AD 47-34-02

Airworthiness directive · Tail Cone Drain Holes · Textron D18C, D18C-T and D18S

Models
D18C, D18C-T, D18S
Registered aircraft
55 matched by model
Product
Aircraft · Small airplane

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

47-34-02 BEECH: (Was Mandatory Note 3 of AD-770-1 and Mandatory Note 4 of AD- 765-1.) Applies to D18S, D18C and D18C-T Airplanes Which Do Not Have Drain Provisions at Bulkhead No. 15.

Compliance required prior to December 1, 1947.

To provide additional drainage, to prevent freezing of trapped moisture in the tail cone which could jam the elevator control system, a 3/4-inch diameter hole should be drilled near the front of the tail cone outer section on the centerline of the lower surface. A suitable marine grommet should be installed to provide for negative pressures. Also a 1/2-inch diameter hole should be drilled on each side of the jack pad through the lower part of bulkhead No. 15.

(Beech Service Bulletin D18-46 covers this same subject.)

Affected TCDS · 2

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

Registered aircraft · 55

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
  • Beech55 aircraft
By year built
19431966
Registered aircraft by year built: 41 aircraft
19431
19453
194615
19472
19482
19491
19501
19512
19526
19534
19542
19581
19661

14 with no year recorded

By model

Aircraft

See all 55 aircraft