Posted April 10, 2018 at 4:12 pm by Jetcraft

2005 Cessna Citation XLS SN 560-5549

HIGHLIGHTS

Dual UNS-1ESPW w/WAAS

Aircell ATG-5000 “Gogo” High Speed Internet

220 Hours Since Engine Overhaul

347 Hours Since APU Overhaul

AIRFRAME

Total Time Since New

5,799 Hours (As of 1 March 2018)

Total Landings Since New

5,047 Landings

Airworthiness Date

22 March 2005

Home Base

San Luis Obispo, CA, U.S.A. (KSBP)

Maintenance Tracking

CAMP

Certification

Currently Operated FAR Part 135

ENGINES

Left Engine

Right Engine

Description

Pratt & Whitney PW525B

Serial Number(s)

DD-0095

DD-0100

Total Hours Since New

5,690 Hours

5,690 Hours

Total Cycles Since New

4,939 Cycles

4,939 Cycles

APU

Description

Honeywell RE100(XL)

Serial Number

P-500

APU Total Time Since New

2,611 Hours

MAJOR INSPECTION STATUS

Inspection

Last Performed

Next Due

Document 1

13-Nov-2017

28-Oct-2018

Document 2

13-Nov-2017

28-Oct-2018

Document 8

23-Dec-2016

16-Dec-2020

Document 9

22-Jul-2016

22-Jul-2020

Document 10

23-Dec-2016

16-Dec-2020

AVIONICS

The Cessna Citation XLS is equipped with an integrated, Honeywell Primus 1000 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)

3-Tube

Honeywell DU-870 Displays

FMS (Flight Management System)

Dual

Universal UNS-1ESPW

DTU (Data Transfer Unit)

Single

Honeywell DL-900

GPS (Global Positioning System)

Dual

Universal UNS-1ESPW

IAC (Integrated Avionics Computer)

Dual

Honeywell S3100-328

ADC (Air Data Computer)

Dual

Honeywell AZ-950

NAV (Navigation Radio)

Dual

Honeywell NV-850

RMU (Radio Management Unit)

Dual

Honeywell RM-855

DME (Distance Measuring Equipment)

Dual

Honeywell DM-850

ADF (Automatic Direction Finder)

Dual

Honeywell DF-850

AHRS (Altitude Heading Reference System)

Dual

Honeywell LCR-93

A/P (Autopilot)

Single

Honeywell PC-400

VHF COM (Very High Freq. Communication)

Dual

Honeywell TR-833

HF COM (High Freq. Communications)

Single

Honeywell KHF-950

WX RADAR (Weather Radar)

Single

Honeywell WU-880

RADIO ALT (Radio Altimeter System)

Single

Honeywell RT-300

XPNDR (Transponder)

Dual

Honeywell XS-852F

EGPWS (Enhanced Ground Proximity Warning System)

Single

Honeywell Mark V

TCAS II (Traffic Collision Avoidance System)

Single

Honeywell TPU-67A

FDR (Flight Data Recorder)

Single

Honeywell SSFDR

CVR (Cockpit Voice Recorder)

Single

L3 Aviation FA-2100

ELT (Emergency Locator Transmitter)

Single

Artex 406-2

CONNECTIVITY

Type of Unit

Description

In Flight Phone

Aircell ST3100

High Speed Internet / Wi-Fi

Aircell “Gogo” ATG-5000

ENTERTAINMENT

Type of Unit

Quantity

Description

Cabin Display Monitor

Single

10.4” LCD Monitor

Airshow System

Single

Airshow 400

WEIGHTS

Gross Weight (Ramp)

20,400 lbs

Max Zero Fuel Weight

15,100 lbs

Max Takeoff Weight

20,200 lbs

Empty Weight

12,565.80 lbs

Max Landing Weight

18,700 lbs

INTERIOR

Description

Number of Passengers

Nine (9)

Galley Location

Forward Refreshment Center

Forward Cabin Configuration

Two (2) Place Side Facing Divan

Mid Cabin Configuration

Four (4) Place Club Arrangement with Two Full Size Pullout Tables

Aft Cabin Configuration

Two (2) Forward Facing Club Seats with Two Half Size Pullout Tables

Lavatory Location(s)

One (1) Aft Belted Lavatory Divided by a Solid Pocket Door

Last Interior Refurbishment

Complete Interior 2008, Seats Reconditioned in September 2015

EXTERIOR

Base Paint Color(s)

Overall Matterhorn White

Stripe Color(s)

Taxco Silver Pearl and Dark Blue Pearl

Last Painted Date

April 2016 at Duncan Aviation

On map

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