AFTER TAKE-OFF

BEFORE DESCENT

VREF for Slats/Krueger - 0?and Flaps - 20?Configuration

BEFORE LANDING

TAKE-OFF WITH SLATS/KRUEGER RETRACTED

PERFORMANCE CORRECTIONS

Take-off Speeds; SLATS - 0? Flaps - 20?Dry and Wet Runway

Take-off Speeds; Slats - 0? Flaps - 20?

Maximum take-off weight as permitted by brake energy requirements Slats - 0o; flaps - 20o; Dry and Wet runway

Maximum Take-off Weight As Permitted By Brake Energy Requirements Slats - 0? Flaps - 20?

HONEYWELL ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)

Honeywell ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) MK. V WITH COLLINS PROLINE 4 V6.1

USER SELECTABLE CALLOUTS

GENERAL

TERRAIN PROXIMITY WARNING

Terrain Awareness Display

ALERTS AND WARNINGS

EGPWS Controls and Indicators

ROCKWELL COLLINS FMS-6100 FLIGHT MANAGEMENT SYSTEM

Rockwell COLLINS FMS-6100 FLIGHT MANAGEMENT SYSTEM

VSPEEDS FUNCTION

BRAKE COOLING

BRAKE KINETIC ENERGY (BKE) AND BRAKE COOLING

GENERAL

MAXIMUM BRAKE ENERGY

BKE DETERMINATION DURING LANDING OR RTO OPERATIONS

FLIGHT PLANNING

REDUCED BKE PROCEDURES

TAXI BKE

BRAKE COOLING FOR QUICK TURN-AROUND AND MULTIPLE BRAKING OPERATIONS

BRAKE KINETIC ENERGY (BKE) CONSIDERATIONS DURING TRAINING FLIGHTS AND FLIGHT/GROUND TESTING

FUSE PLUG INTEGRITY ZONES

USE OF BKE AND COOLING CHART

BKE/Cooling chart. Sheet 1 of 2

BKE/Cooling chart. Sheet 2 of 2

Supplement 12 - MAXIMUM TAKE-OFF WEIGHT = 35,650 LB

MAXIMUM Take-off WEIGHT = 35,650 LB

WEIGHT LIMITATIONS

CENTER-OF-GRAVITY LIMITATIONS

Center-of-Gravity Envelope

CONTAMINATED RUNWAY OPERATIONS

Take-off Distance - Flaps - 20?Weight = 35,650 LB; Runway Contaminated by Slush, Standing Water or Loose Snow; 

Landing Distance Corrections

WEIGHT LIMITATIONS

Maximum Fuel - Zone 2

Center-of-Gravity Envelope

Center Of Gravity Envelope Limits

WEIGHT LIMITATIONS

Maximum Fuel Loading - Zone 2 Metric Measurements

Center-of-Gravity Envelope

Center Of Gravity Envelope Limits Metric Measurements

TAKE-OFF AND LANDING OPERATIONS AT ULAANBAATAR, MONGOLIA (ZMUB)

TAKE-OFF AND LANDING OPERATIONS AT ULAANBAATAR, MONGOLIA (ZMUB)

GENERAL

TAKE-OFF REQUIREMENTS

LANDING REQUIREMENTS

Ulaanbaatar Airport (ZMUB) Layout

OIS 1- TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES

TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES

TAKE-OFF CLIMB GRADIENT CORRECTIONS FOR BANK ANGLES

AFFECTED PERFORMANCE CHARTS

TAKE-OFF CLIMB GRADIENT CALCULATION EXAMPLE

TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 20?

TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 12?

TAKE-OFF 2ND SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; FLAPS - 0?

FINAL SEGMENT CLIMB GRADIENT CORRECTION FOR STEADY BANKED TURN; CLEAN CONFIGURATION

TAKE-OFF AND LANDING IN CROSSWIND CONDITIONS

TAKE-OFF AND LANDING IN CROSSWIND CONDITIONS

CROSSWIND TAKE-OFF PROCEDURE

CROSSWIND LANDING PROCEDURE

Landing Distance Increase for Crosswind Landings Based on Unfactored Dry, Wet, or Contaminated Landing Distances

Maximum Roll Angle at Landing

USE OF CROSSWIND CHART

Contaminated Runway Crosswind Components

RUNWAY SURFACE CONTAMINATION (RSC), Canadian Runway Friction Index (CRFI) EQUIVALENT AND ESTIMATED LANDING BRAKING COEFFICIENT

Supplments Not Incorporated Into This AFM

Performance

LIST OF FIGURES

GENERAL INFORMATION

COMPLIANCE

STANDARD PERFORMANCE CONDITIONS

VARIABLE FACTORS AFFECTING PERFORMANCE

DEFINITIONS

GENERAL

ATMOSPHERIC

AIRSPEEDS

UNIT CONVERSIONS