Big 7 plus Fire

Descripción

The Big 7 EPs and the Fire EPs
Dan Hurley
Test por Dan Hurley, actualizado hace más de 1 año
Dan Hurley
Creado por Dan Hurley hace más de 3 años
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Resumen del Recurso

Pregunta 1

Pregunta
Single engine failure - flight Procedure 1. OEI flight condition - [blank_start]Establish[blank_end] 2. Rotor speed - [blank_start]Trim to maximum[blank_end] 3. Affected engine - [blank_start]Identify[blank_end] 4. Single engine emergency shutdown - [blank_start]Perform[blank_end] 5. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Respuesta
  • Establish
  • Trim to maximum
  • Identify
  • Perform
  • LAND AS SOON AS PRACTICABLE

Pregunta 2

Pregunta
Single engine failure - hover OGE Flight Procedure 1. Collective lever – [blank_start]Adjust to maintain rotor RPM[blank_end] 2. Airspeed – [blank_start]Increase if possible[blank_end] TRANSITION TO OEI - FLIGHT 3. Collective lever – [blank_start]Adjust to OEI-limits or below[blank_end] 4. Rotor speed – [blank_start]Trim to maximum[blank_end] 5. Airspeed – [blank_start]Gain[blank_end], [blank_start]65[blank_end] KIAS (VY) After reaching safe altitude: 6. Collective lever – [blank_start]Reduce to OEI MCP or below[blank_end] 7. Affected engine – [blank_start]Identify[blank_end] 8. Single engine emergency shutdown – [blank_start]Perform[blank_end] 9. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Respuesta
  • Adjust to maintain rotor RPM
  • Increase if possible
  • Adjust to OEI-limits or below
  • Trim to maximum
  • Gain
  • 65
  • Reduce to OEI MCP or below
  • Identify
  • Perform
  • LAND AS SOON AS PRACTICABLE

Pregunta 3

Pregunta
Single engine failure - hover OGE Landing Procedure 1. Collective lever – [blank_start]Adjust to maintain rotor RPM[blank_end] 2. Airspeed – [blank_start]Increase if possible[blank_end] FORCED LANDING 3. Landing attitude – [blank_start]Establish[blank_end] 4. Collective lever – [blank_start]Raise as necessary[blank_end] to [blank_start]stop descent and cushion landing[blank_end] After landing: 5. Affected engine – [blank_start]Identify[blank_end] 6. Single engine emergency shutdown – [blank_start]Perform[blank_end]
Respuesta
  • Adjust to maintain rotor RPM
  • Increase if possible
  • Establish
  • Raise as necessary
  • stop descent and cushion landing
  • Identify
  • Perform

Pregunta 4

Pregunta
Autorotation Procedure 1. Collective lever – [blank_start]Reduce to maintain NRO within limits[blank_end] 2. Airspeed – [blank_start]75 KIAS recommended[blank_end] 3. Double engine emergency shutdown – [blank_start]Perform[blank_end] 8. BAT MSTR sw – [blank_start]OFF[blank_end]
Respuesta
  • Reduce to maintain NRO within limits
  • 75 KIAS recommended
  • Perform
  • OFF

Pregunta 5

Pregunta
Tail Rotor Drive Failure/Fixed-pitch Tail Rotor Control Failure - Forward Flight Procedure 1. Collective lever – [blank_start]Reduce to obtain minimum sideslip angle[blank_end] 2. Airspeed – [blank_start]Maintain 70 KIAS or higher[blank_end] 3. Suitable landing area – [blank_start]Select[blank_end] 4. Shallow approach with nose left – [blank_start]Perform[blank_end] 5. Airspeed – [blank_start]Reduce close to the ground[blank_end] until [blank_start]nose is aligned[blank_end] with [blank_start]the flight direction[blank_end] 6. Landing – [blank_start]Perform[blank_end] If the nose direction changes from left to right at airspeeds higher than 40 kts: 5. Airspeed – [blank_start]Increase[blank_end] 6. Approach – [blank_start]Abort[blank_end], [blank_start]climb to sufficient height[blank_end] for [blank_start]autorotation[blank_end] 7. Autorotation – [blank_start]Perform[blank_end]
Respuesta
  • Reduce to obtain minimum sideslip angle
  • Maintain 70 KIAS or higher
  • Perform
  • Select
  • Reduce close to the ground
  • nose is aligned
  • the flight direction
  • Perform
  • Increase
  • Abort
  • climb to sufficient height
  • autorotation
  • Perform

Pregunta 6

Pregunta
Engine underspeed – governor failure Procedure 1. OEI flight condition – [blank_start]Establish[blank_end] 2. Bleed air consumers – [blank_start]Off[blank_end] 3. VAR NR system NORM/MAN pb – [blank_start]Check MAN[blank_end] 4. Affected engine – [blank_start]Identify[blank_end] 5. N2 TRIM sw – [blank_start]Compensate N2/NRO drop[blank_end] and [blank_start]try to match torque[blank_end] If torque match is not possible: 6. Twist grip (affected engine) – [blank_start]Release stop plate[blank_end] and [blank_start]rotate towards FLIGHT[blank_end] until [blank_start]N2 and NRO stabilize in normal range[blank_end] and [blank_start]FLI needles match[blank_end] 7. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end] If no residual torque (affected engine) is available: 8. Single engine emergency shutdown – [blank_start]Perform[blank_end]
Respuesta
  • Establish
  • Off
  • Check MAN
  • Identify
  • Compensate N2/NRO drop
  • try to match torque
  • Release stop plate
  • rotate towards FLIGHT
  • N2 and NRO stabilize in normal range
  • FLI needles match
  • LAND AS SOON AS PRACTICABLE
  • Perform

Pregunta 7

Pregunta
WARNING LIGHT INDICATIONS - FIRE (ENGINE 1 or ENGINE 2) - On Ground Procedure 1. [blank_start]FIRE sw (affected engine)[blank_end] – [blank_start]Raise guard[blank_end], [blank_start]press[blank_end] NOTE Affected engine will shut down automatically, ACTIVE indicatior light, BOT 1 legend (both EMER OFF SW pnl), and F VALVE CL caution indication (CAD) come on. FIRE legend remains on as long as overheat condition exists. 2. [blank_start]Both FUEL PRIME PUMPS[blank_end] – [blank_start]Check OFF[blank_end] 3. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 1 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end]) NOTE Extinguisher bottle will begin discharging when N1t 50%. After discharge of bottle contents, BOT 1 legend and EXT indicatior light go off; BOT 2pb legend comes on. 4. [blank_start]Clock stop watch[blank_end] – [blank_start]Start[blank_end] ([blank_start]after BOT 1 legend[blank_end] and [blank_start]EXT indicator light go off[blank_end] ([blank_start]EMER OFF SW pnl[blank_end]) 5. [blank_start]Double engine emergency shutdown[blank_end] – [blank_start]Perform[blank_end] 6. Passengers – Alert/Evacuate If situation permits and FIRE warning is still on after 1 minute: 7. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 2 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end]) 8. BAT MSTR sw – OFF
Respuesta
  • Raise guard
  • press
  • Check OFF
  • Press
  • bottle 1 activated
  • EXT indicator light comes on
  • EMER OFF SW pnl
  • Start
  • after BOT 1 legend
  • EXT indicator light go off
  • EMER OFF SW pnl
  • Perform
  • Press
  • bottle 2 activated
  • EXT indicator light comes on
  • EMER OFF SW pnl
  • FIRE sw (affected engine)
  • Both FUEL PRIME PUMPS
  • BOT 1/BOT 2 pb
  • Clock stop watch
  • Double engine emergency shutdown
  • BOT 1/BOT 2 pb

Pregunta 8

Pregunta
WARNING LIGHT INDICATIONS - FIRE (ENGINE 1 or ENGINE 2) - In Flight Procedure 1. [blank_start]OEI flight condition[blank_end] – [blank_start]Establish[blank_end] 2. [blank_start]Airspeed[blank_end] – [blank_start]Reduce if IAS is exceeding 100 kts[blank_end] 3. [blank_start]FIRE sw (affected engine)[blank_end] – [blank_start]Raise guard[blank_end], [blank_start]press[blank_end] NOTE Affected engine will shut down automatically, ACTIVE indicatior light, BOT 1 legend (both EMER OFF SW pnl), and F VALVE CL caution indication (CAD) come on. FIRE legend remains on as long as overheat condition exists. 4. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 1 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end]) NOTE Extinguisher bottle will begin discharging when N1t 50%. After discharge of bottle contents, BOT 1 legend and EXT indicatior light go off; BOT 2pb legend comes on. 5. [blank_start]Clock stop watch[blank_end] – [blank_start]Start[blank_end] ([blank_start]after BOT 1 legend[blank_end] and [blank_start]EXT indicator light go off[blank_end]) ([blank_start]EMER OFF SW pnl[blank_end]) 6. [blank_start]Affected engine[blank_end] – [blank_start]Identify[blank_end] 7. Single engine emergency shutdown – [blank_start]Perform[blank_end] 8. Passengers – Alert 9. [blank_start]LAND AS SOON AS POSSIBLE[blank_end] If FIRE warning is still on after 1 minute: 10. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 2 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end]) If FIRE warning remains on: 11. [blank_start]LAND IMMEDIATELY[blank_end]
Respuesta
  • Establish
  • Reduce if IAS is exceeding 100 kts
  • Raise guard
  • press
  • Press
  • bottle 1 activated
  • EXT indicator light comes on
  • EMER OFF SW pnl
  • Start
  • after BOT 1 legend
  • EXT indicator light go off
  • EMER OFF SW pnl
  • Identify
  • Perform
  • LAND AS SOON AS POSSIBLE
  • Press
  • bottle 2 activated
  • EXT indicator light comes on
  • EMER OFF SW pnl
  • LAND IMMEDIATELY
  • OEI flight condition
  • Airspeed
  • FIRE sw (affected engine)
  • BOT 1/BOT 2 pb
  • Clock stop watch
  • Affected engine
  • BOT 1/BOT 2 pb

Pregunta 9

Pregunta
Engine overspeed – governor failure Procedure 1. Collective lever – [blank_start]Raise as necessary[blank_end] to [blank_start]maintain N2 and NRO within limits[blank_end] 2. VAR NR system NORM/MAN sw – [blank_start]Check MAN[blank_end] 3. N2 TRIM sw – [blank_start]Try to trim NRO[blank_end] to [blank_start]101[blank_end]% [blank_start]with matched torque[blank_end] If step 3. is not possible: 4. Affected engine – [blank_start]Identify[blank_end] 5. Twist grip (affected engine) – [blank_start]Rotate towards IDLE[blank_end] until [blank_start]N2 and NRO stabilize in normal range[blank_end] and [blank_start]FLI needles match[blank_end] 6. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Respuesta
  • Raise as necessary
  • maintain N2 and NRO within limits
  • Check MAN
  • 101
  • Try to trim NRO
  • with matched torque
  • Identify
  • Rotate towards IDLE
  • N2 and NRO stabilize in normal range
  • FLI needles match
  • LAND AS SOON AS PRACTICABLE
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