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elitylski
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Systems controlled and monitored only by FCP
- Aux bat
- Man Fuel Bal L/R
- Environmental control system
- Parking brake
- Emer ldg gr handle
- PMU
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Systems controlled and monitored only by RCP
ISS
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Systems controlled by FCP and monitored by RCP
- Bleed air inflow (G-suit test)
- OBOGS
- Defog operation
- External lights
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Ejection command
BAILOUT, BAILOUT, BAILOUT!
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FEVER check
- Fluctuating fuel flow
- Excessive ITT
- Visual signals
- Erratic engine operations
- Roughness
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Power for Level flight 250 KIAS
93%
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Power for level flight 200 KIAS
50% + altitude
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Power for level flight 150 KIAS
32%
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Rotation airspeed
85 KIAS
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Rotation attitude
7-10° NH
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Pitch for 180 KIAS climb
9° NH
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Pitch for 160 KIAS climb
12.5° NH
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Pitch for 140 KIAS climb
17° NH
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Correct order of trim application
Rudder, elevator, aileron
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Turning tendency left yaw
Pitch up
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Turning tendency right yaw
Pitch down
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Turning tendency Pitch down
Left yaw
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Turning tendency Pitch up
Right yaw
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Lead point for rollout from shallow turn
5 degrees
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Lead point for rollout from steep turn
10 degrees
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Taxi speed limit in congested areas
5-7 KT (fast walk)
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Taxi speed limit in uncongested areas
15 KT
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Memory aid for takeoff/departure preparation while taxiing
- R-NEWS
- Check RAIM and FDE on STAT 2 page of GPS
- Set NAVAIDs/Needles for departure
- Review emergency actions for abort or engine failure on takeoff
- Weather/winds
- Standard Instrument Departure
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When to perform after landing checklist
- Normal taxi speed
- Clear of active RWY
- Return to parking without taking off
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When to perform lineup check
When taxiing onto the active RWY
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Lineup check
- TPPLAN
- TAS NORM
- Panel CWS shows normal lights
- Probes anti-ice on
- Lights on
- ALT select ALT on transponder
- NWS deselect after A/C aligned on RWY
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Static takeoff
- Align with RWY
- Disengage NWS
- Pump brakes
- PCL to 25-30%
- Check instruments
- Release brakes and advance PCL to MAX
- Check instruments when established at MAX power
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Rolling takeoff
- Align with RWY
- Disengage NWS
- Advance PCL to MAX
- Check instruments when established at MAX power
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When to retract gear and flaps after takeoff
- Safely airborne
- Positive climb
- Engine stabilized in MAX
- Engine instruments within limits
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Altitude to initiate climb check
10,000 MSL
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Clime gradient for 160 knot climb (12.5° NH)
1000 ft/NM
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Lead point for level-off
10% VSI
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Before traffic pattern entry technique
- GUTS check
- GPS set
- UHF/VHF set
- TAS set range
- Squawk appropriate code
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Landing parameters Flaps LDG
- Downwind torque 45%
- Final turn 110 KIAS
- Final turn torque 18%
- Final 100 KIAS
- Final torque 16-18%
- Touchdown target 80 KIAS
- Touchdown range 75-90 KIAS
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Crosswind limit for landing flaps
- 10 knots training
- 25 knots emergency
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Landing parameters Flaps TO
- Downwind torque 35%
- Final turn 115 KIAS
- Final turn torque 15%
- Final 105 KIAS
- Final torque 14-16%
- Touchdown target 85 KIAS
- Touchdown range 80-95 KIAS
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Landing parameters Flaps UP
- Downwind torque 30%
- Final turn 120 KIAS
- Final turn torque 12%
- Final 110 KIAS
- Final torque 12-14%
- Touchdown target 90 KIAS
- Touchdown range 85-100 KIAS
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Parameters for Initial
- Airspeed 200 KIAS
- Power 50% + altitude
- Altitude 1,000 AGL
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Parameters for Break
- Airspeed Slow from 200 KIAS to 120-150 KIAS
- Power approx 10%
- Break zone First 3,000 ft of RWY
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Break out from downwind
- Another A/C in final turn not in sight
- Straight in inside 2 miles not in sight
- ELP inside low key and spacing cant be maintained
- Pattern spacing cant be maintained with normal ground track
- Not configured by perch point
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Straight-in approach altitude
500 AGL before 5-mile point
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Straight-in approach when to configure
Prior to 2-mile point
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Lower nose gear to RWY below
80 KIAS
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Closed pullup power reduction
100 feet below pattern altitude for every 10 KIAS in excess of 140 KIAS
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ORM 3-2-1
- Do not descend below 2000 AGL unless:
- On profile for field of intended landing
- Runway in sight with ability to
- Maneuver to land
- 3 Final decision to continue or eject made 300 AGL
- 2 Gear confirmed down at 200 AGL
- 1 A/C on centerline at 100 AGL
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PEL checklist memory aid
- TCCC-BIP
- Turn, climb, clean, check
- Boost pump
- Ignition
- Plan
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2 methods for determine glide distance
- Half-DME plus Key gives required altitude to make a given APT
- Altitude method: (2xAGL)-Key, divide by 1000 for NM glide distance
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Altitude-airspeed exchange
10 knots can be traded for 100 feet
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Altitude loss for gliding 360° turns
- 30° bank: 2,000 feet
- 45° bank: 1,500 feet
- 60° bank: 1,000 feet
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Torque to simulate prop feather
4-6%
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Glide ratio no wind, clean, 125 KIAS, prop feathered
- 2 miles for every 1,000 feet lost (2:1)
- VSI 1,350-1,500 fpm
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Straight and level deceleration
0.1-0.2 NM for every 10 knots above 125 KIAS
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Altitude to terminate slip
300 AGL
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High Key parameters
- 3,000 AGL (2,500 min)
- 120 KIAS
- Gear down
- Flaps up
- 1/3 down runway
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Cross Key parameters
- 2,200 to 2,300 AGL
- 120 KIAS
- Gear down
- Flaps up
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Low Key parameters
- 1,500 AGL
- 120 KIAS
- Gear down
- Flaps TO (as required)
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Base Key Parameters
- 600 to 800 AGL
- 120 KIAS
- Gear down
- Flaps LDG (as required)
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SFL/PEL final approach speed Flaps LDG
110 KIAS
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High key adjustment for headwind
1,000 feet for every 10 knots of headwind
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