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89 Cards in this Set
- Front
- Back
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Aborted Take-Off
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1. Brakes.....apply
2. Throttles...idle 3. Speed brakes....extend 4. Thrust Reversers...as required |
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Engine Fire or Failure During Takeoff (Above V1)
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1. Positive Rate-of-Climb.....gear up.
2. Clear of Obstacles and V2+10....flaps up. 3. Continue climb......Venr. |
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Engine Failure During Coupled Approach
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1. Autopilot and Yaw Damper...Off
2. Airspeed...Vref+10 3. Flaps...Approach until landing is assured |
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Emergency Restart-Two Engines
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1. Altitude...Below FL350
2. Airspeed...200 knots minimum 3. Ingitions...On 4. Boost pumps...on 5. Throttles...Idle |
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Engine Fire
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1. Throttle....Idle
(if the light remains on) 2. Engine Fire Switch...Press 3. Either Fire Bottle Armed Light....Press |
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Fire, Smoke or Odor
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1. Oxygen Masks...Don and 100% or EMER
2. Oxygen Control Valve...Manual Drop 3. Oxgen Mic Switches...Mic Oxy Mask 4. Pass Oxygen...Ensure Passengers on Oxygen |
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Wheel Brake Failure
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1. Brake Pedals....feet off
2. Emer Brake Handle....Pull |
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Battery Overheat
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1. Amperage....check
2. Battery Switch...Emer 3. Amperage...note decrease |
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Rapid Decompression
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1. Oxygen Masks...Don and 100% Oxygen
2. Oxygen Control Valve...Manual Drop 3. Oxygen Mic Switches...Mic Oxy Mask 4. Press Source Selector...Emer 5. Pass Oxygen...Ensure Passengers on Oxygen 6. Emergency Descent (if required) ...Tab 8A |
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Emergency Descent
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1. AP/Trim disc....Press and release
2. Ignitions...On 3. Throttles...Idle 4. Speedbrakes...Extend 5. Airplane Pitch Attitude...(initially)...Target 20 degrees nose down 6. Descend at Maximum Airspeed...Vmo/Mmo (unless structural damage has occured) |
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Autopilot Hardover
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Autopilot/Trim Disengage Switch....Press
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Elevator Trim Runaway
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1. Autopilot/Trim Disengage Switch....Press and hold
2. Pitch Trim CB (LH CB Panel)....Pull 3. Autopilot/Trim Disengage Switch...Release 4. Manual Elevator Trim...Trim as required |
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Thrust Reverser Deploy During Takeoff
Above V1 |
1. Emer Stow Switch (Affected Engine) ...Emer
2. Positive Rate-of-climb...Gear Up 3. Clear of Obstacles and V2+10...Flaps Up 4. Airspeed (until stowed)...125 KIAS max |
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Thrust Reverser Deploy In Flight
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1. Control Wheel/Autopilot...Grip/Disengage
2. Emer Stow Switch (Affected Engine)...Emer 3. Airspeed (Until Stowed)...125 KIAS max |
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Thrust Reverser Unlock Light On Inflight
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1. Emer Stow Switch...Emer
2. Thrust Reverser Levers...Full forward |
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Emergency Evacuation
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1. Parking Brake...Set
2. Throttles...cutoff 3. Engine Fire Switches (if required)...Press 4. Fire Bottle Armed Switches (if required)...Press 5. Battery Switch...Off 6 Evacuate...Safest Exit |
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Vmo
Below 8,000 feet |
261
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Mmo
8,000 feet to 29,315 feet |
276
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Mmo
Above Vmo altitude |
721
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Turbulent Air Penetration
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180
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Max speed for flaps to 20 degrees
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200
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Max speed for flaps beyond 20 degrees
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172
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Vlo and Vle
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172
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Speed Brake Extension
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No limit
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Vmca
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83
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Vmcg
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73
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Maximum tire speed
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165
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N1 Fan Take off and Max Continuous
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106%
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N2 Turbine Take off and Max Continuous
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97%
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N2 Turbine Idle Flight
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49%
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Take off ITT
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710 degrees Celsius
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Starting ITT
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700 degrees Celsius for 2 seconds maximum
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Thrust reverser limitations
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Reverse thrust power reduced to idle by 60 knots
Maximum allowable thrust reverser deploy time...15 minutes in any 1 hour Engine static ground operation T/R deployed....idle power |
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Starter limits
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3 engine starts in 30 minutes with a 60 second rest period between start attempts
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Max Ramp Weight
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15,300 lbs
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Max Takeoff Weight
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15,100 lbs
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Max Landing Weight
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14,400 lbs
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Max Zero Fuel Weight
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11,200 lbs
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Max altitude for takeoff and landing
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14,000 feet
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Max temperature for takeoff and landing
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ISA + 39 degrees Celsius
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Max Water/Slush on the runway
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one half inch
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Max Tailwind component for takeoff and landing
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10 knots
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Max crosswind component with Thrust Reverser Deployed
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25 knots
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Max crosswind component withOUT Thrust Reverser deployed
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29 knots
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Prolonged Ground Operations
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Continuous engine ground static operation upt o and including five minutes at takeoff thrust is limited to ambient temperatures not to exeed ISA + 39 degrees Celsius
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Pitot heat ground operation limitation
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two minutes
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Maximum operating altitude
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43,000 feet
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Max generator load
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300 amps
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Max fuel imbalance
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200 lbs (600 lbs in emergency)
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Maneuving check
ICCEY |
Ignitions-ON
Compute -Airspeed bugs set to Vref for actual aircraft weight Compute-climb power setting for altitude and temp Engine Sync-Off Yaw damper-Off |
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Squat switch inputs-left main
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In flight-enables flight hour meter, digital clock, opens emergency pressurization valve, landing gear handle locking solenoid to be energized (unlocked
On the ground, enables: pressurization solenoid valve to open the outflow valves, gnerator-assisted starts, ground valve to open, pretakeoff pressurization, antiskid locekd wheel protection |
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Squat switch inputs-left and right main in parallel
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In flight, stick-shaker operation, thrust reverser deployment, stick shaker test
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Emergency bus items
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Comm 1
Nav 2 Copilot HSI Cockpit floodlights Voltmeter Emergency exit lights ELT Pilots airspeed Pilots IVSI Copilots airspeed Copilots altimeter Copilots IVSI Windshield bleed air Rain doors Auxiliary gear control Emergency brake Pressurization controller Manual dump valve Cabin altitude/differential pressure indicator Cabin VSI Oxygen pressure gauge Passenger oxygen valve Magnetic compass JET standby attitude indicator N1 tape copilots air-driven gyro and gage Pressurization sources fail to NORMAL Mechanical clock Engine bleed-air anti ice |
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Hot battery bus
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Emergency exist floodlight
Entrance door floodlight Aft baggage light Tail cone light Nose baggage compartment Voltmeter Ignition (start only) Optional ELT |
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Engine make and thrust
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Pratt and Whitney JT15D-4B
2,500 lb. of thrust |
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Oil capacity
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2.08 gallons
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Fuel capacity
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862 gallons
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Landing gear warning horn sounds when...
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Either throttle is less than 70% N2 and the speed is below 150 knots, or the flaps are beyond approach, or the rotary test is in the LDG GEAR position
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Maximum differential cabin pressure
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8.8 psi
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Vacuum controls the _______ system
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Pressurization
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-------is required to be added to the fuel.
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Prist
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To trim the aircraft, the ______must be turned off.
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Yaw damper, autopilot.
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Any thrust reverserver arm or unlock lock activates the
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Master Warning light
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Losing a 225 amp limiter turns on the _____________ light.
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Master Warning
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Loss of one half the power from one side turns on the _______ _______light on the other side.
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Master Warning
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N1 is ________
N2 is _________ |
Performance
Systems |
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There are ______T1 probes
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two
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Max continuous power on one engine time limit
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10 minutes
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210 F causes the _______in the fire extinguisher bottle to go.
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plug
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A good battery should supply power to the hot battery bus and the emergency bus for approximately ____minutes
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30
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The battery bus serves as a ____tie bus.
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generator
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In flight, with the generators on the line, the battery is isolated from any charging source when the battery switch is in either
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Off or EMER
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If manual termination of a start sequence is desired, the swith to press is
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starter disengage
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The voltage read on the voltmeter with the selector switch in BATT is sensed from the
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hot battery bus
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If the generators are not operating, the voltmeter reads battery voltage when the battery switch is in
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BATT or EMER
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The light in each engine start button illuminates to indicate
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closing of the start relay
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The generator field relay opens when (3 things)
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1. an internal feeder fault is sensed
2. an overvoltage condition is sensed 3. an engine fire switch is activated |
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If a battery start is intended, the generator switches should be placed to
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GEN
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When the inverter switch is positioned to AC, normally
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each inverter supplies its own AC buses
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Illumination of the AC FAIL annunciator light and the Master Warning lights indicate
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Failure of both inverters
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Positioning the inverter test switch to the INV 1 position disables
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the No. 1 inverter
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With the battery as the only source of power and the battery switch in the OFF position, the bus(es) powered are:
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Hot battery bus
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With the battery as the only source of power and the battery switch in the EMER position, the following bus(es) are powered:
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emergency and hot batter bus
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With the battery as the only source of power and the battery switch in the BATT position, the following condition exists:
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All DC buses are powered
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With only the hot battery and the emergency buses powered, the following item is inoperative:
1. Nav 1 2. Cockpit floodlights, emergency exit light 3. copilot's compass system, Com 1 4. Nav 2 |
Nav 1
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Regarding the engine starting sequence (battery start) it is normally terminated by
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the speed sensing switch on the starter-generator
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An annunciator panel light will extinguished when the malfunction
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is corrected
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The master warning lights illuminate when a ____annunciator panel light illuminates or when ______ GEN OFF lights illuminate
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red, both
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The rotary test switch illuminates all annunciators in the ANNU position except
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Battery overtemp
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