Ch. 9 EPs Flashcards
The term LAND WITHOUT DELAY is defined as:
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).
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.
The term AUTOROTATE is defined as:
adjusting the flight controls as necessary to establish an autorotational descent and landing.
Emergency Shutdown:
1.
2.
3.
4.
(P.A.R.M.)
Emergency Shutdown:
1. POWER LEVERS – OFF
2. APU – OFF (if applicable)
3. ROTOR BRAKE switch – BRK
4. MSTR IGN – OFF once rotors have stopped
EMERGENCY EXIT AND ENTRANCE – CANOPY JETTISON
1.
2.
3.
(H.A.C.)
EMERGENCY EXIT AND ENTRANCE – CANOPY JETTISON
1. Helmet visors – Down.
2. Area around helicopter – Clear of personnel.
3. CANOPY JETTISON handle – Operate (see caution 2)
If Flares are ignited and lodged in the dispenser, jettison all flare munitions and ________________________________________.
LAND AS SOON AS POSSIBLE.
Dual Engine Failure- Low Altitude / Low Airspeed and Cruise
Dual Engine Failure- Low Altitude / Low Airspeed and Cruise
1. AUTOROTATE – Rapidly lower collective to maintain NR within limits
2. CHOP Button – Reset if an ENGINE CHOP warning message is present
ABORT START PROCEDURES
1.
2.
(P.E.)
ABORT START PROCEDURES
1. POWER lever – OFF
2. ENG START switch – IGN ORIDE for 30 seconds and TGT is below 540o C.
Single Engine Failure- Low Altitude / Low Airspeed and Cruise
1.
Single Engine Failure- Low Altitude / Low Airspeed and Cruise
1. Achieve safe single engine flight conditions or land
Engine 1 or 2 Overspeed – NP Failed High
Engine 1 or 2 Overspeed – NP Failed High
1. Collective – Adjust to maintain NR within limits
2. LAND AS SOON AS PRACTICABLE
NP Failed Low – Low RPM Rotor
1.
NP Failed Low – Low RPM Rotor
1. Collective – Adjust to maintain NR within limits
Engine Compressor Stall
1.
Engine Compressor Stall
1. Collective – Reduce
MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE
1.
2.
3.
4.
5.
(E.C.P.C.L.)
MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE
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
5. LAND WITHOUT DELAY
LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT POSSIBLE
1.
LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT POSSIBLE
1. Airspeed – 100 KTAS minimum (until 10-20 feet above touchdown)
LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT NOT POSSIBLE
1.
2.
3.
(C.P.C)
LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT NOT POSSIBLE
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
TAIL ROTOR FIXED PITCH – LOW AIRSPEED OR HOVER
1.
2.
3.
(C.C.B.)
TAIL ROTOR FIXED PITCH – LOW AIRSPEED OR HOVER
1. Collective – Adjust to minimize Yaw rate
2. Cyclic – Minimize drift
If pedals are jammed
3. Break into BUCS
TAIL ROTOR FIXED PITCH – FORWARD FLIGHT
1.
2.
………
3.
(C.C.B)
TAIL ROTOR FIXED PITCH – FORWARD FLIGHT
1. Collective – Adjust to minimize Yaw rate
2. Cyclic – Oppose yaw
….If pedals are jammed….
3. Break into BUCS
MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE – IN FLIGHT
1.
MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE – IN FLIGHT
1. Achieve safe single engine flight conditions or land
ENGINE 1 OR ENGINE 2 FIRE – IN FLIGHT
1.
2.
3.
(A.I.F)
ENGINE 1 OR ENGINE 2 FIRE – IN FLIGHT
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
APU FIRE – ON GROUND
1.
2.
3.
(A.I.F)
APU FIRE – ON GROUND
1. APU – OFF
2. Illuminated APU FIRE button – Press and RDY light illuminates
3. FIRE DISCH button(s) – Press
APU FIRE – IN FLIGHT
1.
2.
(I.F.)
APU FIRE – IN FLIGHT
1. Illuminated APU FIRE button – Press and RDY light illuminates
2. FIRE DISCH button(s) – Press
HYDRAULIC FAILURE – PRIMARY & UTILITY HYDRAULIC PSI LOW
1.
…..
2.
(E.L)
HYDRAULIC FAILURE – PRIMARY & UTILITY HYDRAULIC PSI LOW
1. EMERG HYD button – Press ON
…..Urgency to land….
2. LAND WITHOUT DELAY
EMERGENCY LANDING IN WOODED AREA (POWER OFF)
1.
EMERGENCY LANDING IN WOODED AREA (POWER OFF)
1. AUTOROTATE – Apply full collective to decay rotor RPM as helicopter settles.
DITCHING (POWER OFF)
1.
2.
3.
4.
(A.C.C.E)
DITCHING (POWER OFF)
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.
BUCS FAIL
1.
BUCS FAIL
1. Transfer flight controls to rear crew station
FLIGHT CONTROL MALFUNCTION – STABILIZATION EQUPMENT/FORCE TRIM
1.
FLIGHT CONTROL MALFUNCTION – STABILIZATION EQUPMENT/FORCE TRIM
1. FMC release button – Press
NVS Failure
1.
2.
(E.P.)
NVS Failure
1. Exit the NOE environment
2. Pilot on the controls, NVS Select Switch – Select alternate sensor (PNVS or TADS)
IHADSS/HDU Failure or IHADSS STALE At night (NVS flight)
1.
IHADSS/HDU Failure or IHADSS STALE At night (NVS flight)
1. Exit the NOE environment
Single MP Operation
1.
…….
2.
Single MP Operation
1. NVS SELECT Switch – Reselect (PNVS or TADS)
…..or…..
2. Crewmemeber (not on controls) – Assume control
Dual MP Failure – MP1 AND MP2 FAIL at night (NVS flight)
1.
Dual MP Failure – MP1 AND MP2 FAIL at night (NVS flight)
1. Exit the NOE environment
CAUTION: Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW
1.
2.
(F.L.)
CAUTION: Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW
1. FUEL page, BOOST button – Press ON
2. LAND AS SOON AS POSSIBLE
