Beech A35 — Airworthiness Directives & records checklist

155 Beech A35s are on the U.S. registry. Here’s what a records review covers for one — the Airworthiness Directives that apply, the known trouble spots, and the checklist a buyer or owner should hold every logbook against.

Registered
155
Applicable ADs
3
Recurring
0
Serial-conditional
30

Airworthiness Directives that apply to the Beech A35

  • one-time
    AD 75-05-02 — Airworthiness Directives; BEECH, CESSNA, NAVION AND PIPER Models 35, A35, B35, C35, D35, E35, F35, G35, 35R, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E3 · 1975-01-01
  • one-time
    AD 59-08-01 — Airworthiness Directives; Beech Models A35, B35, C35 Aircraft · 1959-01-01
  • one-time
    AD 50-42-01 — Airworthiness Directives; Beech Model A35 Airplanes · 1950-01-01

This is the applicability list. Which of these are complied with, their computed next-due dates, and the 30 serial/mod-conditional ADs that actually apply to your aircraft come from its digitized logbooks — that’s the verified report.

Known trouble spots on the A35

V-tail ruddervator / cuff & forward spar (AD 94-20-04)medium

V-tail Bonanzas have a history of ruddervator magnesium-skin cracking and a leading-edge cuff / forward-spar-carry-through AD after in-flight tail failures. Confirm the recurring ruddervator and forward-spar inspections.

Propeller blade / hub AD & overhaul currencymedium

Many Hartzell and McCauley constant-speed props carry blade-shank or hub ADs plus a calendar/hours overhaul interval; blade corrosion and hub grease leaks are common findings. Confirm the prop AD status and last overhaul against the interval.

The records checklist for a Beech A35

Airworthiness Directives
Every applicable AD matched to compliance evidence, with recurring next-due dates.
Annual / 100-hr inspections
A continuous, signed inspection history (14 CFR 91.409) with no gaps.
Service bulletins & letters
Mandatory and recommended SBs/SLs, complied or noted.
Life-limited parts
Airworthiness-limitations items tracked against their limits.
Form 337s / major alterations
Field approvals and STCs on file and reconciled.
Equipment inspections
ELT (91.207), transponder (91.413), altimeter/pitot-static (91.411).
Damage & accident history
NTSB and repair-major records for this exact tail.
Logbook continuity
Unbroken records — the gaps are where value and airworthiness hide.
Run a verified records report on your A35

Enter a tail number and Tailplate reads its logbooks against this list — every AD matched to compliance evidence, next-due dates computed, damage history pulled, and a records-adjusted value.

Look up a tail number →or see the free AD list
Related Beech models

Applicability is derived from the FAA directive corpus and the aircraft’s type certificate; it is advisory and not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.