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%