2014 STAN Visit Weaks

Question 0

Engine Post Shutdown Fire

Answer 0

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

=CAUTION=

Operation of the crank button with the EFSL pulled will cause severe damage to the engine fuel pump

If high TOT still evident after 10 seconds:

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

Question 1

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

Answer 1

12 feet

Question 2

PRI SERVO P SERVO JAM LIMIT HYD2 Press <720psi

Answer 2

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

Question 3

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

Answer 3

HYDRAULIC INDICATING SYSTEM FAILURE.

Question 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 _____.

Answer 4

40-120 KIAS and 1500 60 KIAS

Question 5

An aural gong tone will sound when:

Answer 5

• 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%.

Question 6

Starter “CRANK” limits

Answer 6

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

Question 7

Rotor brake limits

Answer 7

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

Question 8

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

Answer 8

Free Fall Harness

Question 9

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

Answer 9

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

Question 10

The three authorized recoveries during a direct deployment are:

Answer 10

Quick Strop Physical Grip Double Lift Recovery

Question 11

OIL TEMP warning light EP:

Answer 11

ENGINE OIL COOLER FAN FAILURE

Question 12

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

Answer 12

+/- 150

Question 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.

Answer 13

VEMD

Question 14

“I am visual” means:

Answer 14

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

Question 15

Moderate Vibrations call for what bold face steps?

Answer 15

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

Question 16

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

Answer 16

Shall and Will

Question 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.

Answer 17

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

Question 18

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

Answer 18

50’- 0.6NM

Question 19

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

Answer 19

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

Question 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.

Answer 20

50 feet

Question 21

Max Rescue Hatch airspeeds

Answer 21

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

Question 22

Severe or Intolerable Vibrations of Unknown Origins

Answer 22

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

Question 23

Max airspeed with floats armed or inflated? Sideward flight?

Answer 23

90 KIAS and 35 knots.

Question 24

MAJOR FADEC/GOVERNOR FAILURE

Answer 24

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

Question 25

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

Answer 25

135 KIAS and 40 degrees

Question 26

“Gong” aural warning tone limits

Answer 26

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%

Question 27

Low/high Nr warning RPM

Answer 27

345 low/ 380 RPM high