PPC Flashcards

1
Q

What are the calculated values for CONTINUOUS TORQUE AVAILABLE (DUAL ENGINE) at -4° C and 4,000’ PA?

A

105% Calculated, 100% Recorded

Reference: Pg 7-11

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2
Q

What is the MAX TQ AVAILABLE SINGLE ENGINE at +30° C and 4,000’ PA?

A

108%

Reference: Pg 7-6

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3
Q

What is your MAX GWT TO HOVER CONTINUOUS at +30° C and 8,000’ PA for the following conditions: 10 ft (IGE NO LOAD), 40 ft (IGE WITH LOAD), and 80 ft?

A
  • 41,750 Structural Limit
  • 41,250 (IGE No Load)
  • 38,500 (IGE With Load)
  • 37,500 (OGE)

Reference: Pg 7-16

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4
Q

What are your PREDICTED HOVER TORQUES (SINGLE ENGINE) IGE/OGE for -10°C and 100’ PA with 34,000 GWT No-Load and 38,000 GWT Load?

A
  • 92% IGE No-Load
  • 104% OGE No-Load
  • 116% IGE Load
  • 120% OGE Load

Reference: Pg 7-18

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5
Q

What is the DUAL ENGINE PREDICTED HOVER TORQUE for IGE NO LOAD at +20° C and 1,000’ PA with 50,000 GWT?

A

80%

Reference: Pg 7-18

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6
Q

What is your MAX GROSS WEIGHT TO HOVER – OGE (SINGLE ENGINE) at 80ft hover for +28° C and 4,000’ PA?

A

32,000 GWT

Reference: Pg 7-18

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7
Q

What is your GO/NO GO TORQUE for NO LOAD (10 ft) and WITH LOAD (40 ft hover) at +44°C and 4,000 Feet PA?

A
  • 80% @ 10 ft
  • 88% @ 40 ft

Reference: Pg 7-18

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8
Q

At what airspeed will you get the most distance out of your fuel load at +0° C, 4,000’ PA, and 47,500 GWT?

A

130 KIAS

Note: VNE line intercepted prior to MAX Range line. Reference: Pg 7-54

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9
Q

What is your Drag Factor (DUAL ENGINE) for LMTV at 40° C, 2,000’ PA, and 91 Knots IAS?

A

10-14%

91 IAS = 100 TAS. Reference: Pg 7-51

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10
Q

What is the MAX R/C and ENDURANCE IAS at +30° C, 2,000’ PA, and 35,000 GWT?

A

70 KIAS / 74 KCAS

Reference: Pg 7-50

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11
Q

What is your MINIMUM and MAXIMUM SINGLE ENGINE IAS at +0° C, 2,000 PA, with Contingency TQ Available = 116%, and 40,000 GWT?

A
  • Min 20 KIAS / 26 KCAS
  • Max 130 KIAS / 131 KCAS

Reference: Pg 7-49

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12
Q

What is your Validation Factor for (NO LOAD/10 ft HVR) at +16 C and 4,000 PA?

A

74% use 46,000 as lowest GWT for MSN Profile

Item 22 = 50,000, Item 56 = 46,000, Item 98 = 48,500. Reference: Pg 7-18

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13
Q

What is your airspeed limit at +20° C, 1,000’ PA, and 38,000 GWT?

A
  • Weight based Limit 166 KIAS
  • Temp Based Limit 156 KIAS
  • Temp Based Adjustment +4 KIAS
  • 160 KIAS / 160 KCAS

Reference: Pg 5-11

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