Limitations

Question 1

INSTRUMENT LIMIT MARKINGS (AA)

Answer 1

Maximum/Minimum Limits…………………….Red Radial Line
Maximum limits (normal takeoff)…………Orange Radial Line
—-(N1, N2, EGT)
Precautionary Ranges……………………………Amber Arc
Normal Operating Ranges………………………Green Arc

Question 2

Engine Display Panel (TWA)

Answer 2

Maximum Limits (N1, N2, and EGT Only)
—-Red radial/Arc & Flashing digits
Maximum Limit Range, Normal Takeoff (N1, N2, EGT only)
—-Orange Radial/Arc
Precautionary Ranges (EGT Only)…………Amber Arc
Normal Operating Range………………………Green Arc

Question 3

System Display Panel (TWA)

Answer 3

Maximum Limits (oil temp only)…..Red Annunciator Light
Maximum Limits (oil press. only)…Flashing digits
Minimum Limits (oil press. only)….Red Annunciator Light
Precautionary Ranges
(Oil temp/press/hyd quant. only)….Amber Annunc. Light

Question 4

Maximum Tailwind (T/O & LDG)

Answer 4

10 Kts

Question 5

Maximum X-wind (demonstrated)

Answer 5

30 Kts

Question 6

Turbulence Penetration speed

Answer 6

275-285 Kts
.75-.79M
< 10,000’=250 KIAS or Min Maneuver speed (higher of two)
Do not fly less than min maneuver for existing configuration

Question 7

Maximum Ldg Weight

Answer 7

130,000 lbs

Question 8

Maximum Zero Fuel Weight

Answer 8

122,000 lbs

Question 9

Maximum altitude for unpressurized flight following in-flight depressurization

Answer 9

14,000’

Question 10

APU Air switch must be ____ for all in flight operations

Answer 10

OFF

Question 11

Autothrottle must be _________ if engine ______ (______) is detected.

Answer 11

Disconnected, Stall, Surge

Question 12

Minimum altitude for autopilot (enroute)

Answer 12

500’

Question 13

Minimum altitude for autopilot (Cat III landing)

Answer 13

None

Question 14

Minimum altitude for Autopilot-ILS (VFR)

Answer 14

70’ AFL

Question 15

Minimum altitude for autopilot-ILS (IMC)

Answer 15

50’ AFL

Question 16

Minimum altitude for autopilot-non ILS approaches

Answer 16

50’ below MDA

Question 17

Do not conduct Autoland if (5 items)

Answer 17

• ALN mode is not displayed on FMA by 100’ radio alt.
• Either engine becomes inoperative > 50’ above runway
• Automatic ground spoilers are not armed and operational
• Any unusual control position or other abnormal conditions exists in the manual flight control system.
• “RUDDER CONTROL MANUAL” light is illuminated
• Landing overweight

Question 18

EGT temp limit Starting:
On ground?
In flight?

Answer 18

500 c (momentary)
625 c (momentary)

Question 19

Takeoff reserve thrust (EGT)

Answer 19

625 c (5 minutes)
630 c (2 minutes)---Red radial line

Question 20

Maximum thrust (EGT)

Answer 20

590 c (5 minutes)
595 c (2 minutes)---Orange radial line

Question 21

Maximum Cont. Climb (EGT)

Answer 21

Below amber arc (580 c)

Question 22

Max Cruise (EGT)

Answer 22

540 c

Question 23

Minimum oil quantity for dispatch

Answer 23

> 4 hours=12 qts

< 4 hours=4 qts + 2 qts/hour of flight

Question 24

Do not operate revers thrust in ____________.

Answer 24

Flight

Question 25

For powerback, do not exceed ______EPR.

Answer 25

1.3

Question 26

Starter duty cycle

Answer 26

1st attempt: 90 seconds on/5 minutes off ----Can consist of 3-30 second attempts; allow n2 to reduce to zero prior to initiating each start Subsequent attempts: 30 seconds on/5 minutes off

Question 27

Do Not use flap settings between ___ & ____ degrees

Answer 27

13 and 15

Question 28

Do not arm ________ prior to gear extension

Answer 28

Spoiler

Question 29

Use speed brakes only in _____ or _____ configuration Do not extend or retract landing gear while _______are deployed Moving Spd Brk/Spoiler Lever beyond _____ position in flight is prohibited. ______ _______ position if for ground use only.

Answer 29

- UP/RET or 0/EXT - EXT - Full Aft

Question 30

Maximum fuel imbalance

Answer 30

Main tanks-----1500 lbs | Aux Tanks-----400 lbs

Question 31

Definition of icing conditions (ground and takeoff)

Answer 31

RAT 6 c or below and visible moisture in any form is present (such as clouds, fog with visibility one mile or less, rain, snow, sleet, and ice crystals) RAT 6c or below when operating on ramps, taxiways, or runways where surface snow, standing water, or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes. RAT 6c or below and the temperature - dew point spread is 3c or less. Note: One engine taxi is authorized if no significant precipitation (snow, sleet, or freezing rain) is occurring that could adhere to or collect in the engine inlet.

Question 32

Definition of icing conditions (in flight)

Answer 32

RAT 6c or less and visible moisture is present in any form (such as clouds, rain, snow, sleet, and ice crystals)

Question 33

When engine anti ice must be used (ground/takeoff/flight)

Answer 33

Engine anti-ice system must be on when icing conditions exist or are anticipated.

Question 34

Air foil anti ice should be used....

Answer 34

in flight when icing conditions exist or are anticipated.

Question 35

Air foil anti-ice limitations

Answer 35

-Do not use until reaching 1000' AFL after takeoff -Minimum duct pressure is 20 psi -Operating in flight maintain sufficient thrust to keep associated "ICE PROTECT TEMP LOW" light extinguished. Application of "Tail De-ice" is required: ---Once every 20 minutes --One minute prior to extending landing flaps --After leaving icing conditions, prior to turning system off.

Question 36

Maximum brake temp for Takeoff

Answer 36

205c

Question 37

Maximum tire speed

Answer 37

195 kts