2014 STAN Visit Weaks Flashcards Preview

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Flashcards in 2014 STAN Visit Weaks Deck (28):
0

Engine Post Shutdown Fire

1. FADEC CONTROL SWITCH - CHECK OFF
2. BOOST PUMPS - CHECK OFF

If high TOT still evident after 10 seconds:

3. EMERGENCY FUEL SHUTOFF LEVER - SHUT OFF
4. CRANK BUTTON - DEPRESS UNTIL TOT DECREASES

If TOT continues to rise or does not decrease:

5. EMERGENCY ELECTRICAL CUTOFF - OFF
6. ROTOR BRAKE - ON
7. EVACUATE AIRCRAFT

1

When conducting a free fall deployment, a minimum of _______ water depth is required

12 feet

2

PRI SERVO P
SERVO JAM
LIMIT
HYD2 Press <720psi

PRIMARY HYDRAULIC SYSTEM FAILURE
1. CRUISE AIRSPEED 75-100 KIAS
2. AVOID ABRUPT MANEUVERS

3

The PRI SERVO P light illuminates in flight with no other symptoms. You call for the ______ EP in the Red Book.

HYDRAULIC INDICATING SYSTEM FAILURE.

4

Fuel may be jettisoned at airspeeds between ____ and ___ KIAS at any rate of climb or descent up to ____ fpm. The landing gear will be down when jettisoning fuel below _____.

40-120 KIAS and 1500
60 KIAS

5

An aural gong tone will sound when:

• Takeoff − Accelerate to IAS >75k in TOP range.
• Cruise Flight − IAS >75k for 5 seconds in TOP range.
• Torque 1 + 2 >102.5%.
• Excessive load factor.
• Excessive fore or aft cyclic (on the ground).
• N1 exceeds the MTOP N1 +0.4%, i.e., 102.3%.

6

Starter "CRANK" limits

20 secs per attempt, 5 mins cooling between attempts
3 attempts
After 3rd, allow for 30 mins of cooling

7

Rotor brake limits

<170 RPM
13 seconds per application
5 mins cooling between each attempt
10 mins after the 3rd application

8

During a planned MADPU or SADPU recovery of the swimmer and survivor a proper choice of deployment is:

Free Fall
Harness

9

What are the first four corrective action steps for Smoke and Fume Elimination?

1. HEAT/COOL SWITCHES - OFF
2. RAM AIR - OPEN
3. CABIN SLIDING DOOR - OPEN
4. PILOT WINDOWS - OPEN

10

The three authorized recoveries during a direct deployment are:

Quick Strop
Physical Grip
Double Lift Recovery

11

OIL TEMP warning light EP:

ENGINE OIL COOLER FAN FAILURE

12

WARNING: Vertical speed shall be less than ____ fpm for the collective to hold a vertical speed of zero when activating IAS-VS.

+/- 150

13

The _____ should be used to verify whether a gear box chip warning light is associated with the Main Gearbox or the Tail Rotor Gearbox.

VEMD

14

"I am visual" means:

I have acquired sufficient visual cues to maintain a hover or visual contact with the surface.

15

Moderate Vibrations call for what bold face steps?

1. CRUISE AIRSPEED - 75 to 120 KIAS
2. AVOID ABRUPT MANEUVERS
3. LAND AS SOON AS POSSIBLE

16

The words ____ and ____ are used to indicate a mandatory requirement.

Shall and Will

17

During a Dual Boost Pump/Ejector Failure, the unusable fuel may be as much as _____ in the left system and as much as _____ in the right system.

13-14% or 280 pounds LEFT
3-4% or 60 pounds RIGHT

18

The GPS index for a CATCH should be _____ to ensure accuracy in Waypoint identification.

50'- 0.6NM

19

What are the four corrective action steps for Smoke and Fume Elimination?

HERC PILOT
1. HEAT/COOL SWITCHES - OFF
2. RAM AIR - OPEN
3. CABIN SLIDING DOOR - OPEN
4. PILOT WINDOWS - OPEN

20

Due to degradation of depth perception below _____ feet while wearing NVGs, the SP shall continue to scan instruments, particularly RADALT, to prevent inadvertent descent and water contact.

50 feet

21

Max Rescue Hatch airspeeds

Hatch open and locked: 80 KIAS fwd/ 35 knots sideward
Hatch movement: 60 KIAS fwd/ 30 knots sideward

22

Severe or Intolerable Vibrations of Unknown Origins

Landing/Hover Checklist (200' at a min)
Land/Ditch Immediately

23

Max airspeed with floats armed or inflated?
Sideward flight?

90 KIAS and 35 knots.

24

MAJOR FADEC/GOVERNOR FAILURE

1. Complete the Big 4
2. TRNG SWITCH - FLT
3. FADEC BACKUP SWITCH (affected engine) - CONFIRM - BACKUP

25

With HI NR switch on, your airspeed is restricted to _____ KIAS and AOB is restricted to ______.

135 KIAS and 40 degrees

26

"Gong" aural warning tone limits

1. Takeoff-Accelerate to IAS >/= 75kts in TOP range.
2. Cruise Flight-IAS >/= 75kts for 5 seconds in TOP range.
3. Torque 1 + 2 > 102.5%
4. Excessive load factor
5. Excessive fore or aft cyclic (on the ground)
6. N1 exceeds the MTOP N1+0.4%, i.e., 102.3%

27

Low/high Nr warning RPM

345 low/ 380 RPM high