AD 68-21-04

final rule

Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft

AD Number
68-21-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 65-90 Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft
aircraft Textron Aviation Inc. 65-A90 Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft
aircraft Textron Aviation Inc. 65-A90-1 Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft
aircraft Textron Aviation Inc. B90 Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft

Unsafe Condition

Ice damage to engine when operating in icing conditions above 15,000 feet MSL.

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

Required Actions

Install seal strips and a spring lockdown assembly on the Inertial Separator Vane and an automatic ignition (re-light) system per Beechcraft Service Instructions #0115-010. Equip the airplane with the applicable FAA Flight Manual as specified in the same service instructions. Maintain Emergency Order Amending Type Certificate No. 3A20 until required actions are completed.

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

Compliance Time

within one year after the effective date of this Airworthiness Directive

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

Affected Aircraft

BEECHCRAFT Models 65-90, 65-A90, 65-B90 (Serial Numbers LJ-1 through LJ-406) and 65-A90-1 (Serial Numbers LM-1 through LM-129)

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

Federal Register Abstract

Ice Damage to Engine

Applicability Source Text

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AD Number:
68-21-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft
Subject:
Ice Damage to Engine
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/17/1968
Make:
Textron Aviation Inc.
Model:
65-90 | 65-A90 | 65-A90-1 | B90
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: 68-21-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-668

AD NUMBER:   68-21-04

SUBJECT HEADING:   Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 17, 1968.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
68-21-04 BEECHCRAFT: Amendment 39-668. Applies to Models 65-90, 65-A90 and 65-B90 aircraft (Serial Numbers LJ-1 through LJ-406) and 65-A90-1 aircraft (Serial Numbers LM-1 through LM-129).

Compliance required as indicated.

To reduce the possibility of engine damage and malfunction while operating in icing conditions above 15,000 feet MSL, within one year after the effective date of this Airworthiness Directive, unless already accomplished, accomplish the following:

(A) Install seal strips and a spring lockdown assembly on the Inertial Separator Vane and an automatic ignition (re-light) system in accordance with the method outlined in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(B) Equip the airplane with the applicable FAA Flight Manual as set forth in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(C) The Emergency Order Amending Type Certificate No. 3A20 dated May 24, 1968, as amended September 19, 1968, shall remain in force and effect as to each individual aircraft covered by this Airworthiness Directive until paragraphs (A) and (B) have been accomplished.

This amendment becomes effective October 17, 1968.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_68-21-04.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
68-21-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft
Subject:
Ice Damage to Engine
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/17/1968
Make:
Textron Aviation Inc.
Model:
65-90 | 65-A90 | 65-A90-1 | B90
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: 68-21-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-668

AD NUMBER:   68-21-04

SUBJECT HEADING:   Airworthiness Directives; BEECHCRAFT Models 65-90, 65-A90, 65-B90 and 65-A90-1 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 17, 1968.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
68-21-04 BEECHCRAFT: Amendment 39-668. Applies to Models 65-90, 65-A90 and 65-B90 aircraft (Serial Numbers LJ-1 through LJ-406) and 65-A90-1 aircraft (Serial Numbers LM-1 through LM-129).

Compliance required as indicated.

To reduce the possibility of engine damage and malfunction while operating in icing conditions above 15,000 feet MSL, within one year after the effective date of this Airworthiness Directive, unless already accomplished, accomplish the following:

(A) Install seal strips and a spring lockdown assembly on the Inertial Separator Vane and an automatic ignition (re-light) system in accordance with the method outlined in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(B) Equip the airplane with the applicable FAA Flight Manual as set forth in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(C) The Emergency Order Amending Type Certificate No. 3A20 dated May 24, 1968, as amended September 19, 1968, shall remain in force and effect as to each individual aircraft covered by this Airworthiness Directive until paragraphs (A) and (B) have been accomplished.

This amendment becomes effective October 17, 1968.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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