CDU Control Display Unit EHSI Electronic Horizontal Situation Indicator
CFIT Controlled Flight Into Terrain
EICAS Engine Indication and Crew Alerting System
CFP Computer Flight Plan
CG Center of Gravity ENG OUT Engine Out
CLB Climb EPR Engine Pressure Ratio
CMD Command ETOPS Extended Range Operation With Twin Engine Airplanes
CON Continuous
CRM Crew Resource Management EXT Extend
F
CRT Cathode Ray Tube F Fahrenheit
CRZ Cruise FCOM Flight Crew Operations Manual
CWS Control Wheel Steering
D F/D Flight Director
DA Decision Altitude FAA Federal Aviation Administration
DA(H) Decision Altitude (Height)
FAF Final Approach Fix
D/D Direct Descent FAR Federal Aviation Regulation
DDG Dispatch Deviations Guide
FCC Flight Control Computer
DES Descent FMA Flight Mode Annunciator
DIR Direct FMC Flight Management Computer
DME Distance Measuring Equipment
FMS Flight Management System
E
EADI Electronic Attitude Director Indicator F/O First Officer
FPA Flight Path Angle
ECON Economy FPM Feet Per Minute
EEC Electronic Engine Control FPV Flight Path Vector
G
EFB Electronic Flight Bag GA Go-Around
EGT Exhaust Gas Temperature GLS GPS Landing System
Copyright . The Boeing Company. See title page for details.
0.3.2 FCT 737 (TM) October 31, 2006
GP Glide Path ISFD Integrated Standby Flight Display
GPS Global Positioning System
K
GPWS Ground Proximity Warning System K Knots
KCAS Knots Calibrated Airspeed
G/S Glide Slope
GS Ground Speed KGS Kilograms
H KIAS Knots Indicated Airspeed
HAA Height Above Airport L
HDG SEL Heading Select LBS Pounds
HSI Horizontal Situation Indicator LDA Localizer-type Directional Aid
HUD Head Up Display LNAV Lateral Navigation
I LOC Localizer
IAF Initial Approach Fix LRC Long Range Cruise
IAN Integrated Approach Navigation M
M Mach
IAS Indicated Airspeed
MAP Missed Approach Point
ICAO International Civil Aviation Organization
MASI Mach/Airspeed Indicator
MAX Maximum
IFR Instrument Flight Rules
MCP Mode Control Panel
IGS Instrument Guidance System
MCT Maximum Continuous Thrust
ILS Instrument Landing System
MDA(H) Minimum Descent Altitude (Height)
IM Inner Marker
MEA Minimum Enroute Altitude
IMC Instrument Meteorological Conditions
MEL Minimum Equipment List
IP Instructor Pilot
MFD Multifunction Display
IRS Inertial Reference System
MM Middle Marker
IRU Inertial Reference Unit MMO Maximum Mach Operating Speed
Copyright . The Boeing Company. See title page for details.
October 31, 2006 FCT 737 (TM) 0.3.3
MOCA Minimum Obstruction Clearance Altitude QRH Quick Reference Handbook
MOD Modify R
MORA Minimum Off Route Altitude RA Radio Altitude Resolution Advisory
MSL Mean Sea Level RAT Ram Air Turbine
N RDMI Radio Distance Magnetic Indicator
NAV Navigation
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