, but might as well be:

100. Transfer Pump Failure (possible “NO FUEL TRANSFER” light)
Check total and nacelle fuel quantity
If no fuel remains in wing tanks:
Transfer pump – OFF
If fuel remains in wing tanks and necessary to use otherwise trapped 28 gallons:
Transfer pump – OVERRIDE
If light remains on:
NOTE: Consider altering flight plan; 28 gallons fuel trapped/unusable
Land as soon as practicable

101. Boost Pump Failure (possible “FUEL CROSSFEED” light)
Failed boost pump is identified by momentarily placing the crossfeed switch in the CLOSED position. The red LH or RH FUEL PRESSURE light will illuminate indicating the failed boost pump
Failed boost pump - OFF
Crossfeed - OPEN
NOTE: Determination of range with resorting to suction lift is dependent on fuel load remaining on the side opposite the failed boost pump (all fuel comes from tanks opposite failed boost pump).
Land as soon as practicable
Above 13,000’, power loss will begin until fuel stabilizes due to pressure differential
Suction lift limited to 10 hours between pump overhauls

102. Fuel Siphoning Airspeed – 140 KIAS Land as soon as practicable
NOTE: Extreme nose-low attitudes will aggravate the fuel siphoning condition.