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Engine Failure Below V1
Abort
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Engine Failure Above V1
Climb to a safe altitude
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Engine Fire
- Throttle idle
- Illuminated switch lift cover and push
- Either armed bottle push
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Engine Failure During Final Approach
- AP disconnect
- Increase thrust
- Vapp or more
- Flaps approach
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Emergency Restart 2 Engines
- Igniters
- Pumps
- Throttles idle
-
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TR Deploy In Flight
- Grip control wheel
- AP off
- Emer stow
- Throttle check idle
- Slow to 150
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TR Unlock In Flight
Emer stow
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Cabin Decompression
- Mask on 100%
- Mask mic
- Emergency descent as required
-
Emergency Descent
- AP off
- Throttles idle
- Speed brakes
- Pitch 20 degrees
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Environmental System Smoke or Odor
-
-
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Batt O Temp
- Note amps
- Emer
- Note amp drop
-
-
-
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Emergency Evacuation
- Parking brake
- Throttles off
- Engine fire buttons
- Blow bottles if fire suspected
- Pax Safety lights
- Batt off
-
-
-
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Fuel Limits Config AL
- Minimum fuel is 500 per side
- No X-Feed in descent
- Fuel imbalance 200 max
-
Fuel Limits Configuration AM
- Pumps on when low fuel light (180 +- 20 lbs)
- Max fuel imbalance 200
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Starter Limit
3 in 30 minutes with 90 seconds in between
-
Battery Start Limit
- 3 per hour
- If limit exceeded deep cycle and capacity check required
-
3 cross starts = how many battery starts
1
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Takeoff Thrust Limit on the Ground
5 minutes
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Pitot Static Limits on Ground
- 2 minutes on
- 2 minutes off
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Electrical Limit on Ground
- 125 amps in low idle
- 225 amps in high idle
- Transient 300 amps for 4 minutes
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Unusable Fuel
Fuel in the tanks when gauge reads zero
-
Max Operating Limit Speeds
- Mmo .755 Mach
- Vmo 292 above 8000, 262 below 8000
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Flap Speeds
- 200 for takeoff and approach
- 173 for full
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Gear Speeds
- 250 to drop and fly around
- 200 to raise
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Max TO and Land Altitude
14000
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-
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Max Water/Slush on Runway
1/2 inch
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Land On Grass or Gravel
No
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Takeoff With Anti Skid Inop
Prohibited
-
Takeoff With Frost Prohibited With Frost On
- Leading edge
- Upper wing surface
- Windshield
-
Takeoff With Ice, Snow, Slush Prohibited
- Leading edge
- Upper wing surface
- Flight control surfaces and hinge gaps
- Engine inlets
- Stabilizer
- Top of engine pylons
- Top of fuselage
- Windshield
- AOA vane
- Static ports
- Upper surface of nose
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Visual/Tactile check of wing required when Temps below 50F and any of the following
- Visible moisture
- Water presrnt on upper wing
- Dew point spread 3C or less
- Atmospheric conditions conducive to frost
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AP with comparison monitor illuminated
Prohibited
-
AP altitudes
- 1000 AGL entoute
- 300 non precision
- 180 ILS
-
Anti ice on when
- Visible moisture
- Temps at or below 10C
-
Tail de ice when
- Visible moisture
- Temps between 10C and -35C
-
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Generator load limits in flight
- 225 amps at idle
- 300 amps with power
-
Boundary Layer Energizers
- 16 per wing
- All must be present
-
Cabin press limits
- 0 to 9 psi
- Depressurize for takeoff and landing
-
EFIS ground operation with NOSE AVN FAN annunciator
30 minutes
-
Takeoff into IMC with NOSE AVN FAN
Prohibited
-
Dispatch in VMC with NOSE AVN FAN
Allowed as long as NOSE AVN FAN ILLUMINATED ON GROUND checklist is followed
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Takeoff With IC HOT illuminated
Prohibited
-
Takeoff With PFD reverted
Prohibited
-
Dual PFD SG reversion to MFD
Prohibited
-
VOR NAV FD when changing VOR frequency
Must go to HDG first
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Masks not approved above
40000' cabin altitude
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Prolonged operation of pax masks above 25000
Not recommended
-
To qualify as quick donning mask
Must be stowed in container
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Cold soak period
2 hours at -10C or colder
-
Cabin temp must be at 0 degrees C for how long if cold soaked
- 15 minutes for flight above FL250
- This ensures proper operation of pax oxygen masks
-
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Max TR power limit
- 71.4 N1 above -18C
- 68.3 N1 below-18C
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Max TR time
3 minutes in 10 minutes
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Ground idle switch and touch and go
Must be in high idle
-
Is emer door connected to annunciator panel?
No
-
25 volt battery provides how many volts for engine start?
24
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What are the 3 positions of the battery switch?
- BATT batt relay closed
- OFF batt relay open
- EMER batt relay open, emer relay connects to hot battery bus
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What switch position should batt be in to charge batt with gpu?
Any position
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What are the 3 positions of the GEN switches?
GEN gcu closes power relay connects GEN to its feed bus
OFF opens power relay removing power from bus
RESET sends signal to GCU to close the field relay
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3 major functions of GCU
- Regulate 30VDC down to 28.5VDC
- Parallel generators to within 10% of load
- Protect generators and elec system
-
GCU relays
Power relay for under voltage or reverse current
Field relay for over voltage, feeder fault or fire switch
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Items on hot batt bus
- (L) Lights (nose, entrance, tail bag)
- (O) Oil chip detector
- (V) Volt meter ( with BATT in BATT)
- (E) Emer items (ELT test, emer bus if in emer, emer BATT pack)
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Emer power in flight
In BATT emer bus powered thru xfeed bus (10 min)
In EMER power from hot batt bus (30 min)
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Emer bus items
- N1 tapes
- Comm 1
- Nav 1
- DG 1
- RMU 1
- Stdby pitot static heat
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Does the battery disconnect switch require DC power to function?
Yes....that's why the batt switch must be in batt
-
What supplies AC power?
2 each 250V inverters
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Where are taxi lights?
On the gear
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Where is the emergency lighting battery pack?
In the floor opposite the stairs
-
What charges the emergency battery pack?
Either generator
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What causes master warning?
- Any red annunciator
- Dual generator failure
- TR arm or unlock in flight
-
What causes master caution?
- Any Amber annunciator
- GND IDLE in flight
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Fuel capacity
5440 lbs (806 gallons)
-
When does fuel lo level come on?
180 lbs +- 20
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Boost pump positions
- ON is on
- OFF pump cannot be activated
- NORM is off unless start, xfeed, or lo fuel press
-
Xfeed sequence
- Pump on
- Xfeed valves open
- 3 second delay
- Motive flow closes
-
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Accessory gearbox has
- Oil pump
- Fuel pump
- Starter generator
- Hydraulic pump
-
Do you need prist?
No because fuel-oil heat exchanger
-
When does lo oil press illuminate?
20 psi
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Abort start when
- No ignition 10 seconds after moving throttle
- ITT rapid rise
- No idle in 30 seconds after moving throttle
- No N1 by 25% N2
-
How many amps before pushing 2nd starter button?
200
-
Pushing fire button causes
- Arm both bottles
- Fuel cutoff
- Hydraulic cutoff
- Open field relay
- Disable TR
-
Tailcone fire
Fuse plus on each bottle melts discharging contents into tailcone. No cockpit indication.
-
Pylon precoolers
Use bypass air to regilate air for use by various systems
-
BLD AIR O'HEAT means
Bleed air from precooler exceeds limits
-
All anti ice valves fail open except
Wing crossflow
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Emer press in these 3 conditions
- Emer selected
- Cabin altitude exceeds 14500
- ACM O'HEAT occurs if flight
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In emer press are the normal flow control valves open or closed?
Closed
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DC power loss which way do flow control valves and emer press valves fail?
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Max differential
8.9 +- 0.1
-
Cabin limit valves limit cabin to
13000 +-1500
-
If automatic pressurization fails how can you control pressurization?
Manual toggle switch
-
Does cherry picker require electrical power?
No
-
CAB ALT illuminates when
10000, or 14500 if in high altitude mode and below FL245
Any time cabin altitude exceeds 10000 above FL245
-
What does pressurization controller require?
-
Max cabin altitude at FL450
7800
-
What hydraulically operated systems do you lose with DC power failure?
-
Can you operate the gear on the emer bus?
Yes
-
Gear horn goes off when
Throttle below 70 N2 and speed bow 150 with gear not locked
Flaps beyond 15 and gear not locked - cannot be silenced
-
Can you have asymmetrical flaps?
No because of mechanical interconnection
-
Hydraulic failure and flaps extended
They stay extended unless flap handle is moved
-
Electrical failure with speed brakes extended
They trail
-
Hydraulic failure with speed brakes extended
They stay extended unless retracted or throttle advance beyond 85 N2
-
EROS masks are limited to what cabin altitude?
40000
-
Pax o2 masks are limited to what cabin altitude?
25000
-
Tail de ice temps
- Airspeed below 150 -40C
- Airspeed above 150 -35C
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