Chapter 9 (underlined)

Question 1

Land As Soon As Possible

Answer 1

The term LAND AS SOON AS POSSIBLE is defined as landing at the nearest suitable landing area (e.g., open field) without delay. (The primary consideration is to ensure the survival of occupants.)

Question 2

Land As Soon As Practicable

Answer 2

The term LAND AS SOON AS PRACTICABLE is defined as landing at a suitable landing area. (The primary consideration is the urgency of the emergency.)

Question 3

Autorotate

Answer 3

The term AUTOROTATE is defined as adjusting the flight controls as necessary to establish an auto-rotational descent and landing.

Question 4

Emergency Engine Shutdown

Answer 4

The term EMER ENG SHUTDOWN is defined as engine shutdown without delay. 1. ENG POWER CONT lever(s) - OFF. 2. ENG FUEL SYS selector(s) - OFF. 3. FUEL BOOST PUMP CONTROL switch(es) - OFF. … TGT …….. 538 C ………: 4. AIR SOURCE HEAT/START switch - As required. 5. ENGINE IGNITION switch - OFF. 6. Starter button - Press ……

Question 5

Lockout

Answer 5

The term LOCKOUT is defined as manual control of engine RPM while bypassing DEC functions. ENG POWER CONT lever - Pull down and advance full forward while maintaining downward pressure, then adjust to set % RPM R as required.

Question 6

Emergency APU Start

Answer 6

The term EMER APU START is defined as APU start to accomplish an emergency procedure. 1. FUEL PUMP switch - APU BOOST. 2. APU CONTR switch - ON.

Question 7

Single Engine Failure

Answer 7

1. Collective - Adjust to maintain % RPM R. 2. External cargo/stores - Jettison (if required). 3. Establish single-engine airspeed. If continued flight is not possible: 4. LAND AS SOON AS POSSIBLE ……….. is possible: 5. ………..

Question 8

Dual Engine Failure

Answer 8

AUTOROTATE

Question 9

Decreasing % RPM R

Answer 9

1. Collective - Adjust to control % RPM R. 2. Establish a single-engine airspeed. 3. ENG POWER CONT lever (low % TRQ/TGT TEMP engine) - LOCKOUT 4. ………

Question 10

Increasing % RPM R

Answer 10

1. ENG POWER CONT lever (high % TRQ/TGT TEMP engine) - Retard. 2. …….. ……. ENG POWER CONT lever ….. FLY and IDLE… the HMU…… If this occurs: 3. …… 4. Perform EMER ENG SHUTDOWN (affected engine). 5. ……

Question 11

Engine Compressor Stall

Answer 11

1. Collective - Reduce. If conditions persists: 2. ENG POWER CONT lever (affected engine) - Retard 3. ……. If stall condition recurs: 4. Establish single engine airspeed. 5. EMER ENG SHUTDOWN …(affected engine)… 6. …….

Question 12

Engine High-Speed Shaft Failure

Answer 12

1. Collective - Adjust. 2. Establish single engine airspeed. 3. EMER ENG SHUTDOWN …(affected engine). Do not…… 4. ……

Question 13

Lightning Strike

Answer 13

1. ENG POWER CONT levers - Adjust as required to control % RPM. 2. LAND AS SOON AS POSSIBLE.

Question 14

Loss Of Tail Rotor Thrust In Flight

Answer 14

1. Airspeed - Adjust to 80 KIAS or above. 2. AUTOROTATATE - Maintain airspeed at or above 80 KIAS. 3. ENG POWER CONT levers - OFF (during deceleration when intended point of landing is assured)

Question 15

Loss Of Tail Rotor Thrust or Tail Rotor Quadrant Caution Appears with Loss Of Control at Low Airspeed/Hover (Right Rotation)

Answer 15

1. Collective - Reduce. 2. ENG POWER CONT levers - OFF (5 to 10 feet above touchdown).

Question 16

Tail Rotor Quadrant Caution Appears In Cruise Flight

Answer 16

1. Collective - Adjust to determine controllability (Fixed Right or Left). 2. ……

Question 17

Loss Of Control at Low Airspeed/Hover or Tail Rotor Quadrant Caution Appears (Left Rotation)

Answer 17

1. ENG POWER CONT lever(s) - Retard to decrease % RPM R below 100% and begin a partial power descent. 2. Collective - Adjust to preserve % RPM R. 3. ENG POWER CONT levers - OFF (5-10 feet above touchdown). 4. Collective - Adjust for landing.

Question 18

Pedal Bind/Restrictions or Drive With No Accompaying Caution

Answer 18

1. Apply pedal force to oppose the drive. 2. …… 3. …… If….. 4. …… 5. …… If….. 6. …… 7. …… 8. ……

Question 19

1 Tail RTR Servo appears and Back Up Pump On does not appear or #2 Tail RTR Servo On does not appear

Answer 19

1. TAIL SERVO switch - BACKUP 2. …… 3. ……

Question 20

Main XMSN Press (low) or Main XMSN Oil Temp (high)

Answer 20

1. LAND AS SOON AS POSSIBLE. If time permits: 2. ….. 80 …. 3. EMER APU START. 4. ……

Question 21

Chip Input MDL - LH or Chip Input MDL - RH

Answer 21

1. Establish single engine airspeed. 2. ENG POWER CONT lever (affected engine) - IDLE. 3. LAND AS SOON AS POSSIBLE.

Question 22

Chip Main MDL Sump, Chip Access MDL LH or RH or Chip Tail XMSN or Chip INT XMSN/Tail XMSN Oil Temp or INT XMSN Oil Temp

Answer 22

LAND AS SOON AS POSSIBLE

Question 23

Main Transmission Failure

Answer 23

1. Collective - Adjust only enough to begin a descent with power remaining applied to the main transmission throughout the descent and landing. 2. LAND AS SOON AS POSSIBLE.

Question 24

Engine/Fuselage Fire On Ground

Answer 24

1. ENG POWER CONT levers - OFF. 2. ENG EMER OFF handle - Pull if applicable. 3. FIRE EXTGH switch - MAIN/RESERVE as required. 4. EMER ENG SHUTDOWN - Perform (other engine)

Question 25

APU Compartment Fire

Answer 25

1. APU fire T-handle - Pull. 2. FIRE EXTGH switch - MAIN/RESERVE as required.

Question 26

Engine Fire In-Flight

Answer 26

1. Establish single engine airspeed. 2. ENG POWER CONT lever (affected engine) - OFF. 3. ENG EMER OFF handle - Pull. 4. FIRE EXTGH switch - MAIN/RESERVE as required. 5. LAND AS SOON AS POSSIBLE.

Question 27

Electrical Fire In-Flight

Answer 27

1. BATT and GENERATORS switches - OFF. 2. LAND AS SOON AS POSSIBLE.

Question 28

#1 Fuel FLTR Bypass and #2 Fuel FLTR Bypass

Answer 28

LAND AS SOON AS POSSIBLE

Question 29

#1 Fuel Press or #2 Fuel Press

Answer 29

If the caution appears and the situation is critical: 1. ENG FUEL SYS selector on affected engine - XFD. 2. FUEL BOOST PUMP CONTROL switches - NO. 1 PUMP or NO. 2 PUMP - ON (As applicable). 3. LAND AS SOON AS POSSIBLE. 4. EMER ENG SHUTDOWN after landing. .......... is not critical: 1. ...... 2. ...... 3. ......

Question 30

#1 Fuel Press and #2 Fuel Press

Answer 30

1. LAND AS SOON AS POSSIBLE. 2. EMER ENG SHUTDOWN after landing.

Question 31

#1 HYD Pump and #2 HYD Pump

Answer 31

LAND AS SOON AS POSSIBLE. ......restrict control......

Question 32

#1 HYD Pump or #2 HYD Pump and Back Up Pump On does not appear

Answer 32

1. Airspeed - Adjust ......comfortable...... 2. BACKUP HYD PUMP switch - ON. If BACK-UP PUMP ON advisory still does not appear: 3. FPS and BOOST switches - Off (for #2 HYD PUMP caution). 4. LAND AS SOON AS POSSIBLE.

Question 33

#1 PRI Servo Press or #2 PRI Servo Press

Answer 33

1. SVO OFF switches - Check both are centered. 2. If the caution appears with the SVO OFF switch centered, move the SVO OFF switch to turn off the malfunctioning servo. 3. LAND AS SOON AS POSSIBLE.

Question 34

#1 RSVR Low and #1 HYD Pump with Back-Up Pump on

Answer 34

1. ...... If the BACK-UP RSVR LOW caution also appears: 2. SVO OFF switch - 1ST STG. 3. LAND AS SOON AS POSSIBLE.

Question 35

#2 RSVR Low and #2 HYD Pump with Back-Up Pump on

Answer 35

1. ...... 2. ...... If the BACK-UP RSVR LOW caution also appears: 3. SVO OFF switch - 2ND STG. 4. LAND AS SOON AS POSSIBLE.

Question 36

Collective Boost Servo Hard Over or Power Piston Failure

Answer 36

1. BOOST switch - Off. 2. ......

Question 37

Emergency Landing In Wooded Areas - Power Off

Answer 37

1. AUTOROTATE. ...... 2. Collective adjust ......

Question 38

Ditching - Power Off

Answer 38

1. AUTOROTATE. 2. ...... 3. ...... 4. ...... 5. ......

Question 39

Flight Control or Main-Rotor System Malfunctions

Answer 39

1. LAND AS SOON AS POSSIBLE. 2. EMER ENG(S) SHUTDOWN after landing.

Question 40

Stabilator Malfunction - Auto Mode Failure

Answer 40

1. Cyclic mounted stabilator slew-up switch - Adjust if necessary ...... 2. AUTO CONTROL switch - Press ON once after establishing a comfortable airspeed. If automatic control is not regained: 3. ...... 4. ...... If manual control is not possible: 5. ...... 6. ......

Question 41

Uncommanded Nose Down Pitch Attitude Change

Answer 41

1. Cyclic - Adjust as required. 2. Collective - Maintain or increase. 3. Cyclic mounted stabilator slew-up switch - Adjust as required ...... 4. ...... 5. ......

Question 42

Uncommanded Nose Up Pitch Attitude Change

Answer 42

If an ...... 1. Cyclic - Adjust as required. 2. Collective - Reduce as required. 3. ...... 4. ......

Question 43

(#1 and #2 Generator Failure) #1 CONV and #2 CONV and AC ESS BUS OFF

Answer 43

1. ..... 2. ...... 3. ...... If cautions still appear: 4. ...... 5. ...... 6. EMER APU START. 7. ...... 8. ......

Question 44

#1 or #2 Chip Engine #1 or #2 Engine Oil Press #1 or #2 Engine Oil Temp

Answer 44

1. Establish single engine airspeed. 2. ENG POWER CONT lever (affected engine) - Retard ...... If oil pressure ..... or ..... oil temperature.....: 3. EMER ENG SHUTDOWN ...(affected engine)... 4. .....