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MD80 Memory Items > Limitations > Flashcards

Limitations Flashcards

1
Q

INSTRUMENT LIMIT MARKINGS (AA)

A

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

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2
Q

Engine Display Panel (TWA)

A

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

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3
Q

System Display Panel (TWA)

A

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

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4
Q

Maximum Tailwind (T/O & LDG)

A

10 Kts

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5
Q

Maximum X-wind (demonstrated)

A

30 Kts

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6
Q

Turbulence Penetration speed

A

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

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7
Q

Maximum Ldg Weight

A

130,000 lbs

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8
Q

Maximum Zero Fuel Weight

A

122,000 lbs

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9
Q

Maximum altitude for unpressurized flight following in-flight depressurization

A

14,000’

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10
Q

APU Air switch must be ____ for all in flight operations

A

OFF

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11
Q

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

A

Disconnected, Stall, Surge

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12
Q

Minimum altitude for autopilot (enroute)

A

500’

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13
Q

Minimum altitude for autopilot (Cat III landing)

A

None

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14
Q

Minimum altitude for Autopilot-ILS (VFR)

A

70’ AFL

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15
Q

Minimum altitude for autopilot-ILS (IMC)

A

50’ AFL

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16
Q

Minimum altitude for autopilot-non ILS approaches

A

50’ below MDA

17
Q

Do not conduct Autoland if (5 items)

A
  • 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
18
Q

EGT temp limit Starting:
On ground?
In flight?

A 
500 c (momentary)
625 c (momentary)
19
Q

Takeoff reserve thrust (EGT)

A 
625 c (5 minutes)
630 c (2 minutes)---Red radial line
20
Q

Maximum thrust (EGT)

A 
590 c (5 minutes)
595 c (2 minutes)---Orange radial line
21
Q

Maximum Cont. Climb (EGT)

A

Below amber arc (580 c)

22
Q

Max Cruise (EGT)

A

540 c

23
Q

Minimum oil quantity for dispatch

A

> 4 hours=12 qts

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

24
Q

Do not operate revers thrust in ____________.

A

Flight

25
Q

For powerback, do not exceed ______EPR.

A

1.3

26
Q

Starter duty cycle

A

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

27
Q

Do Not use flap settings between ___ & ____ degrees

A

13 and 15

28
Q

Do not arm ________ prior to gear extension

A

Spoiler

29
Q

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.

A
  • UP/RET or 0/EXT
  • EXT
  • Full Aft
30
Q

Maximum fuel imbalance

A

Main tanks—–1500 lbs

Aux Tanks—–400 lbs

31
Q

Definition of icing conditions (ground and takeoff)

A

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.

32
Q

Definition of icing conditions (in flight)

A

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

33
Q

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

A

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

34
Q

Air foil anti ice should be used….

A

in flight when icing conditions exist or are anticipated.

35
Q

Air foil anti-ice limitations

A

-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.

36
Q

Maximum brake temp for Takeoff

A

205c

37
Q

Maximum tire speed

A

195 kts

MD80 Memory Items (2 decks)

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