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Hawker 400XP/BJet 400A > Flight Safety Rev2/2011 > Flashcards

Flight Safety Rev2/2011 Flashcards

1
Q

Engine Failure During Takeoff
(Below V1-Takeoff Aborted)

A
  1. Brakes. Apply
  2. Thrust. IDLE
  3. Thrust Revers. Deploy
  4. Rev Lights. Verify
  5. Revrse. Thrust. As Req.
  6. Speed Brakes. Extend
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2
Q

Engine Failure During Takeoff
(Above V1-Takeoff Continue)

A
  1. Nose Up Pitch @ (VR).
    13-15 degrees
  2. Landing Gear UP
    (When Positive Rate)
  3. Airspeed. V2
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3
Q

Engine Fire - Bell Sounds
LFT or RT Engine Fire Push
Illuminates!

A
  1. Thrust (affectd Eng).
    IDLE
    *If Engine Fire Push Still Illuminated * Then
  2. Thrust Lvr Affected ENg
    CUTOFF
  3. Illuminated Fire SW
    PUSH
  4. Either Fire Bottle Switch
    PUSH
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4
Q

Engine Fire Detector Failure
Left or Right Fire Det Fail Light illuminated

A

If the Fire Det Fail annunc. Illuminates following an engine fire push SW illumination, the fire should be considered to still be burning.

  1. Engine Fire Proced.
    Complete Chck List
  2. Remaining Fire Bottle SW
    PUSH
  3. Land
    Nearest Suitable Airport
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5
Q

IF Engine FIRE Det Fail
Annunciation illuminates without an ENG FIRE Push SW illumination or Anyother indication of an engine fire:

A

Repair Fault prior to the next flight.

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6
Q

Engine Failure in Landing Configuration

A
  1. Thrust (operating eng)
    As Required
  2. Airspeed
    VREF
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7
Q

Dual Engine Flameout

A

Immediate Relight
1. N2 Verify ABV 52%

Caution: Engine Damage may result if an immediate relight is attempted BELOW 52% N2

  1. Ignitions ON
    IF N2 is Not ABV 52% or neither engine delights then:
  2. Battery. EMER
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8
Q

Inadvertent Thrust REV
Deployment During T/O
(Below V1 - Takeoff Abort)

   L TR ARM.   R TR ARM
   UNLOCK.     UNLOCK
   DEPLOY.       DEPLOY
                    OR
A
  1. Brakes. Apply
  2. Thrust. IDLE
  3. T/R’s. Both Deploy
  4. Rev Lights. Verify
  5. Rev. Thrust. As Required
  6. Speed Brakes. Extend
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9
Q

Inadvertent T/R Deployment
During Takeoff
(Above V1- Takeoff Cont.)

Unlock. Unlock
Deploy. OR. Deploy

L TR PUSH. R TR PUSH
EMER STOW. EMER STOW
OR

A
  1. Emer Stow Affected Eng
    PUSH
  2. Nose Up Pitch Attitude @ VR Rotation
    13-15. Degrees
  3. Landing Gear
    When positive Rate:
    UP
  4. Airspeed
    V2 Min
    IF T/R Will Not Stow and lock
  5. T/R. Affected Engjne
    CUTOFF
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10
Q

Inadvertent T/R Deployment
IN a FLIGHT

Unlock. Unlock
Deploy. OR. Deploy

L TR PUSH. R TR PUSH
EMER STOW. EMER STOW
OR

A
  1. Emer Stow Push Switch
    Affected ENG
    PUSH
  2. Altitude
    Below 30k Feet
  3. Airspeed
    Until TR stows and locks
    Below 135 KIAS
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11
Q

Inadvertent Overspeed

A
  1. Thrust IDLE
  2. Speed Brakes. Extend
  3. IF acft is in nose down attitude initiate a wings level pull-up without exceeding structural limits. (3.2G)
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12
Q

Loss of Airspeed Indication

A
  1. Autopilot. Disconnect
  2. Airspeed. Slow to Maintain 0.2 AOA.
  3. Thrust. As Req.
  4. Speed Brakes. As Req.

Slow to 0.25 AOA w Speed. Takes Extended.

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13
Q

Electrical Fire or Smoke

A
  1. Oxygen masks
    Don
  2. Smoke Goggles
    Don
  3. Mic Selectors
    Oxy Mask
  4. SPKR Switches (PIC & SIC)
    ON or Don Headset
  5. Interphone SW Pilot
    ON
  6. Smoke Removl Procedures
    OF Needed
  7. Faulted Circuits
    Isolate
  8. Battery
    EMER
  9. Master Gen SWITCHES
    EMER
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14
Q

Environmental system smoke or odor

A
  1. Oxygen masks
    Don
  2. Smoke Goggles
    Don
  3. Mic Selectors
    Oxy Mask
    . SPKR Switches (PIC & SIC)
    ON or Don Headset
  4. INTPH SW Pilot
    ON
  5. Cabin Pressure Source
    Isolate SEL L ENG or R ENG
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15
Q

Smoke Removal

A

Oxygen masks
Don
2. Smoke Goggles
Don
3. Mic Selectors
Oxy Mask
4. SPKR Switches (PIC & SIC)
ON or Don Headset
5. INTPH SW Pilot
ON
6. Checklist

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16
Q

Cabin Decompression

A
  1. Oxygen masks
    Don
  2. Smoke Goggles
    Don
  3. Mic Selectors
    Oxy Mask
  4. SPKR Switches (PIC & SIC)
    ON or Don Headset
  5. INTPH SW Pilot
    ON
  6. Decompression chck list
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17
Q

Emergency Descent

A
  1. Thrust
    Idle
  2. Speed Brakes
    Extend
  3. Autopilot
    OFF
  4. Initiate Moderate Bank
    45 degree Bank
  5. Descend to 10,000 ft or Min Safe Alt.
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18
Q

Overpressurization

A
  1. Cabin Pressure Source
    OFF
  2. Oxygen masks
    Don
  3. Mic Selectors
    Oxy Mask
  4. SPKR Switches (PIC & SIC)
    ON or Don Headset
  5. INTPH SW Pilot
    ON
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19
Q

Loss BOTH Generators

L GEN OFF. And. R GEN OFF

A
  1. Gen FLD and START/GEN CB’s - Aft Main Panel
    CHECK
  2. Generator Reset L & R
    Reset/Norm
20
Q

Pitch Trim Runaway or Failure!
Roll Trim Runaway or
Failure!
Rudder Trim Runaway or
Failure!

A
  1. Trim Interrupt/AP Disengage Switch
    PUSH & HOLD
21
Q

Power Brake Failure

A
  1. Emergency Brake Handle.
    Break Safety Wire and remove guard clip.
  2. Emergency Brakes
    Apply Gradually
22
Q

Autopilot Trim Fail

AP PITCH
 TRIM FAIL

AP ROLL
TRIM FAIL
A
  1. Trim Indicators
    Check for proper position for flight condition.
  2. Trim interrupt/AP Disengage Switch
    PUSH
23
Q

Autopilot Overspeed Recovery

A
  1. Thrust
    IDLE
24
Q

Flight Director Malfunctions

A
  1. Trim interrupt/AP Disengage Switch
    PUSH
25
Q

Maximum Operating Airspeed

A

VMO S.L to 8,000 Ft.
264

VMO 8,000 to 11,000 Ft.
264 to 320 linear Variatn

VMO 11,000 to 26,000 Ft.
320

Limiting Mach Mmo ABV
26,000 ft
0.78

26
Q

Flap Extension and Operation
VFE/VFO. Flaps 10 and 20
VFO Flaps 30 degrees
VFE Flaps 30 degrees

A
  1. VFE/VFO Flaps 10 & 20
    200
  2. VFO Flaps 30
    170
  3. VFE Flaps. 30
    165
27
Q

Landing Gear & Lights

Landing Gear Normal VLO
Landing Gear Ext VLE
Landing Gear Emer VLO
Landing Lights VLL

A

Landing Gear Normal VLO
200
Landing Gear Ext VLE
200
Landing Gear Emer VLO
150
landing Lights. VLL
200

28
Q

SpeedBrakes Ext & Ops

VSB

A

VSB
NO LIMIT

29
Q

Minimum Controllable Airspeed
Airborne & Ground

Airborne Vmca Flaps 0
Airborne Vmca Flaps 10&20
Ground. Vmcg. Flaps 0,10,20

A

Airborne Vmca Flaps 0
96
Airborne Vmca Flaps 10&20
89
Ground. Vmcg. Flaps 0,10,20
88

30
Q

Windshield Wipers

Vww

A

Vww
200
(If Installed)

31
Q

Tire Limiting Speed

V tire

A

V tire
165
True speed on the ground

32
Q

Engine Speeds

Takeoff N1 Fan
Takeoff N2 Turbine
Idle N2 Turbine, Engine EFC ON
Idle N2 Turbine, Engine EFC OFF (in non icing condition)

A

Engine Speeds

Takeoff N1 Fan
104%
Takeoff N2 Turbine
96%
Idle N2 Turbine, Engine EFC ON
52%
Idle N2 Turbine, Engine EFC OFF (in non icing condition)
46%

33
Q

Engine Temperatures

Takeoff ITT
Starting ITT
ITT for maximum continuous thrust

A

Takeoff ITT
700 C
Starting ITT
550c to 600c for 4 Sec Max
600c to 700c for 2 Sec Max

ITT for maximum continuous thrust
680c

34
Q

Engine Oil

Oil Temp takeoff and max continuous thrust
Oil Pressure takeoff and max continuous thrust
Minimum oil temperature for Starting
Oil pressure at idle RPM

A

Oil Temp takeoff and max continuous thrust
10 to 121 c
Oil Pressure takeoff and max continuous thrust
60 to 83 PSI
Minimum oil temperature for Starting
-40 c
Oil pressure at idle RPM
40 PSI minimum

35
Q

Thrust Reverser Limitations

Full Reverse Cutoff Speed

Time for Continuous Rev Thrust above reverse idle

Deployed Time during taxi operations

A

Thrust Reverser Limitations

Full Reverse Cutoff Speed
55 KIAS or above
Time for Continuous Rev Thrust above reverse idle
30. SECs Max
Deployed Time during taxi operations
5. Seconds

36
Q

External Power Assisted Start
Limited to three (3) cycles as follows:
Secs ON. Mins OFF
1st Cyc:
2nd CYC:
3rd CYC:

A

Secs ON. Mins OFF
1st Cyc: 30. 5
2nd CYC: 30. 15
3rd CYC: 30. 60

37
Q

Battery Start

Do not attempt battery start if battery voltage is below____volts.

38
Q

Generator Assisted Start

Do not attempt to start the second engine until the generator load is below _____AMPS.

39
Q

Starter Generator Limits

Ground Operation

Max Generator Load

A

Starter Generator Limits

Ground Operation

Max Generator Load

280 AMPS Each Generator

40
Q

Starter Generator Limits

In flight Operation
Both Generators Operating Up to 41,000 ft _____
Both Generator’s Operating Above 41,000 ft.______

A

In flight Operation
Both Generators Operating Up to 41,000 ft _280 AMPS

Both Generator’s Operating Above 41,000 ft _260 AMPS

41
Q

Limitations

In Flight Operation:
One Gen Operating Up to 29,000 ft.

One Generator Operating Up to 29,000 ft Icing Cond

Transient below 20,000 ft. 30 secs Max

One Generator Operating From 29,000 ft. To 41,000 ft.

One Generator Operating Above 41,000

A

In Flight Operation:

One Gen Operating Up to 29,000 ft.
400
One Generator Operating Up to 29,000 ft Icing Cond
440
Transient below 20,000 ft. 30 secs Max
525
One Generator Operating From 29,000 ft. To 41,000 ft.
280
One Generator Operating Above 41,000
260

42
Q

Structural Limitations

          RK 1-343.  344 & After Max Rmp.    Max T/O Max Ldg Max Zero
A

1-343. 344 & Aftr
Max Rmp. 16,300. 16,500
Max T/O. 16,100. 16,300
Max Ldg. 15,700
Max Zero. 13,000

43
Q

Maneuvering Load Factors

Flaps 0
Flaps. 10,20 and 30

A

Flaps 0
-1.0 to +3.2 G

Flaps. 10,20 and 30
0 to. +2.0 G

44
Q

Takeoff & Landing Ops

Airfield Op Press Altitude
Ambient Temperature
Max Tailwind for TO @ LDG
Max Fuel Unbalance T/O
Max Fuel Unbalance. LDG

A

Airfield Op Press Altitude
Up to 10,000 feet

Ambient Temperature
-40 c to ISA +35 c

Max Tailwind for TO @ LDG
10 knots

Max Fuel Unbalance T/O
100 lbs

Max Fuel Unbalance. LDG
300 ibs

45
Q

Fuel Limits

Min Fuel Temp
Max Fuel Temp

A

Min Fuel Temp
-40 c

Max Fuel Temp
+50 c

46
Q

Enroute Operations

Cert Ceiling
Ambient Air Temp
Max Fuel Unbalance
Yaw Damper
Ext of Gear, Flaps, Ldg Lights
Refrigerant AC

A

Cert Ceiling
45,000.

Ambient Air Temp
-65 c to ISS +35 c

Max Fuel Unbalance
300 lbs

Yaw Damper
Operable and on for flight in icing cons or flight above 28,000 ft.

Ext of Gear, Flaps, Ldg Lights
Prohibited above 20,000 ft

Refrigerant AC
Prohibited above 18,000 ft

47
Q

EGPWS WARNING

Hawker 400XP/BJet 400A (1 decks)

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