AD 88-20-01

final rule

Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes

AD Number
88-20-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. A36 Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes
aircraft Textron Aviation Inc. B36TC Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes
aircraft Textron Aviation Inc. F33A Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes

Unsafe Condition

The Mortell 931 sound deadener material on the aft side of the firewall could cause a potential fire in the cabin.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove the Mortell 931 sound deadener material from the aft side of the firewall per Beech Service Bulletin 2249. Flights may be conducted under FAR 21.197 to a location where this AD can be accomplished. Equivalent compliance may be approved by the FAA Wichita Aircraft Certification Office.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within the next 100 hours time-in-service after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Beech Model F33A (serial numbers CE-1162 through CE-1223), A36 (serial numbers E-2383 through E-2405, E-2407 through E-2409), and B36TC (serial numbers EA-468 through EA-470, EA-472 through EA-474)

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Firewall Material

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_88-20-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
88-20-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes
Subject:
Firewall Material
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/19/1988
Make:
Textron Aviation Inc.
Model:
A36 | B36TC | F33A
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 88-20-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6017

AD NUMBER:   88-20-01

SUBJECT HEADING:   Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 19, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-20-01 BEECH: Amendment 39-6017. Applies to the following airplanes certificated in any category:

MODEL	SERIAL NUMBER
F33A	CE-1162 through CE-1223
A36	E-2383 through E-2405
E-2407 through E-2409
B36TC	EA-468 through EA-470
EA-472 through EA-474

Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent a potential fire in the cabin, accomplish the following:

(a) Remove the Mortell 931 sound deadener material from the aft side of the firewall in accordance with the instructions in Beech Service Bulletin Number 2249, dated April 1988.

(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

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

All persons affected by this directive may obtain copies of this document referred to herein upon request to Beech Aircraft Corporation, Commercial Service, Dept. 52, P.O. Box 85, Wichita, Kansas 67201-0085; or may examine this document at the FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

This amendment, 39-6017, becomes effective on October 19, 1988.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_88-20-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
88-20-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes
Subject:
Firewall Material
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/19/1988
Make:
Textron Aviation Inc.
Model:
A36 | B36TC | F33A
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 88-20-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6017

AD NUMBER:   88-20-01

SUBJECT HEADING:   Airworthiness Directives; Beech Model F33A, A36 and B36TC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective October 19, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-20-01 BEECH: Amendment 39-6017. Applies to the following airplanes certificated in any category:

MODEL	SERIAL NUMBER
F33A	CE-1162 through CE-1223
A36	E-2383 through E-2405
E-2407 through E-2409
B36TC	EA-468 through EA-470
EA-472 through EA-474

Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent a potential fire in the cabin, accomplish the following:

(a) Remove the Mortell 931 sound deadener material from the aft side of the firewall in accordance with the instructions in Beech Service Bulletin Number 2249, dated April 1988.

(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

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

All persons affected by this directive may obtain copies of this document referred to herein upon request to Beech Aircraft Corporation, Commercial Service, Dept. 52, P.O. Box 85, Wichita, Kansas 67201-0085; or may examine this document at the FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

This amendment, 39-6017, becomes effective on October 19, 1988.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.