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Atlas B767 > Limitations > Flashcards

Limitations Flashcards

(54 cards)

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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

Study These Flashcards
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

Study These Flashcards
A

max 3.25 degrees

min 2.5 degrees

25
Autoland wind limitations
HW/XW: 25 kts XW CAT II/III: 15 kts Tailwind: 10 kts
26
HF Radios
DO NOT USE during REFUELING
27
Circuit breaker reset policy
Reset of FUEL PUMP or FUEL PUMP CONTROL prohibited in flight. Reset not recommended, if required reset once after 2 min cooling period
28
Engine Starter Duty Cycle
Continuous for 5 minutes | Cool for 30 seconds per minute of operation
29
Engine starter re-engagement N2
0% recommended 0-20% Permissible 21-30% only in case of fire >30% may result in starter damage
30
Continuous ignition must be on encountering:
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
Vibration Display
Flight crew shall not blank engine vibration display during takeoff
32
Reverse Thrust
Don't use in flight | Don't back up with reverse thrust
33
Flaps
Max altitude with flaps extended is 20,000'
34
Maneuvering Load Limits
Flaps Up +2.5/-1.0 | Flaps Down +2.0/0.0
35
Speedbrakes
Do not extend in flight with flaps 25 or 30 | Do not extend in flight below 800' AGL.
36
UNABLE RNP
Pilots MUST go around unless visual references can be established and maintained
37
Approaches NOT AUTHORIZED
FAA: RNAV (RNP) ICAO: RNP (AR) RNAV (RNP1) Departures- with Radius-to-fix (RF) required
38
Fuel Loading (-300)
Center tank: 85,200 lbs | L/R Main tanks: 43,097 lbs
39
Fuel Loading (-200)
Center tank: 30,551 lbs | L/R Main tanks: 43,097 lbs
40
Fuel Usage 1 (no center take fuel)
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
Fuel Usage 2 (fuel in center tank)
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
Center tank fuel pumps
must be OFF when CTR L/R FUEL PUMP message | Both center tank fuel switches must be OFF when above message
43
Max fuel imbalance
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
Fuel Tank Temperatures
Must be at least 3C above fuel freezing point Max fuel temp 49C Jet B and JP4 fuels prohibited
45
Engine and wing anti-ice
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
Ops in Ice Crystals (GE)
engine anti-ice ON when ice crystal conditions exist, even below -40C Auto ice detection ON
47
Window Heat
ON for all normal flight conditions
48
RVSM
Max diff between alts is 200' in flight
49
Flap Speed (-300)
``` 1--250 5--230 15--210 20--210 25--180 30--170 ```
50
Flap Speed (-200)
``` 1--240 5--220 15--210 20--195 25--190 30--162 ```
51
Landing Gear operating and extended
270/0.82 Mach (lower)
52
GPWS
Look-ahead function prohibited within 15 mn of takeoff, approach or landing at airports not in GPWS database Prohibited during QFE operations
53
Ground Proximity Terrain Override to OVRD if:
FMS in IRS NAV only | prior to takeoff, FMS position updating not accomplished or runway position not verified
54
Weather Radar
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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