Preflight 1 Flashcards

1
Q

Before Exterior Inspection

A

1) Ensure all locking pins are removed from doors and hatches.
2) Ensure Defensive System Safety Pins are installed.
3) Check 781s and ensure all airplane switches are in their normal shutdown positions.
4) Ensure Fuel Vents are Free of Obstructions
5) Must be done before any electrical power is supplied.

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2
Q

Exterior Inspection

A

1) The exterior structure of the plane
2) Radiation hazard Exists at the SPEAR Pods during operation and BIT Check.
3) Radiation hazard exists at the mid high and low band transmit antennas during transmit mode.
4) Avoid DF antennas while transmitting.
5) Start the Walk Around in a clockwise manner starting at crew entrance door.
6) Pilot can wave the inspection if high winds, slippery or other hazardous conditions.

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3
Q

Before Starting Engines Checklist

A

1) Check Set Oxygen System, Flight Publications individual lights and clocks prior to initiating checklist.
2) Pilot and Copilot will set HOT MIC TALK< LISTEN ON
3) Quick Don oxygen mask system is the primary use equipment unless dictated otherwise.
4) Suction Boost Pumps - if inoperative can damage engine driven hydraulic pump

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4
Q

Starting Engines Checklist

A

1) Normal Start Sequence 3, 4, 2, 1.
2) if a malfunction exists - expect to hear “STOP START” followed by a description.
3) During Start engine should accelerate smoothly and continuously.

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5
Q

If you see a Prop Low Oil Light during Engine Start?

A

1) Place Condition to Ground Stop
2) DO NO FEATHER THE ENGINE
3) Do not move condition level from position until engine rotation has stopped.
4) Follow Starting engine start limits.

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6
Q

How fast should the Engine stabilize on speed?

A

1) In 60 seconds or less
2) If Low density altitude or high temperature 28 deg C or in high altitude - its 70 seconds.
3) Whenever you engage the starter … its the same as holding it for 60 seconds.

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7
Q

NO Engine Rotation

A

1) You have 5 seconds
2) Stop Start
3) Ground Idle - Ground Stop - Release Starter

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8
Q

Ignition by when?

A

1) 35% RPM

2) Motor Engine until 25% RPM

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9
Q

1) Engine does not accelerate smoothly to ground idle RPM

or

2) Rapid Increase in TIT is indicated

A

1) Stalled Start
2) STOP START
3) Ground Idle and Ground Stop
4) Motor Engine until 25% RPM
5) Wait for TIT to drop below 200 before starting and follow starter limits

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10
Q

Start Sequence

A

1) RPM Indication
2) Fuel Flow
3) Ignition
4) Oil Pressure
5) Hydraulic Pressure
6) Parallel
7) Starter
8) Series
9) Peak TIT

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11
Q

1) RPM means what?
2) Fuel Flow means what?
3) Ignition means what?

A

1) An indication on RPM instrument
2) Indication of Fuel Flow towards 300 PPH. Note: If enrichment is on then fuel flow will spike above 300 PPH then rapidly decrease to 300 PPH.
3) Should Immediately follow fuel flow and occur by 35%

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12
Q

1) Oil Pressure Mans what?
2) Hydraulic Pressure menas what?
3) Parallel Means what?

A

1) Positive Oil Pressure (Both engine and gearbox) must be indicated by 35% RPM
2) Should be observed after observation of oil pressure. Must have a positive indication by engine on speed. Normal 30 seconds after on speed.
3) Indicated by secondary fuel pump pressure light on by 65% RPM.

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13
Q

1) Starter Means what?
2) Series Means what?
3) Peak TIT means what?

A

1) Release the engine ground start switch at 60% RPM.
2) Indicated by secondary fuel pump pressure light going out. Also oby drop in TIT at 65%
3) Observe max tit rise - disregard overshoot at 94%.

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14
Q

Before Taxi

A

1) If you can’t check your navaids or Instruments its ok… as long as they are all checked prior to BEFORE TAKEOFF CHECKLIST.
2) Recommended that Oil Cooler augmentation off during operations with all 4 in Low Speed Ground Idle.
3) Do not downspeed engines when taxi speed, wind or combination of two exceeds 30 Knots.
4) 20 knots is max speed for taxi on hard surfaces.
5) If stopped in the turn - record in 781. If stopped taxi 5 feet forward to re-align the main gear.
6) in 30 knot winds at 90 degrees - nose wheel steering can overcome crosswinds.
7) In 60 knot winds at 90 degrees - nose wheel steering, rudder, aileron, differential power and differential braking can overcome crosswinds.

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15
Q

Reverse Taxi

A

1) Make sure the area is clear
2) Make sure you only reverse Symmetrical
3) Oil temp is critical during reverse taxi - make sure to monitor.
4) Taxi airplane forward 5 feet to re-align the main landing gear.
5)

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16
Q

Plane Dimensions

A

1) 169 Feet 8 inches - wing span

2) 38 Feet - vertical stab

17
Q

Take-Off

A

1) If FF, Torque, or TIT are not similar above crossover - PROP ISSUE EXISTs
2) if FF Torque or TIT are not similar - Perform Temp Control Check.
3) Nose wheel steering is required to continue a take-off after engine failure.
4) A rolling take-off is preferred if TOLD permits.
5) Smooth take off - rotate 5 knots below take-off speed.
6) The pilot monitoring will monitor instruments and adjust throttles to assure proper take-off power.

18
Q

Instrument Take-Off

A

1) Set The flight Director System indicators.
2) Align horizon bar on ADI with Wings of miniature airplane.
3) Set Departure course on the HSI (a. Set heading marker to the most logical position. b. Check HSI and RMI to ensure indicators are correct. c. Flight director switch manual and nav aid for the departure).

4) Align Airplane on the runway - use nose wheel steering until rudder control becomes effective.
5) 5 knots before take-off speed rotate and establish 7 degree nose up attitude on the ADI.
6) Establish a definite climb and indicated by altimeter and VSI. Then retract the gear.
7) Retract the flaps after the plane accelerates to take-off speed +20.
8) Climb out at 4 engine climb speed.

19
Q

Escape Maneuvers

A

1) Departure/Approach.
- Immediately and simultaneously rotate the airplane to at least 7 degrees pitch up.
- roll wigs level
- add maximum power
- continue until warning ceases.

  • If flaps up - no less than flaps up approach speed.
  • if Flaps 100/50 - no less than obstacle clearance.

2) Enroute
- immediately and simultaneously rotate 7 degrees pitch up.
- roll wings level adn add max power
- continue until warning has ceased.
- Rotate the airplane to maintain a max climb angle.

  • Flaps up - no less than 160.
  • Flaps 50/100 - no slower than 130.
  • Do not delay pull up for diagnosis of the low altitude warning.
  • Flaps 100 - consider raising the flaps to 50 percent once a positive rate of climb is established and appropriate airspeed exists. Consider lowering the flaps to 50 percent to increase lift and the stall margin.
20
Q

Wind shear on take-off

A

1) Maintain Obstacle Clearance Speed with max power.
2) Keep until out of shear condition.

3) If wind shear occurs immediate after takeoff - Ground impact is a concern - Target Max Effort Obstacle Clearance Speed ( 10 below obstacle clearance speed).

21
Q

Penetrations

A

1) Before reaching initial approach fix begin the descent checklist
2) Flight Idle and smoothly establish descent at least 4,000 FPM
3) Follow the published penetration procedure
4) Start level off 1,000 feet above the published minimum. Establish 170 Knots at the published minimum inbound altitude.
5) Complete the before landing checklist prior to reaching final approach fix.

22
Q

Landing

A

1) If Landing performance is critical - use max reverse thrust, max anti skid braking
2) At high true airspeeds and/or high ambient conditions with the throttles at flight idle - abrupt movement of the throttles into the ground range could result in pitchlock.
3) If Flaps are less than 70%, landing gear warning may not occur in time to warn aircrew that the landing gear is not down and preclude a gear-up touchdown.

4) Retarding the throttles below flight IDLE at airspeeds above 115 Knots could result in power-loss on one or more engines.
- Refers to flight idle to maximum reverse in less than 1 second.
- if this occurs maintenance action is required.

23
Q

WInd Shear

A

1) An unusually steep or shallow rate of descent required to maintain glidepath.
2) An unusually high or low power setting required to maintain approach speed.
3) A large variation between reported surface wind and displayed winds on final approach.

24
Q

Wind Shear Decreasing headwind

A

1) Add power and increase pitch to regain the proper glidepath.
2) Once speed and glidepath are regained - prompt reduction of power is necessary.
3) It will now require less power and greater rate of descent to maintain profile.

25
Q

Wind Shear Increasing Headwind

A

1) Use 50 percent flaps for landing
2) Crosscheck/monitor ground speed
3) minimize power changes, especially large power reductions
4) use the flight director to maximum extent possible.

26
Q

Define Severe Windshear

A

1) +/- 15 knots airspeed
2) +/- 500 FPM altitude change
3) +/- degrees pitch attitude change
4) +/- 2.5 dot glideslope deviation
5) unusual power requirements for an extended period of time.

27
Q

Wind Shear Recovery

A

1) Announce a go-around
2) Set maximum power (if you are going to touch down then target threshold speed)
3) copilot monitor and call sink rate and airspeed.
4) Navigator engineer monitor Radar altimeter
5) If 100 flap landing - go to 50 flap landing - never get slower than obstacle clearance.
6) Do not retract landing gear until recovery is complete with two positive rates.
7) when clear of wind shear - adjust pitch and power.
8) When conditions permit report the encounter with ATC.

28
Q

Crosswind landings

A

1) Upwind wing has a tendency to rise when reverse thrust is applied.
2) If flaps are 100 - move to 50 before applying reverse thrust.

29
Q

After Landing

A

1) Do not downspeed the engines when taxi speed, wind or combination of two exceeds 30 knots.
2) Engine shutdown should not be accomplished when taxi speed, wind velocity is greater than 20 knots.
3) It recommended that engines be run a minimum of 2 minutes in low speed ground idle before shutdown.

4) Oil cooler augmentation be placed to OFF.
- keep oil in limits - but preference is for them to be off before shutdown.