Reading...
Play button
Play button
Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
90 Cards in this Set
- Front
- Back
|
Take off decision speed
|
V1
|
|
|
Takeoff safety speed
|
V2
|
|
|
Climb speed
|
V35
|
|
|
Maneuvering speed
|
Va
|
|
|
Landing approach climb speed
|
Vapp (1.3 Vs1)
|
|
|
Single engine enroute climb speed
|
Venr
|
|
|
Maximum flap extended speed
|
Vfe
|
|
|
Maximum landing gear extended speed
|
Vle
|
|
|
Maximum landing gear operating speed
|
Vlo
|
|
|
Minimum airspeed in flight at which directional control can be maintained
|
Vmc 83 knots flaps zero
76 knots flaps 15 |
|
|
minimum airspeed on the ground at which directional control can be maintained with one engine suddengly inoperative using only aerodynamic controls
|
Vmcg, 79 knots
|
|
|
Maximum Operating Limit Speed
|
Vmo or Mmo
|
|
|
Rotation speed
|
Vr
|
|
|
Airspeed equal to the landing 50 foot point with flaps in landing position and landing gear extended (1.3 Vso)
|
Vref
|
|
|
stalling speed or minimum steady flight speed in the landing configuration
|
Vso
|
|
|
stalling speed or the minimum steady flight speed obtained in a specified configuration
|
Vs1
|
|
|
Best Angle of Climb speed (multiengine, flaps15)
|
Vx 124 knots
|
|
|
Best Rate of climb speed, (multiengine flaps 15)
|
Vy 191 knots
|
|
|
Maximum ramp weight
|
12,625
|
|
|
Maximum takeoff weight
|
12,500
|
|
|
Maximum Landing Weight
|
11,525 pounds
|
|
|
Maximum Zero Fuel Weight
|
9,700 pounds
|
|
|
Engine type
|
Williams FJ44-3A-24
|
|
|
Engine start maximum tailwind
|
12 knots
|
|
|
Engine start maximum crosswind
|
16 knots
|
|
|
Starting: maximum time to light-off
|
10 seconds
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for a ground battery start
|
10,000 feet
|
|
|
Maximum airport elevation for ground external power start
|
10,000 feet
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/Maximum Power Current Capacity for start
|
800/1000 amps
|
|
|
Start cycle limitations
|
three engine starts in 30 minutes
three cycles of operation with a 60-second rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 minutes
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Ground operation greater than 75% N2with engine, wing or windshield anti-ice on
|
2 minutes
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Hydraulic Fluid
|
MIL-PRF-83282
|
|
|
Fuel boost pumps on when....
|
Fuel Low Level lights illuminate (approximately 220 pounds or less)
|
|
|
Approved oils
|
Mobile Jet II
Mbil 254 |
|
|
Maximum speeds
|
Mmo .737 (above FL290)
Vmo 278 KIAS between 8,000 and 29,000 Vmo 260 KIAS below 8,000 |
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS
Intentional selection of ground flaps in flight is prohibited |
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
no limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Altitude for Take Off
|
10,000 feet
|
|
|
Maximum Tailwind for Take-off and Landing
|
10 knots
|
|
|
Minimum Temperature for take-off
|
-54 C
|
|
|
Maximum fuel imbalance
|
200 pounds (but 600 pounds has been demonstrated)
|
|
|
Minimum cabin temperature prior to take-off
|
0 C (because of the oxygen masks)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 feet
|
|
|
Maximum generator current
|
300 amps to 41,000 feet
250 amps above 41,000 feet |
|
|
Maximum altitude to extend flaps or gear
|
18,000 feet
|
|
|
Load factors
|
Flaps up: -1.52 G to +3.6G at 12,500 pounds
Flaps 15 to 35: 0 to +2 G at 12,500 pounds |
|
|
Normal cabin pressurization
|
0 to 8.9 PSI
|
|
|
N1 redline
|
102.9%
|
|
|
ITT redline
|
1001C
|
|
|
ITT redline one engine running
|
878C
|
|
|
N2 redline
|
100.8%
|
|
|
Oil temp redline
|
149C
|
|
|
Oil pressure redline
|
22 psi
|
|
|
Autopilot minimum altitude ILS
|
70 feet
|
|
|
Autopilot minimum altitude non-precision
|
240 feet
|
|
|
Autopilot minimum altitude cruise
|
1,000 feet
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions (except approach and landing)
|
160 KIAS
|
|
|
What position should the flaps be in during icing conditions? (except approach and landing?)
|
zero degrees, flaps up
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail decing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Engine failure below V1
|
Brakes-as required
Throttles-idle Speed brakes-extend |
|
|
Engine failure above V1
|
1. Maintain directional control
2. Accelerate to Vr 3. Rotate at Vr 4. Landing gear up 5. Wing X/Flow switch if anti ice is on 6. AT 1500 AGL retract flaps at V2+10 and accelerate to Venr |
|
|
Engine failure during final approach
|
1. Thrust-increase as required
2. Airspeed Vapp 3. Flaps-take-off and approach |
|
|
Engine Fire
|
1. Throttle on affected engine to idle
IF LIGHT REMAINS ON 2. Engine fire switch, lift cover and push 3. Either bottle illuminated BOTTLE ARMED light-push |
|
|
Engine restart-two engines
|
1. L/R Boost switches-BOTH ON
2. Throttle-OFF, then IDLE 3. If altitude allows, INCREASE AIRSPEED TO 230 KIAS |
|
|
Electrical fire or smoke
|
1. Oxygen Masks -DON and EMER
2. Microphone select switches-MIC OXY MASK |
|
|
Environmental system smoke or odor
|
1. Oxygen Masks-DON and EMER
2. Microphone select switches-MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Masks-DON and EMER
2. Microphone select switches-MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxygen Masks DON and 100% OXYGEN
2. Microphone select switches-MIC OXY MASK 3. Emergency Descent-AS REQUIRED 4. Passenger Oxygen-Make sure passengers are receiving oxygen |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press and release
2. Throttles-IDLE 3. Speed brakes-EXTEND 4. Airplane pitch attitude-INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Battery Overtemp
|
1. Volt/Amp-Note
2. Battery switch-EMER 3. Volt/Amp-Note |
|
|
Autopilot malfunction
|
1. AP TRIM DISC Button-Press and Release
|
|
|
Electric Elevator Trim Runaway
|
1. AP TRIM DISC Button-Press and Release
2. Throttles-As required 3. Speed brakes-As required 4. Manual Elevator Trim-As required 5. PITCH TRIM Circuit Breaker (L Panel) Pull |
|
|
Emergency Evacuation
|
1. Parking brake-set
2. Throttles-both off 3. L/R Engine Fire Switches-Both press 4, Illuminated Bottle Armed buttons-push 5. Battery switch-off 6. ELT-On 7. Escape route-choose best |
