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Atlas B767 > Limitations > Flashcards

Limitations Flashcards

1
Q

Approved Operations

A

Visual (VFR)
Instrument (IFR)
Icing
Extended Overwater (ETOPS, except -200SF)

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2
Q

Runway slope

A

+/-2 percent

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3
Q

Max operating altitude

A

43,100’ PA

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4
Q

Max T/O and LDG alt

A

8,400’ PA

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5
Q

Max t/o and ldg tailwind

A

10 kts

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6
Q

Ground wind limits for entry and lower cargo doors

A

40 kts while opening or closing

While open:

  • 65 kts (-300)
  • 60 kts (-200)
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7
Q

Main deck cargo compartment door operation

A

May be operated and held at CANOPY or FULLY OPEN in steady wind up to 40 kts

If FULLY OPEN, block wind with fuselage

If winds oscillate door or exceed 40 kts, move to CANOPY

Wind gusts up to 60 kts in CANOPY only

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8
Q

MTW (641GT)

A

409,000 lbs

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9
Q

MTOW (641GT)

A

408,000

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10
Q

MLW (641GT)

A

320,000 lbs

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11
Q

MZFW (641GT)

A

295,000

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12
Q

Min inflight weight (641GT)

A

179,000

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13
Q

Turbulent air penetration speed

A

290/.78 Mach (whichever lower)

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14
Q

Preflight Oxygen Quantity

A

1350 ETOPS

1250 nonETOPS

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15
Q

Supplemental Oxygen Bottles (-300 Freighter)

A

O2 bottles with masks by supernumerary seats, rigid barrier, and crew lab must be full before flights with supernumeraries.

Portable bottle with mask must be stored in supernumeraries area

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16
Q

When must the smoke barrier door be closed?

A

Taxi, takeoff, flight and landing

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17
Q

Max cabin diff pressure

A
  1. 10 psi

0. 125 psi (for T/O and LDG)

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18
Q

APU Start cycle limits

A

3 attempts in 60 minutes

Time between attempts (APU selector OFF) 1 min

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19
Q

APU Bleed Air limit

A

17,000’

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20
Q

Autopilot engaged- Aileron trim

A

use of aileron trim with autopilot engaged prohibited

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21
Q

Autopilot engaged minimum altitudes

A

Takeoff/Go-Around: 250’ AGL
Non-ILS approach: 50’ below MDA/DA
Single Channel ILS: 100’ AGL
Autoland (two or three autopilots): touchdown/rollout

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22
Q

Autoland with erroneous RA

A

Do not use autoland with either L or R RA providing erroneous altitude

23
Q

Flap setting with autoland

24
Q

Glideslope angle w/autoland

A

max 3.25 degrees

min 2.5 degrees

25
Q

Autoland wind limitations

A

HW/XW: 25 kts
XW CAT II/III: 15 kts
Tailwind: 10 kts

26
Q

HF Radios

A

DO NOT USE during REFUELING

27
Q

Circuit breaker reset policy

A

Reset of FUEL PUMP or FUEL PUMP CONTROL prohibited in flight.

Reset not recommended, if required reset once after 2 min cooling period

28
Q

Engine Starter Duty Cycle

A

Continuous for 5 minutes

Cool for 30 seconds per minute of operation

29
Q

Engine starter re-engagement N2

A

0% recommended
0-20% Permissible
21-30% only in case of fire
>30% may result in starter damage

30
Q

Continuous ignition must be on encountering:

A

Eng start selector in the CONT position when:

Mod to heavy rain
Mod to severe turb
Volcanic Ash
Icing conditions
Standing water or slush on runway

Continuous ignition is automatically provided when engine anti-ice is on or with LE flap extension

31
Q

Vibration Display

A

Flight crew shall not blank engine vibration display during takeoff

32
Q

Reverse Thrust

A

Don’t use in flight

Don’t back up with reverse thrust

33
Q

Flaps

A

Max altitude with flaps extended is 20,000’

34
Q

Maneuvering Load Limits

A

Flaps Up +2.5/-1.0

Flaps Down +2.0/0.0

35
Q

Speedbrakes

A

Do not extend in flight with flaps 25 or 30

Do not extend in flight below 800’ AGL.

36
Q

UNABLE RNP

A

Pilots MUST go around unless visual references can be established and maintained

37
Q

Approaches NOT AUTHORIZED

A

FAA: RNAV (RNP)
ICAO: RNP (AR)
RNAV (RNP1) Departures- with Radius-to-fix (RF) required

38
Q

Fuel Loading (-300)

A

Center tank: 85,200 lbs

L/R Main tanks: 43,097 lbs

39
Q

Fuel Loading (-200)

A

Center tank: 30,551 lbs

L/R Main tanks: 43,097 lbs

40
Q

Fuel Usage 1 (no center take fuel)

A

Use tank-to-engine fuel feed for t/o and ldg with all operable main tank boost pumps on and the crossfeed valves closed

41
Q

Fuel Usage 2 (fuel in center tank)

A

Use center tank fuel for all ops with all operable boost pumps on and the crossfeed valves closed until center tank fuel is depleted, then use *Fuel Usage 1

42
Q

Center tank fuel pumps

A

must be OFF when CTR L/R FUEL PUMP message

Both center tank fuel switches must be OFF when above message

43
Q

Max fuel imbalance

A

2,500 lbs when total main tank is 48,000 lbs or less

1,500 lbs when total main tank fuel exceeds 79,800 lbs

44
Q

Fuel Tank Temperatures

A

Must be at least 3C above fuel freezing point
Max fuel temp 49C
Jet B and JP4 fuels prohibited

45
Q

Engine and wing anti-ice

A

ON when icing exists except when OAT below -40C SAT
Auto ice detection switches in AUTO during flight
Must be on when thrust reduced for descent or speed reduction in visible moisture with the TAT less than 10C including SAT less than -40C

46
Q

Ops in Ice Crystals (GE)

A

engine anti-ice ON when ice crystal conditions exist, even below -40C
Auto ice detection ON

47
Q

Window Heat

A

ON for all normal flight conditions

48
Q

RVSM

A

Max diff between alts is 200’ in flight

49
Q

Flap Speed (-300)

A 
1--250
5--230
15--210
20--210
25--180
30--170
50
Q

Flap Speed (-200)

A 
1--240
5--220
15--210
20--195
25--190
30--162
51
Q

Landing Gear operating and extended

A

270/0.82 Mach (lower)

52
Q

GPWS

A

Look-ahead function prohibited within 15 mn of takeoff, approach or landing at airports not in GPWS database

Prohibited during QFE operations

53
Q

Ground Proximity Terrain Override to OVRD if:

A

FMS in IRS NAV only

prior to takeoff, FMS position updating not accomplished or runway position not verified

54
Q

Weather Radar

A

Avoid operation in hangar or within 50’ of fueling ops or fuel spill

Avoid operating when people in area normally enclosed by aircraft nose radome

Atlas B767 (1 decks)

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