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Atlas 767 > Limitations > Flashcards

Limitations Flashcards

1
Q

Why are some items bold and shaded for easy identification?

A
  • Memory Recall Items.
  • Safety of Flight
  • Time sensitive, not allowing reference to FCOM
  • No Placard, Marking, light, or indication.
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2
Q

Noise Level

A

ICAO Annex 16 Volume 1 Noise Requirements

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3
Q

Runway Slope

A

+/- 2%

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4
Q

Max Op ALT

A

43,100’

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5
Q

Max TO/LNDG Altitude

A

8,400’ PA

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6
Q

Turbulent Air Penetration

A

290 KIAS / .78M whichever is lower

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7
Q

Max TO / LNDG Tailwind COMPONENT

A

10 KTS

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8
Q

Ground Wind Limit for all doors

A
  • 40 KTS while opening or closing

- 60/65 KTS (300/200) while open.

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9
Q

TO/LNDG X-WIND GUIDLINES

A 
Good / Dry - 40/40
Good / Wet - 25/40
Good-Med. - 20/35
Med. - 17/25
Med. - Poor - 15/17
Poor - 13/15
Nil - N/A
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10
Q

Minimum In-Flight Weight Limit

A
  • Does not include usable fuel
  • 300P - 179,000 #
  • 300F - 177,300#
  • 200SF - 168,000#
  • MW - 76,203 kgs
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11
Q

Max Weights (300P)

A
  • MTW 409,000 #
  • MTOW - 408,000 #
  • MLW - 320,000#
  • MZFW - 295,000#
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12
Q

MTW (all)

A
  • 300P - 409 K#
  • 300F - 413 K#
  • 200SF - 312 K# / 317 K#
  • MW - 146,056 kg
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13
Q

MTOW (all)

A
  • 300P - 408 K#
  • 300F - 412 K#
  • 200SF - 310 K# / 315 K#
  • MW - 145,149 kg
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14
Q

MLW (all)

A
  • 300P - 320 K#
  • 300F - 326 K#
  • 200SF - 272 K#
  • MW - 122,469 kg
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15
Q

MZFW

A
  • 300P - 295 K#
  • 300F - 312.3 K#
  • 200SF - 253 K#
  • MW - 112,490 kg
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16
Q

O2

A
  • 1350 psi ETOPS

- 1250 psi NON-ETOPS

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17
Q

Cabin Pressurization

A

Max Differential - 9.10 psi

Max Differential for TO / LNDG .125 psi (236’ below QFE)

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18
Q

APU Starter

A
  • Maximum 3 attempts in 60 Minute Period

- 1 Minute minimum between attempts (APU SEL - OFF)

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19
Q

APU BL AIR

A

Not Available above 17,000’

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20
Q

AUTOPILOT - Aileron trim

A
  • Don’t use aileron trim with autopilot engaged.
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21
Q

AutoPilot Engaged Minimum Heights

A
  • TO / GA - 250’ AGL
  • Non-ILS - 50’ below MDA
  • Single Channel ILS - 100’ AGL
  • AutoLand - Touchdown/Rollout
  • MW - On TO, do not engage CWS below 200’ AGL or CMD Mode below 1000’ AGL
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22
Q

FLCH

A
  • Do not use FLCH on final approach below 1000’ AGL
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23
Q

AutoLand Advisory

A
  • Touchdown assumed 2500’ from threshold.
  • AutoLand will be made with FLAPS 25 or 30.
  • Do not use Autoland for an overweight landing.
  • Do not use with apparent erroneous RA information.
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24
Q

Maximum Autoland Wind Components

A
  • Headwind / X-Wind - 25 KTS
  • X-Wind CAT II/III - 15 KTS
  • Tailwind - 10KTS
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25
Q

Circuit Breakers

A
  • Do NOT reset tripped FUEL PUMP circuit breakers.
  • Other CBs may be reset once, after a 2 Min Cooling Period, if safety related.
  • MX resets CBs on ground.
26
Q

Radios

A
  • Do not use the Center VHF Radio for voice Comm.
  • Do not use the HF Radios during refueling
  • Do not TX on both HF Radios at once.
27
Q

Doors

A
  • Check the armed slides and girt bar prior to taxi, TO, and landing whenever PAX are carried.
  • Verify Flight Deck Access System once each flight day.
28
Q

Engine Thrust Rating

A
  • CF6-80C2B6F - 60,200 #
  • CF6-80C2B7F - 62,100 #
  • PW4060 - 60,200 #
  • JT9D-7R4D / CF6-80A - 46,900 #
29
Q

N1 RPM Limits

A
  • CF6 - 80C - 117.5%
  • CF6 - 80A - 117.0%
  • PW4060 - 111.4%
  • JT9D-7R4D - 104.7%
30
Q

N2 RPM Limits

A
  • CF6 - 80C2B6/7F - 112.5%
  • CF6 - 80A - 110.5%
  • PW4060 - 105.5%
  • JT9D - 7R4D - 102.5%
31
Q

CF6 - 80C EGT Limits

A
  • START - 750 (GRND)
  • START - 750 (In-Flight)
  • TO - 960 (5 Minutes / 10 min* for SE Ops)(LBOOk)
  • Max CONT - 925
  • NOT 640, 645, 650-9, MW; These are 5 minute A/C.
32
Q

GE Starter Duty Limits

A
  • Continuous for 5 minutes.
  • Cool 30 seconds per minute of operation
  • Re-engament N2
  • 0% Recommended, 0-20% Permissible, 21-30% - Only In Case of Fire, 31% may result in starter damage.
33
Q

Oil

A
  • Minimum Pressure - 10 (35 for JT9D)(70 for PW4060)
  • Max TEMP - 160 (CONT) 175 (15 Min)
  • (135/163 (20 Min)(JT9D)) (163/177 (20 Min)(PW4060))
  • 17 QTS to Dispatch
  • Note: PW4060 must be warmer than 50C before TO
34
Q

Ignition

A

Continuous Ignition must be ON (Starter SEL - CONT):

  • MOD and HVY Rain
  • MOD and SEV Turbulence
  • Volcanic Ash
  • Icing Conditions
  • TO / LNDG
  • Standing Water or Slush on the RNWY
  • AUTO with Engine Anti-Ice ON
  • AUTO with LE Flap extension
35
Q

Vibration Display

A

Do not blank during TO.

36
Q

Reverse Thrust

A
  • GRND OPS ONLY / Intentional selection in-flight prohibited.
  • DO NOT BACK THE AIRPLANE USING REV.
37
Q

Flaps

A

Do not extend below 20,000’

38
Q

Load Limits

A

Flaps Up - -1.0 - 2.5g
Flaps Down - 0 - 2.0g
Flaps 25/30 - 1.5 - 2.0g, linear relation, MTOW - MLW

39
Q

Speedbrakes

A
  • Use of Speedbrakes in flight with FLPS beyond 20 is not recommended.
  • Do not use speedbrakes below 800’ AGL
40
Q

ATC CLRNC data, received through the FMC that can only be viewed by using the flight deck printer ….

A

Must be independently verified with the originating ground station.

41
Q

Navigational equipment

A
  • ETOPS - L+R CDU, 2 FMCs, L+C IRU, LNAV A/P
  • NAT HLA PBCS / RNP4 - same^^
  • NAT non-PBCS / RNP10 / Class II - same^^ less 1 FMC
  • Intl. Class 1 - 1 FMC, 1 CDU, C+1 IRU, LNAV A/P
  • RVSM - 2 ADC, ALT HOLD, Altitude Alerting, and XPNDR.
42
Q

Surveillance

A

CDU, FMC, SATCOM, ACARS

43
Q

Center Tank Pumps

A
  • Do not cycle center tank pump ON/OFF/ON with any continuos low pressure indication.
44
Q

Max Fuel Quantity

A 
Center Tank - 85,200#
Main Tanks - 43,097# each
Total -171.4 K#
(762 Same, except Center Tank - 30,551#)
(762 Total - 116.7 K#)
45
Q

Fuel Balance

A
  • Fill Main tanks first.
  • No more than 22.0 K# in Center Tanks with less than full Main Tanks.
  • Actual ZFW + C Fuel < MZFW, with less than full mains.
  • Max imbalance is 1500# - 2500# when total main tank fuel is 79,800# - 48,000#.
  • Jettison active - no less than 10,300# in wing tanks
46
Q

Fuel Temp

A
  • In flight fuel temperature must be held +3 degrees above freezing point (-40 for Jet A)
  • The use of Fuel System Icing Inhibitors does not change the minimum fuel tank temperature limit.
47
Q

Which Fuels can we not use?

A
  • JP4 and Jet B

- If in doubt, double check current GE and/or PW specs.

48
Q

Icing Conditions

A
  • OAT, or TAT in-flight, is less than 10 degrees C, and

- visible moisture, standing water… (visibility is 1 mi or less)

49
Q

Auto Ice Detect System (-300F)

A
  • Engine anti-ice ON for ground operations.

- In flight, use the auto system.

50
Q

Engine Anti-Ice

A
  • Engine Anti-Ice must be ON during ground ops when icing conditions are anticipated.
51
Q

Ice Crystal Operating Conditions

A
  • Engine Anti-Ice ON (NOT AUTO) @ any temp.
  • Wing Anti-Ice ON in Ice Crystal Icing, below 22000’
  • ICI Characteristics:
  • Amber/Red Radar returns below A/C
  • Apparent Rain, odd noise, &/or abnormally low temp.
  • A/T unable to maintain airspeed.
  • EICAS TAT stays near 0 C
52
Q

Window Heat

A

ON for all normal ops.

53
Q

RVSM Equipment

A
  • STBY Altimeters do not meet accuracy requirements.
  • 200’ Max in-flight difference between CAPT and FO.
  • 40’ 45’ or 50’ Max difference on the ground at sea level, 5000’ and 10000’ Field Elevations.
  • 75’ Max difference with Field Elevation.
54
Q

VMO / MMO

A
  • Barber Pole / .86
55
Q

Flap Speeds 763 / 762

A
  • Flaps 1 - 250 / 240
  • Flaps 5 - 230 / 220
  • Flaps 15 - 210 / 210
  • Flaps 20 - 210 / 195
  • Flaps 25 - 180 / 190
  • Flaps 30 - 170 / 162
56
Q

VLO/LE

A

270 kts / .82 whichever is lower.

57
Q

Look Ahead Terrain Alerting

A
  • Not for NAV.
  • Authorized to Deviate from ATC for EGPWS Alert.
  • For airfields not in EGPWS database, look-ahead terrain alerting not authorized within 15 nm. Check INTAM.
58
Q

Dimensions

A

WS - 156’1” (47.6 M) / 166’11” (50.88M)
L - 159’2” (48.51M) / 180’3” (55M)
H - 52’ (15.85M)
TR - 129’ (39.3M) / 146’ (44.6M)

59
Q

JT9D EGT Limits (PW4060)

A
  • Starting (Ground) - 535
  • Starting (Flight) - 625 (650)
  • Takeoff - 625 (650) - 5 Minutes
  • Max Continuous - 600 (625) - Continuous
60
Q

EGT Limits (MW) (GE CF6-80A)

A
  • Starting - Ground - 750
  • Starting - Flight - 750
  • Takeoff - 940 - 5 Minutes
  • Max Continuous - 895 - Continuous

Atlas 767 (14 decks)

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