Dq’s TD 15 Flashcards
For Running Landings in Primary..
Use a shallow approach angle to arrive at 50ft AGL at 40KIAS. Maintain the aircraft in trim above 50ft AGL and align with the landing direction below 50ft AGL. Do not exceed 300fpm rate of decent at touchdown and adjust the cyclic to attain an aircraft attitude that maintains a touchdown speed appropriate for conditions. Smoothly reduce the collective for braking.
Main transmission oil pressure values
Minimum 1bar; caution range 1-1.5bar; continuous operation 1.5-5.0bar; maximum 5.0bar
Warning light is acceptable in range from 1 to 1.4bar durning pressure buildup phase
RFM 2-10 / 2.12.5
XMSN OIL PRESS WARNING LIGHT
One xmsn oil pressure indication is below 1 bar
Power - reduce
LAND AS SOON AS PRACTICABLE
If both indications are below 1 bar
LAND IMMEDIATELY
NOTE descend with minimum power
RFM 3-9
Main XMSN oil temp values
Continuous operation -10 to 105 C
Maximum 105 C
RFM 2-11 / 2.12.6
CAUTION INDICATION XMSN Oil Temp
XMSN oil temperature and pressure indication:
Check
If indications are within limits:
LAND AS SOON AS PRACTICABLE
If indications are above limit:
Reduce power as much as possible
If oil temperature indication remains above limit:
LAND AS SOON AS POSSIBLE
RFM 3-38
Single engine failure IGE
Collective lever:
Adjust to OEI limits or below
Landing attitude: Establish
Collective lever:
Raise as necessary to stop decent and cushion landing
After Landing:
Affected engine: Identify
Single engine emergency shutdown:
Perform
RFM 3-45 / 3.4.1
Single engine failure flight
OEI flight condition: establish
Rotor speed: Trim to maximum
Affected engine: Identify
Single engine emergency shutdown:
Perform
LAND AS SOON AS PRACTICABLE
RFM 3-48 / 3.4.4
TFR Donating Blood
After donating blood (200cc or more) aircrew members will be restricted from flying duties for 72 hours
AR 40-8 page 2 para 7
TFR Alcohol
After consuming alcohol, aircrew members will not fly for a period of 12 hours and until no residual effects remain
AR 40-8 page 2 para 7
TC 3-04.93 DVE
Degraded visual environment (DVE) is a state of reduced visibility whereby spatial situational awareness and aircraft control cannot be maintained with the same precision as in normal visual meteorological conditions
page 9-2 / para 9-8