For Sale: 1986 BEECHCRAFT 58

Formerly N3079P, Current Hour Meter 271.3, Gross Weight: 5,500 lbs., Empty Weight: 3,755 lbs., Useful Load 1,744 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.

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

2000: Complete Refurbishment by Phoenix Aviation with New Milburn Leather Upholstery, Oyster White Trim, Essential Carpet, Rated 6/10. Club Seating, Arm Rests, Collapsible Writing Desks, Stereo Intercom Jacks

2000: Complete Refurbishment by Phoenix Aviation with New Paint (White Base, Alpine Green, Platinum, Light Burgundy). 2007: Paint Touch-Up on Engine Cowls, Landing Gear, Radome, Wheel Rims; Nose Erosion Boot Installed. Wing Leading Edges Stripped, Prepped, Primed, and Painted.

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.

166 Gallons Usable 

USED, GOOD Condition.

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.

LINKS TO LOGBOOK ACCESS, OIL ANALYSIS & AIRWORTHINESS RECORDS FURNISHED UPON REQUEST: COPY AND PASTE THE URL  LINK BELOW TO SEE YOU TUBE VIDEO: https://youtu.be/JSKYnufqQh8

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.

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).

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.

MAINTENANCE NOTATIONS - 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. 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. Landing Gear Shock Struts Were Resealed, The Flap Motor Was Replaced, New Wing Bolts & Tail Hardware were Installed, Wings Re-Installed, Wing Bolts Coated with Corrosion-Preventative Compound, New Interior Upholstery was Installed & Props were Overhauled. 1990: Precise Pulse Lights Installed.