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AJX Study > Mikes limitations > Flashcards

Mikes limitations Flashcards

1
Q

*Dimensions - Length

A
  • 53.67m
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2
Q

*Dimensions - Height

A
  • 15.85m
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3
Q

*Dimensions - Span

A
  • 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 (300ER)

A
  • 401,000
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8
Q

Max T/O Weight (300ER)

A
  • 400,000
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9
Q

Max Lnd Weight (300ER)

A
  • 320,000
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10
Q

Max Zero Fuel Weight (-300)

A
  • 291,300 with winglets
  • 288,000 without winglets
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11
Q

*Flap Speeds

A
  • 250 F1
  • 230 F5
  • 210 F15/20
  • 180 F25
  • 170 F30
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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
  • 340kts with winglets
  • 360kts without winglets
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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
  • FLEX INF
  • ATIS
  • Takeoff Data
  • Pre-Departure Clearance
  • Oceanic Clearance
  • Weight and Balance
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29
Q

*Max N1 RPM

A
  • 117.50%
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30
Q

*Max N2 RPM

A
  • 112.50%
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)
  • Total
A
  • 42,671 lb
  • 84,490 lb
  • 169,832 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
  • Actual Zero Fuel Weight
  • Max Zero Fuel Weight
  • 10,300 lb
  • 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
  • Use center tank fuel for all ops with operable fuel boost pumps ON and crossfeed closed, then use Fuel Usage I
  • Intentional dry running of center tank pump prohibited
  • 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 or 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
  • (PAX, 300 BCF) FMS is in IRS NAV Only
  • Unless FMS Position has been updated within 5 min prior to takeoff
  • 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
  • GOOD = .40+ = 13+
  • MEDIUM to GOOD = .36-.39 = 12
  • MEDIUM = .30-.35 = 10-11
  • MEDIUM TO POOR = .26-.29 = 9
  • POOR = .20-.25 = 7-8
  • VERY POOR = .19- = 6-
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
  • Wet snow…………………………51mm
  • Dry snow (takeoff)…………..71mm
  • Dry snow (landing)………..153mm
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

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