Mikes limitations Flashcards
*Dimensions - Length
- 53.67m
*Dimensions - Height
- 15.85m
*Dimensions - Span
- 47.57m
*Landing Gear Speeds (VLE): Normal
- Retraction: 270 Kts
- Extension: 270 Kts/.82M
- Extended: 270 Kts/.82M
*Landing Gear Speeds: Alternate
- 250 Kts/.75M
*Max T-O/Ldg Tailwind
RWY Length:
- 2,001 m or above = 15 Kts
- 2,000 m or below = 10 Kts
Max Taxi Weight (300ER)
- 401,000
Max T/O Weight (300ER)
- 400,000
Max Lnd Weight (300ER)
- 320,000
Max Zero Fuel Weight (-300)
- 291,300 with winglets
- 288,000 without winglets
*Flap Speeds
- 250 F1
- 230 F5
- 210 F15/20
- 180 F25
- 170 F30
*Do not extend flaps above _________
- 20,000 ft
*Runway Slope Limit
- +/- 2%
*Max Operating Pressure Altitude
- 43,100 ft
Max Takeoff and Landing Pressure Altitude
- 8,400 ft
*Photoluminescent Charging:
- 15 minutes = 6.5 hrs
- 30 minutes = 11 hrs
Verify Ops check of flight deck access system has been accomplished ________
- Once each flight day
*Cat D Circling speed:
- 141 - 165 Kts (1.23 VS1G)
*Max Airspeed
- .86 M
- 340kts with winglets
- 360kts without winglets
*Max Cabin Diff Pressure
- 9.1 PSI
*Max Allowable Cabin Diff Pressure for Takeoff/Lnd
- 0.125 PSI (236 ft below airport pressure altitude)
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
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
*On takeoff, do not engage CWS or CMD mode ____________
- Below 200 ft AGL
*Max allowable wind conditions for autoland:
- Headwind: 25 Kts
- Tailwind: Op Limit (15/10)
- Crosswind: 25 Kt
*Use of _______ with autopilot engaged is prohibited
- Aileron trim
Do not use ___________ for ATC communications with ACARS operational.
- Center VHF
Messages that can be transmitted and received over ACARS if they are verified per approved operational procedures:
- FLEX INF
- ATIS
- Takeoff Data
- Pre-Departure Clearance
- Oceanic Clearance
- Weight and Balance
*Max N1 RPM
- 117.50%
*Max N2 RPM
- 112.50%
*Max EGT/time limit, Takeoff
- 960 C / 5 min
*Max EGT, Continuous
- 925 C
*Max EGT, Starting
- 750 C (870 C for 40 sec)
*Min Oil Pressure
- 10 PSI
*Max Oil Temp/time
- 175 C, 15 min
- 160 C, continuous
Max time for takeoff thrust rating (including derated takeoff and reduced takeoff thrust):
- 5 min
Reverse Thrust is for _______ only
- Ground use
Engine ignition must be ________
- On for takeoff and landing
Engine Limit Display Markings Max and min limits: ______ Precautionary limits: _____
- Red
- Amber
The flight crew shall not blank ____________during takeoff.
- Engine vibration display
*Max allowable diff between altitude display for RVSM Between Capt/Copilot, Capt/Copilot vs field elevation
- 40 ft
- 75 ft
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
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
*Ground alignment of IRS has been demonstrated to be satisfactory between ______
- 78.2 N and 78.2 S latitudes
*In NAV mode the IRS will provide valid magnetic heading and track between ______
- 73 N and 60 S latitudes
*The FMCS will provide navigation, guidance, and map display between ________
- 87 N and 87 S latitudes
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
*Max Allowable Fuel Weight
- Left Main Tank / Right Main Tank
- Center Tank (300ER/F)
- Total
- 42,671 lb
- 84,490 lb
- 169,832 lb
*________ 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
- Actual Zero Fuel Weight
- Max Zero Fuel Weight
- 10,300 lb
- Fuel Usage II.
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
Fuel Usage II (300 ER/F)
- 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
Do not reset a ____________ or ____________
- Tripped fuel pump or fuel pump control circuit breaker
Use of ________ and __________ fuels are prohibited.
- Jet B
- JP4
*Max Tank Fuel Temp
- 49 C
*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
EGPWS: Do not use ______ for navigation
- Terrain display
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
- (PAX, 300 BCF) FMS is in IRS NAV Only
- Unless FMS Position has been updated within 5 min prior to takeoff
- During QFE Operations
*Max Crosswind
- DRY
- WET (Grooved)
- WET (Ungrooved)
- FLOODED
- 33
- 25
- 20
- 10
*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
*Max Crosswind SLUSH
- Depth 2 mm or less 15
- 3 ~ 12 mm 10
*Measured Coefficient of Friction and RCR
- GOOD
- MEDIUM to GOOD
- MEDIUM
- MEDIUM to POOR
- POOR
- VERY POOR
- 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-
*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
*The braking action will usually be reported by dividing runway ______________ , then _______________________________.
- Three sections then the worst braking action among three sections should be applied
*Takeoff and landing not permitted when depth:
- Water or slush
- Wet snow
- Dry snow (takeoff)
- Dry snow (landing)
- Water or slush………………….13mm
- Wet snow…………………………51mm
- Dry snow (takeoff)…………..71mm
- Dry snow (landing)………..153mm
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
*Min inflight weights
- PAX
- 300F
- 300BCF
- 179,000 lbs
- 177,300 lbs
- 180,400 lbs
- Note: the Min Inflight Weight does not include usable fuel
*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
*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
Total number of PAX (without infants) shall not exceed _____________ (because of emergency evacuation). And shall not exceed the number for which seating accommodation.
- 290
*APU altitude limits
- For electric
- For bleed
- 43,100 ft
- 17,000 ft
*Turbulence penetration speed
- 290/.78
- 250 < 15,000
*Wingtip Strike
- ~15* at 2 ANU
*IFR Min Safe ALT: MEA, _____ above obstacle with in ____ of course.
- 2,000 ft
- 5 NM
*Touchdown Zone (ANA)
- 750 ft to 2,000 ft from threshold
