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*Dimensions - Length
176' 4" (53.67m)
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*Dimensions - Height
52' (15.85m)
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*Dimensions - Span
156' 1" (47.57m)
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*Landing Gear Speeds (VLE): Normal
- Retraction: 270 Kts
- Extension: 270 Kts/.82M
- Extended: 270 Kts/.82M
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*Landing Gear Speeds: Alternate
250 Kts/.75M
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*Max T-O/Ldg Tailwind
- RWY Length:
- 2,001m or above = 15 Kts
- 2,000m or below = 10 Kts
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Max Taxi Weight (-300)
290,700
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Max T/O Weight (-300)
288,700
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Max Lnd Weight (-300)
280,000
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Max Zero Fuel Weight (-300)
278,000
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*Flap Speeds
- (300/300ER,F)
- 1 245/250
- 5 225/230
- 15/20 205/210
- 25 175/180
- 30 165/170
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*Do not extend flaps above _________
20,000 ft
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*Runway Slope Limit
+/- 2%
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*Max Operating Pressure Altitude
43,100 ft
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Max Takeoff and Landing Pressure Altitude
8,400 ft
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*Photoluminescent Charging:
- 15 minutes = 6.5 hrs
- 30 minutes = 11 hrs
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Verify Ops check of flight deck access system has been accomplished ________
once each flight day
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*Cat D Circling speed:
141 - 165 Kts/1.23 VS1G)
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*Max Cabin Diff Pressure
9.1 PSI
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*Max Allowable Cabin Diff Pressure for Takeoff/Lnd
0.125 PSI (236 ft below airport pressure altitude)
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Engine Anti-Ice must be ON during all ground and flight ops when icing conditions exist or are anticipated, except ________
when the temperature is below -40 C SAT
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Icing Conditions exist when:
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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*On takeoff, do not engage CWS or CMD mode ____________
below 200 ft AGL
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*Max allowable wind conditions for autoland:
- Headwind: 25 Kts
- Tailwind: Op Limit (15/10)
- Crosswind: 25 Kt
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*Use of _______ with autopilot engaged is prohibited
aileron trim
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Do not use ___________ for ATC communications with ACARS operational.
center VHF
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Messages that can be transmitted and received over ACARS if they are verified per approved operational procedures:
FAT POW
- FLEX INF
- ATIS
- Takeoff Data
- Pre-Departure Clearance
- Oceanic Clearance
- Weight and Balance
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-
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*Max EGT/time limit, Takeoff
960 C / 5 min
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*Max EGT, Continuous
925 C
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*Max EGT, Starting
750 C (870 C for 40 sec)
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*Max Oil Temp/time
- 175 C, 15 min
- 160 C, continuous
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Max time for takeoff thrust rating (including derated takeoff and reduced takeoff thrust):
5 min
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Reverse Thrust is for _______ only
ground use
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Engine ignition must be ________
on for takeoff and landing
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Engine Limit Display Markings
Max and min limits: ______
Precautionary limits: _____
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The flight crew shall not blank ____________during takeoff.
engine vibration display
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*Max allowable diff between altitude display for RVSM
Between Capt/Copilot
Capt/Copilot vs field elevation
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With a single FMC, during VOR approaches one pilot must have ________, no later than ___________.
raw data from the VOR on RDMI or HSI in the VOR mode
no later than FAF
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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________
18 hrs duration
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*Ground alignment of IRS has been demonstrated to be satisfactory between ______
78.2 N and 78.2 S latitudes
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*In NAV mode the IRS will provide valid magnetic heading and track between ______
73 N and 60 S latitudes
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*The FMCS will provide navigation, guidance, and map display between ________
87 N and 87 S latitudes
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Do not operate weather radar ________
in a hangar or within 50 ft of any personnel or fuel spill
(hangar/personnel restriction does not apply to test mode)
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*Max Allowable Fuel Weight Left Main Tank Right Main Tank Center Tank (300ER/F)
- 42,671 lb
- 42,671 lb
- 84,490 lb
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*________ 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 ______
22,050 lb
1. actual Zero Fuel Weight Max Zero Fuel Weight
2. 10,300 lb
3. Fuel Usage II.
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Fuel Usage I
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.
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Fuel Usage II (300 ER/F)
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.
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Do not reset a ____________ or ____________
- tripped fuel pump
- fuel pump control circuit breaker
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Use of ________ and __________ fuels are prohibited.
-
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*Min Tank Fuel Temp: Fuel Freezing Point
+3 C
Note: the use of fuel system icing inhibitor additives does not change min fuel tank temp limit.
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EGPWS: Do not use ______ for navigation
terrain display
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EGPWS: Do not use the look ahead terrain alerting and terrain display functions:
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
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*Max Crosswind
DRY
WET (Grooved)
WET (Ungrooved)
FLOODED
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*Max Crosswind (ICE or SNOW)
BRAKING ACTION:
GOOD
MEDIUM to GOOD
MEDIUM
MEDIUM to POOR
POOR
- 20
- 20 (15 - RWY less than 2500m)
- 20 (15 - RWY less than 2500m)
- 15 (10 - RWY less than 2500m)
- 10
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*Max Crosswind SLUSH
Depth
- 2 mm or less 15
- 3 ~ 12 mm 10
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*Measured Coefficient of Friction and RCR
GOOD
MEDIUM to GOOD
MEDIUM
MEDIUM to POOR
POOR
COF RCR
- .40 + 13+
- .36-.39 12
- .30-.35 10-11
- .26-.29 9
- .20-.25 7-8
- .19- 6-
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*Braking Action (US vs JCAB vs ICAO)
MEDIUM =
VERY POOR =
MEDIUM = FAIR
VERY POOR = NIL
If ICAO POOR, confirm COF to determine if JCAB POOR or VERY POOR
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*The braking action will usually be reported by dividing runway ______________ , then _______________________________.
three sections
then the worst braking action among three sections should be applied.
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*Takeoff and landing not permitted when depth:
water or slush
wet snow
dry snow (takeoff)
dry snow (landing)
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)
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When the braking action is ______ (or _____) (or the braking coefficient is ____ and below), no takeoff or landing is permitted.
- VERY POOR (or NIL)
- .19 and below
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*Min inflight weights
PAX300F
300BCF
- 179,000 lbs
- 177,300 lbs
- 180,400 lbs
Note: the Min Inflight Weight does not include usable fuel.
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*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.
- +2.5g to -1.0g
- +2.0 to 0.0 g
Note:+2.0 g+1.5 g
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*Fuel Freezing Points
Jet A
Jet A-1
JP5
JP8
- -40 C Jet A
- -47 C Jet A-1
- -46 C JP5
- -47 C JP8
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Total number of PAX (without infants) shall not exceed _____________ (because of emergency evacuation). And shall not exceed the number for which seating accommodation.
290
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*APU altitude limits
For electric ____
For bleed ______
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*Turbulence penetration speed
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*Wingtip Strike
~15* at 2 ANU
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*IFR Min Safe ALT:
MEA, _____ above obstacle with in ____ of course.
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*Touchdown Zone (ANA)
750 ft to 2,000 ft from threshold
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