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Exterior: |
Azko Nobel Matterhorn White (AHS-G-35) base, Acry Glo Ocean Blue Metallic (H10592) Top Trim, Acry Glo Cobalt Blue Metallic (H10593) Second Trim and Registration Number, Acry Glo Harvest Gold Metallic (H10653) Third Trim and Exit Markings (Completed 12/1/2008 @ 2315 Hours) |
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Interior: |
Volo Spinneybeck Sand Leather Seats, Tapis Corporation Crospoint Medium Beige Interior Covering, Ivory Ultra Leather Headliner and Window Pane Panels, Shearing Light Tan Sheepskin Seats (Pilot and Co-Pilot), Davis and Davis Pecan Honey Beige Carpet (Completed 12/1/2008 @ 2315 Hours) |
Configuration: |
2+8, Center Club Configuration. Aft Three-Place Bench Seat. Forward Side-Facing Potty Seat. Forward Left-Hand Refreshment Center, Forward Right-Hand Storage Cabinet. Dual Executive Writing Tables in Club Area |
Total Time Airframe: |
4020.3 Hours |
Total Landings: |
3395 |
Total Time Left Engine: |
4020.3 Hours / 3395 Cycles Since New |
Total Time Right Engine: |
4020.3 Hours / 3395 Cycles Since New |
CZI Due: |
4200 Hours |
MPI Due: |
4088 Hours |
Engine Type: |
Honeywell TFE 731-2-3B |
Engine Serial Numbers: |
P-99549, P-99548 |
Engines are on Honeywell MSP Gold |
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Avionics Consisting Of: |
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|---|---|
| Honeywell 5-Tube EFIS-50 | |
| Dual Honeywell DB-438 Audio Systems | |
| Dual Collins VHF-22C Com Transceivers with 8.33 KHZ Spacing | |
| Dual Honeywell VNS-41 Navigation Receivers (VOR/Localizer/Glide Slope) | |
| Dual Honeywell VN 411 Marker Beacon Receivers | |
| Dual ACSS NXT-700 Mode S Transponders with ADS-B Out – (L3) ST02609LA | |
| Dual Honeywell KFC-3100 Autopilot / Flight Director Systems | |
| Dual Honeywell KAU-491 AHRS | |
| Honeywell DFS-43 ADF | |
| Honeywell VD-441B DME | |
| Allied Signal CAS 67A TCAS II | |
| Honeywell Primus 880 Color Weather Radar | |
| Honeywell KDC-481 Dual Central Air Data Computers | |
| Allied Signal MK-VII EGPWS with Windshear | |
| Universal UNS-1Ew (WAAS) FMS CDU with LPV Monitor and Digital Data Transfer | |
| Universal 120 Cockpit Voice Recorder (CVR) | |
Options: |
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|---|---|
| Dee Howard Thrust Reversers | |
| Cargo Door | |
| Aft Raisebeck Locker | |
| N1 DEECS | |
| Skandia Ease (Engineered Acoustically Suppressed Environment) Sound Control System | |
| Airshow 400 | |
| Precise Flight Pulsating Recognition and Landing Lights – SA8172NM-D | |
| Cabin Power Disconnect Switch – SA8177NM-D | |
| Emergency Exit Lighting System – ST00159WI | |
| ARTEX Emergency Locator Transmitter – ST00322DE-D | |
| Revue Thommen 2″ Standby Altimeter – ST01412WI | |
| Whelen LED Wingtip Navigation Light Assemblies | |
| Lone Start DC Converter with 4 DC Outlets (28 Volts to 14 Volts Converter) |
Operating Weights: |
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|---|---|
| Maximum Ramp Weight: | 17,900 Pounds |
| Maximum Takeoff Weight: | 17,700 Pounds |
| Maximum Landing Weight: | 16,000 Pounds |
| Maximum Zero Fuel Weight: | 13,500 Pounds |
| Fuel Capacity (usable)@ 6.75 lbs/gallon | 4,124 Pounds (610.96 Gallons) |
| Empty Weight: | 11,109 Pounds |
| Useful Load with Full Fuel: | 2,391 Pounds |
Maintenance: |
|
| No Known Damage History | |
| MSP Gold Engine Program | |
| CAMP Maintenance Tracking: | Phase A: c/w April 2018 @3790 hr, due April 2019 |
| Phase B: c/w April 2018 @ 3790 hr, due April 2020 | |
| Phase C: c/w April 2016 @ 3387 hr, due April 2020 | |
| Phase D: c/w April 2016 @ 3387 hr, due April 2024 | |
| 12 yr: c/w November 2012 @ 2688 hr, due November 2024 |
| Most recent AD 2018-19-04 released concerning a Flap Structure Mod per S.B 31-27-35 is Not Applicable to this aircraft. |
| Download Spec-Sheet (PDF) |
| CAMP AD/SI Compliance and CAMP Status Report available upon request. |
| Information Effective: April 29, 2019 |
| Asking Price: *** SOLD *** Contact Us |
Aircraft and specifications are subject to verification by inspection. Aircraft is subject to availability, prior sale, or removal from the market without further notice. All photos on this site are the exclusive property of Eastern Aircraft Exchange, Inc. and are not to be used without prior authorization.