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1986 BEECH BARON 58 - Recent Part 135

Current Price: 140,000.00 USD

BASIC INFO, DIMENSIONS, INSPECTION STATUS, PERFORMANCE:

Formerly N3079P
Current Hour Meter 271.3
Gross Weight: 5,500 lbs.
Empty Weight: 3,755 lbs.

Annual Due June 2025 
IFR Certification Due: January 2026
ELT Battery Due: July 2026

Cabin Dimensions 
Length: 12 Ft 7 Inches
Height: 4 Ft 2 Inches
Width: 3 Ft 6 Inches

Wingspan 37 Ft 10 Inches
Length 29 Ft 10 Inches
Tail Height 9 Ft 9 Inches

Performance:
Max Cruise 232 MPH/202 Knots
Service Ceiling 20,688 Ft
Max Range 1,229 nm

Always Hangared
Complete Airframe & Engine Logbooks
1991 and 1997 Accident History

AVIONICS:

Bendix/King KX-155 Digital Nav/Com with Glide Slope Receiver
Bendix/King KLN-94 GPS and KA-92 Antenna
Bendix/King KY-196 Digital Com Transceiver
Bendix/King KN-53 Digital Nav Transceiver
Bendix/King KI-204 VOR Nav Indicator w/GS & Localizer
Bendix/King KDI-572 DME Display
Mid Continent MD-41-528 GPS Annunciation Control
Collins PN-101 H.S.I.
PS Engineering PMA-8000BT Audio Panel/Intercom/Marker 
S-TEC 60-2 Autopilot with Yaw Damp (Installed DEC 2020)
Appareo Stratus ESG ADS-B Transponder (In & Out)
Electric Trim on Control Wheel
Push-to-Talk & Map Light on Co-Pilot Yoke
Barometric Backup Altimeter
Electric True Airspeed Indicators (2)
JPI EDM-760 Engine Analyzer
5-Digit Thumbwheel Altitude Reminder
BFG WX-1000E Storm Scope
Push-To-Talk & A/P Disengage on Pilot Yoke
2nd Artificial Horizon (Electric)
Avionics Master Switch
Altitude Encoder
Narco ELT-10 ELT
True Blue Power USB Jacks (Crew)
Astro-Tech LC-2 Digital Chronometer

FEATURES/EQUIPMENT:
GAMIjectors
D'Shannon (Cooling) Baffle Kits
SLICK MAGS
Stainless Steel Fastener Kit
Flaps-30 Degrees Gear Warning System
Gear Up Warning Light Mounted on Glare Shield (337)
Dual Control Wheels and Toe Brakes
Redesigned King Air Style Panel
Compass & Map Lights
Overhead Lights
Ventilation Nozzles
Vent Blower
Parking Brake
Tinted Windows
MICRO Vortex Generators
Lighter
Clock
Prop Sync
OAT Gauge
Hour Meter
166 Gallons Useable Fuel 
Landing / Taxi Lights
Strobes
Static Wicks
Stall Warning
Precise Pulse Lights
Pitot Heat
Fire Extinguisher
Annunciator & Panel Lights
Cabin/Overhead Lights
Courtesy Step & Handle
6-Place Intercom Jacks
Rosen Sun Visors
Brackett Air Induction Filters
300 Lb Nose Baggage Capacity
Polished Spinner Cones
Amsafe Lap Belts & Shoulder Harnesses
ENGINES & PROPS:
TCM IO-550-C6 300-HP Engines, 1700-Hour TBO:

Left - S/N 815442-R 
Zero-Timed by TCM (Factory Reman) in June 2000
Installed on N929D in August 2000
Overhauled at 1388.3-TTSN by SIGNATURE in 2012
1188.2-SMOH, 2576.5-TTE as of June 2024 Annual
Compression Results From June 2024 Annual, Cylinders 1-6:
42/80, 60/80, 59/80, 42/80, 63/80, 60/80
ALL CYLINDERS BORESCOPED During 2024 Annual.
The Aircraft Was Flown for 45 Minutes at 75% Power and the Cylinders Were Re-Checked. Cylinder 1 Read 39/80 and Cylinder 4 Revealed 37/80. The Exhaust Valve was Lapped with a Compound for a Better Seal, Cylinders were Flushed, and Hardware was Re-Installed Resulting in 47/80 on Cylinder 1 and Cylinder 4 Improved to 62/80. The Minimum Orifice Reading is 43/80, Per TCM Manual.

Right - S/N 815441-R 
Zero-Timed by TCM (Factory REMAN) in June 2000
Installed on N929D in August 2000
Overhauled at 1388.3-TTE by SIGNATURE in 2012
1188.2-SMOH, 2576.5-TTE as of June 2024 Annual
Compression Results From June 2024 Annual, Cylinders 1-6:
61/80, 70/80, 44/80, 69/80, 34/80, 65/80
ALL CYLINDERS BORESCOPED During 2024 Annual.
The Aircraft Was Flown for 45 Minutes at 75% Power and the Cylinders Were Re-Checked. Number 3 Passed With 50/80. Cylinder 5 Failed, Showing 38/80. The Exhaust Valve was Lapped with a Compound for a Better Seal, Cylinders were Flushed, and Hardware was Re-Installed Resulting in a Reading of 46/80 on Cylinder 3 and Cylinder 4 Improved to 54/80. The Minimum Orifice Reading is 43/80, Per TCM Manual.
  
Motors Equipped with FACTORY CYLINDERS

McCauley 3AF32C512-B 3-Blade Constant Speed Props:

Left Prop - S/N 981334 Overhauled by East Coast Prop in 2012; 1172.6-SPOH at June 2024 Annual, TTP Unknown 

Right Prop - S/N 960328 Overhauled by Sensenich in 2012.
1113.4-SPOH at June 2024 Annual, 8921.2-TTP

Note: The 2nd Right Hand Prop Entry Dated 9/25/14 in Left Prop Log Should Read 9/25/15
INTERIOR/EXTERIOR:
2007: Paint Touch-Up on Engine Cowls, Landing Gear, Radome, Wheel Rims; Nose Erosion Boot Installed. Wing Leading Edges Stripped, Prepped, Primed, and Painted.

2000: Complete Refurbishment by Phoenix Aviation with New Paint & Interior (White Base, Alpine Green, Platinum, Light Burgundy) and Milburn Leather Upholstery, Oyster White Trim, Essential Carpet, Rated 6/10.

Club Seating
Arm Rests
Collapsible Writing Desks
Stereo Intercom Jacks
ACCESS TO SHIP RECORDS:

LINK TO LOGBOOK ACCESS & OIL ANALYSIS:
https://mega.nz/file/LUQhAB5Y#gSGRe9R-IQ0ZU4r3qUIV7wGDfxDiZ9FTtyxdXMAcTEQ

LINK TO AIRWORTHINESS RECORDS (FORM 337s and STCs):
https://mega.nz/file/PQZhTYaS#DUARGFXjBx8_F8X2hhYvCAeG3cUMrVBe9fyKje0IyQI

LINK TO YOU TUBE VIDEO:
https://youtu.be/JSKYnufqQh8

Maintenance Remarks:

2021: Left and Right Reinforcement Plates on Inboard Wing Replaced Due to Cracks
2017: OCT - AD 90-08-14 Dye Penetrant Inspection of Forward Wing Spar, Next Inspection at 13,775 Hours Total Airframe Time, New Engine Mounts Installed.
2015: Janitrol Heater Overhaul.
2012: Repaired Forward Inboard/Outboard Aft Aux Wing Fuel Bladder, Installed D'Shannon Cooling Baffle Kits on Engines, MOTORS OVERHAULED by SIGNATURE and Re-Installed with New Lord Mounts and Flex Hoses, AD 09-08-14 Spar Inspection C/W - No Defects, Stainless Steel Fastener Kit Installed.
2009: (MAR) New LH Wing Bladder Installed
2000: AUG - New Exterior Paint & Interior by Phoenix Aviation. White Base, Alpine Green, Platinum, and Light Burgundy Striping. Milburn Leather Upholstery, Oyster White Trim, and Essential Carpet in the Cabin, NEW WINDSHIELD Installation.
During the Annual Inspection, the Nose Gear Partially Retracted, Bending the PROP TIPS. Pitot Masts and Tubes Were Replaced. A Micro Vortex Generator Kit and New Door Seals Were Also Installed. OCT - Flight Hour Meter Replaced, Factory REMANS Installed with New Slick Mags and Overhauled Fuel Injectors.
1997: (May) Accident Description - "After a Normal Touch and Go landing the Nose Gear Collapsed Upon Striking Three Wild Pigs on the Runway Centerline. At No Time Were the Pigs Visible Prior to Touchdown. Major Structural Fuselage Skin Damage Aft of The Nose Landing gear, ENGINES AND Props." The Shimmy Dampener Was Overhauled. Part Replacement Included a Serviceable Nose Strut Assembly, New Nose Drag Brace Assembly and Associated Hardware, New Nose Gear Doors, New Heater Duct Work, New Alternators, New Pitot Tubes, and Masts, Front Nose Skins (Bulkhead and Keel), Dye Penetrant Was Used to Check the Gear Retract Linkage Arm. New Lord Mounts and Bolts Were Included With 2 Reman Engines, S/N 810400-R and S/N 810399-R at 4770 HM. SEE FORM 337 for Details.
1996: New Wings Bolts and Doubler Kit 58-4008 Installed Due to Cracks in the Forward and Aft Carry-Through Spar at 4540-TTAF.
1991: IRAN Performed - a Zyglo Black Light and Eddy Current Methods Were Used in All Visual Inspections. Stabs Were Removed and Spars Inspected. Flight Controls Were Removed, Checked for Cracks and Corrosion, Reinstalled and Rigged. The Wings Were Removed and Inspected for Corrosion Along With the Fuselage and All Wing and Fuselage Attach Fittings. The Right-Hand Forward Corner Carry-Through Spar and Left-Hand Corners of the Aft Web on the Forward Carry-Through Were Repaired IAW SB 2269 and Kit 58-4008-98 and 110. In Addition, Landing Gear Shock Struts Were Resealed, The Flap Motor Was Replaced, New Wing Bolts and Tail Hardware Were Installed. Wings Were Re-Installed and Wing Bolts Were Coated With MIL-C-16173D Corrosion Preventative Compound. New Interior Upholstery Was Installed in the Cabin by Thunderbird Aviation. Overhauled Props Were Included.
1990: Precise Pulse Lights Installed.

Notable Periodic and/or Recurring ADs Affecting N929D:
2018-03-03:c Left & Right Forward, Lower Carry Thru Spar Cap Due at 15,000 Hours TTAF
2005-12-13: Recurring Inspection to Prevent Wing Spar Cap Failure at 10,000 Hours TTAF
90-08-14: Recurring 500-Hr Spar Web Inspection - Due at 13,775-TT (233 Hours).

This Aircraft was Enrolled in a PIP/Progressive Inspection Program while Under Care by The Airline Training Center of Phoenix from 1987 - 2000. Multiple Parts Were Replaced Due to Normal Wear, Defects, and/or Life Limits During the Period, Including Landing Gear Actuators, Engines and Props. See the Aircraft Records for Details.

Hours Flown Since 2018 to Present (Annual to Annual):

2018: No Annual
2019: 13,399.3-TT to 2022: 13,471.4 = 72.1 Hours
2020 and 2021: No Annuals
2022: 13,471.7-TT to 2023: 13,510.4-TT = 39.4 Hours
2023: 13,510.4-TT to 2024: 13,542.4-TT = 32 Hours
144 Hours Since 2018, Or An Average of 23 Hours Per Year Since 2018

Note: The Aircraft Was Out of Annual From January 2020 to February 2022, 2 Years and 1 Month.

Aircraft Operated/Based in AZ, OH, PA, VA

Aircraft Subject to Inspection Upon Verification of Specifications. Within 24 hours after the conclusion of the auction, (a) a $5,000 US dollar deposit is to be wired to the seller, or an escrow account set up and paid for by the buyer and (b) a written sales agreement outlining the terms of the sale will be executed by both buyer and seller. Pick-up/delivery to be at KROA, Roanoke, VA USA. within 7 days after the end of the auction. The Buyer or a representative of the buyer is welcome to survey the aircraft at his/her own expense prior to acceptance. Airworthiness issue(s), if discovered during the aircraft survey, will be addressed by the seller prior to finalizing the sale. Ferry fees, delivery expenses, and taxes are the responsibility of the Buyer.

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