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Atlas Air B767 > Limitations > Flashcards

Limitations Flashcards

1
Q

MAX OPERATING ALT?

A

FL431

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2
Q

MAX T/O + LAND ALT?

A

8,400’

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3
Q

TURB AIR?

A

290KTS/.78M (Whichever is lower)

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4
Q

MAX T/O + LAND TAILWIND?

A

10KTS

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5
Q

DOOR LIMITS?

A
  • TRANSIT = 40 KTS
  • OPEN = 65 KTS
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6
Q

T/O + LAND XWIND (Runway Cond 6)?

A

40KTS

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7
Q

T/O + LAND XWIND (Runway Cond 5)?

A

T/O = 25KTS LAND = 40KTS

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8
Q

MIN IN-FLIGHT WEIGHT?

A

179,000lbs

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9
Q

MTW? MTOW? MLW? MZFW?

A
  • 409,000lbs
  • 408,000lbs
  • 320,000lbs
  • 295,000lbs
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10
Q

MIN O2?

A
  • ETOPS = 1350psi
  • NON-ETOPS = 1250psi
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11
Q

MAX CABIN DIFF PRESS?

A
  • 9.1 PSI
  • T/O + LAND = 0.125 PSI
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12
Q

APU START LIMIT (per 60 minutes)?

Time between attempts?

A
  • 3 TOTAL ATTEMPTS/HR
  • 1 MIN OFF
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13
Q

APU BLD AIR inflight limitation?

A

Not available above 17,000’

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14
Q

A/P ENG - AILERON TRIM?

A

Use of aileron trim with A/P engaged is prohibited.

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15
Q

A/P MIN ALTS?

A

T/O + G/A = 250’ AGL NON ILS = 50’ below MDA SINGLE ILS = 100’ AGL AUTOLAND = Touchdown/Rollout

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16
Q

AUTOLAND MAX WIND COMPONENTS?

A
  • HEADWIND/XWIND = 25KTS
  • CAT2/3 XWIND = 15KTS
  • TAILWIND = 10KTS
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17
Q

HF RADIOS?

A

Do not operate during refueling ops.

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18
Q

CB RESET POLICY?

A
  • Do not reset FUEL PUMP - All others only after 3 min cooling
19
Q

DOOR MOUNTED ESCAPE SLIDES?

A

Must be armed and engagement of the girt bar with door sill verified prior to taxi, takeoff, or landing with passengers.

20
Q

FLIGHT DECK DOOR?

A

Operational check has been accomplished once each flight day.

21
Q

ENG THRUST RATING?

A

60,200lbs

22
Q

ENG EGT STARTING?

A

GND = 750C (unlimited time) FLT = 870C (max 40 seconds)

23
Q

ENG EGT TAKEOFF?

A

960C * authorized to max 10 minutes at T/O thrust in event of thrust loss during takeoff

24
Q

ENG EGT MAX CONT?

A

925C

25
Q

ENG STARTER LIMITS?

A

NORM = 1 MIN ON/1 MIN OFF EXTENDED = 0-5 MIN ON/OFF Until 0% N2 or 5-10 MIN ON/20 MIN OFF

26
Q

ENG OIL MIN PRESS?

A

10

27
Q

ENG OIL MAX TEMPS?

A

MAX = 160C (Continuous) or 175C (15 Min Max)

28
Q

ENG OIL MIN DISPATCH QTY?

A

17

29
Q

CONT IGNITION CONDITIONS?

A
  • MOD/HVY RAIN - MOD/SVR TURB - VOLCANIC ASH - ICING COND - STANDING WATER OR SLUSH
30
Q

MAX FLAP EXTEND ALTITUDE?

A

FL200

31
Q

SPEEDBRAKE LIMITS?

A
  • Use in flight w/flaps beyond 20 not recommended - No use in flight below 800’ AGL
32
Q

MAX FUEL WEIGHTS PER TANK?

A

C = 85k lbs L/R = 43k lbs

33
Q

CENTER TANK MAX FUEL?

A

22,050lbs with less than full main tanks, provided weight of fuel in center plus actual ZFW does not exceed MZFW and balance limits are observed.

34
Q

CTR L/R FUEL PUMP message displays?

A

Respective Switch must be OFF

35
Q

CTR L/R FUEL PUMP message displays when the center tank is empty.

A

BOTH CENTER FUEL SWITCHES OFF

36
Q

MAX FUEL IMBALANCE?

A

2000lbs (+/- 500lbs) So up to 2,500 when main tank is 48k lbs or less Down to 1,500 when main tank exceeds 79,800k lbs

37
Q

MIN FUEL TANK TEMP?

A

3 degrees above freezing point of fuel used -37C for Jet A which has FP of -40C

38
Q

ENG A/I ON?

A

During all GND and FLT OPS when icing conditions exist or are anticipated. * except OAT below -40C SAT

39
Q

ENG A/I ON DURING DESCENT?

A

Must be ON with ENG thrust reduced for descent or speed reduction while in viz moisture with TAT less than 10C, including SAT less than -40C

40
Q

ENG + WING A/I ON?

A

At or below FL220 and prior to reducing thrust for descent, in viz moisture with TAT less than 10C, including SAT less than -40C

41
Q

RVSM LIMITS?

A

SL = 40’(CA vs FO) 75’ (Field Elevation) 5000’ = 45’/75’ 10,000’ = 50’/75’

42
Q

MAX SPEEDS?

A

No max op speed shall be deliberately exceeded. VMO is indicated by max operating airspeed pointer on airspeed indicator.

43
Q

WX RADAR?

A

Do not operate in hangar or within 50’ of personnel or fuel spill.

44
Q

Mmo

A

.86M

Atlas Air B767 (16 decks)

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