AD 84-08-04

Airworthiness directive · Oil Return Line Check Valve · Textron A36TC and B36TC

Effective
October 15, 1984
Models
A36TC, B36TC
Data sheet
TCDS3A15
Registered aircraft
481 matched by model
Product
Aircraft · Small airplane
Amendment
39-4931

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed January 21, 2026.

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The airworthiness directive

84-08-04 BEECH: Amendment 39-4931. Applies to Model A36TC (S/Ns EA-1 thru EA-241 ((modified in accordance with Beech Service Instructions No. 1191)), and EA-243 thru EA-272), and Model B36TC (S/Ns EA-242, EA-273 thru EA-382, EA-384 thru EA-396, EA-398 thru EA- 404, EA-406 thru EA-409, EA-411 thru EA-415, and EA-418) airplanes certificated in any category.

Compliance: Required as indicated, unless already accomplished.

To prevent loss of engine oil due to blockage of the turbocharger oil return line check valve, accomplish the following:

(a) Prior to further flight after the effective date of this AD:

(1) Inspect the turbocharger oil return line check valve per Beechcraft Service Bulletin No. 2027 to determine if a P/N 101-389011-55 check valve is installed. This valve may be identified by the blue color and the P/N on the valve outlet end fitting.

(i) If a Beech P/N 101-389011-55 check valve is not installed, the airplane may be returned to service without further action.

(ii) If a Beech P/N 101-389011-55 check valve is installed, prior to return to service and within each additional five hours time-in-service until replaced, inspect and clean this valve in accordance with Beech Service Bulletin No. 2027.

(b) Within the next 25 hours time-in-service after the effective date of this AD on airplanes on which a Beech P/N 101-389011-55 check valve is installed, modify this part to, or replace it with, a Beech P/N 101-389011-69 check valve in accordance with Beech Service Bulletin No. 2027.

(c) The repetitive inspections in paragraph (a)(ii) are not required when a Beech P/N 101-389011-69 check valve is installed.

(d) An equivalent method of compliance with this AD may be used if approved by the Manager, Wichita Aircraft Certification Office, Room 100, 1801 Airport Road, Mid- Continent Airport, Wichita, Kansas 67209, telephone (316) 946-4400.

This amendment becomes effective on October 15, 1984, to all personsexcept those to whom it has already been made effective by priority letter from the FAA dated April 25, 1984.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 481

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Beech399 aircraft
  • Raytheon82 aircraft
By year built
19792002
Registered aircraft by year built: 408 aircraft
197936
198069
198146
198235
198335
198427
19856
19864
19874
19889
19894
19909
19919
19928
199311
199413
19958
19966
199710
199813
199914
200011
200118
20023

73 with no year recorded

By model

Aircraft

See all 481 aircraft