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PR-ITB 2004 Cessna Caravan 208
PT-ORA 1991 Learjet 55C
S/N 146

Airframe: 10,700 TT  (6655 Landings)Engines: TFE731-3Cr-3B Converted to -3CR (STC ST01051CH-D) in 2011
Not on MSP or JSSI or ESP
Left Engine: 8151.1 TT   5034 Cycles (3833.8 Hrs. SMOH--1633.6 SHSI)     S/N P-94208C
Right Engine: 8757.4 TT   5471 Cycles (3819.3 Hrs. SMOH-- 1633.6 SHSI)  S/N P-94205C

Avionics:

2 Collins VHF-22C Com’s 

Proline 4 EFIS

2 Collins VIR 32 Nav’s

Collins 85 AUTO PILOT

2 TDR-94D Xpdr’s

Collins  ALT 55 Radar Altimeter

2 Collins ADF 60's

WXR-250B Radar

2 Collins DME 42’s

EGWPS Honeywell Mark VII

FMS 2 Universal UNS-1F

CVR-30

HF Com Bendix/King 950

Artex C406-2 ELT

SELCAL 2800-0012-105

TCAS-4000

RVSM

ADC 85L Air Data Computer

Inspection Status:
300 Hr. Phase A1-A6 12 Month Completed 02/27/2014
600 Hr. Phase B1-B6 24 Month Completed 06/03/2013
1200 Hr. Phase C1-C6 48 Month Completed 06/03/2013
2400 Hr. Phase D1-D6 96 Month Completed 09/18/2009
12 Year Completed 08/20/2003 Due August 2015
12,000 HR Completed 07/14/1983 Due in 1300 Hrs.
6000 Hr. Gear Inspection Completed @ 6849 Hrs. on 08/20/1983 2149 Hrs Remaining 

Weights: 

BOW 13426 lbs.Empty Wt. 13287 lbs.
Max Zero Fuel 15000 lbs.
Max Take Off Wt. 21500 lbs.
Max Landing Wt. 18000 lbs

Price: Accepting Offers

Prices are in U.S. Dollars, FOB St. Paul, Minnesota, U.S.A., and are subject to change without notice. Prices do not include taxes, duties or tariffs. The accuracy of the above specifications are only offered as to the best of our knowledge at the time this document was printed. Aircraft is subject to prior sale and/or removal from the market. Aircraft to be sold "as is, where is." All specifications and representations of the aircraft are subject to verification by the buyer before purchase.

Aircraft Description

Interior config
ACTUAL INTERIOR CONFIGURATION

STC ST09568SC -"Conversion of Learjet Air Conditioning System Using R12 to Using R134a Refrigerant"
STC ST02005CH-D -"Installation of Honeywell N1 Digital Electronic Engine Control (DEEC) with J2 Extension Harness"
STC ST00506DE-D -"Collins TCAS-4000 TCAS II System Displayed on VSI/TRA Indicators with Dual Collins TDR-94D Mode S Transponders";
STC ST00503DE-D  -“Installation of Honeywell MK-VII Enhanced Ground Proximity Warning System (EGPWS) with Windshear Warning Displayed on Aircraft EFIS”;
STC ST00673WI-D-“Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation”  
STC ST01182WI-D -“Installation of a Universal UNS-1F”
STC ST00507DE-D -)"Installation of an ARTEX 406 MHz Emergency Locator Transmitter (ELT) With Navigation Interface"
STC ST00951WI-D -“Installation of Collins Air Data Computer 85L on Learjet Models 55B and 55C” –2 Configuration”; 
STC ST01050SE-D - "Group Aircraft Approval for Reduced Vertical Separation Minimum (RVSM)" Class 1 Configuration;
STC ST01183WI-D -"Installation of an Aft Belted Toilet with External Service Installation";
SA00276SE – “ Installation of emergency medical stretcher, oxygen, and electrical systems”;
STC ST01051CH-D -Installation of an AlliedSignal Inc TFE731-3C/3CR Turbofan engine(s);
Installed Dual VHF-22C Comm System with CTL-22C Controls
Installed VIR-32 VHF NAV receivers with CTL-32 controls;
Installed new MEDCO locks 6ea P/N 60-0450-229-66 on SPPR door, SPPR switch panel door, fuselage tank fill door and oxygen system door;
Installed Flight Display Systems - Cabin Audio/Video Entertainment System;
Installed Lighted Control Wheel Chart Holders;
Installed JET CALL SELCAL,
Both engines with TFE731-72-3639 converted to TFE731-3CR-3B (2100 Hrs. THSI); 
Both engines with TFE731-76-3067 "Install Digital Electronic Engine Control (N1 DEEC)".

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