Daily Questions TD 28

Engine Oil Temperature High Procedure: 1. OEI flight condition-_____ 2. Affected Engine-_____ 3. Twist grip (affected Engine)-________ 4. Oil Temperature indicator(affected engine)-______ *if engine temp decreases below limit 5. ________________ *if oil Temp still remains above limit 6. Single emergency shutdown:_______ 7.__________

1. Establish 2. Identify 3. Adjust to 20-30% Torque 4. Monitor 5. LAND AS SOON AS PRACTICABLE 6. Perform 7. LAND AS SOON AS PRACTICABLE

Tail Rotor Drive/Fixed pitch Tail Rotor Control Failure (fwd flight) Procedure: 1. Collective Lever:_____ 2. Airspeed:______ 3. Suitable Landing area:_____ 4. Shallow approach with nose left:______ *if Airspeed can be reduced to 40 Kts with nose still pointing left: 5. Airspeed:______ 6. Landing:_____ *if nose direction changes from left to right at airspeeds higher than 40Kts: 5. Airspeed:_____ 6. Approach:______ 7. Autorotation:______

1. Reduce to obtain minimum side slip angle 2. Maintain 70 KIAS or higher 3. Select 4. Perform 5. Reduce close to the ground until nose is aligned with flight direction 6. Perform 5. Increase 6. Abort, climb to sufficient height for autorotation 7. Perform

The 6 flight conditions that are conducive to settling with power:

1. Steep approach at high rate of descent 2. Downwind approach 3. Formation flight (turbulence from other acft) 4. Hovering above max ceiling 5. Not maintaining altitude control during OGE hover 6. During masking/unmasking

What 3 conditions must exhist simultaneously for settling with power to occur?

1. Vertical or near vertical decent of at least 300 ft/min 2. Slow fwd Airspeed, less than. ETL 3. Rotor system is using 20-100% pwr available with insufficient power remaining to stop descent

As it pertains to performing above T/R Drive failure procedure: 1. The procedure will vary depending on flight conditions, _______, and_____of the helicopter 2. Landing surface should be____ (eg concrete, asphalt) and_____. 3. _____crosswind is advantageous 4. _____is advantageous 5. In final phase of flare, the helicopter can yaw to the___ due to friction effects. 6. Before touchdown, the ground speed should be reduced to a______.

1. power setting, mass 2. hard, flat 3. left 4. headwind 5. Left 6. minimum

Settling with power is defined as:

A condition of powered flight where the ACFT settles in it's own down wash. also known as: vortex ring state

What are the minimum power application and maximum operation Engine Oil Temperature limits?

-10° to 115°

During a fixed pedal setting approach adjust Airspeed to____knots or above until final. Upon establishing___knots while maintaining less than____FPM of descent, if the nose is_____of ground track, ____ the approach; if the nose is_____, ______ approach. Arrive over the ____ of the landing area approximately___AGL ________. If the nose is to the left, maintain altitude with the collective while______fwd speed until the acft is _____with landing area. If nose yaws to the _____past the centerline, apply _____. Collective application will accelerate the right yaw. When the acft is aligned with the intended landing direction and a ______can be accomplished, the IP will announce the_______.

70; 40, 300; Right, abort; Left, continue; First 1/3, 5, at or above ETL; decreasing, aligned; right, fwd cyclic; successful landing, maneuver complete.

Second APM disengagement failure [AP WARN LT/AP1+AP2 CAUT) Procedure: 1.___________

Flying controls: Hands on