AD 73-12-11

Airworthiness directive · Carburetor Air Box Valve · Textron 19A, 23, A23-19 and 4 more

Effective
July 27, 1973
Models
19A, 23, A23-19, B19, B23, C23, M19A
Data sheet
TCDSA1CE
Registered aircraft
926 matched by model
Product
Aircraft · Small airplane
Amendment
39-1691

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.

On this page

The airworthiness directive

73-12-11 BEECH: Amdt. 39-1662 as amended by Amendment 39-1691. Applies to Models 23, B23, and C23 (Serial Numbers M-1 through M-554 and M-1095 through M-1361, except M-3); Sundowner C23 (Serial Numbers M-1362 through M-1420, M-1423, M-1425, M- 1430, M-1438, M-1439, M-1442, M-1447, and M-1453 through M-1473); Models A23-19, 19A, M-19A, and B19 (Serial Numbers MB-1 through MB-520); and Sport B19 (Serial Numbers MB- 521 through MB-585) airplanes which do not have carburetor alternate air boxes modified in accordance with Beechcraft Service Instruction 0574-241 (installation of Beech P/N 23-9011-1S, 3S, or 5S Kits).

Compliance: Required as indicated, unless already accomplished.

To prevent engine power loss caused by ingestion of pieces of failed carburetor air valves, accomplish the following:

A) Prior to further flight, except that the airplane may be ferried to the inspection location and at subsequent intervals not to exceed 25 hours' time in service, inspect the carburetor air box for the following:

1) Wear and looseness between the carburetor alternate air valve and its shaft.

2) Looseness of rivets which hold the valve plates together.

3) Looseness and wear of the cap screws which attach the valve plates to the shaft.

If any of these conditions are found, accomplish Paragraph B below.

B) Within 120 days after the effective date of this AD, remove the existing carburetor air box valve and install Beech P/N 23-9011-1S or 23-9011-3S or 23-9011-5S Kit, as applicable, in accordance with Beechcraft Service Instructions 0574-241, or later FAA-approved revision or any alternate modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. The repetitive inspections specified in Paragraph A may be discontinued when this modification is accomplished.

This AD Amendment 39-1662 cancels and supersedes AD 72-01-04.

Amendment 39-1662 became effective June 18, 1973.

This amendment 39-1691 becomes effective July 27, 1973, to all persons except those to whom it was made effective by letter dated July 9, 1973.

Affected TCDS · 1

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

Registered aircraft · 926

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
  • Beech926 aircraft
By year built
19621983
Registered aircraft by year built: 780 aircraft
196230
196381
19644
19651
196638
196719
196850
196940
197012
197114
197222
197341
197471
197552
197671
197756
197867
197938
198028
198118
198213
198314

146 with no year recorded

By model

Aircraft

See all 926 aircraft