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Posted May 29, 2018 at 12:28 pm by Jetcraft

2002 Bombardier Learjet 45 SN 45-181

HIGHLIGHTS

Engines Enrolled on Honeywell MSP

Airframe Enrolled on Smart Parts Plus

Phase A Completed in February 2018

AIRFRAME

Total Time Since New

4’460.7 Hours

Total Landings Since New

3’551 Landings

Entry into Service Date

September 2001

Home Base

Namibia

Program Coverage

Bombardier Smart Parts Plus

Maintenance Tracking

CAMP

Certification

Currently Operated under Namibian Registration

ENGINES

Left Engine

Right Engine

Description

Honeywell TFE731-20BR

Serial Number(s)

P-116360

P-116358

Total Hours Since New

4’445 Hours

4’460 Hours

Total Cycles Since New

3’447 Cycles

3’487 Cycles

Program Coverage

Honeywell MSP

MAJOR INSPECTION STATUS

Inspection

Last Performed

Next Due

Phase A

4’460 Hours, February 2018

4’760 Hours, January 2019

Phase B

4’365 Hours, September 2016

4’965 Hours, September 2018

Phase C

4’071 Hours, October 2014

5’252 Hours, October 2018

Phase D

4’365 Hours, September 2016

6’765 Hours, August 2024

4’800 Hour Check

N.A.

4’800 Hours

9’600 Hour Check

N.A.

9’600 Hours

Landing Gear Inspection

N.A.

10’000 Landings

AVIONICS

The Bombardier Learjet 45 is equipped with an integrated, Honeywell Primus II avionics suite. A general summary of this aircraft’s avionics suite is as follows:

Type of Unit

Quantity

Unit Description

EFIS (Electronic Flight Instrument System)

Quad

Display Units DU-870

FMS (Flight Management System)

Dual

Universal UNS-1C

GPS (Global Positioning System)

Dual

Universal UNS-1C

NAV (Navigation Radio)

Dual

Honeywell RNZ-850

DME (Distance Measuring Equipment)

Dual

Honeywell RNZ-850

ADF (Automatic Direction Finder)

Dual

Honeywell RNZ-850

A/P (Autopilot)

Single

Honeywell IC-600

VHF COM (Very High Freq. Communication)

Dual

Honeywell RCZ-833

HF COM (High Freq. Communications)

Dual

Honeywell KHF-950

SELCAL

Dual

Honeywell KHF-950

RADAR

Single

Honeywell WU-660

RADAR ALT (Radar Altimeter)

Single

Honeywell RT-300

XPNDR (Transponder)

Dual

Mode S Honeywell RCZ-833

GPWS (Ground Proximity Warning System)

Single

Honeywell EGPWS Mk V

TCAS (Traffic Collision Avoidance System)

Single

TCAS 2000

CVR (Cockpit Voice Recorder)

Single

Honeywell CVR

FDR (Flight Data Recorder)

Single

L3 Technologies FA-2100

ELT (Emergency Locator Beacon)

Single

Artex C406-2

ENTERTAINMENT

Type of Unit

Description

Display/ Monitor

One (1) Monitor

DVD/CD Player

Yes

NAVIGATION & COMPLIANCE

RVSM

TCAS 2000

RNP 10

NAT MNPS

WEIGHTS

Gross Weight (Ramp)

21’750 lb.

Max Zero Fuel Weight

16’000 lb.

Max Takeoff Weight

21’500 lb.

Empty Weight

16’357.3 lb.

Max Landing Weight

19’200 lb.

Current Basic Operating Weight

14’433 lb.

INTERIOR

Description

Number of Passengers

Nine (9)

Galley Location

Forward

Forward Cabin Configuration

Four (4) Executive Seats with Fold Out Tables

Aft Cabin Configuration

Four (4) Executive Seats with Fold Out Tables

Lavatory Location(s)

Aft Belted Lavatory

EXTERIOR

Base Paint Color

White

Stripe Colors

Blue and Red

Last Painted Date

2001

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