PPC Flashcards

1
Q

What is the weight and balance classification for the AH64E?

A

Class 2

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2
Q

Where can weight and balance information be found?

A

-10 (CH. 6)
AR 95-1 (CH 5+7)

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3
Q

What is the formula for computing the CG?

A

ARM = Moment ÷ Weight X 100

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4
Q

What chart is used to compute the forward and aft CG limits for a given gross weight?

A

Chapter 6
- Center of Gravity Limits Chart

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5
Q

The 365-4 must be checked for accuracy every ______ days?

A

90 (days)

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6
Q

What is the rule of thumb associated with the weight recorded in the LOAD block?

A

1% for 200lbs / 1K for 200lbs

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7
Q

What are the allowable ranges for ETF’s ATF’s?

A

ETF: .85 to 1.096
ATF: .90 to 1.096

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8
Q

What Horizontal Velocity (VH)?

A

Madimum speed level flight with MAX CONT PWR (100%) applied
OR 793 degrees Celsius

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9
Q

What are the three reasons that an engine’s performance is limited (MTA)?

A

TGT ^ +10C (879 ±5)
NG/MACH ▼ +10C
FUEL

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10
Q

The aircrew determines if OGE power is available during the hover power check by comparing:

A

Predicted Hover TQ (IGE) value
vs.
OGE GO/NO GO TQ

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11
Q

IAW the ATM what’s the only mandatory information to record in the REMARKS section?

A

SE 67% of VNE

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12
Q

What are the three performance page modes?

A

Current
Max
Plan

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13
Q

The basic weight and moment are entered on the ______ page?

A

Weight

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14
Q

How is performance page validated?

A

1) A/C basic weight and moment against 365-4
2) ETF for engine 1+2 values against the HIT log
3) CUF PERF values against PPC
4) Verify CUR PERF against hover power check

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15
Q

What are the three methods to determine if OGE power is available?

A

1) Compare hover TQ OGE to MTA (DE)
2) MAX GWT OGE to current GWT
3) Color of Hover TQ OHE to MAD GWT OGE (Yellow NO OGE)

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16
Q

When will the VNE True Airspeed change to 67% of VNE?

A

12% TQ split between the engines