TD-14 Flashcards
When planning a VFR flight determine distance +/- __ nautical mile, ground speed +/-___ knots, and estimated time in route +/-___ minute for each leg of the flight. Magnetic headings +/-___° and fuel requirements must be determined in accordance with ____ +/-____ pounds.
1
5
1
5
AR 95-1
100
A standard for hover flight are to maintain heading +/-___, altitude ___ +/-________, drift not to exceed __ feet (__ feet OGE). During hovering turn, maintain constant rate of turn not to exceeded ___° in __ seconds. A thorough crew briefing must be performed prior to flight which includes crew coordination to ______ limits. When landing from a hover press the ____ switch while lowering the collective to effect a smooth, controlled descent with minimal _____ at touchdown.
10 degrees
3ft
1ft IGE (+/- 5ft OGE)
2
10
30
6
aircraft
FTR
drift
The types of takeoff are _______, ____________, ________, ____________. For normal takeoff, adjust cyclic to attain an accelerated altitude (__ degrees maximum nose low is recommended), and smoothly increase the collective (normally ____ FLI more than hover) so that the helicopter gains speed and height.
Normal
Constant Angle
Vertical
Level Acceleration
5
0.5
During a VMC approach, adjust the _________ as necessary to establish a maintain a ___________ angle. Maintain entry __________ until the rate of closure appears to be _______________. Above ___________, maintain ground track alignment in the aircraft and _________. Below _________,__________ the aircraft with the landing direction.
Collective
Constant
Airspeed
Increasing
50ft AGL
trim
50ft AGL
align
While performing traffic pattern flight, climb at ____FPM, fly ___ KIAS on the crosswind and base legs and __ KIAS on the downwind leg. Commence the turn to crosswind with approximately ___ feet of the pattern altitude and begin level off approximately ___ feet prior to pattern at altitude. On the base leg, the descent and deceleration should be accomplished in the first ___.
500
65
90
300
50
2/3
Engine Oil Pressure
Minimum _______
Caution range ____________
Continuous operation ________
Maximum continuous ______
NOTE: Exceeding ____ oil pressure is allowed for transient operation during the start cycle and warm up at __________ only.
1.3 bar
1.3 bar to 1.5 bar
1.5 bar to 5.0 bar
5.0 bar
5.0 bar
Ground idle
CAUTION INDICATIONS = ENG OIL P (SYSTEM 1 OR 2)
Procedure
1. Engine oil pressure - ________
2. OEI flight conditions - _________
3. Affected engine - _________
4. Single engine emergency
shutdown - ________
5. LAND AS SOON AS
______________
Check
Establish
Identify
Perform
PRACTICABLE
What are the minimum power application and maximum operation Engine Oil Temperature limits?
- Minimum power application 3-
3.9 cst +/- -10 degrees Celsius. - Max Operating Temp = 115
degrees Celsius.
