1
Q
Where must the hover power check be performed?
A
Near the take off point and in the direction of take off
2
Q
Which crewmember verifies the hover power check?
A
The pilot not on controls will monitor the aircraft instruments and verify the power check
3
Q
When must the crew conduct additional hover power checks?
A
Increase of 1000 lbs GWT, 5 degrees C, or 1000 ft PA in conjunction with the perf page data and/or PPC
4
Q
What are the 4 ways in which the 701D engine will limit (droop)?
A
TGT limiting
Ng Aerodynamic speed limit
Ng Physical speed limit
Fuel Flow limit
5
Q
During the engine start sequence, the message “ATS1 HANG” displays on the EUFD? What is the required procedure?
A
ENG Start Switch to IGN ORIDE, then OFF
