Emergency Procedures Study Guide Flashcards

1
Q

The term LAND WITHOUT DELAY is defined as:

A

a landing in which the primary consideration is continued control of the aircraft and survival of the occupants. It is meant to be more urgent than Land As Soon As Possible. The situation may not permit the aircrew to continue to maneuver the aircraft to a suitable landing area (e.g. open field).

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

The term LAND AS SOON AS POSSIBLE is defined as:

A

landing at the nearest suitable landing area (e.g. open field) without delay. The primary consideration is to ensure the survival of occupants.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

The term LAND AS SOON AS PRACTICABLE is defined as:

A

landing at a suitable landing area. The primary consideration is the urgency of the emergency.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

The term AUTOROTATE is defined as:

A

adjusting the flight controls as necessary to establish an autorotational descent and landing.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

(PARM)
Emergency Shutdown:
1.____________________________________________________
2.____________________________________________________
3.____________________________________________________
4.____________________________________________________

A
  1. POWER LEVERS – OFF
  2. APU – OFF (if applicable)
  3. ROTOR BRAKE switch – BRK
  4. MSTR IGN – OFF once rotors have stopped
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

(HAC)
EMERGENCY EXIT AND ENTRANCE – CANOPY JETTISON
1. ______________________________________________________
2. ______________________________________________________
3. ______________________________________________________

If Flares are ignited and lodged in the dispenser, jettison all flare munitions and ____________________________.

A
  1. Helmet visors – Down.
  2. Area around helicopter – Clear of personnel.
  3. CANOPY JETTISON handle – Operate (see caution 2)

LAND AS SOON AS POSSIBLE.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

(AC)
Dual Engine Failure - Low Altitude / Low Airspeed and Cruise
1. _________________________________________________
2. _________________________________________________

A
  1. AUTOROTATE – Rapidly lower collective to maintain NR within limits
  2. CHOP Button – Reset if an ENGINE CHOP warning message is present
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

(PE)
ABORT START PROCEDURES
1. ______________________________________________________
2. ______________________________________________________

A
  1. POWER lever – OFF
  2. ENG START switch – IGN ORIDE for 30 seconds and TGT is below 540* C
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Single Engine Failure- Low Altitude / Low Airspeed and Cruise
1. __________________________________________________

A
  1. Achieve safe single engine flight conditions or land
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Engine 1 or 2 Overspeed – NP Failed High 1._______________________________________________
LAND AS SOON AS PRACTICABLE

A
  1. Collective – Adjust to maintain NR within limits
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

NP Failed Low – Low RPM Rotor
1. ____________________________________________

A
  1. Collective – Adjust to maintain NR within limits
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Engine Compressor Stall
1. _______________________

A
  1. Collective – Reduce
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

(ECPC)
MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE
1. _____________________________________________
2. _____________________________________________
3. _____________________________________________
4. _____________________________________________
- _____________________________________________

A
  1. EMERG HYD button – Press on
  2. Collective Reduce – Compromise between rate of turn and rate of descent
  3. POWER LEVERS – Off (10-20 feet above touchdown)
  4. Collective – Increase to cushion touchdown
    - LAND WITHOUT DELAY
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT POSSIBLE
1.______________________________________

A
  1. Airspeed – 100 KTAS minimum (until 10-20 feet above touchdown)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

(CPC)
LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT NOT POSSIBLE
1. _____________________________________
2. _____________________________________
3. _____________________________________

A
  1. Collective – Reduce (compromise between rate of turn and rate or descent)
  2. POWER LEVERS – Off (5-10 feet above touchdown)
  3. Collective – Increase to cushion touchdown
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

(CCB)
TAIL ROTOR FIXED PITCH – LOW AIRSPEED OR HOVER
1. _______________________________________
2. _______________________________________
If pedals are jammed
3. _______________________________________

A
  1. Collective – Adjust to minimize Yaw rate
  2. Cyclic – Minimize drift
    If pedals are jammed
  3. Break into BUCS
17
Q

(CCB)
TAIL ROTOR FIXED PITCH – FORWARD FLIGHT
1. ____________________________________
2. ____________________________________
If pedals are jammed
3. ____________________________________

A
  1. Collective – Adjust to minimize Yaw rate
  2. Cyclic – Oppose yaw
    If pedals are jammed
  3. Break into BUCS
18
Q

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE – IN FLIGHT
1. _____________________________________

A
  1. Achieve safe single engine flight conditions or land
19
Q

(AIF)
ENGINE 1 OR ENGINE 2 FIRE – IN FLIGHT
1. ___________________________________
2. ___________________________________
3. ___________________________________
- ___________________________________

A
  1. Achieve safe single engine flight conditions or land
  2. Illuminated ENG FIRE button – Press and RDY light illuminates
  3. FIRE DISCH button(s) – Press
    - LAND AS SOON AS POSSIBLE
20
Q

(PIF)
ENGINE 1 OR ENGINE 2 FIRE – ON GROUND
1. _____________________________________________
2. _____________________________________________
3. _____________________________________________
- _____________________________________________

A
  1. POWER LEVERS – OFF
  2. Illuminated ENG FIRE button – Press and RDY light illuminates
  3. FIRE DISCH button(s) – Press
    - EMERGENCY SHUTDOWN PERFORM
21
Q

(AIF)
APU FIRE – ON GROUND
1. _____________________________________________
2. _____________________________________________
3. _____________________________________________
- ____________________________________

A
  1. APU – OFF
  2. Illuminated APU FIRE button – Press and RDY light illuminates
  3. FIRE DISCH button(s) – Press
    - EMERGENCY SHUTDOWN PERFORM
22
Q

(IF)
APU FIRE – IN FLIGHT
1. _____________________________________
2. _____________________________________
- _____________________________________

A
  1. Illuminated APU FIRE button – Press and RDY light illuminates
  2. FIRE DISCH button(s) – Press
    - LAND AS SOON AS POSSIBLE
23
Q

HYDRAULIC FAILURE – PRIMARY & UTILITY HYDRAULIC PSI LOW
1. ______________________________________
Urgency to land
- ______________________________________

A
  1. EMERG HYD button – Press ON
    - LAND WITHOUT DELAY
24
Q

EMERGENCY LANDING IN WOODED AREA (POWER OFF)
1. ___________________________________

A
  1. AUTOROTATE – Apply full collective to decay rotor RPM as helicopter settles.
25
Q

(ACCE)
DITCHING (POWER OFF)
1. ____________________________________
2. ____________________________________
3. ____________________________________
4. ____________________________________

A
  1. AUTOROTATE (apply full collective to decay rotor RPM as helicopter settles)
  2. Canopy – JETTISON prior to entering water
  3. Cyclic – Position in direction of roll
  4. Exit when rotor has stopped
26
Q

BUCS FAIL
1. _________________________________

A
  1. Transfer flight controls to rear crew station
27
Q

FLIGHT CONTROL MALFUNCTION – STABILIZATION EQUPMENT/FORCE TRIM
1. _______________________________

A
  1. FMC release button – Press
28
Q

NVS Failure
1. _____________________________________________________
2. _____________________________________(PNVS or TADS)

A
  1. Exit the NOE environment
  2. Pilot on the controls, NVS Select Switch – Select alternate sensor (PNVS or TADS)
29
Q

IHADSS/HDU Failure or IHADSS STALE
At night (NVS flight)
1. ___________________________________

A
  1. Exit the NOE environment
30
Q

(NC)
Single MP Operation
1. _______________________________
or
2. _______________________________

A
  1. NVS SELECT Switch – Reselect (PNVS or TADS)
    or
  2. Crewmemeber (not on controls) – Assume control
31
Q

Dual MP Failure – MP1 AND MP2 FAIL
at night (NVS flight)
1. _________________________________

A
  1. Exit the NOE environment
32
Q

CAUTION:
Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW
1. ___________________________________________
LAND AS SOON AS POSSIBLE

A
  1. FUEL page, BOOST button – Press ON