AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT
AIRFRAME
TOTAL TIME: 7,717.2
LANDINGS: 6,662
ENGINES
Honeywell TFE731-20BR-1B Enrolled on Honeywell MSP Gold
Left Engine – 2,381.2 Since MPI/CZI
Right Engine – 2,370.9 Since MPI/CZI
MPI/CZI Interval 3,000/6,000
MAINTENANCE & INSPECTION:
A (1-6) Due January 2024
B (1-6) Due October 2024
C (1-6) Due August 2025
D (1-6) Due August 2029
SB 40-11-01 Gross T/O Weight Increase
The Honeywell Primus 1000 avionics system comes standard; it includes four large-format EFIS (ERO Frequency Information Systems) and a 3-D approach navigation system through Dual Universal UNS-1EW FMS. For the first time in a Learjet, there are no restrictions on the lateral and vertical approach guidance simulations.
AVIONICS EQUIPMENT:
Honeywell Primus 1000 System w/ Four Tube EFIS
COMMUNICATION: (2) Honeywell RCZ-851 Comms 8.33 kHz Spacing
VHF NAVIGATION: (1) Honeywell RNZ-851B NAV FM Immunity/with ADF
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
COCKPIT DISPLAY SYSTEM: (4) Honeywell DU-870 Integrated Avionics System Displays
WEATHER RADAR: Primus 660 Color Weather Radar System
TRANSPONDER: Dual Honeywell RCZ-833M, w/Mode S Diversity Transponders
AUTOMATIC DIRECTION FINDER: (2) Honeywell RNZ-851 ADF
DISTANCE MEASURING EQUIPMENT: (2) Honeywell DME
HIGH FREQUENCY RADIO: (1) 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 LCR-93 AHRS
FLIGHT MANAGEMENT SYSTEMS/GPS: (2) Universal UNS-1EW FMS / WAAAS
TERMINAL COLLISION AVOIDANCE SYSTEM: Honeywell TCAS-2000 (TCAS II)
TERRAIN AWARENESS AND WARNING SYSTEM*: Honeywell Mark V EGPWS (TAWS A) with windshear caution
EMERGENCY LOCATOR TRANSMITTER: ARTEX C406-2-247 three frequency ELT
ADDITIONAL AVIONICS:
SOLID STATE COCKPIT VOICE RECORDER: Honeywell SSCVR (2) Hour
WIFI: ATG-2000
SATCOM: Aircel Axxess II
ADS-B: (STC STO4159CH) by Weststar 7/16/2019
The Learjet 45’s cabin holds eight seats (in a double club layout) with plenty of room to swivel, recline, and track. The cabin’s length and width are 19.8 feet and 5.1 feet, respectively. Don’t be misled by these measurements; the interior of the Learjet 45 was designed to offer the most usable passenger space possible so that the passengers do not feel claustrophobic.
Other fine points of the cabin’s design make it functional and comfortable, from worktables that fold down from the walls to an extra pressure relief port on the door for added passenger safety. The noise level in the cabin never exceeds 72 dB, and a two-zone temperature control system ensures that both the cabin and the cockpit are kept comfortable.
INTERIOR: (original) Floorplan 45-3
Standard (9) passenger Double Club seating with Belted Lavatory Configuration, LR45XR Spinneybeck Sabrina 765 Beige Leather passenger seats, with three stowable Executive Tables with Leather Tabletop Inserts. The left and right-side ledges are High Gloss Wood Veneer with leather accent and the Hardware is Brushed Satin Nickel. Verasol Putty 85400 on pleated window shades. The Cabin Headliner & Window line in Tapis Sand Ultra 3850 Ultra leather. The Sidewalls are in Tapis pattern. The cabin lighting includes PSU Indirect Lighting and Dropped Aisle Accent Lighting. The carpet is AIP Landings Loop Tiger’s Eye. The right-side refreshment center has a Hardwood Bullnose Edge stained to match. Left Hand Cabinet behind Pilots seat. The Cabinetry is High Gloss Veneer. The Flight Deck includes covered in Grey Sheepskin. Passenger seats are fire blocked. The aft cabin includes a Left Side Belted Flushing Toilet with stowable (pocket) privacy doors.
An external compartment provides fifty cubic feet of baggage space with an additional fifteen cubic feet of storage in the interior.
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