Aircraft management for owners and co-owners

Manage your aircraft in one private workspace.

Track maintenance, AD references, squawks, aircraft time, oil, and documents. Coordinate co-owners and pilots. Add logbook scanning only when you need it.

Add my aircraft See what is included
Searchable records Maintenance readiness Owner operations

Three connected offerings

Use what you need. Keep it tied to the same aircraft.

Start with the aircraft workspace, add private group scheduling when ownership is shared, and purchase logbook review only when digitizing existing records is useful.

01
Core workspace · no scan required

Aircraft management

Your day-to-day supplemental tracking view for the airplane.

  • Maintenance tracking, inspections, AD references, and squawks
  • Meter baselines, airframe time, flights, and oil by engine
  • Aircraft documents and controlled record sharing
Create an aircraft workspace
02
For private ownership groups

Co-owner scheduling

A shared operational calendar connected to the aircraft.

  • Member reservations, scheduling rules, and conflict handling
  • Aircraft handoffs and mobile postflight reports
  • Contract pilot coordination and private messaging
Explore co-owner scheduling

MyAviatorList is a supplemental digital tracking copy. It does not replace required aircraft maintenance records.

How the pieces connect

Start with the aircraft. Add tools when they solve a real job.

Manual records, optional scanned history, maintenance readiness, owner scheduling, and postflight reporting all feed the same aircraft picture.

01

Add your aircraft

Set its registration, components, current airframe time, and the meter you actually use. No logbook scan is required.

02

Build the record your way

Enter maintenance manually, upload documents, or use the optional logbook review to structure older aircraft history.

03

Keep it ready and coordinated

See inspections, AD references, and squawks while owners coordinate reservations, handoffs, and contract pilots.

04

Close every flight

Record meter time, oil by engine, and new squawks so the schedule and maintenance picture stay connected.

Optional aircraft logbook add-on

Turn old logbooks into a useful aircraft history.

When an aircraft already has years of paper records, the optional review creates searchable history for maintenance tracking, controlled sharing, and buyer due diligence—while keeping uncertainty visible for your mechanic, broker, or seller.

Maintenance timeline AD references Meter readings Recurring patterns
Start your review

Sample aircraft summary

Beechcraft Baron 58

Identifiers redacted for privacy

Digital working copy Supplemental review ready PDF
Maintenance history
AD references
Times and components

Verified Record

Overview

  • Aircraft: Beechcraft 58 Baron, Reg NME*, S/N TH-***
  • Total tach (last logged): 2370.5 hr (latest consistent operating meter/Hobbs 2026-02-24; older logs mix tach/hour-meter/Hobbs labels). Engine serial: LH Continental IO-520-CB8B S/N 1008620, RH Continental IO-520-CB8B S/N 1008824 (Continental rebuilt engines installed 2013-10-01)
  • Condition impression: Later records show a substantially upgraded and actively maintained Baron, but the history also includes spar/corrosion/door repairs and uneven historical AD paperwork quality
  • Record confidence: Medium — post-2013 records are strong and detailed, but earlier logs contain date placeholders, meter inconsistencies, duplicated pages, and many vague AD entries

Current Times (Best Estimate)

  • Current airframe time (TTAF/AFTT): ≈ 5338.1 hr as of 2026-02-24 (basis: explicit ACTT entry, confidence: High)
  • Current engine time(s):
    • LH Continental IO-520-CB8B / S/N 1008620: TSN/TTE ≈ Unknown (rebuilt engine total-since-new not supported by provided entries), confidence: Low; SMOH/TSO ≈ 1010.8 hr (basis: 2026-02-24 LH engine annual entry), confidence: High; notes: Continental rebuilt engine tested 2013-07-18, installed 2013-10-01 at Hobbs 1359.7 / aircraft time 4326.7
    • RH Continental IO-520-CB8B / S/N 1008824: TSN/TTE ≈ Unknown, confidence: Low; SMOH/TSO ≈ 1010.8 hr (basis: 2026-02-24 RH engine annual entry), confidence: High; notes: Continental rebuilt engine tested 2013-08-02, installed 2013-10-01; a few later entries miswrite the S/N as 1008624/1006824, but the later consistent engine log identity is 1008824
  • Current propeller time(s):
    • LH Hartzell PHC-J3YF-2UF / S/N ED1898: TSN ≈ Unknown (not supported), confidence: Low; SPOH/TSO ≈ 735.5 hr (basis: 2026-02-24 airframe hours summary; prop overhauled Jan 2017 and later carried at TSO 0 on 2017-01-17), confidence: High; notes: current left prop identity consistently supported
    • RH Hartzell PHC-J3YF-2UF / S/N ED3745A: TSN ≈ Unknown (not supported), confidence: Low; SPOH/TSO ≈ 735.5 hr (basis: 2026-02-25 RH prop annual entry), confidence: High; notes: overhauled Jan 2017
  • Assumptions/data quality: Older logs interchange tach/hour-meter/Hobbs; several entries contain obvious typos (e.g., 2000 TT 5440.2 outlier, right-engine S/N variants, occasional registration typos NEM*/NME*/NME*)

Aircraft History & Records

  • Registrations: N4W* (prior), NME* (changed by 2005-06-03). Clerical variants NEM*/NME*/NME* also appear.
  • Major damage/repair history (from logbook):
    • 1980-12-06: crack in tail cone repaired during 100-hr
    • 1995-12-18: wing spar/carry-through cracking noted under AD 90-08-14; cracks stop-drilled, later followed by repeated inspections with no further cracks noted
    • 2005-05-04: cabin door damaged area repaired with fabricated internal doubler
    • 2005-06-03: paint strip/refinish entry states external corrosion removed, treated, epoxy primed, and repainted
    • 2021-08-10: aft cabin floor/support channel corrosion from STA 118.5 to 179.0; LH/RH support channels replaced, primed, treated with ACF-50, FAA Form 337 referenced
    • 2026-02-24: engine mount repaired by outside facility (Advanced Welding Technologies 8130 referenced), reinstalled/primed/painted
  • Preventive/protective maintenance noted:
    • Repeated gear/wheel bearing lubrication and rigging checks
    • Corrosion treatment with ACF-50/CorrosionX, battery-box cleaning, priming, paint touch-up
    • Fuel strainer/filter cleanings, deice boot patching, anti-chafe tape installation, propeller servicing/lubrication
  • AD/SB compliance and STCs/337s documented:
    • 2013: both engines replaced with Continental rebuilt IO-520-CB8B engines
    • 2013: Garmin GTN-750 installation per STC SA02019SE-D
    • 2019: Garmin GFC600 autopilot, dual G5s, GTX345 ADS-B, new pilot panel
    • 1994: D’Shannon gap seal kit STC SA1471CE
    • 1995: Norton radome kit/STC SA15GL with weather radar system (later radar removed)
    • 1996: pneumatic deice boots installed
    • Multiple 337-referenced avionics, windows, and structural/corrosion items
  • Usage patterns: The aircraft shows long historic periods of low/intermittent use, then moderate use after the 2013 engine replacement (about 1011 hr in roughly 12.4 years, ~82 hr/year)

Usage Statistics

  • Last logged time: 2370.5 hr (2026-02-24) - Hobbs; latest ACTT 5338.1 hr same date
  • Hours last 12 months (approx): 89.9 hr (monthly avg ≈ 7.5 hr/month)
  • Hours last 5 years (approx): 363.5 hr (avg ≈ 72.7 hr/year)
  • Hours last 10 years (approx): 833.2 hr (avg ≈ 83.3 hr/year)
  • Hours since engine overhaul (2013-10-01 at Hobbs 1359.7 / A/C time 4326.7): ≈ 1010.8 hr SMOH/TSO
  • Oil-change intervals (historical sample): median ≈ 43.5 hr, mean ≈ 53.5 hr (range 28.9-154.1 hr)
  • Significant gaps:
    • 1975-06-11 → 1978-10-19 ≈ 1226 days
    • 1980-12-06 → 1984-02-03 ≈ 1154 days
    • 1994-12-18 → 1997-05-21 ≈ 885 days
    • 2011-03-07 → 2012-08-03 ≈ 515 days
    • 2020-04-20 → 2021-08-10 ≈ 477 days
    • 2024-12-24 → 2026-02-24 ≈ 427 days
  • Data quality note: Use calculations rely primarily on consistent ACTT/Hobbs progression after excluding obvious outliers and mislabeled entries
  • Interpretation: Recent utilization is moderate, not high; the aircraft is not a “hanger queen,” but long historic inactivity periods raise the usual storage/corrosion/stuck-valve concerns on an aging piston twin

Compliance

  • Annual/Phase/Progressive inspections: Annuals are well represented through 2026-02-24. Later annuals (especially 2013 forward) are substantially better documented than early records.
  • 100-hour inspections: Numerous historical 100-hour inspections appear, especially through the 1970s-2000s and again with engine/prop component log entries in later years; latest clearly documented 100-hour style engine/prop inspections are 2024-12-24
  • Engine AD/SB compliance: Recurrent Bendix ignition-switch AD work is documented many times; wing spar/carry-through AD 90-08-14 is one of the best documented recurring items; engine mount AD 91-15-20 appears first as inspections and later as mount installation/terminating-style action in 2013
  • Avionics/Certification: Latest pitot/static/altimeter/transponder certification found 2025-09-11 by Duncan Aviation; 91.411/91.413 status appears current through September 2027 based on that entry
  • ELT tests: ELT checks appear regularly; latest explicit inspection/test 2026-02-24. Battery last explicitly replaced 2024-12-24 with expiry 11/2026
  • Life-limited parts: Not supported by provided logbook entries
  • Summary: Inspection currency appears current in the provided logs, but AD paperwork quality ranges from strong recent examples to historically weak shorthand entries

Service Bulletins & Value-Adding Modifications

Service Bulletins Completed:

SB NUMBER DATE DESCRIPTION VALUE IMPACT PERFORMED BY
Beech SB 2269 Rev 1 1995-12-18 Wing spar/carry-through crack inspection under AD 90-08-14; cracks stop-drilled High - major safety relevance Million Air of Evansville
Beech SB53-2269 Rev 2 2013-10-01 Spar carry-through inspection under AD 90-08-14; left front not due because recent kit install, others inspected High - major structural AD support Cape Fear Airworks
Beech MSB2269 2024-12-24 500-hr dye-penetrant spar web inspection under AD 90-08-14; no relevant indications High - best recent AD documentation Aircraft Maintenance Services, Inc.
Beech SB 2362 Rev 1 1992-12-15 Engine vibrator/engine mount inspection per AD 91-15-20 High - engine-mount safety Million Air of Evansville
Beech SB 2362 Rev 1 1994-01-24 Right-side engine mount visual inspection; owner declined magnetic inspection/kit at that time Medium - safety relevant, but incomplete follow-through that day Million Air of Evansville
Beech SB 2399 1992-06-13 AD 91-17-01 ELT-battery-related compliance entry Low - regulatory/ELT value Robert Kloe IA
Garmin STC SB 22026 Rev A 2023-06-06 GTN 750 software updated from 6.62 to 6.72 Medium - improves supportability/current software Powell Avionics
Garmin STC SB 22123 Rev A 2023-06-06 Dual G5 software updated from 6.20 to 8.02 Medium - improves supportability/current software Powell Avionics
Continental SB11-3 2026-02-24 Both alternators fitted with overhauled drive couplings per SB11-3 Medium - reliability/preventive value Home Safe Aviation
Hartzell SB 118E / 136H / 159A / 174 / 155A 2002-10-08 Prop overhaul paperwork for ED3745A notes these SBs complied with Medium - overhaul/value preservation H & H Propeller Service
Hartzell SB 118F / 136T / 165E / 226 / 150A 2004-02-04 Prop overhaul paperwork for ED1898 notes these SBs complied with Medium - overhaul/value preservation H & H Propeller Service
Hartzell SB 118F / 136J / 245 / 348 2017-01-10 Prop overhaul paperwork for ED1898 notes these SBs complied with Medium - current prop overhaul pedigree H & H Propeller Service
Hartzell SB 118F / 136I / 245 / 348 2017-01-10 Prop overhaul paperwork for ED3745A notes these SBs complied with Medium - current prop overhaul pedigree H & H Propeller Service

  • Garmin GTN 750 navigator

  • Garmin GFC600 autopilot

  • Dual Garmin G5 flight instruments

  • Garmin GTX345 ADS-B In/Out transponder

  • PS Engineering PMA8000BT audio panel/intercom

  • GAMI injector kits on both rebuilt Continental engines

  • Hartzell PHC-J3YF-2UF propellers

  • BFGoodrich pneumatic deice boot system (left-wing boot replaced 2026)

  • LP Aero replacement windshield/cabin windows

  • D’Shannon gap seal kit

  • Refurbished interior and repaint (2005), still effectively part of the current aircraft configuration

  • Beechcraft utility door kit installed 1988-10-21, removed 1988-10-23

  • Legacy autopilot and associated components removed 2019 during Garmin GFC600 install

  • Legacy stormscope and radar system removed 2019

  • KLN90B / KNS-80 / KR-21 / KY-196 legacy nav/comm stack removed 2013

  • Apollo 360 MAP GPS removed 2005

  • ADF system removed 1994

  • Propeller alcohol deice system deactivated 2017 (still noted as deactivated in 2026 anti-ice plumbing entry)

Unclear Status:

  • EI ASC-5A clock/altitude alerter (installed 2005; not clearly referenced near end of logs)
  • Some older fuel-flow instrumentation changes from the 1990s/2000s are not clearly carried forward in later logs

Assessment: The avionics package is a strong value driver. The 2013 engine replacement, 2019 Garmin/GFC600 panel, boots, GTN/G5/GTX345, and prop-overhaul pedigree add meaningful utility and resale appeal. The only caution is to verify current ice-equipment configuration and placarding because the prop alcohol deice system was later deactivated.

Observations

For Pistons:

  • Compression checks (selected historic values):
    • 2014-11-15 RH: 75/75/75/76/75/76; LH: 77/74/76/72/77/74
    • 2015-12-11 RH: 66/?/70/69/72/70; LH: 68/?/70/58/72/60
    • 2017-01-17 RH: 70/72/72/72/71/74; LH: 76/74/75/70/73/73
    • 2018-02-02 RH: 67/?/?/?/74/67; LH: 69/?/75/70/73/52
    • 2020-04-20 RH: 58/70/60/60/60/45 (then #6 cylinder replaced with O/H unit same entry); LH: 58/52/60/70/58/58
    • 2024-12-24 RH: 60/66/60/70/70/58; LH: 60/60/66/64/58/70
    • 2026-02-24 RH: 64/63/60/70/61/68; LH: 60/60/64/60/62/68
      Trend: Generally serviceable but not pristine; several cylinders have lived in the high-50s/low-60s. The clearest event was RH #6 at 45/80 in 2020, which was followed immediately by cylinder replacement, and later readings appear stabilized.

All Types:

  • Oil/filter findings: Repeated entries from 2014 through 2026 say filters were cut and inspected with no findings/no abnormal material
  • Recurring maintenance items:
    • Landing gear rigging/uplock/downlock hardware, actuator/motor/rod-end/door adjustments
    • Brakes, tires, wheel bearings, and brake hydraulic seals
    • Fuel quantity/fuel sender/fuel cell issues over many years
    • Cabin heater/Janitrol system items
    • Periodic avionics/instrument repairs and upgrades
  • Evidence of care:
    • 2013 engine change with good component detail
    • 2019 major Garmin/GFC600 upgrade with test flight and W&B update
    • Repeated cut-open filter inspections, recent borescopes, and detailed annuals
    • Corrosion findings were typically treated, primed, and documented rather than ignored
  • Red flags:
    • Historical AD paperwork is often too vague
    • Confirm the exact details of the 2026 engine-mount repair from the referenced 8130/work order
    • 2021 aft-cabin corrosion was real structural corrosion repair, not just preventive treatment
    • Wing spar carry-through cracking existed historically; later monitoring looks diligent, but that area remains a mandatory buyer focus

Engine Data

For Pistons:

  • Engine: Continental IO-520-CB8B, S/N 1008620 (LH). Continental rebuild paperwork dated 2013-07-19 / test date 2013-07-18; installed 2013-10-01
  • Engine: Continental IO-520-CB8B, S/N 1008824 (RH). Continental rebuild paperwork dated 2013-08-05 / test date 2013-08-02; installed 2013-10-01
  • SMOH: ≈ 1010.8 hr each (to 2026-02-24). Recommended TBO: Unknown / not supported by provided logbook entries
  • Cylinders:
    • RH #6 cylinder replaced with O/H unit on 2020-04-20 after 45/80 compression
    • 2024/2026 entries show valve/rotocoil work rather than wholesale cylinder replacement
  • Magnetos: Bendix-type system supported by recurring AD 76-07-12 switch checks; 500-hr magneto inspections documented in multiple engine entries, including detailed 2024 work per Bendix S1200 series manual

Airworthiness Directives (last compliance)

FAA COMPLIANCE REQUIREMENT: Per FAR Part 43.9 and 43.11, each AD must show the specific compliance method and action taken, not just "complied with"

AD NUMBER LAST COMPLIANCE DATE COMPLIANCE METHOD ACTION TAKEN NEXT DUE MECHANIC/IA
64-26-02 1988-10-10 Not stated Entry says parts on back order for induction air filter AD; no clear completion shown Unknown IA 22326
71-15-20 2009-05-19 Not stated Only listed as complied during annual; likely typo for 91-15-20 Unknown 561920478 IA
72-22-01 2007-05-14 Not stated in last entry Recurrent uplock-roller AD repeatedly referenced; earlier entries specifically describe greasing/inspection Not clearly stated in last entry Unclear
73-2201 1988-10-10 By inspection and lube Landing gear uplock rollers inspected/lubed Unknown IA 22326
74-03-02 Unknown Unknown Only listed as “landing gear shock strut pistons D-NC” Unknown Unknown
74-20-11 1974-10-16 By installation Installed bonding wires on Grimes strobe-light assemblies Not stated BD Sasser / Stevens Beechcraft
AD NOTE 75-05-03 1975-06-11 Not completed in entry Parts on order for elevator trim tab rods; no clear closeout in same entry Unknown Tom Atchley / Stevens Beechcraft
76-04-07 Unknown Unknown Only emergency-window note shown Unknown Unknown
76-07-12 2024-12-24 Inspection of ignition switches Ignition-switch inspection during annual Not stated in last entry (2024-01-16 entry gave next due 5286.9) Ryan Turiak A&P3653585IA
76-07-12R1 2024-12-24 Inspection of ignition switches Ignition-switch inspection Not stated Ryan Turiak A&P3653585IA
76-07-18 Unknown Operational change/swap “Both igniters switched D/C”; systems checked OK on ground run Unknown A&P561868744
76-13-5 Unknown Unknown Listed as “Electrical Power D.N.A.” N/A Unknown
76-22-02 Unknown Unknown Listed as “Seat Belt Rollers D.N.A.” N/A Unknown
77-02-04 Unknown Unknown Listed as “Wing Tip Strobes D.N.A.” N/A Unknown
77-05-06 Unknown Unknown Listed as “Fuel Cells C/W” only Unknown Unknown
77-12-06 Unknown Hub overhaul reference Propeller hubs overhauled at recorded hours; no clear dated compliance entry in provided text Unknown Unknown
77-13-22 1988-10-10 By inspection Crankcase-crack inspection noted; earlier 1979 entry also says complied Unknown IA 22326
77-15-17 Unknown Unknown Only listed as D.N.A. N/A Unknown
77-21-04 Unknown Unknown Description not legible Unknown Unknown
78-05-06 1979-12-03 By inspection only Fuel-cell related AD entry specifically says complied by inspection only Unknown Charles P. Easton IA 1001949
79-01-01 / 79-0101 1979-12-03 Not stated Listed among complied ADs; separate undated page calls it screws in control system Unknown Charles P. Easton IA 1001949
79-18-05 1979-12-03 Not stated Listed among complied ADs during 100-hr Unknown Charles P. Easton IA 1001949
82-07-03 1994-12-15 Applicability determination Janitrol heater AD found N/A to S50 type heater N/A AP2184/07
84-01-64 1984-02-03 Not stated “Check ADs thru 84-01-64 VFR - Comply” only Unknown IA 11746TB
84-09-01 1989-06-03 (best associated date) Not stated Emergency-window note on AD list page; details poor Unknown Unknown
84-26-00 1992-06-13 Inspection “Engine air inlet AD 84-26-00 OK” Unknown Robert Kloe IA
84-26-02 1995-12-18 Replacement Induction air filters replaced Next due 1117.8 tach (as written) Million Air of Evansville
84-26-04 1994-01-24 Replacement Installed new engine air filters both engines Unknown Million Air of Evansville
86-21-04 1987-01-18 Not stated Only “Check AD show 86-21-04” Unknown Delmer Lockwin IA 1174678
87-15-06R1 (documented as 87-1506R1) 1989-06-03 Applicability/reference list Seat-related note says N/A by service/reference N/A/Unknown Unknown
88-03-06 1989-06-04 Applicability determination “Oil filt not installed” N/A Unknown
88-17-03 1989-06-04 Applicability determination “N/A by model # engine” N/A Unknown
88-21-02 1989-06-03 Applicability/reference list Seal-related note says N/A by service/reference N/A Unknown
90-08-?? Unknown Unknown Partial AD number only in flap-actuator entry Unknown Unknown
90-08-14 2024-12-24 500-hr dye-penetrant inspection per MSB2269 Spar web inspected; no relevant indications noted Due again at AFTT 5732.9 Ryan Turiak A&P3653585IA
91-15-20 2013-10-01 Installation/terminating-style action Installed LH & RH engine mounts P/N96*-910010-85; earlier inspections per SB 2362 Rev 1 documented Entry says “100 hr re-inspect” Cape Fear Airworks A&P1759842IA
91-17-01 1992-06-13 Per SB 2399 ELT battery replaced Unknown Robert Kloe IA
92-22-01 1999-11-03 Not clearly separated Annual entry states C/W AD 92-22-01 amid landing gear/wheel work Unknown Unknown
93-05-06 1994-12-15 Applicability determination Ignition-switch AD N/A due Bendix P/N10*-357230-1 N/A AP2184/07
93-08-17 1994-12-15 Per SB M91-10 Rev 1 Oil pick-up tube check; found N/A to listed engines N/A AP2184/07
94-01-03 1995-12-18 Applicability determination “R2 TCM mags - Bendix N/A” N/A Million Air of Evansville
94-09-07 1994-12-15 Applicability determination Engine mount bracket AD found N/A N/A AP2184/07
95-03-02 1995-12-18 Applicability determination Brackett air filters N/A N/A Million Air of Evansville
95-03-14 1995-12-18 Applicability determination TCM-engine AD N/A per engine since-new/overhaul dates N/A Million Air of Evansville
96-12-07 2007-05-14 Not stated in last entry Recurrent compliance referenced; earlier 1997 entry specifies TCM/Bendix impulse per MSB 639-645 Unknown Unclear
96-20-07 2003-09-26 Heater inspection/cleaning Heater burner pulled/cleaned/inspected; note says 2 years or 500 hrs 2 years or 500 hrs (as written) John Barnes
97-14-15 1997-09-19 Not stated Cabin door handle AD referenced during annual Unknown Million Air of Evansville
97-15-20 2002-07-17 Not stated Listed on annual AD page; likely typo/variant, no method shown Unknown Unknown
98-04-24 2001-07-22 AFM insertion Complied by inserting copy of AD in AFM Not stated Unclear
99-05-13 Unknown Unknown Only listed in undated flap-actuator entry Unknown Unknown
99-09-15 Unknown Unknown Only listed in undated flap-actuator entry Unknown Unknown
2000-16 2022-02-26 Handwritten, unclear Dense handwritten block references inspection/performance/replacement, but exact method/action is not legible enough to verify Appears to mention future due, not legible Williams A&P 237825035
2000-18-02 2000-04-17 Applicability determination Not applicable because elevator skins not replaced after 1998-12-31 N/A IA 450963498
2001-08-01 2001-06-05 (as documented) Applicability determination Heater regulator / valve AD noted not applicable because specified equipment not installed N/A Richard C. Pluhbe A&P450963498
2001-11-03 2002-04-08 Unknown Handwritten AD reference only Unknown Unknown
2001-17-13 2004-02-05 Applicability determination Heater pressure regulator/pilot cut-off valve not installed N/A IA450963498
2001-23-10 2002-04-08 Unknown Handwritten AD reference only Unknown Unknown
2002-09-08 2003-04-10 Overhaul reference Prop blade removed and propeller overhauled 2002-10-08 by H&H Not stated IA 450963498
2002-11-07 2003-11-10 Unknown AD reference only on W&B page Unknown Unknown
2003-01-01 2004-02-05 By inspection Fuselage inspected for missing rivets; none missing Not stated Richard C. Polak IA 450963498
2003-13-12 2004-02-05 Applicability/compliance note not fully legible Prop annual references blade-separation AD Unknown IA 450963498
2003-13-17 2004-02-05 Applicability determination Does not apply due to propeller/work configuration N/A Richard C. Riddle IA
2007-08-08 Part 4 2026-02-24 Lubrication Uplock rollers lubricated Not stated Scott Tholen A&P 3696868
08-13-17 2010-05-10 Replacement Replaced 10 circuit-breaker switches Not stated PF Flyers / IA SC1920478
11-5-99 2002-04-08 Unknown Handwritten AD reference only Unknown Unknown
13-16-01 2013-10-01 Record search No elevators or balance weights changed; no further action required N/A Cape Fear Airworks
14-05-29 2014-11-15 Applicability determination N/A because no Superior cylinders installed N/A Cape Fear Airworks A&P1759842IA
16-16-12 2017-01-17 Applicability determination N/A because all Continental cylinders installed N/A Cape Fear Airworks A&P3694900 IA
17-04-06 2018-02-02 Applicability determination N/A by altimeter model/date of manufacture N/A Cape Fear Airworks
17-06-03 2018-02-02 Applicability determination N/A by heater model installed N/A Cape Fear Airworks
17-16-01 2018-02-02 Applicability determination N/A by ELT brand installed N/A Cape Fear Airworks
AD Note 07-26-09 2017-01-10 Prop overhaul note Prop overhaul paperwork references this AD note during overhaul Not stated H & H Propeller Service

Notes:

  • This AD table lists ALL ADs found in the provided logbook entries
  • WARNING: Any AD showing only "complied with" without specific method/action may not meet legal requirements
  • Additional applicable ADs may exist that are not documented in these logbook entries

Current Part Numbers

Include ALL: engines, props, cylinders, mags, filters, batteries, tires, pumps, avionics, instruments, etc.
(Show most-recent installation for each unique component - sorted by category then component)

COMPONENT PART NUMBER SERIAL NUMBER DATE INSTALLED (LOG) TSO/PMA STATUS NOTES
Airframe battery (forward) RG-25 70063786 2026-02-24 Unknown Main battery
Airframe battery (aft) RG-25 70063854 2026-02-24 Unknown Main battery
Voltage regulator #1 B-00387-1 81117602 2025-04-18 Unknown Replaced old 60-389017-3 S/N50*
Standby attitude indicator 1U149-010-0 T99117P 2025-08-18 Unknown Overhauled replacement
Gear motor circuit breaker 7271-8-30 Unknown 2024-12-24 Unknown Replaced
LH engine mixture control cable 50-389012-29 Unknown 2024-12-24 Unknown Rigged per AMM
Rudder/static wick SW10-96 Unknown 2024-12-24 Unknown Missing wick replaced on rudder and RH elevator
Belly scupper drain S-43 Unknown 2024-12-24 Unknown Installed missing drain
Main brake discs 164-02706 Unknown 2026-02-24 Unknown Both main discs replaced
Main brake linings 066-09700 Unknown 2026-02-24 Unknown All linings replaced
Nose wheel felt seal 154-00100 Unknown 2024-12-24 Unknown Nose wheel bearing seal
Main gear uplock cable springs 100942C0020-31 Unknown 2026-02-24 Unknown Both mains
Nose gear retract rod/drag brace hardware Various incl. NAS6204-8D / 105740X-ZM0290 / 130909B192 Unknown 2026-02-24 Unknown Multiple trim/gear hardware renewals
Deice boot, LH wing SMR5057-01 1229 2026-02-24 STC installation Installed per STC SA02006NY / Form 337
ELT ELT-10 Narco 38393 In service by 2024-01-16 Unknown Battery expiry noted 11/2026
Standby altimeter 5934P-3 407089 1999-12-06 Unknown Still present and tested 2025-09-11
Engine LH IO-520-CB8B 1008620 2013-10-01 Rebuilt Continental engine Latest ETSO 1010.8 hr on 2026-02-24
Engine RH IO-520-CB8B 1008824 2013-10-01 Rebuilt Continental engine Latest ETSO 1010.8 hr on 2026-02-24
Engine mounts 96-910010-85 Unknown 2013-10-01 Unknown Installed as AD 91-15-20 terminating-style action
Engine mounts (Barry) 96068-01 Unknown 2013-10-01 Unknown Eight new Barry mounts logged
GAMI injector kit LH #13AA 23166 2013-10-01 STC installation Six nozzles replacing Continental P/N 62335D13AA
GAMI injector kit RH #13AA 23167 2013-10-01 STC installation Six nozzles replacing Continental P/N 62335D13AA
Oil filter (latest) AA48108-2 Unknown 2026-02-24 Unknown Latest oil-filter P/N used both engines
Earlier oil filter CH48109-1 Unknown 2015-12-11 Unknown Recurrent earlier oil-filter P/N
Engine air filter BA-6205 Unknown 2026-02-24 Brackett Recurrent current induction-air filter element
LH vacuum pump 442CW-12 200945 2022-09-20 Rapco Removed S/N 154011
RH vacuum pump RAP442CW-12 208747 2024-12-24 Overhauled Failed vacuum pump replaced
LH alternator ALT-9522R H-A011815 2026-02-24 Overhauled Installed with drive coupling below
LH alternator drive coupling 646655 H-5120017 2026-02-24 Overhauled Per Continental SB11-3
RH alternator ALT-9522R H-Z120872 2026-02-24 Overhauled Installed with drive coupling below
RH alternator drive coupling 646655 H-5120014 2026-02-24 Overhauled Per Continental SB11-3
RH prop governor 210622 2124362 2026-02-24 Overhauled Replaced removed 210662 S/N 1438169
LH prop governor 210662 1144679L 2013-10-01 Overhauled Installed during engine change
RH propeller Hartzell PHC-J3YF-2UF ED3745A In service by 2017-01-17 overhaul/install cycle Unknown Current TSO 735.5 hr
LH propeller Hartzell PHC-J3YF-2UF ED1898 In service by 2017-01-17 overhaul/install cycle Unknown Current TSO 735.5 hr
Fuel-flow transducer (LH) 680501/X 87589 1996-05-28 Unknown Earlier Shadin transducer; later FF transducer P/N 680501A installed 2015
Fuel-flow transducer (later replacement) 680501A Unknown 2015-12-11 Unknown Same K-factor 29.4
Heater fuel pump 58-920054-11 / CA476284E-1 1444 (Batch 212811) 2023-03-02 Unknown Janitrol heater rear fuel pump
Heater ignition unit 12C60-1 680306/6800306 2004-02-05 Unknown Cabin heater ignition unit
Exhaust stack LH outboard assembly A96-950002-9 075413 2024-01-16 Unknown Aerospace Welding Minneapolis
Exhaust stack LH outboard assembly A96-950002-7 074649 2024-01-16 Unknown Aerospace Welding Minneapolis
Exhaust stack LH outboard assembly A96-950002-55 075453 2024-01-16 Unknown Aerospace Welding Minneapolis
Exhaust stack LH outboard assembly A96-950002-47 074764 2024-01-16 Unknown Aerospace Welding Minneapolis
Valve-cover gasket APS-655528-5 / 655528 Unknown 2026-02-24 Unknown Used in recent valve/rocker-cover work
Rotocoil 652112 Unknown 2026-02-24 Unknown Recent exhaust-valve rotocoil replacements
RH spark plug replacement noted RHB32S Unknown 2024-01-16 Unknown #1 lower spark plug replacement recorded on LH engine log
GTN 750 GPS/NAV/COM Unknown 1ZA011855 2013-05-23 STC installation Software updated 2023-06-06
Garmin G5 EFIS / Attitude 011-03809-00 4JQ025012 2019-03-05 STC installation Tested 2025-09-11
Garmin G5 EFIS / HSI 011-03809-00 4JQ024885 2019-03-05 STC installation Tested 2025-09-11
Garmin GTX345 transponder 011-03302-00 3EG023934 2019-03-05 STC installation ADS-B In/Out
PS Engineering PMA8000BT audio panel Unknown CBT2655 2013-05-23 Unknown 6-place intercom
Garmin GA-35 GPS/WAAS antenna GA-35 125697 2016-07-06 Unknown Replaced inoperative antenna
GA 60 transponder antenna KA 60 Unknown 1994-06-02 Unknown No later removal found
Com antenna CI-122 Unknown 1994-02-11 Unknown Com antenna
Nav antenna CI-120/200GS Unknown 1994-02-11 Unknown Nav antenna
Com antenna #1 CI-138 Unknown 1994-08-31 Unknown Replaced #1 com antenna
Audio panel legacy removed KMA-24H Unknown Removed 2013 Unknown Not current
Remote directional gyro SG832B 1591 1981-04-04 Unknown Present in later repairs; exact current status not fully re-logged
Standby/encoding altimeter 3252013-1101 / 3252013-0101 5041465 / Unknown In service before 1995-03-24 TSO noted in 1995 transponder install entry Legacy encoder/altimeter references before 1999 standby altimeter swap
Main tires 072-364-0 LH 2348T00310 / RH 2347T00281 2024-01-16 Unknown Condor 6.50-8 8-ply mains
Brake caliper seals MS28775-222 Unknown 2024-12-24 Unknown RH MLG caliper rebuild
Vacuum central filters D9-14-5 Unknown 2026-02-24 Unknown Replaced
Inline pressure filters 2J4-7 Unknown 2026-02-24 Unknown Replaced

Geographical History

  • Maintenance/ops timeline (key locations from logbook):
    • 1974-1977: Greer, SC / Knoxville & Tri-City, TN / Burlington, NC
    • 1978-1985: Illinois / Denver, CO / Evansville, IN
    • 1986-1989: Fresno, Bakersfield, Tulare, CA
    • 1993-1999: Oklahoma / Evansville, IN / Chesterfield, MO / NC
    • 2005-2007: Texas / Tennessee / Colorado / South Carolina
    • 2013-2017: Brunswick County, NC
    • 2017-2024: Columbia, SC / Loris, SC / Fayetteville, NC
    • 2025-2026: Moran, KS and Duncan Aviation pitot/static entry in Sept 2025
  • Environmental risks by location:
    • Coastal/humid Carolinas: elevated corrosion risk
    • Gulf-coast Texas: corrosion/humidity exposure
    • California interior / Colorado / Kansas: generally drier exposure
    • Midwest seasonal moisture/salt environments: moderate corrosion risk
  • Implication: Corrosion risk is real, not theoretical — the logs actually document corrosion remediation in 2005, 2018, 2021, 2026, consistent with a long Southeast/humid-climate operating history

Assessment

External Reference Check

  • Accident history (public sources only): I did not find a matching public accident/incident result for NME* or former registration N4W* in the limited NTSB/ASN-focused searches I reviewed. (aviation-safety.net)
  • Known issues for Beech 58 (public sources only): Public Beech/Baron references commonly flag engine-mount problems, the wing forward spar carry-through inspection area, a relatively tender nose gear/gear-system wear point, and tail/elevator hinge or attach-hardware looseness/wear. (aviationconsumer.com)
  • Which of these appear in the provided logbook: Engine-mount AD work and later mount repair do appear; spar carry-through inspections/crack repair definitely appear; landing-gear motor/actuator/rigging/hardware work is recurrent; elevator/trim-hardware wear and play issues also appear.
  • External/logbook boundary note: The public-source comments above are only type context; aircraft-specific conclusions here are based on the provided logbook, not on generic Baron reputation. (aviationconsumer.com)

Maintenance Pattern Analysis

Troubleshooting Patterns Detected:

Fuel quantity system

  • Fuel quantity system: repeated repairs over decades
    • Chronology: 1980 printed-circuit boards replaced but not calibrated → 1981 calibrated → 1993 LH fuel quantity repaired → 2005 circuit-board kit and overhauled transmitters → 2014 broken wire at RH fuel-quantity PCB repaired → 2016 five of six sending units found faulty and overhauled/calibrated
    • Pattern: repair → calibration → circuit-board/transmitter replacement → wiring repair → sender overhaul
    • Interpretation: Aging Baron fuel-quantity systems commonly need recurrent attention; the 2016 work looks thorough and calibrated, but it is a genuine recurring system
      Landing gear system
  • Landing gear system: heavy recurring attention over long periods
    • Chronology: numerous annual retraction/emergency-extension checks from the 1970s onward → 2017 gear actuator and electric motor removed for overhaul → 2020 landing gear motor replaced → 2024 large amount of rigging/hardware renewal → 2026 another extensive gear/hardware/tension overhaul
    • Pattern: inspect/lube → overhaul/replace → re-rig → recheck
    • Interpretation: This is a major maintenance focus area on this airplane; later work appears detailed and methodical rather than casual
      Cabin heater / Janitrol
  • Heater system: repeated maintenance over many years
    • Chronology: 1997 heater overhaul → 2000/2001 heater AD/applicability entries → 2004 ignition unit in heater → 2015 heater removed for overhaul → 2020 heater duct holes repaired after inop squawk → 2023 rear heater fuel pump replaced
    • Pattern: overhaul → AD/applicability review → component replacement → troubleshooting/duct repair → fuel-pump replacement
    • Interpretation: Not unusual for an older Janitrol-equipped twin, but definitely a recurring budget/safety item

Frequently Maintained Components:

  • Brakes/tires/wheel bearings: serviced repeatedly throughout the record vs typical wear-item expectations
  • Landing gear rigging/hardware/uplock components: more frequent than average single-engine aircraft, but not abnormal for an aging Baron
  • Fuel indication system: more frequent than desirable
  • Heater system: frequent enough to merit specific prebuy attention

"Parts Throwing" Indicators:

  • Fuel quantity system: Multiple different pieces addressed over time (PCB, transmitters, wiring, senders)
    • Concern level: Medium
    • Why: The system was not merely “cleaned and deferred”; it eventually got more complete corrective work, but it kept needing attention over many years
  • Avionics/instrument work in 1994-1995: numerous instrument/HSI/flux-detector/heading-system entries
    • Concern level: Low
    • Why: Much of that period appears to be upgrade/reconfiguration work rather than undiagnosed shotgun troubleshooting

AD Compliance Validation

  • Properly documented ADs:
    • AD 74-20-11
    • AD 90-08-14 (especially 1993, 1997, 1998, 2013, 2024)
    • AD 91-17-01
    • AD 98-04-24
    • AD 2000-18-02
    • AD 2003-01-01
    • AD 2007-08-08 part 4
    • AD 08-13-17
    • AD 13-16-01
    • AD 14-05-29
    • AD 16-16-12
  • INCOMPLETE DOCUMENTATION (may not meet FAR 43 requirements):
    • Many historical entries that only say “C/W ADs,” “AD list current,” or list the AD number with no method/action
    • Recurrent Bendix switch AD entries often say only “ops check” or “C/W” without interval/paragraph detail
    • Several old AD list pages are effectively index pages, not compliant maintenance entries
    • Some AD numbers are malformed/possibly mistyped (e.g., 71-15-20, 97-15-20, 84-26-00, 64-26-02, 87-1506R1)
  • Missing information that buyer should verify:
    • Original 337/supporting data for 1995 spar crack stop-drill/repair
    • Underlying work order/8130 for 2026 engine-mount repair
    • Full AD status sheet used at the latest annual
    • Whether older recurring ADs were tracked continuously or only referenced at annuals
  • Risk assessment: Documentation quality is mixed — recent spar AD documentation is good, but the legacy AD trail has enough shorthand and ambiguous entries to warrant a line-by-line prebuy verification

Intangible Concerns & Risk Factors

  • Maintenance style: Improved materially over time; 2013-forward records are much more detailed and confidence-inspiring than many earlier entries
  • Shop changes: Many over 50 years, but there is decent continuity within eras (Cape Fear → AMS Columbia → Sarvis → Home Safe)
  • Low utilization: Historic long gaps create the usual piston-twin risks of corrosion, sticky valves, dried seals, and stale squawks surfacing after return to service
  • Recurrent items: Gear system, brakes, heater, and fuel indication should be assumed continuing ownership budget items
  • Paperwork quality: Good recent mechanical detail; only fair overall due to older shorthand, typos, duplicate pages, and weak AD wording
  • AD compliance quality: Mixed to below ideal historically; some entries look professional and specific, while others are close to “pencil-whipped” by modern documentation standards

Bottom Line

Life story: This is a long-record Baron 58 that was modernized heavily, got rebuilt Continental engines in 2013, a major Garmin/GFC600 panel in 2019, and still shows active recent maintenance through early 2026. The logs also show real prior structural/corrosion events — spar cracking historically monitored under AD 90-08-14, cabin door repair, 2021 aft-cabin corrosion repair, and 2026 engine-mount repair — but most of those concerns do appear to have documented corrective action and later follow-up rather than being simply ignored.

Type-specific recommendations before purchase (minimum): Beech-specialist prebuy with spar carry-through review and NDI history verification; direct inspection of 2021 aft cabin corrosion repair and surrounding structure; direct inspection of 2026 engine-mount repair and supporting 8130/work order; full landing-gear rigging/actuator/gearbox evaluation; borescope both engines with special attention to recent valve/rotocoil work; verify current ice-system configuration/placards; audit all ADs/337s/STCs against original logbooks and FAA file.

BOTTOM LINE: This airplane is not a “walk away” candidate, but it is also not a casual “logs look good” purchase. The combination of strong modern upgrades and generally solid recent maintenance is attractive, but the buyer should proceed only with a very thorough Beech-savvy prebuy focused on spar history, corrosion repairs, landing gear, engine-mount paperwork, and legacy AD documentation.

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