Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

HAC Studying > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

The following should be performed for all emergencies

A
  1. Maintain control of the aircraft
  2. Alert crew
  3. Determine the precise nature of the problem
  4. Complete the applicable emergency procedure or take action appropriate for the problem
  5. Determine the landing criteria and land as required
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Land immediately

A

Execute a landing without delay

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

Land as soon as possible

A

Execute a landing at the first site at which a safe landing can be made

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

Land as soon as practicable

A

Extended flight is not recommended. The landing site and duration of the flight are at the discretion of the pilot in command

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

Engine Malfunction in Flight

A

*1. Control Nr
Warning: Flying with greater than 110% torque with on engine inoperative may result in unrecoverable decay of Nr in the event of a dual-engine failure
*2. CONTGCY PWR switch - ON
*3. Single-engine conditions - Establish
*4. ENG ANTI-ICE switches - As required
Warning: With engine anti-ice on, up to 18% torque available is lost. Torque may be reduced as much as 49% with improperly operating engine inlet anti-ice valves.
*5. External cargo/stores/fuel - Jettison/dump, as required
*6. Identify malfuntion

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Engine High-Side Failure in Flight

A

*1. EMIF - Perform
Note: Ng does not pass through the EDECU and is a highly reliable signal
Note: Torque signal may be erratic or drop off for high side conditions drive by EDECU failure
*2. PCL (malfunction engine) - Retard to set:
a. Torque 10% below good engine
b. Matched Ng
c. Matched TGT

Note: With high collective settings, Nr may increase slowly, making high-side failure confirmation difficult

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

Engine High-Side Failure on Deck

A

*1. PCL (malfunctioning engine) - IDLE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Engine Low-Side Failure

A

*1. EMIF - Perform

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Engine Torque or TGT Spiking/Fluctuations

A

If an engine is spiking/fluctuating and inducing secondary infection in Ng, Np, and/or Nr:
*1. EMIF - Perform
If fuel contamination is suspected:
*2. Land as soon as possible

Warning: PCL movement during engine fluctuations may precipitate an engine failure.

Note: Maintaining a low power setting when moving the PCL will minimize the Nr decay rate if the malfunctioning engine fails.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Compressor Stall

A

*1. EMIF - Perform
*2. PCL (malfunctioning engine) - IDLE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Engine High-Speed Shaft Failure

A

*1. EMIF - Perform
*2. PCL (malfunctioning engine) - OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Abort Start Causes

A
  1. Ng does not reach 14% within 6 seconds of starter initiation
  2. No oil pressure within 30 seconds after start initiation (do not motor engine)
  3. No light-off within 30 seconds after moving PCL to IDLE
  4. ENG STARTER advisory disappears before reaching 52% Ng
  5. TGT is likely to exceed 851 degrees before idle speed is attained

Caution: During aborted starts, failure to immediately stop fuel flow may result in engine overtemperture

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Abort Start EP

A

To abort start:
*1. PCL - OFF
*2 ENGINE IGNITION switch - OFF
If engine oil pressure is indicated:
*3 Starter - Engage

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Engine Malfunction During Hover/Takeoff

A

*1. Control Nr
*2. CONTGCY PWR switch - ON
If a suitable landing site exists or unable to transition to forward flight:
*3. Set level attitude, climate drift, cushion landing
If able to transition to forward flight:
*4. EMIF - Perform

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Dual- Engine Failure

A

*1. Autorotation - Establish
*2. Immediately Landing/Ditching emergency procedure - Perform
If time and altitude permit:
*3. Engine Air Restart emergency procedure - Perform

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Single-Engine Failure in Flight

A

*1. EMIF - Perform

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Engine Air Restart

A

Caution: Receiving engine Ng less than 24% prior to advancing PCL to IDLE may result in hot start.

*1. APU Emergency Start Procedure - Perform

Note: Failure to ensure AIR SOURCE ECS/START switch is in ENG prior to crossbleed start will result in a failed engine start.

*2. ENGINE IGNITION switch - NORM
*3. Fuel selector lever - DIR or XFD
*4. PCL - OFF
*5. Starter - Engage, motor engine
*6. PCL - IDLE (TGT 80 or less, if time permits)
*7. PCL - Advance to FLY after start dropout

Warning: If APU is unavailable, and a crossbleed start is necessary, maximum torque available will be reduced during the start sequence. Depending on operating conditions, level flight may not be possible

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

APU Emergency Start

A

*1. ECS - OFF
*2. AIR SOURCE ECS/START switch - APU
*3. FUEL PUMP switch - APU BOOST
*4. APU CTRL switch - ON
*5. APU GENERATOR switch - ON

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Ground Resonance

A

Caution: If ground resonance is encountered and an immediate safe takeoff is not possible priority shall be given to immediate reduction of main rotor speed.

If safe takeoff is possible:
*1. Take off immediately

If safe takeoff is not possible:
*2. PCLs - OFF
*3. Rotor brake - Apply

Warning: Ground resonance can occur rapidly (within three seconds), and produce violent vibrations resulting in difficulty reaching PCLs and pilot-induced oscillations. Vibrations can grow severe enough to result in dynamic departure of rotor blades and potential dynamic rollover.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Unusal Vibrations on Deck

A

Caution: Application of the rotor brake may aggravate lead/lag tendencies and cause a mechanical failure

Caution: Continued operations with unusual on-deck vibrations may result in rotor system damage or mechanical failure.

*1. Collective - Lower
*2. PCLs - OFF
*3. Rotor brake - Apply as required

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Hung Droop Stops

A

*1. Reengage rotor to greater than 75% Nr

22
Q

Low Rotor RPM

A

*1. Control Nr

23
Q

Main Transmission Malfunction

A

Warning: Possible indications of main transmission imminent failure may include: yaw attitude excursions with no control input, an increase in power required for fix collective settling, failure of a main generator or hydraulic pump, increased noise, increased vibration levels, or abnormal fumes in the cabin

If failure is imminent:
*1. Land immediately

If secondary indications are present:
*2. Land as as possible

Note: A minimum power airspeed and low altitude flight profile (approximately 80 feet and 80 KIAS) permits a quick flare to ditching

Warning: Operation of the main gearbox with no oil pressure may result in loss of tail rotor drive

Note: A loss of all main transmission lubricating oil may result in unreliable temperature indications from the main transmission temperature gauge and temperature sensor (caution)

24
Q

Tail/Intermediate Transmission Malfunction

A

Warning: Possible indications of tail rotor imminent failure may include tail/intermediate transmission cautions accompanied by strong medium-frequency vibrations and or hot metal fumes or any other associated indications

If failure is imminent:
*1. Land immediately

If failure is not imminent:
*2. Land as soon as possible.

Warning: High power setting require maximum performance of the tail rotor drive system failure

Note: Transiting at an altitude sufficient to enter an autorotation is recommended

Note: An INT XMSN OIL HOT or TAIL XMSN OIL HOT caution occurring simultaneously with a WCA MISCOMPARE alert may be an indication of a mission computer/backup computer card failure

25
#1/#2 Input Chip Caution
*1 Main Transmission Malfunction emergency procedure - Perform
26
Loss of Tail Rotor Drive (Altitude and Airspeed Sufficient to Establish Autorotation)
*1. PAC call - "AUTO, AUTO, AUTO" *2. Autorotation - Establish. Center tail rotor pedals. *3. Drive failure - Attempt to verify *4. Immediate Landing/Ditching emergency procedure - Perform *5. PCLs - OFF when directed (prior to the flare)
27
Loss of Tail Rotor Drive (Altitude and Airspeed Not Sufficient to Establish Autorotation)
*1. PAC call - "HOVER, HOVER, HOVER" *2. Collective - Lower *3. PNAC - Hands on PCLs *4. PCLs- OFF when directed (approx. 20 to 30 feet)
28
Types of Loss of Tail Rotor Control Malfunctions
1. Tail rotor control cable failures 2. Servo Failure 3. Restricted flight controls
29
Tail Rotor Control Cable Failure
Indicated by TAIL ROTOR QUADRANT; if both cables fail tail rotor control will be lost. Tail rotor will assume, a preset spring-loaded position setting. GW 19,500, level flight balanced flight occurs at about 25 and 145 KIAS and will yaw left between 25-145 and right outside of 25/145. As weight changes the range goes in or out.
30
Tail Rotor Servo Failure
Loss of both #1 HYD PUMP and BACKUP PUMP results in both stages of the tail rotor servo being unpressurized. Normal yaw is available between 40 and 120 KIAS. Roll on landing above 40 KIAS is recommended. Once on deck and torque is reduced, the aerodynamic load on the tail rotor are reduced and yaw control should be regained.
31
Restricted Flight Controls
A yaw trim malfunction, induced by the AFCS computer can produce 30 pounds of force at the pedal Internally jammed yaw trim actuator can produce up to 80 pounds of force until clutch slippage relieves this force. Pilot can override trim force by applying opposite pedal until even then depress trim. Malfunction within the yaw boost servo or tail servo can produce much higher forces at the pedals, affected servos must be turned off. Hardover failure of the yaw boost servo will increase control forces as much as 250 pounds.
32
Tail Rotor Quadrant Caution
*1. Check for tail rotor control If tail rotor control is not available: *2. Loss of Tail Rotor Control Emergency procedure - Perform Note: Removing hydraulic power with a single tail rotor cable failure will disconnect the other cable
33
Loss of Tail Rotor Control
*1. Collective/airspeed - Adjust, as required to control yaw
34
Hydraulic System Warning
*1. Land Immediately
35
#1 and #2 HYD PUMP Failure
*1. Restrict flight control movement *2 Land as soon as possible
36
#1 Primary Servo or #1 Transfer Module Leak
*1. SERVO Switch - 1st OFF *2. Land as soon as practicable If the BACK UP RSVR LOW caution also appears or the backup fails: *3. Land as soon as possible. Be prepared for loss of tail rotor control If the #2 PRI SERVO PRESS caution and/or HYD warning appears: *4. Land immediately Warning: Failure to ensure BACKUP HYD PUMP switch is in AUTO or ON position prior to landing with a #1 RSVR LOW or #1 HYD PUMP caution present will result in loss of tail rotor directional control when the weight on wheels is activated.
37
#2 Primary Servo or #2 Transfer Module Leak
*1. SERVO switch - 2nd OFF *2. Land as soon as practicable Caution: Landing with the BACKUP HYD PMP switch in OFF position with a #2 HYD PUMP caution will result in loss of pilot assist servos when the weight on wheels is activated If the BACKUP RSVR LOW caution also appears or backup pump fails: *3. Land as soon as possible. Be prepared for loss of the pilot-assist servos If the #1 PRI SERVO PRESS caution and/or HYD warning appears: *4. Land Immediately
38
Boost Servo Hardover
*1. PAC call - "BOOST, BOOST, BOOST" *2. SAS/BOOST pushbutton - OFF
39
Utility Hydraulic Cautions
*1. Stop dome
40
AFCS Degraded Caution
*1. Safe altitude and airspeed - Establish (waveoff/ITO, as required)
41
Stabilator Auto Mode Failure
*1. PAC call - "STAB, STAB, STAB" *2. Cyclic - Arrest pitch rate *3. Collective - Do not reduce *4. STABILATOR MAN SLEW switch - Adjust to 0 degrees Stab Angle/KIAS Limit 0/150 10/100 20/80 30/60 40/45
42
Unusual Attitude Recovery
*1. Level wings *2. Nose on horizon *3. Center ball *4. Stop rate of climb/descent *5. Control airspeed
43
Electrical Power Failure/Dual Generator Failure
*1. Safe altitude and airspeed - Establish *2. Stabilator - Check position visually, slew as required *3. APU Emergency Start procedure - perform *4. CMPTR PWR/RESET, SAS 1, SAS 2, TRIM, AUTO PLT, STABILATOR AUTO CONTROL pushbuttons - ON
44
#1/#2 FUEL FLTR BYPASS OR #1/#2 FUEL PRESS CAUTION
*1. Fuel selector lever (affected engine) - XFD (DIR if currently in XFD)
45
#1 AND #2 FUEL FLTR BYPASS OR #1 AND #2 FUEL PRESS CAUTION
*1. Land as soon as possible, Be prepared for dual-engine failure *2. APU Emergency Start Procedure - Perform
46
External Engine Fire
*1. Confirm fire *2. EMIF - Perform *3. PCL (affected engine) - OFF *4. Engine T-handle (affected engine) - PULL *5. FIRE EXTGH switch - MAIN (RESERVE if required or ac power is off) If airborne and fire continues: *6. Land immediately If fire appears extinguished: *7. Land as soon as possible
47
Internal Engine Fire
*1. Starter - Engage. Motor engine
48
APU Fire
*1. APU T-handle - Pull *2. Confirm fire *3. FIRE EXTGH switch - RESERVE (MAIN if required and available) If airborne and fire continues: *4. Land immediately If fire appears extinguished: *5. Land as soon as possible
49
Cockpit Fire/Cabin Fire
If source is known: *1. Affected power switches and circuit breakers - OFF/PULL *2. Portable fire extinguisher - As required If fire continues or source is unknown: *3. Cabin/doors/vents/ECS - Close/OFF, as required *4. Unnecessary electrical equipment and circuit breakers - OFF/Pull If fire continues: *5. Land as soon as possible
50
Smoke and Fumes Elimination
*1. Airspeed - Adjust, as required *2. Doors/window/vents - Open *3. Aircraft - Yaw, as required
51

HAC Studying (1 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions