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Piper PA34-200T Seneca II: Difference between revisions
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The usable fuel in this aircraft is 61.5 gallons in each wing or a total of 123 gallons. | The usable fuel in this aircraft is 61.5 gallons in each wing or a total of 123 gallons. | ||
==== Gyro | ==== Gyro Pressure Limits ==== | ||
The operating limits for the pressure system are 4.5 to 5.2 inches of mercury for all operations as indicated by the gyro pressure gauge. | The operating limits for the pressure system are 4.5 to 5.2 inches of mercury for all operations as indicated by the gyro pressure gauge. | ||