Limitations

Question 1

Max Ramp/Taxi Weight - 
Max Takeoff Weight - 
Max Landing Weight - 
Max zero fuel Weight - 
Min operating Weight -

Answer 1

48,300
48,200
38,000
32,000
22,150

Question 2

Max pressure altitude for takeoff and landing
Max operating altitude
Max temperature for takeoff and landing
Min temperature for takeoff

Answer 2

14.000ft
41,000
ISA +35C
-40C

Question 3

Max runway slope for takeoff and landing

Max tailwind component for takeoff and landing

Answer 3

+/- 2%

10kts

Question 4

A tactile check of the ___, ___, and ___ is required when one of the following is present: (3)

Answer 4

wing leading edge, wing forward upper surface and wing rear upper surface

1) OAT is <= 0C
3) Atmospheric conditions conducive to frost

Question 5

Cowl Anti-ice must be on during ground operations when

Answer 5

OAT is < 10C and visible moisture is present including fog with vis </= 1 mile or ground surfaces are contaminated with snow, ice, standing water or slush

Question 6

Wing Anti-ice must be on during ground operations when

Answer 6

OAT is <= 5C and

1) visible moisture in any form is present below 400ft AGL, 2) any precipitation,
3) runway is wet or contaminated

Question 7

The maximum demonstrated crosswind form takeoff and landing is ___ knots and ___(is/is not) considered limiting.

Answer 7

24 kts; not

Question 8

Max glide path angle < 1500’ MSL

> 1500’ MSL?

Answer 8

4.49 deg

Check AFM Supplement 11

Question 9

If above 40,000’, ____ or ____ must be selected on for each engine.

Answer 9

One air conditioning unit (pack) or cowl anti-icing must be on for each engine

Question 10

Before the first flight of the day, if aircraft is cold-soaked (temp below ___ for more than ___ hours):

1)
2)

Answer 10

-30 deg C; 8 hours

1) motor engine 60 sec and check fan rotation before initiating engine start
2) actuate thrust reversers until deploy and stow cycles are < 5 sec

Question 11

Oil temperatures:

Min start -
Max continuous -
Max permissible - ___ (___ min max)

Answer 11

Min start - -40 deg C
Max cont - 155 deg C
Max perm - 163 deg C (15 min max)

Question 12

Oil pressure

Min idle -
Takeoff -
Max Continuous -
Max transient after cold start - ___ (___ psi ___min max)
Engine must remain at ___ until pressure ___

Answer 12

Min idle - 25 psi
Min Takeoff - 45 psi
Max Continuous - 115 psi
Max transient - 156 psi (130 psi for 10 min max)
Engine at IDLE until pressure returns to normal range

Question 13

Max Oil consumption of ___oz/hr (gal/hr)

Engine oil must be checked within ___ to ___ after shutdown; engine must be ___ if that period is exceeded.

Max refill is ___ without dry-motoring engine.

Answer 13

6.4 oz/hr or 0.05 gal/hr

Oil checked 15 min to 2 hrs after shutdown; motored

2 quarts

Question 14

Continuous ignition must be on: (5)

Answer 14

1) takeoff with high crosswind component
2) takeoff or landing on contaminated runway
3) flight in moderate or greater turbulence
4) flight in moderate or greater rain
5) flight in vicinity of thunderstorms

Question 15

Engine starting limits:
Max ___% N2 for starter use or engagement

Max ___ consecutive ___ sec start cycles with ___ min cooling between additional cycles

Max ITT for ground start (Thrust lever to IDLE) -
Max ITT for air start -

Dry motoring (IGN off and thrust lever in SHUTOFF)

1) max ___ sec then ___ min off
2) subsequent cycles: ___ sec then ___ min off

Answer 15

55% N2
3; 30 sec; 5
Ground - 120 deg C
Air - 90 deg C
Dry motoring:
  1) 90 sec; 5 min off
  2) 30 sec; 5 min off

Question 16

Auto throttle (ATS) prohibited:

1) unless ___ thrust data is avail from ___
2) unless ___ confirmed on takeoff roll prior to ___ KIAS
3) during ___ - engine ops
4) during CAT ___ ops
5) below first indication of ___
6) during ___
7) below ___ft with flaps

Answer 16

1) N1; FMS perf thrust limit page
2) T/O N1 confirmed prior to 80 KIaS
3) single engine ops
4) CAT II ops
5) stall
6) go-around
7) 100 ft with flaps

Question 17

Thrust reversers:

1) Do not attempt a ___ after TR are deployed
2) ___ the aircraft with TR is prohibited
3) takeoff with any TR ___ is prohibited
4) during landing TR is limited to ___% N1 below ___ KIAS
5) max demonstrated crosswind component on a dry runway is ___ kits and is/is not considered limiting

Answer 17

1) go around
2) backing the aircraft
3) icon or caution alert EICAS msg
4) 60% N1 below 60 KIAS
5) 24 kts and IS limiting

Question 18

Max fuel imbalance for taxi, takeoff or landing -

Max imbalance in flight -

Max fuel quantity at 6.75 lbs/gal- 
  Main - 
  Aux - 
  Tail - 
  Total -

Answer 18

400 lbs

800 lbs

Main - 4860 lbs
Aux - 7168 lbs
Tail - 3112 lbs
Total - 20,000 lbs

Question 19

Reduce max wing and aux fuel quantity by \_\_\_% if gravity fueling 
  Wings - 
  Aux - 
  Tail - 
  Total - 

To avoid AUX HEAVY message, max is ____ lbs

Answer 19

7%
 Main - 4520 (340 lbs less) x 2
 Aux - 6660 lbs (508 lbs less)
 Tail - 0 no fuel
 Total - 15,700 lbs (4300 lbs less)

Question 20

Takeoff with up to ___ lbs in the AUX tank is permitted if at least ___ lbs in each wing and ___ in tail

For takeoff weights up to ___ lbs with more than 500 lbs in AUX, each wing must have ___ lbs. for takeoff weights above that consult AFM Limitations.

Answer 20

500 lbs; 1500 lbs in each wing

Up to 42,400 lbs with 500 lbs in AUX; 1500 lbs in each wing

Question 21

Min fuel for go-around is ___ lbs each wing and max ___ deg pitch

Min Engine fuel temp for takeoff -

Min bulk fuel for takeoff and flight -

Approved fuels: (6)
Mixing of fuel grades is/is not permitted

Answer 21

500 lbs each wing; 10 deg pitch

5 deg C; 10 deg C above fuel freezing point (FPP)

Jet A, A1, B, JP 4, 5, 8
Mixing fuels IS permitted

Question 22

APU:
Min temp for start -
Hung start if

Answer 22

-40 deg C for start

Hung if