Chapter 9 (underlined) Flashcards
Land As Soon As Possible
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.)
Land As Soon As Practicable
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.)
Autorotate
The term AUTOROTATE is defined as adjusting the flight controls as necessary to establish an auto-rotational descent and landing.
Emergency Engine Shutdown
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 ……
Lockout
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.
Emergency APU Start
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.
Single Engine Failure
- 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. ………..
Dual Engine Failure
AUTOROTATE
Decreasing % RPM R
- Collective - Adjust to control % RPM R. 2. Establish a single-engine airspeed. 3. ENG POWER CONT lever (low % TRQ/TGT TEMP engine) - LOCKOUT 4. ………
Increasing % RPM R
- 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. ……
Engine Compressor Stall
- 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. …….
Engine High-Speed Shaft Failure
- Collective - Adjust. 2. Establish single engine airspeed. 3. EMER ENG SHUTDOWN …(affected engine). Do not…… 4. ……
Lightning Strike
- ENG POWER CONT levers - Adjust as required to control % RPM. 2. LAND AS SOON AS POSSIBLE.
Loss Of Tail Rotor Thrust In Flight
- 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)
Loss Of Tail Rotor Thrust or Tail Rotor Quadrant Caution Appears with Loss Of Control at Low Airspeed/Hover (Right Rotation)
- Collective - Reduce. 2. ENG POWER CONT levers - OFF (5 to 10 feet above touchdown).
Tail Rotor Quadrant Caution Appears In Cruise Flight
- Collective - Adjust to determine controllability (Fixed Right or Left). 2. ……
Loss Of Control at Low Airspeed/Hover or Tail Rotor Quadrant Caution Appears (Left Rotation)
- 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.
Pedal Bind/Restrictions or Drive With No Accompaying Caution
- Apply pedal force to oppose the drive. 2. …… 3. …… If….. 4. …… 5. …… If….. 6. …… 7. …… 8. ……
1 Tail RTR Servo appears and Back Up Pump On does not appear or #2 Tail RTR Servo On does not appear
- TAIL SERVO switch - BACKUP 2. …… 3. ……
Main XMSN Press (low) or Main XMSN Oil Temp (high)
- LAND AS SOON AS POSSIBLE. If time permits: 2. ….. 80 …. 3. EMER APU START. 4. ……
Chip Input MDL - LH or Chip Input MDL - RH
- Establish single engine airspeed. 2. ENG POWER CONT lever (affected engine) - IDLE. 3. LAND AS SOON AS POSSIBLE.
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
LAND AS SOON AS POSSIBLE
Main Transmission Failure
- 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.
Engine/Fuselage Fire On Ground
- 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)
APU Compartment Fire
- APU fire T-handle - Pull. 2. FIRE EXTGH switch - MAIN/RESERVE as required.
Engine Fire In-Flight
- 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.
Electrical Fire In-Flight
- BATT and GENERATORS switches - OFF. 2. LAND AS SOON AS POSSIBLE.
1 Fuel FLTR Bypass and #2 Fuel FLTR Bypass
LAND AS SOON AS POSSIBLE
1 Fuel Press or #2 Fuel Press
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. ……
1 Fuel Press and #2 Fuel Press
- LAND AS SOON AS POSSIBLE. 2. EMER ENG SHUTDOWN after landing.
1 HYD Pump and #2 HYD Pump
LAND AS SOON AS POSSIBLE. ……restrict control……
1 HYD Pump or #2 HYD Pump and Back Up Pump On does not appear
- 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.
1 PRI Servo Press or #2 PRI Servo Press
- 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.
1 RSVR Low and #1 HYD Pump with Back-Up Pump on
- …… If the BACK-UP RSVR LOW caution also appears: 2. SVO OFF switch - 1ST STG. 3. LAND AS SOON AS POSSIBLE.
2 RSVR Low and #2 HYD Pump with Back-Up Pump on
- …… 2. …… If the BACK-UP RSVR LOW caution also appears: 3. SVO OFF switch - 2ND STG. 4. LAND AS SOON AS POSSIBLE.
Collective Boost Servo Hard Over or Power Piston Failure
- BOOST switch - Off. 2. ……
Emergency Landing In Wooded Areas - Power Off
- AUTOROTATE. …… 2. Collective adjust ……
Ditching - Power Off
- AUTOROTATE. 2. …… 3. …… 4. …… 5. ……
Flight Control or Main-Rotor System Malfunctions
- LAND AS SOON AS POSSIBLE. 2. EMER ENG(S) SHUTDOWN after landing.
Stabilator Malfunction - Auto Mode Failure
- 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. ……
Uncommanded Nose Down Pitch Attitude Change
- Cyclic - Adjust as required. 2. Collective - Maintain or increase. 3. Cyclic mounted stabilator slew-up switch - Adjust as required …… 4. …… 5. ……
Uncommanded Nose Up Pitch Attitude Change
If an …… 1. Cyclic - Adjust as required. 2. Collective - Reduce as required. 3. …… 4. ……
(#1 and #2 Generator Failure) #1 CONV and #2 CONV and AC ESS BUS OFF
- ….. 2. …… 3. …… If cautions still appear: 4. …… 5. …… 6. EMER APU START. 7. …… 8. ……
1 or #2 Chip Engine #1 or #2 Engine Oil Press #1 or #2 Engine Oil Temp
- 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. …..