N7474C - 1991 BOEING 747 400
Aircraft Summary
General
Year
1991
Manufacturer
BOEING
Model
747-400
Serial Number
24730
Registration #
N7474C
Condition
Used
Description
The plane does not have engines.
Airframe
Total Time
16470
Total Landings
13617
Airframe Notes
Exterior Height 63’ 5”
Wing Span 195’ 8”
Length 231’ 10”
Engine Program
Engine Maintenance Program
None
Engine 1
Engine 1 Notes
The plane does not have engines.
Auxiliary Power Unit
APU
Yes
APU Notes
Manufacturer & Model Pratt & Whitney Canada 901A
Serial Number PCE900229
Total Time Since New 13,402 (As of May 2019)
Total Cycles Since New 7,280
Last Shop Visit February 2014
Avionics
Avionics/Radios
ACARS
COMMUNICATION MANAGEMENT UNIT SINGLE COLLINS
AIRPLANE PERSONALITY UNIT SINGLE COLLINS
ALTITUDE ALERT SYSTEM
CREW ALERTING CARD SINGLE BECO
AIRCRAFT CONDITION MONITORING
DATA MANAGEMENT UNIT SINGLE TELEDYNE
QUICK ACCESS RECORDER SINGLE TELEDYNE
AIR DATA COMPUTING
AIR DATA COMPUTER TRIPLE HONEYWELL
AIR DATA STANDBY
STANDBY AIRSPEED INDICATOR SINGLE KOLLSMAN
STANDBY ALTIMTER INDICATOR SINGLE TKK
AIR TRAFFIC CONTROL SYSTEM
DUAL ATC CONTROL PANEL SINGLE COLLINS
ATC TRANSPONDER DUAL COLLINS
AUTOPILOT/FLIGHT DIRECTOR SYSTEM
COMPUTER-FLIGHT CONTROL TRIPLE COLLINS
PANEL-AFCS MODE CONTROL SINGLE COLLINS
MODULE - STAB TRIM/RUDDER DUAL BOEING
AUTOMATIC DIRECTION FINDER
ADF RECEIVER SINGLE BOEING
DISTANCE MEASURING EQUIPMENT
DME INTERROGATOR DUAL COLLINS
EMERGENCY LOCATOR TRANSMITTER
ELT TRANSMITTER SINGLE ELTA
ELT CONTROL PANEL SINGLE BAE SYSTEMS
ENHANCED GROUND PROXIMITY WARNING SYSTEM
EGPWS COMPUTER SINGLE HONEYWELL
FLIGHT MANAGEMENT COMPUTER SYSTEM
FLIGHT MANAGEMENT COMPUTER DUAL HONEYWELL
FLIGHT MANAGEMENT CONTROL DISPLAY TRIPLE HONEYWELL
GLOBAL POSITIONING SYSTEM
MULTI-MODE RECEIVER TRIPLE COLLINS
INTEGRATED DISPLAY SYSTEM
INTEGRATED DISPLAY UNIT SIX COLLINS
INTEGRATED INTERFACE UNIT TRIPLE COLLINS
ILS NAVIGATION SYSTEM
MULTI-MODE RECEIVER TRIPLE COLLINS
RADIO ALTIMTER SYSTEM
RADIO ALTIMETER TRANSMITTER/RECEIVER TRIPLE THALES
SELCAL SYSTEM
SELCAL DECODER DUAL MOTOROLA
STANDBY ATTITUDE REFERENCE SYSTEM
STANDBY ATTITUDE INDICATOR SINGLE SFENA
STATIC INVERTER/ILS PROCESSOR SINGLE SFENA
STANDBY MAGNETIC COMPASS
STANDBY COMPASS SINGLE AMETEK
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
TCAS COMPUTER SINGLE COLLINS
VHF COMMUNICATION SYSTEM
TRANSCEIVER A DUAL COLLINS
TRANSCIEVER B SINGLE COLLINS
CONTROL PANEL DUAL GABLES
VHF OMNIRANGE NAVIGATIONAL SYSTEM
VOR/MKR RECIEVER SINGLE HONEYWELL
VOICE RECORDER SYSTEM
COCKPIT VOICE RECORDER SINGLE FAIRCHILD
CVR CONTROL PANEL UNIT SINGLE FARICHILD
UNDER WATER LOCATOR DEVICE SINGLE DUKANE
WEATHER RADAR SYSTEM
WEATHER RADAR CONTROL PANEL SINGLE COLLINS
WEATHER RADAR RECEIVER/TRANSMITTER DUAL COLLINS
Exterior
Exterior Notes
Base White/Beige
Stripe Red
Interior
Interior Notes
Configuration State Room | 4 Zones (B - E) | Galley | Upper Deck
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