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Omni 767 > Limitations > Flashcards

Limitations Flashcards

1
Q

L/R Tank Capacity

LBS

A

40,300lbs

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2
Q

Center Tank Capacity

LBS

A

Between 79,9 and 80,1

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3
Q

Total Fuel Capacity

LBS

A

Between 160,3 and 160,7

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4
Q

767-200 Turn Radius

767-300 Turn Radius

A

129’0”

146’0”

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5
Q

767-200 Length

767-300

A

159’2”

180’3”

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6
Q

767-200 Wingspan

767-300

A

156’1”

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7
Q

767-200 Height

767-300

A

52’0”

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8
Q

Minimum Oil Quantity

A

17 qts

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9
Q

767-200 Tail-strike pitch

767-300

A
  1. 1 deg

9. 6 deg

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10
Q

Average Burn Rate

A

11,000pph

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11
Q

Flap 30 Approach mandatory when

A

Runway less than 7000ft

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12
Q

Autobrake mandatory when

2

A

Rwy -7000ft

A/B 3+ when CatIII, Wet/Slippery, Rollout distance limited

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13
Q

Assumed Temp not allowed when

2

A

Windshear/windshear advisory

Contaminated Rwys

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14
Q

Turbulence Speed

A

290kts/M 0.78

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15
Q

Max Take off and Ldg TW component

A

15kts

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16
Q

CAT II/CAT III Max Wind components

HW
XW
TW

A

25kts

15kts (30 for Cat I)

15kts

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17
Q

Max Flap extension Altitude

A

20,000ft

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18
Q

Engine warmup procedures in Icing and cold weather conditions

A

Run engine up to 60%N1 for 30 seconds at intervals of no greater than 30 minutes.

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19
Q

Speedbrake usage not allowed when…

2

A

Below 800ft RA
Or
Flaps in Landing position

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20
Q

The Navigation and display system does not support operations at a Latitude greater than

A

87 degrees North or South

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21
Q

In Flight Apu Bleed air is available up to

A

17,000ft

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22
Q

Icing conditions exist when

A

OAT or TAT is 10c and visible moisture in any form is present

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23
Q

Apu’s electrical power availability

A

Throughout the airplane’s operating envelope

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24
Q

When does the Cabin Altitude light come on

A

10,000ft

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25
Q

On Descent when does the Cabin Altitude light go out

A

8,500ft

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26
Q

At what Cabin Altitude does the Outflow valve automatically close

A

11,000ft

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27
Q

At what Cabin Altitude will the Outflow Valve re-open

A

9,500ft

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28
Q

At what Cabin Altitude will the Masks drop

A

14,000ft

29
Q

Gear Limit Speeds
Retract
and
Extend/Extended

A

270kts

270kts/0.82M

30
Q

Flap Setting Numbers

A 
1
5
15
20
25
30
31
Q

Flap Limit Speeds 767-200/300

A 
767-200/300
Flap 1 -    250/250
Flap 5 -   225/230
Flap 15 - 210/210
Flap 20 - 205/210
Flap 25 - 190/180
Flap 30 - 170/170
32
Q 
Flap Maneuvering Speeds
1
5
15
20
25
30
A 
1 - Vref30+60
5 - Vref30+40
15-Vref30+20
20-Vref30+20
25-Vref25
30-Vref30
33
Q

ICAO Holding Altitudes/Speeds

A

Through 14,000ft - 230kts
14,000-20,000 - 240kts
20,000-34,000 - 265kts
34,000+ - 0.83M

34
Q

FAA Holding Speeds

A

Through 6,000ft - 200kts
6,001-14,000 - 230kts exempt. (DCA/JFK 210kts)
14,001+ - 265kts

35
Q

Max Operating Altitude

A

43,100

36
Q

Lowest Altitude FLCH can be used

A

1000ftAGL

37
Q

Turbulent air penetration speed

A

290kts/ 0.78M

38
Q

Max Allowed in-Flight difference between Capt and F/O altimeter in RVSM ops

A

200ft

39
Q

No WX radar operations within ____ of refueling ops or fuel spill

A

50ft

40
Q

Do the ABORTED ENGINE START Checklist when

4

A
  1. EGT does not increase by 25seconds after fuel control switch is moved to RUN
  2. EGT quickly nears or exceeds start limit
  3. Oil pressureindication is not normal after engine stabilization
  4. No N1 Rotation by 30 seconds after N2 stabilizes
41
Q

Engine Start Duty Cycle

A

Up to 5 minutes on followed by 30second cooldown for each minute on
Two 5 minute cycles, followed by a 10 minute cool period

42
Q

Oil temp requirement for T/O

A

Must be above the bottom of the Temp Scale before T/O

43
Q

Fuel Jettison rate

A

1300ppm

44
Q

Main Gear Width

A

30’6”

45
Q

Minimum O2 pressure required for DX
ETOPS
Non-ETOPS

A

1500psi

1250psi

46
Q

Minimum A/P engagement altitude

A

200ft AGL

47
Q

Cargo door limitations

Operate

Leave Open

A

40kts

65kts

48
Q

Engine oil warmup requirements

A

Oil temp must be above the bottom of temp scale

49
Q

Engine warmup/cool-down recommendation

A

3minutes

50
Q

Cold WX Engine Start

A

If Engine cold soaked for more than 4 hrs at -34c do not start

51
Q

APU Starter Duty cycle

A

3 consecutive starts/attempts within 60minutes

52
Q

Min Fuel temp

A

3c above the freeze point of the fuel being used

53
Q

When does fuel config light come on?

A
  1. +1200lbs in Center tank and fuel pumps off
  2. Less than 2200lbs
  3. Imbalance greater than 2000 +-500
54
Q

Fuel control Switch to Run when

A

Above 20%

Minimum 15%

55
Q

N495AX Do not use autopilot below ____ RA at airport pressure above _______

A

100ft RA

8,400ft

55
Q

Can we use aileron trim with A/P engaged

A

No

55
Q

When are flight crew not allowed to blank engine VIB displays

A

During Take off

56
Q

767-300 MRW

A

413,000

57
Q

767-300 MTOW

A

412,000

58
Q

767-300 MLW

A

320,000

59
Q

767-300 MZFW

A

295,000

60
Q

767-200 MRW

A

396,000

61
Q

767-200 MTOW

A

395,000

62
Q

767-200 MLW

A

300,000

63
Q

767-200 MZFW

A

260,000

64
Q

767-300winglets (N342AX) MRW

A

409,000

65
Q

767-300winglets (N342AX) MTOW

A

408,000

66
Q

767-300winglets (N342AX) MLW

A

320,000

67
Q

767-300winglets (N342AX) MZFW

A

295,000

Omni 767 (10 decks)

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