Airframe
TOTAL TIME: 3,664.7
LANDINGS: 2,766
Engine(s)
Honeywell TFE731-20BR-1B Enrolled on Honeywell MSP Gold
Left Engine – 2,865.3 Since New
Right Engine – 2,901.3 Since New
MPI/CZI Interval 2,500/5,000
APU: Honeywell RE100 Enrolled on Honeywell MSP Gold
PROGRAMS:
ENGINES & APU – Enrolled MSP Gold
CAMP – Enrolled Maintenance Tracking Program
Avionics/Radios
The Honeywell Primus 1000 digital avionics suite is certainly up to par with the high-performing jet; its four cathode ray tube screens are located at logical positions on the control panel. The designers of the Learjet 45paid a lot of attention to
arranging the avionics in an easy-to-use, logical layout, ultimately making the pilot’s job easier – and each flight safer.
Honeywell Primus 1000 System w/ Four Tube EFIS
COMMUNICATION: (2) Honeywell RCZ-851 Comms 8.33 kHz Spacing
VHF NAVIGATION: (1) Honeywell RNZ-851 NAV FM Immunity/with ADF
VHF NAVIGATION: (1) Honeywell RNZ-851B NAV FM Immunity
CLEARANCE DELIVERY: Honeywell CD-850 Clearance Delivery Module
FLIGHT DIRECTOR: Honeywell Primus 1000 IC-600 Integrated Avionics System Display
AUTOPILOT: Honeywell Primus 1000 IC-600 Integrated Avionics System
Honeywell Primus 1000 System w/ Four Tube EFIS
COMMUNICATION: (2) Honeywell RCZ-851 Comms 8.33 kHz Spacing
VHF NAVIGATION: (1) Honeywell RNZ-851 NAV FM Immunity/with ADF
VHF NAVIGATION: (1) Honeywell RNZ-851B NAV FM Immunity
CLEARANCE DELIVERY: Honeywell CD-850 Clearance Delivery Module
FLIGHT DIRECTOR: Honeywell Primus 1000 IC-600 Integrated Avionics System
COCKPIT DISPLAY SYSTEM: (4) Honeywell DU-870 Integrated Avionics System
Displays
DATA ACQUISITION UNIT: Honeywell DA-800
WEATHER RADAR: Primus 880 Color Weather Radar System
LIGHTNING DETECTION: Honeywell LSZ-860 Lightning Detection System
WEATHER: Heads Up XM Weather System
TRANSPONDER: (2) Honeywell Primus II, w/Mode S Diversity Transponders ?
AUTOMATIC DIRECTION FINDER: (1) Honeywell Primus II RNZ-851 ADF
DISTANCE MEASURING EQUIPMENT: (2) Honeywell DME
HIGH FREQUENCY RADIO: (2) Honeywell KHF-950 HF Radio w/Selcal
RADIO ALTIMETER: (1) Honeywell RT-300 Radar Altimeter
AIR DATA COMPUTER: (2) Honeywell AZ-850 Air Data Computers
ALTITUDE HEADING REFERENCE SYSTEM: (2) Honeywell AHZ800 AHRS
FLIGHT MANAGEMENT SYSTEMS/GPS: (2) Universal UNS-1C+ FMS
DATA base: Advanced Performance Database
TERMINAL COLLISION AVOIDANCE SYSTEM: Honeywell TCAS-2000 (TCAS II)
with Change 7
TERRAIN AWARENESS AND WARNING SYSTEM*: Honeywell Mark V EGPWS
(TAWS A) with windshear caution
*[NOTE: Class A TAWS meets European regulations] ???
EMERGENCY LOCATOR TRANSMITTER: ARTEX C406-2 ELT
ADDITIonAL AVIONICS:
SOLID STATE COCKPIT VOICE RECORDER: Honeywell SSCVR (2) Hour meets
JAR requirements
TELEPHONE: Aircell ST3100
Additional Equipment
BATTERY: New Concorde Lead Acid Batteries
ANGLE OF ATTACK: (2) Angle of Attack Indicators
OXYGEN: Increased Capacity - 40 Cu. Ft.
ENTERTAINMENT: AIRSHOW 400
BATTERIES: Concorde 38-amp Lead Acid
Jump Seat
Dual Electronic Flight Bags
Jump Seat
Gross Weight Increase
Exterior
Overall Matterhorn White with Yellow and Black Accent Stripes
Interior
Standard (8) passenger Double Club seating with Belted Lavatory Configuration, Townsend
Classic Cow Nugget Tan Leather passenger seats, with 2 Left & 2 Right stowable Executive
Tables with Leather Table Top Inserts. The left and right side ledges are High Gloss Wood
Veneer with leather accent and the Hardware is Brushed Satin Nickel. Window shades are
pleated fabric. The Cabin Headliner & Windowline in Tapis Off White Ultra leather. The
Sidewalls are exquisite accenting fabric. The cabin lighting includes PSU Indirect Lighting
and Dropped Aisle Accent Lighting. The carpet is accenting wool. The right side
refreshment center has a Hardwood Bullnose Edge stained to match. Left Hand Cabinet
behind Pilots seat. The Cabinetry is Figured Makore High Gloss Veneer. The Flight Deck
includes covered in Gray Sheepskin. Passenger seats are fireblocked. The aft cabin includes a
Left Side Belted Flushing Toilet with stowable (pocket) privacy doors. External Baggage
Compartment.
Inspection Status
Fresh A (1-6) C/W, December 2015
B (1-6) Due, October 2016
C (1-6) Due, October 2019
Recent GKN Windshields
Flap Actuator Replacement (AD2010-06-13 is no longer applicable)
