• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/66

Click to flip

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;

66 Cards in this Set

  • Front
  • Back
Required Crew Members
2
Certification
Day, Night, Icing, VFR, IFR
Max runway slope: ± of runway length.
0.02
Runway surface:
Paved
Max tailwind:
10 Knots
Max temperature for aircraft:
ISA+35°C
Min/Max takeoff & landing pressure altitude:
-1000, 8000 (ER/LR) 10,000 (XR)
Min/Max SAT at FL370:
-65/-21.5°C
Min/Max SAT for takeoff:
-40/52°C
Min TAT above FL250:
-45°C
Min SAT below FL250:
-54°C
Mx inspection needed when landing below:
-40°C
VLO for gear retraction/extension:
200/250 KIAS
VLE:
250 KIAS
VA:
200 KIAS
Max flap ext. speed for flaps 9:
250 KIAS
Max flap ext. speed for flaps 18:
200 KIAS
Max flap ext. speed for flaps 22:
200 KIAS
Max flap ext. speed for flaps 45:
145 KIAS
Max flap ext. speed for flaps 45 (XR):
160 KIAS
Above 10,000' with YD disengaged, max speed for flaps 22 XR
180 KIAS
Above 10,000' with YD disengaged, max speed for flaps 45 XR
145 KIAS
For non-XR, when flaps are extended to/retracted from 45, momentary airspeed deviations between 145 and 160 KIAS will not require a Mx inspection.
145 and 160 KIAS
For non-XR, when flaps are extended to/retracted from 22, momentary airspeed deviations between 200 and 210 KIAS will not require a Mx inspection.
200 and 210 KIAS
Max airspeed after T/O without retrimming:
160 KIAS
Max airspeed for turbulent air penetration below 10,000': ___ and above 10,000': ___
200 KIAS / 250 KIAS or .63M whichever is lower
Min/Max fuel tank temperature is:
-40/52°C
Max N1:
100%
For all models, min/max oil pressure < 88% N2:
34/110 psi
On ER/LR, min/max oil pressure >= 88% N2:
50/110 psi
On XR, min/max oil pressure >= 88% N2:
48/110 psi
On XR, operation between 34 and 48 psi is permitted for:
T/O and go-around phases
Max oil pressure may be exceeded during start if the oil temp is below: ___ . The engine must remain at IDLE until oil presure is less than: 110 psi
21°C .
All aircraft will display oil pressure <= ___ in green
110 PSI
Aircraft will display oil pressure in range ___ and ___ psi in amber permitted all operation modes. Limited to ___ mins. Operation in the oil pressure amber range between ___ and ___ in amber. Limited to ___ min. Total over-pressure time may not exceed
111 and 115 PSI / 5 minutes / 116 and 155 psi / 2 minutes
Min oil temp for start:
-40°C
To increase N2 above 83% , the engine oil temp must be 40°C Or, run the engine for at least ___ minutes OR complete a static runup to ___ , allow the engines to stabilize and ensure that the oil pressure is <=
8 minutes / 88% N2 / <= 83 psi
LP and HP spool vibration limits maybe exceeded up to ___ IPS for ___. during takeoffs and go-arounds. Else ___ seconds
2.5 IPS for 5 minutes / 10 seconds
Max ITT for start on all engines:
800°C
All ER/LR takeoff thrust ratings/ITT limits (948°) are time limited to:
5 minutes
All XR, takeoff thrust ratings/ITT between ___ and ___ are time limited to ___ seconds. Takeoff thrust ratings/ITT up to ___ are permitted up to a max of ___ min.
971°-992° / 5 min
Dry motoring continuous operation:
5 minutes ON & 5 minutes off
Engine starting cycle, 1-4: ___ ___ and 5th cycle
1 minute ON & 1 minute OFF - 1 minute ON & 5 minutes OFF
After start, the engines must run at idle or taxi thrust for ___ min for cold engines and ___ min for warm.
4 min - 2 min
Engine is considered cold, if it's been shut down for at least:
90 minutes
Engines must run for at least ___ minutes at idle or taxi thrust before shutdown.
2 minutes - 3 to 5 minutes recommended
Max altitude for starting APU:
FL300
Max operational altitude for APU:
FL370
The APU will automatically shutdown at ____ rotor speed
104%
APU EGT may exceed ___ up to ___ for maximum of __ minutes
680 up to 717°C - 5
Min battery temp for APU start:
-20°C
Start cycle for the APU: After 1-2 attempts: ___ 3rd attempt ___.
1 minute off - 30 minutes off
Max APU generator load above FL300:
300a
Min AP engagement height:
500 AGL
AP disengagement height is: ____ for visual approaches, ___ for CAT I, ___ ft for CAT II, and before __________ for non precision approaches.
200 ft for visual approaches, 200 ft for CAT I, 50 ft for CAT II, Before leaving MDA for Non-Precision
Max ISIS duration when operating only on batteries is ___ minutes. May be extended to 45 minutes if pitot #3 is turned off in non-icing conditions
40 minutes
Max altitude for flap extension:
FL2000
Max differential pressure:
7.8 psi
Max differential over-pressure:
8.1 psi
Max differential negative-pressure:
-0.3 psi
Min temp for manual anti-ice operation: ___ C SAT on ground and TAT in-flight.
-40° C
Max temp for anti-ice operation:
10°C
Holding configuration in icing:
Landing-gear UP, flaps 0 and min airspeed of 200 KIAS
Max windshield wiper operating speed:
170 knots
Do not operate windshield wiper:
on a dry windshield
Max imbalance allowed between tanks:
800 lbs