TD 14 Flashcards
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 +- ____ degrees and fuel requirements must be determined IAW ___+___lbs.
1,5,1,5, AR 95-1, 100
The standards for hover flight are to maintain heading +/- ___, altitude ___ +/- _____, drift not to exceed ___feet (___OGE). During a hover 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. When landing from a hover press the ___ switch while lowering the collective to affect a smooth, controlled descent with minimal ____ at touchdown.
10 degrees, 3 ft, 1 ft IGE, 2, 10, 30, 1, monitor mm, FTR, drift
The types of takeoff are (5 of them)
Normal, constant angle, vertical, level acceleration, and B/O2 max performance
For a normal takeoff adjust the 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.
5, 0.5
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.
Collective, constant, airspeed, increasing, 50ft AGL, trim, 50 ft AGL, align
While performing a 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 when within approximately ___feet of the pattern altitude 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 ____.
500, 65, 90, 50, 50, two thirds
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.
Minimum 1.3 BAR
Caution Range. 1.3 BAR - 1.5 BAR
Continuous Operation 1.5 BAR - 5.0 BAR
Maximum Continuous 5.0 BAR
5.0 BAR, ground idle
CAUTION INDICATIONS - ENG OIL P
(SYSYEM 1 or 2)
Procedure 1 Engine Oil Pressure — check 2 OEI Flight condition — 3 Affected engine — 4 Single engine emergency shutdown — 5 LAND AS SOON AS \_\_\_\_\_\_
1 Engine Oil Pressure — check 2 OEI Flight condition — establish 3 Affected engine — identify 4 Single engine emergency shutdown — perform 5 LAND AS SOON AS PRACTICABLE
What are the minimum power application and maximum operation Engine Oil Temperature limits?
Minimum
Oil viscosity 3cST and 3.9 cST — -10 degrees C
Maximum
115 degrees C
Engine Oil Temperature High
Procedure
1 OEI flight condition —
2 Affected engine —
3 Twist grip (affected engine) —-
(TWIST GRIP caution comes on)
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 _______
1 OEI flight condition — establish
2 Affected engine — identify
3 Twist grip (affected engine) —- adjust to 20-30%
(TWIST GRIP caution comes on)
4 Oil temperature indicator (affected engine) — monitor
If engine oil temperature decreases below limit:
5 LAND AS SOON AS PRACTICABLE
If engine oil temperature still remains above limit:
6 single engine emergency shutdown — perform
7 LAND AS SOON AS PRACTICABLE
WARNING LIGHT INDICATIONS - LOW FUEL (1 and/or 2)
Procedure
Fuel quantity indication — Check
If positive fuel indication in the main tank:
2 Both fuel pump XFER sw (Fwd + Alt) —
check ___
3 Both fuel pump XFER circuit breakers (Fed + alt) — check ___
If both FUEL LOW warning lights remain on:
4 LAND WITHIN ________
If one FUEL LOW warning light remains on:
4 Expect ______
Fuel quantity indication — Check
If positive fuel indication in the main tank:
2 Both fuel pump XFER sw (Fwd + Alt) —
check on
3 Both fuel pump XFER circuit breakers (Fed + alt) — check in
If both FUEL LOW warning lights remain on:
4 LAND WITHIN 9 minutes
If one FUEL LOW warning light remains on:
4 Expect single engine failure
SINGLE ENGINE FAILURE — takeoff
Procedure
1 Collective lever —
REJECTED TAKEOFF
2 Landing Attitude —
3 Collective lever —
After landing Affected engine — 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 PRACTICABLE
1 Collective lever — adjust to maintain rotor RPM
REJECTED TAKEOFF
2 Landing Attitude — establish
3 Collective lever — Raise as necessary to stop descent and cushion landing
After landing Affected engine — identify Single engine emergency shutdown — perform
TRANSITION TO OEI - FLIGHT
2 Collective Lever — adjust to OEI limits or below
3 Rotor speed — trim to maximum
4 Airspeed — gain, 65 KIAS
After reaching safe altitude
5 Collective lever — reduce to OEI MCP or below
6 Affected engine — identify
7 Single engine emergency shutdown — perform
8 LAND AS SOON AS PRACTICABLE
