TD 14

Question 1

When planning a VFR flight determine distance ±__ nautical mile, ground speed ±__ knots, and estimated time en route (ETE) ±__ minutes for each leg of the flight. Compute magnetic headings ±5 degrees and fuel requirements must be determined IAW ______ ±____ lbs.

Answer 1

1

5

1

AR 95-1

100

Question 2

The standards for hover flight are to maintain heading ±__, altitude ___ ±__, drift not to exceed __ feet (__ feet OGE). During a hovering turn, maintain a constant rate of turn not to exceed __ degrees in __ seconds. A thorough crew briefing must be performed prior to flight which includes crew coordination to ________ limits for ___________ and ________. When landing from a hover press the FTR switch while lowering the collective to affect a smooth, controlled descent with minimal _____ at touchdown.

Answer 2

10

3 ft

1 ft

2

10

90

4

monitor

mast moment

landing

FTR

drift

Question 3

The four types of takeoff are, __________________________________.
For a normal takeoff adjust cyclic to attain an accelerative attitude (__ degrees maximum nose low is recommended) and smoothly increase the collective (normally ___ FLI more than hover power) so that the helicopter gains speed and height.

Answer 3

normal, constant angle, vertical and level acceleration

5

0.5

Question 4

During a VMC approach adjust the _________ as necessary to establish and maintain a _________ angle. Maintain entry _________ until the rate of closure appears to be ________. Above _________ maintain ground track alignment and the aircraft in _____. Below __________, _______ the aircraft with the landing direction.

Answer 4

collective

constant

airspeed

increasing

50 ft AGL

trim

50 ft AGL

align

Question 5

While performing traffic pattern flight, climb at ____ FPM, fly ___ KIAS on the crosswind and base legs and ___ KIAS on the downwind leg. Commerce the turn to crosswind when within approximately ___ feet of the pattern attitude and begin level off approximately ____ feet prior to traffic pattern altitude. On the base leg the descent and deceleration should be accomplished in the first ___.

Answer 5

500

65

90

50

300

2/3

Question 6

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.

Answer 6

1. 3 bar
2. 3 – 1.5 bar
3. 5 – 5.0 bar
4. 0 bar
5. 0 bar

ground

Question 7

CAUTION INDICATIONS – (ENG OIL P SYSTEM 1 or 2)

Procedure

1. Engine oil pressure – _______
2. OEI flight condition – _______
3. Affected engine – _______
4. Single engine emergency shutdown – _______
5. LAND AS SOON AS _____________

Answer 7

Check

Establish

Identify

Perform

PRACTICABLE

Question 8

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

Answer 8

Minimum oil viscosity 3 cst and 3.9 cst, -10° C
Minimum oil viscosity 5 cat, 0° C
Maximum operating temperature, 115° C

Question 9

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 oil temperature decreases below limit:
5. LAND AS SOON AS _______________

If engine oil temperature still remains above limit:

6. Single engine emergency shutdown –
7. LAND AS SOON AS _______________

Answer 9

Establish

Identify

Adjust to 20-30% torque (TWIST GRIP caution indication comes on)

Monitor

PRACTICABLE

Perform

PRACTICABLE

Question 10

WARNING LIGHT INDICATIONS – LOW FUEL (1 and/or 2)

Procedure
1. Fuel quantity indication – Check
If positive fuel indication in the main tank:
2. Both fuel pump XFER sw (Fwd + Aft) – Check ___
3. Both fuel pump XFER circuit breakers (Fwd + Aft) – Check ___

If both FUEL LOW warning lights remain on:
4. LAND WITHIN ________

If one FUEL LOW warning light remains on:
4. Expect __________________

Answer 10

ON

in

10 minutes

single engine failure

Question 11

Single engine failure – takeoff

Procedure
1. Collective lever –

REJECTED TAKEOFF

2. Landing attitude –
3. Collective lever –

After landing:

4. Affected engine –
5. Single engine emergency shutdown –

TRANSITION TO OEI – FLIGHT

2. Collective lever –
3. Rotor speed –
4. Airspeed –

After reaching safe altitude:

5. Collective lever –
6. Affected engine –
7. Single engine emergency shutdown –
8. LAND AS SOON AS __________

Answer 11

Adjust to maintain rotor RPM

Establish

Raise as necessary to stop descent and cushion landing

Identify

Perform

Adjust til OEI-limits or below

Trim to maximum

Gain, 65 KIAS (Vy)

Reduce to OEI max continuous power or below

Identify

Perform

PRACTICABLE