1986 Beechcraft Baron 58

Formerly N3079P

Current Hour Meter 271.3

Gross Weight: 5,500 lbs.

Empty Weight: 3,755 lbs.

Useful Load: 1,745 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

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

Bendix/King KX-155 Digital Nav/Com with Glide Slope Receiver

Bendix/King KY-196 Digital Com Transceiver

JPI EDM-760 Engine Analyzer

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

Complete Refurbishment by Phoenix Aviation: Milburn Leather Upholstery, Oyster White Trim, Essential Carpet.

Club Seating

Arm Rests

Collapsible Writing Desks

Stereo Intercom Jacks

Complete Refurb in 2000 by Phoenix Aviation Using 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.

COPY/PASTE THE URLs BELOW IN YOUR BROWSER WINDOW TO ACCESS.

LINK TO LOGBOOK ACCESS & OIL ANALYSIS:                                                                 

https://mega.nz/file/fEAQkT7L#-GdFM5KK_di2Jh6faRFiM0lHKmtM8ki22KMHMNZomM4

LINK TO AIRWORTHINESS RECORDS (FORM 337s and STCs):

https://drive.google.com/file/d/1sJuvFWQ2iF6K9eSJV2x1CO1em7elaMlN/view?usp=sharing

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.

1991 & 1997 Inccidents: Details Outlined Above Under MAINTENANCE. Notations Recorded and Documented in Ship Logbooks & Form 337s.