Limitations

Question 1

Maximum zero fuel weight:

Answer 1

49,000 lbs

Question 2

Maximum ramp weight:

Answer 2

75,000 lbs

Question 3

Maximum takeoff weight:

Answer 3

74,600 lbs

Question 4

Maximum landing weight:

Answer 4

66,000 lbs
ASC 007 lowers it to 58,500 lbs for Cat C approaches

Question 5

Maximum permissible fuel imbalance in-flight:

Answer 5

• Up to weight 55,000 = 2000lbs
• Greater than 55,000 less than 60,500 = consult chart
• 60,500 to 75,000 = 400 lbs

Question 6

Maximum cabin differentials:

Answer 6

9.94 psi

0. 3 psi for taxi, takeoff or landing

Question 7

Single engine autopilot coupled go-around:

Answer 7

Not Approved

Question 8

Minimum autopilot engagement height:

Answer 8

200 ft

Question 9

Minimum autopilot disengage height:

Answer 9

• 60 ft from an ILS Approach

- 50 ft below MDA/DA from an LNAV/VNAV Approach

Question 10

Use of auto-throttles on single-engine approach:

Answer 10

Not permitted

Question 11

Use of speed brakes with the HMG in operation:

Answer 11

Slow Operation (approx 3 seconds for full range of movement)

Question 12

IDG electrical load limit:

Answer 12

45% (18kVa) when ambient temperature is greater than 43°c (110°f)

Question 13

Speed brakes not approved for extension in-flight when:

Answer 13

Flaps are at 39°, or landing gear extended

Question 14

Take off permitted with automatic ground spoilers inoperative provided:

Answer 14

• Antiskid is operative
• 20° flaps are used
• Cowl and wing anti-ice systems are not used

Question 15

Usable fuel capacity:

Answer 15

29,500 lbs

Question 16

Wing anti-icing must be turned on:

Answer 16

If icing conditions are imminent, or immediately upon detection of ice formation on wings, winglets or windshield edges

Question 17

Cowl anti-icing is required on the ground:

Answer 17

When SAT is +10°c or below and visible moisture, precipitation or wet runways are present

Question 18

Cowl anti-icing is required in flight:

Answer 18

As indicated in the cowl anti-icing table, when visible moisture or precipitation is present or when signs of icing are observed

Question 19

Procedure to shed engine ice in flight is:

Answer 19

Quickly retard one engine at a time to idle, hold for 5 seconds and then accelerate engine to 85% LP RPM for 2 seconds

Question 20

Take off is permitted with anti-skid inoperative, provided:

Answer 20

• Runway is dry
• Ground spoilers are operative
• 20° flaps are used
• Cowl and wing anti-ice systems are not used

Question 21

Do not operate weather radar on the ground:

Answer 21

• During refueling of the airplane
• Within 300 ft of fueling operations
• Within 49 ft of ground personnel

Question 22

A current FMS database is required for:

Answer 22

GPS Approaches

Question 23

Localizer based approaches must be flown using the following displayed / coupled navigation source:

Answer 23

NAV (green data)

Question 24

The following approaches may be flown using FMS as the displayed / coupled source:

Answer 24

RNAV (GPS)
VOR, VOR/DME, VOR/DME RNAV
NDB
GPS

Question 25

TCAS operation with one engine inoperative:

Answer 25

TA only as operating mode

Question 26

Maximum speed for RVSM operations:

Answer 26

0.85 M

Question 27

Crew and passenger oxygen masks are not approved for use above:

Answer 27

40,000 ft cabin altitude | Newer Scott EROS crew masks is approved for use to a cabin altitude of 45,000 ft

Question 28

General EICAS range marking colors:

Answer 28

Green or White = Normal Range Values Amber = Caution Range Values Red = Warning Range Values

Question 29

APU starting limits (battery power):

Answer 29

Three consecutive start attempts, followed by 1 hour cooldown

Question 30

APU starting limits (external DC power):

Answer 30

3 start attempts, 15 minute cool down in between each attempt

Question 31

Maximum APU operating altitude:

Answer 31

37,000 ft

Question 32

APU generator electrical load limit:

Answer 32

- 100% (40kVa) Sea Level to 37,000 ft | - 85% between 30,000 and 37,000 at speeds faster than 0.85 M

Question 33

Maximum engine TGT prior to ground start:

Answer 33

200 °c

Question 34

Maximum takeoff TGT:

Answer 34

800°c 5 minutes both engines 10 minutes on one engine

Question 35

Maximum continuous TGT:

Answer 35

715°c

Question 36

Maximum crosswind component for engine start:

Answer 36

25 knots

Question 37

Maximum tailwind component for engine start:

Answer 37

25 knots

Question 38

Stabilized engine operation on the ground (static) is prohibited between:

Answer 38

60% and 72% LP RPM

Question 39

Maximum runway slope for takeoff and landing operations:

Answer 39

+/- 2%

Question 40

Maximum tailwind component approved for takeoff and landing:

Answer 40

10 knots

Question 41

Maximum approved airport pressure altitude for takeoff or landing:

Answer 41

15,000 ft

Question 42

Maximum operating altitude:

Answer 42

45,000 ft

Question 43

Maximum operating altitude with the yaw damper inoperative, coupled with failure of the mach trim compensation:

Answer 43

41,000 ft

Question 44

Maximum landing gear extension altitude:

Answer 44

20,000 ft

Question 45

Maximum altitude for extending flaps 39°:

Answer 45

20,000 ft

Question 46

Maximum altitude for extending flaps 10 or 20 degrees:

Answer 46

25,000 ft

Question 47

Minimum control speed, air:

Answer 47

106 kcas

Question 48

Minimum control speed, landing:

Answer 48

99 kcas

Question 49

Minimum control speed, ground:

Answer 49

109 kcas

Question 50

Maneuvering speed (Va):

Answer 50

206 kcas

Question 51

Flaps extended speeds (Vfe / Mfe):

Answer 51

Takeoff (10°): 250 kcas / 0.60 m T/O APP (20°): 220 kcas / 0.60 m Down (39°): 180 kcas / 0.60 m

Question 52

Landing gear extended speed (Vle / Mle):

Answer 52

250 kcas / 0.70 M

Question 53

Landing gear operation speeds (Vlo / Mlo):

Answer 53

``` 225 kcas / 0.70 M (normal operation) 175 kcas (alternate operation) ```

Question 54

Minimum speeds with yaw damper inoperative:

Answer 54

210 knots above 20,000 ft | Use reference table below 20,000 ft

Question 55

Maximum speed with Mach trim or electric elevator trim inoperative:

Answer 55

0.75 M

Question 56

Turbulence penetration speeds:

Answer 56

270 kcas / 0.75 M above 10,000 ft | 240 kcas below 10,000 ft

Question 57

Maximum tire speed:

Answer 57

195 knots

Question 58

Maximum speed with emergency stabilizer trim armed, autopilot engaged and a jammed elevator:

Answer 58

270 kcas / 0.75 M

Question 59

Max demonstrated crosswind for takeoff and landing

Answer 59

24 knots