Aircraft Total Time: 2794.0 hrs. since new. Last Annual performed July, 2008.
Engines: 429.0 hrs. Since NEW TCM Continental TSIO-520-WB3F’s, (including all NEW: Accessories, 100 Amp Alternators, baffles, hoses, turbo-supercharger, starters, intercooler, oil coolers, magnetos, wastegate controller & exhaust, and engine mounts.) Both Engine’s valve lifter sets and original Irska starters were replaced November ’08 with Energizer starters for enhanced reliability. Compressions and Borescope reports performed by TCM Engineering Tech Rep on October, 2008 as excellent at ABS Clinic.
Props: 618.0 hrs Since Overhaul, fresh “teardown, inspection, pack & reseal” 11/’08
Mode S Transponder, Altimeter, Encoder & Static Certification: 11/’08
Damage History: NONE
Always hangared by every owner since new delivery.
Third from the last Baron 58 P’s ever build. First placed into initial service early 1986.
Useful Load: 1640.0 lbs (FAA re-weigh and balance performed April ’07)
Paint: Custom Base Coat / Clear Coat. All new Stainless Screws. 8 out of 10 (see pix)
Interior: Refurbished 2004 with tasteful corporate colors. 8 out of 10 (see pix)

Installed Airframe Equipment:

•Full FAA Certified Flight Into Known Icing (FIKI) Package including: BFG lightweight de-ice boots, New Windshield and PPG “Hot Plate” (new ’06), Electro-thermal Prop De-Ice, Heated Pitot & Static, Alternate Static, heated Stall Warning and wing ice light.

•190 Gallon (useable) Fuel System, including new Security Locking Fuel Caps, 100LL restrictor and anti-siphon flapper valves (New ’07). New Fuel Cells (11/’03)

•Air Conditioning System, completely rebuilt and converted from R-12 to new environmentally friendly (and more efficient) R-134 refrigerant (6/’07).

•Oxygen: Supplemental 15 cu. ft., Pilot, Co-Pilot and 6 Pax manifold installed. Bottle Hydrostatic (07/’06). Pilot’s mask has microphone for Com functions.

•Highly sought after “New Style” Beech full dual flight controls (no throw-over yoke), new throttle quadrant, and “proper” locations for gear & flaps control. (Approximately only 50 58P’s have this significant improvement that is universally desired). Co-Pilot brakes are also installed.

•Completely New Custom “double wide panel” fabricated in 2006, to include Dual Flight Instruments and full redundancy of both Electric and Pneumatic Flight Instruments. This included electric standby Castleberry 300-14EL 3 ½” Gyro Horizon, and complete overhaul of Pilot’s pneumatic KI-256 FD/GH in 4/’06

•All New Wing Bolts, Nuts and Washers. Fittings Inspected and lubed. (7/’07)

•Tail Elevator completely Re-Skined (03/’07) top and bottom, to eliminate problematic recurrence of cracks with original “bonded” elevator design.

•Reiff Turbo-XP Engine Pre-Heater system installed (11/’06) both engines.

•New C&D Ceramic Lined Gas-fired cabin heater installed. New Design eliminates recurring mandatory AD for inspection, now 2,000 hr overhaul limit.

•Woodward Propeller Synchro-Phaser, Overhauled and Upgraded (1/’07)

•Woodward Propeller Un-Feathering Accumulators.

•MicroDynamics Vortex Generator (VG) Kit greatly enhances slow flight controllability, lowers Vmc, improves Single Engine performance and handling.

•Insight GEM 1200 Engine Analyzer installed, with probes for continuous and simultaneous monitoring of each cylinders’ EGT, CHT, as well as both Turbo-Supercharger’s TIT. Includes “normalize” function to easily discern problem trends, as well as digital and visual EL graphics display of all functions. Memory module records 50 hours of continuous engine data, which can be downloaded via IR Link for post-flight analysis, graphing and trending.

•Forward Baggage Compartment completely free of any avionics or any shelf for other equipment, permitting easy loading of 300 lbs. without restriction. Careful attention given to eliminate any critical CG issues, by strategically distributing all new avionics and re-locating other equipment into the Radome, below baggage compartment floor area, and to tail equipment bay of the aircraft. Now, any normal passenger seating and baggage loading is within CG limits. Aft Baggage also remains unrestricted to original 120 lbs. capacity.

•Window Liners & Shades: Rosen Pilot & Co-Pilot Sun Visors with articulating extension arms. Passenger Windows with Gale R. Calhoon Tinted Window Liners.



Installed Avionics Equipment:
Extensive complete Avionics upgrade program performed by Elliott Aviation to completely replace all previously existing avionics, instrument panels, equipment, wiring and antennae. All new double-shielded low-loss cables and wire used throughout, as well as all existing nav/com/pulse antennae removed, inspected for corrosion, and replaced and re-sealed with all new elements. Over $170,000 expended across 14 month program of retrofitted avionics equipment to make this Baron 58P the safest, best equipped, and most intelligently designed Baron panels flying today. All equipment selections were based on “best-in-class” determination, utilizing predominantly Garmin, L3, Honeywell and Bendix/King. Full engineering and design drawings are available, as well as all new wiring diagrams. Phase I was completed in April, 2007, Phase II just completed in June, 2008. This was designed with “open architecture” for easy upgrade at minimum cost when the ADS-B/In-Out standards are set and equipment is made available.

•Multi-Function Display: Garmin GMX-200 with Radar, Traffic, and Electronic Jeppesen Approach, Taxi and Enroute (Hi & Lo) Charts is installed. Displays weather information from Bendix Radar, L3 Stormscope, and Garmin Satellite Data Link, including TFR’s, Metars, TAF’s, Sigmets, Airmets, Winds Aloft, Freezing Levels, NexGen Radar, Cloud and Echo Tops and much more. Additionally, will display (pop-up page if not already showing this) for the Enhanced Ground Proximity System (EGPWS) as well as the Traffic Collision Avoidance System (TCAS-1). Additionally, provides Pilot with control of onboard XM Radio entertainment channels. Database update easily performed by front panel insertion of SD Memory card.

•EFIS / HSI. Pilot’s: Sandel 3500 EHSI is Pilot’s Primary Navigation Display, selectable between display of: Nav 1, Nav 2, GPS 1, GPS 2, ILS 1, ILS 2. Provides bearing pointers, 120 degree sector view, 360 compass view. Includes internal database for all special use airspace, airports, navaids in W. Hemisphere. (Unit modified and updated (5/’08) to new Hi-Intensity LED back-lighting, to provide direct sunlight readability and 20,000 hrs MBTF. Additionally, database was updated at this time). Capable of overlaying TCAS-1 and Stormscope threats for any navigation page. Co-Pilot’s HSI: King KI-525 on Co-Pilot’s Panel, hard-wired to display only Nav. information from Garmin GNS-430W Navigator.

•Flight Director / Autopilot: King KFC-200 FD/full 3-Axis AP with freshly overhauled and aligned KI-256 FD/Gyro Horizon. Includes Servo’ed Altimeter/Encoder with KAS-297 Altitude Pre-Select /Alerter Module. Fitted with Yaw Damper, Pilot’s CW Pitch Sync, AP Disconnect, Go-Around and Electric Elevator Trim. All servos rebuilt, pitch trim most recently (04/’08). A very powerful, well-tuned and maintained system. All FD/AP annunciators are above ADI, Autopilot Control Console located in central pedestal below quadrant.

•Radar Sensor/Radome: Bendix RS-181A Digital Color Radar (Overhauled and aligned 6/’08) displayed on Garmin GMX-200 Multi-Function Display. Norton Radome in excellent condition, no patches or repair, 3-M Erosion Cap installed.


•GPSS Roll Steering Computer: DAC GDC-31 Roll Steering Computer interfaces the Garmin GNS-530 WAAS ARINC 429 steering commands to the KFC-200 FD/AP to provide full-time course guidance for all modes of Enroute Guidance, WAAS LPV and other GPS approaches. This provides the autopilot the capability to turn anticipate, track all approach transitions, even DME Arc Approaches, flies Missed Approach Procedures, and even will provide proper entry into holding patterns, flying them precisely until cleared otherwise. Simple Pilot’s Panel Switch-Annunciator controls “HDG/GPSS” function.

•Compass System: KCS-55A Compass System, driving Sandel EHSI & King HSI. Re-calibrated (04/’07), Slaving Accessory and Annunciator on Pilot’s Panel.

•COM/NAV/LOC/GS/GPS #1: Garmin GNS-530W WAAS unit installed in center stack, performs the preponderance of the communication and navigation duties of the aircraft. New WAAS GPS Receiver provides LPV accuracy guidance world-wide. Unit is also wired to optionally display TCAS-1, Stormscope, and Satellite Data Link Weather pages. Converted to new Ver 3.1 Software (6/’08), additional display and terrain avoidance capability has been added. Mid-Continent Annunciator on Pilot’s Panel to advise CDI mode, Message and GPS Integrity.

•COM/NAV/LOC/GS/GPS #2: Garmin GNS-430W WAAS installed on Co-Pilot’s panel, provides complete redundancy for all Com/Nav functions and has identical LPV Nav Accuracy capabilities of Pilot’s GNS-530W. This unit provides Nav output to both Pilot’s and Co-Pilot’s HSI’s. Additionally, Traffic Information Service (TIS) from Ground-Based ATC Radar is data-linked through the GTX-330 Mode S Transponder to display on this unit, including a pop-up page if there is a traffic or terrain threat.

•Audio System / Intercom: Garmin GMA-347 Digital Audio System / Marker Beacon Receiver is tied to all applicable audio inputs & outputs. This controls all Pilot, Co-Pilot and Passenger intercom, entertainment and communications functions. This includes distribution of the XM Radio Channels to all occupants, as well as intercom capability for all 6 seats (pilot and/or co-pilot can easily be isolated). All six seats are wired with both conventional mic/phone jacks, as well as aircraft-powered Leco connectors for Bose Noise-Cancelling Headsets. Additionally, the unit provides cell phone connection capabilities through the crew’s headsets. Lastly, an “ATC Re-Play” button is on the Pilot’s Control Yoke to allow the GMA-347 to replay any of the last several ATC communications (3 minutes)

•Transponder / ATC Data-Link: Garmin GTX-330 Mode S Transponder is installed and connected to Garmin GNS-430W to display Traffic Information Services (TIS). Upgraded (04/’08) to include Enhanced Surveillance Capability (required in Europe) information tags. Configured to automatically turn-on and off at a groundspeed threshold of 30 knots. Provides monitoring of flight time, as well as encoded flight level being transmitted to ATC. Pilot’s CW mounted “Ident” button.

•Satellite FIS Data Link: Garmin GDL-69A Satellite Data Link Receiver provides full US (and soon Canadian) high bandwidth XM Weather FIS Information including: Nex-Rad Radar / Lightning / Winds Aloft / TFR’s / Sigmets / Airmets /TAF’s / METAR’s and a total of 19 types of critical information to the pilot through the GMX-200 Multi-Function Display. A limited sub-set of the FIS data can also be displayed on the GNS-530W unit, as well.

•Passenger Entertainment: Garmin GDL-69A (above) also provides XM radio and selection of over 150 stereo entertainment channels (music, news, talk, sports, etc) and is routed through the Garmin GMA-347 to all occupants’ headphone jacks. Control by the Crew is affected through the XM Radio “Page” on the GMX-200 Multi-Function Display. Control for the aft 4 passenger seats is accomplished by a Garmin GRC-1 Wireless Remote Controller (with a small LCD Screen showing the channel, artist, song, etc) and the Garmin GRT-10 Wireless Processor. This controls the channel selection and volume for the XM Programming.

•Radio Altimeter: Bendix/King KRA-405 2100 ft. RadioAltimeter, with KNI-415 Indicator, Dual Antenna, DH Set, DH Light and Sonalert Audio Alarm.

•DME:King KN-63 DME with KDI-572 Indicator (Nav 1, Nav 2, Hold Switching tied to Garmin GNS’s) located below Pilot’s EHSI. Output also displayed into Sandel EHSI when Nav 1, Nav 2, LOC 1, LOC 2 information is displayed.

•Traffic Collision Avoidance System (TCAS-1): L3 Skywatch 899-HP System with TCAS certified NY-156 Antenna. Active Interrogation displays all transponder equipped threats out to 35 miles, wired to display on Multi-Function Display (via pop-up page), GNS-530W Screen and Sandel 3500 EHSI. Recently modified and upgraded (4/08) to include “VIP” (voice intruder protection) which calls out traffic within 3 mile limit. Pilot’s Mounted Mode Controller and VIP Mute.

•Enhanced Ground Proximity Warning System (EGPWS): Honeywell KGP-560 EGPWS, with MW-41 Annunciator on Pilot’s Panel. Configured and certified as TAWS-B. Western Hemisphere Database. Provides EGPWS Pop-Up Page on Multi-Function Display, visual alert on annunciator and un-muted call outs on phones and speaker.

•Air Data Computer / Fuel Totalizer: Shadin Digi-Data provides fuel consumption / fuel remaining / fuel reserves at destination constantly, as well as “low fuel” warnings.


•Emergency Locator-Transmitter (ELT): Artex ME-406 Satellite ELT

•Ground Com Switch: Powers up GNS-430 Comm #2 and GMA-347 Audio System directly from battery bus (without ship’s master being on)