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Aviation > AJX B767 Limitations > Flashcards

AJX B767 Limitations Flashcards

1
Q

*Dimensions - Length

A

176’ 4” (53.67m)

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2
Q

*Dimensions - Height

A

52’ (15.85m)

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3
Q

*Dimensions - Span

A

156’ 1” (47.57m)

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4
Q

*Landing Gear Speeds (VLE): Normal

A

Retraction: 270 Kts
Extension: 270 Kts/.82M
Extended: 270 Kts/.82M

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5
Q

*Landing Gear Speeds: Alternate

A

250 Kts/.75M

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6
Q

*Max T-O/Ldg Tailwind

A

RWY Length:
2,001 m or above = 15 Kts
2,000 m or below = 10 Kts

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7
Q

Max Taxi Weight (-300)

A

290,700

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8
Q

Max T/O Weight (-300)

A

288,700

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9
Q

Max Lnd Weight (-300)

A

280,000

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10
Q

Max Zero Fuel Weight (-300)

A

278,000

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11
Q

*Flap Speeds

A 
300/300ER,F 
1                    245/250
5                   225/230
15/20            205/210
25                 175/180
30                 165/170
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12
Q

*Do not extend flaps above _________

A

20,000 ft

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13
Q

*Runway Slope Limit

A

+/- 2%

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14
Q

*Max Operating Pressure Altitude

A

43,100 ft

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15
Q

Max Takeoff and Landing Pressure Altitude

A

8,400 ft

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16
Q

*Photoluminescent Charging:

A

15 minutes = 6.5 hrs

30 minutes = 11 hrs

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17
Q

Verify Ops check of flight deck access system has been accomplished ________

A

once each flight day

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18
Q

*Cat D Circling speed:

A

141 - 165 Kts/1.23 VS1G)

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19
Q

*Max Airspeed

A

.86 M

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20
Q

*Max Cabin Diff Pressure

A

9.1 PSI

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21
Q

*Max Allowable Cabin Diff Pressure for Takeoff/Lnd

A

0.125 PSI (236 ft below airport pressure altitude)

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22
Q

Engine Anti-Ice must be ON during all ground and flight ops when icing conditions exist or are anticipated, except ________

A

when the temperature is below -40 C SAT

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23
Q

Icing Conditions exist when:

A

OAT or TAT in flight is 10 C or below and visible moisture (or vis 1 mile or less)

OAT 10 C or below when operating on ramps, taxiways, or runways where snow, water, slush etc. may be ingested by engines or freeze on engines, nacelles, or engine sensor probes.

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24
Q

*On takeoff, do not engage CWS or CMD mode ____________

A

below 200 ft AGL

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25
Q

*Max allowable wind conditions for autoland:

A

Headwind: 25 Kts
Tailwind: Op Limit (15/10)
Crosswind: 25 Kt

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26
Q

*Use of _______ with autopilot engaged is prohibited

A

aileron trim

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27
Q

Do not use ___________ for ATC communications with ACARS operational.

A

center VHF

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28
Q

Messages that can be transmitted and received over ACARS if they are verified per approved operational procedures:

A

FAT POW

FLEX INF
ATIS
Takeoff Data
Pre-Departure Clearance
Oceanic Clearance
Weight and Balance
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29
Q

*Max N1 RPM

A

117.5%

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30
Q

*Max N2 RPM

A

112.5%

31
Q

*Max EGT/time limit, Takeoff

A

960 C / 5 min

32
Q

*Max EGT, Continuous

A

925 C

33
Q

*Max EGT, Starting

A

750 C (870 C for 40 sec)

34
Q

*Min Oil Pressure

A

10 PSI

35
Q

*Max Oil Temp/time

A

175 C, 15 min

160 C, continuous

36
Q

Max time for takeoff thrust rating (including derated takeoff and reduced takeoff thrust):

A

5 min

37
Q

Reverse Thrust is for _______ only

A

ground use

38
Q

Engine ignition must be ________

A

on for takeoff and landing

39
Q

Engine Limit Display Markings
Max and min limits: ______
Precautionary limits: _____

A

Red

Amber

40
Q

The flight crew shall not blank ____________during takeoff.

A

engine vibration display

41
Q

*Max allowable diff between altitude display for RVSM
Between Capt/Copilot
Capt/Copilot vs field elevation

A

40 ft

75 ft

42
Q

With a single FMC, during VOR approaches one pilot must have ________, no later than ___________.

A

raw data from the VOR on RDMI or HSI in the VOR mode

no later than FAF

43
Q

Two IRS in conjunction with two FMCS, meet requirements of FAA Advisory Circular 25-4 as the sole means of navigation for flights of up to________

A

18 hrs duration

44
Q

*Ground alignment of IRS has been demonstrated to be satisfactory between ______

A

78.2 N and 78.2 S latitudes

45
Q

*In NAV mode the IRS will provide valid magnetic heading and track between ______

A

73 N and 60 S latitudes

46
Q

*The FMCS will provide navigation, guidance, and map display between ________

A

87 N and 87 S latitudes

47
Q

Do not operate weather radar ________

A

in a hangar or within 50 ft of any personnel or fuel spill

hangar/personnel restriction does not apply to test mode

48
Q

*Max Allowable Fuel Weight
Left Main Tank
Right Main Tank
Center Tank (300ER/F)

A

42,671 lb
42,671 lb
84,490 lb

49
Q
  • ________ of fuel may be loaded in the center tank with less than full wing tanks, if all following conditions are met:
    1. wt of fuel in center plus______ does not exceed _______ and balance limits observed.
    2. If fuel jettison installed/activated no less than _____ lb fuel must be in wing tanks
    3. Fuel must be used in accordance with ______
A

22,050 lb

  1. actual Zero Fuel Weight
    Max Zero Fuel Weight
  2. 10,300 lb
  3. Fuel Usage II.
50
Q

Fuel Usage I

A

Use tank to engine fuel feed for takeoff and landing with following procedures:

  • position all operable main tank boost pumps to on
  • Close crossfeed valve.
51
Q

Fuel Usage II (300 ER/F)

A
  1. Use center tank fuel for all ops with operable fuel boost pumps ON and crssfeed closed, then use Fuel Usage I
  2. Intentional dry runnign of center tank pump prohibited
  3. Crossfeed valve(s) is open for minimum fuel operation and may be opened to correct fuel imbalance.
52
Q

Do not reset a ____________ or ____________

A

tripped fuel pump

fuel pump control circuit breaker

53
Q

Use of ________ and __________ fuels are prohibited.

A

Jet B

JP4

54
Q

*Max Tank Fuel Temp

A

49 C

55
Q

*Min Tank Fuel Temp: Fuel Freezing Point

A

+3 C

Note: the use of fuel system icing inhibitor additives does not change min fuel tank temp limit.

56
Q

EGPWS: Do not use ______ for navigation

A

terrain display

57
Q

EGPWS: Do not use the look ahead terrain alerting and terrain display functions:

A

Within 15 NM of takeoff, approach or landing at an airport or runway not contained in the EGPWS airport database or:

  • (PAX, 300 BCF) FMS is in IRS NAV Only or
  • unless FMS Position has been updated within 5 min prior to takeoff or
  • during QFE Operations
58
Q 
*Max Crosswind
   DRY
   WET (Grooved)
   WET (Ungrooved)
   FLOODED
A

33
25
20
10

59
Q 
*Max Crosswind (ICE or SNOW)
BRAKING ACTION:
   GOOD
   MEDIUM to GOOD
   MEDIUM
   MEDIUM to POOR
   POOR
A 
20
20 (15 - RWY less than 2500m)
20 (15 - RWY less than 2500m)
15 (10 - RWY less than 2500m)
10
60
Q

*Max Crosswind SLUSH

A

Depth
2 mm or less 15
3 ~ 12 mm 10

61
Q

*Measured Coefficient of Friction and RCR

   GOOD
   MEDIUM to GOOD
   MEDIUM
   MEDIUM to POOR
   POOR
   VERY POOR
A

COF RCR
.40 + 13+ GOOD
.36-.39 12 MEDIUM to GOOD
.30-.35 10-11 MEDIUM
.26-.29 9 MEDIUM TO POOR
.20-.25 7-8 POOR
.19- 6- VERY POOR

62
Q

*Braking Action (US vs JCAB vs ICAO)
MEDIUM =
VERY POOR =

A

MEDIUM = FAIR
VERY POOR = NIL

If ICAO POOR, confirm COF to determine if JCAB POOR or VERY POOR

63
Q

*The braking action will usually be reported by dividing runway ______________ , then _______________________________.

A

three sections

then the worst braking action among three sections should be applied.

64
Q 
*Takeoff and landing not permitted when depth:
water or slush
wet snow
dry snow (takeoff)
dry snow (landing)
A

water or slush………………….13mm (.51 in)
wet snow…………………………51mm (2.01 in)
dry snow (takeoff)…………..71mm (2.80 in)
dry snow (landing)………..153mm (6.01 in)

65
Q

When the braking action is ______ (or _____) (or the braking coefficient is ____ and below), no takeoff or landing is permitted.

A 
VERY POOR (or NIL)
.19 and below
66
Q

*Min inflight weights
PAX
300F
300BCF

A

179,000 lbs
177,300 lbs
180,400 lbs

Note: the Min Inflight Weight does not include usable fuel.

67
Q

*Flight Maneuvering Load Limits
Flaps Up
Flaps Down

Note: with flaps 25 and 30, positive limits vary linearly from _____ at max landing weight to _____ at max takeoff weight.

A

+2.5g to -1.0g
+2.0 to 0.0 g

Note:
+2.0 g
+1.5 g

68
Q 
*Fuel Freezing Points
Jet A
Jet A-1
JP5
JP8
A
  • 40 C Jet A
  • 47 C Jet A-1
  • 46 C JP5
  • 47 C JP8
69
Q

Total number of PAX (without infants) shall not exceed _____________ (because of emergency evacuation). And shall not exceed the number for which seating accommodation.

A

290

70
Q

*APU altitude limits
For electric
For bleed

A

43,100 ft

17,000 ft

71
Q

*Turbulence penetration speed

A

290/.78

250 < 15,000

72
Q

*Wingtip Strike

A

~15* at 2 ANU

73
Q

*IFR Min Safe ALT:

MEA, _____ above obstacle with in ____ of course.

A

2,000 ft

5 NM

74
Q

*Touchdown Zone (ANA)

A

750 ft to 2,000 ft from threshold

Aviation (1 decks)

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