AD 76-03-05

final rule

Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes

AD Number
76-03-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 35-B33 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
aircraft Textron Aviation Inc. 35-C33 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
aircraft Textron Aviation Inc. E33 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
aircraft Textron Aviation Inc. F33 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
aircraft Textron Aviation Inc. G33 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
aircraft Textron Aviation Inc. P35 Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes

Unsafe Condition

Contact of the tachometer cable housing with the battery relay

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

Required Actions

Install a tachometer cable housing stand-off bracket on the battery box and secure the tachometer cable housing to this bracket in accordance with Beechcraft Service Instruction No. 0784-241 or later FAA-approved revisions or by any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

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

Compliance Time

within the next 50 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 Models 35-B33, 35-C33, E-33, F-33, G-33 (Serial Numbers CD-388 thru CD-981 and CD-983 thru CD-1304); and Model P-35 (Serial Numbers D-6842 thru D-7139 and D-7141 thru D-7309)

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

Federal Register Abstract

Housing Cable and Battery Relay

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_76-03-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-03-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
Subject:
Housing Cable and Battery Relay
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/17/1976
Make:
Textron Aviation Inc.
Model:
35-B33 | 35-C33 | E33 | F33 | G33 | P35
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: 76-03-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2510

AD NUMBER:   76-03-05

SUBJECT HEADING:   Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 17, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-03-05 BEECH: Amendment 39-2510. Applies to Models 35-B33, 35-C33, E-33, F-33 and G-33 (Serial Numbers CD-388 thru CD-981 and CD-983 thru CD-1304); and Model P-35 (Serial Numbers D-6842 thru D-7139 and D-7141 thru D-7309) airplanes.

Compliance: Required as indicated unless already accomplished.

To preclude contact of the tachometer cable housing with the battery relay, within the next 50 hours' time in service after the effective date of this AD, install a tachometer cable housing stand-off bracket on the battery box and secure the tachometer cable housing to this bracket in accordance with Beechcraft Service Instruction No. 0784-241 or later FAA-approved revisions or by any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective February 17, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-03-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-03-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes
Subject:
Housing Cable and Battery Relay
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/17/1976
Make:
Textron Aviation Inc.
Model:
35-B33 | 35-C33 | E33 | F33 | G33 | P35
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: 76-03-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2510

AD NUMBER:   76-03-05

SUBJECT HEADING:   Airworthiness Directives; BEECH Models 35-B33, 35-C33, E-33, F-33, G-33, P-35 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 17, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-03-05 BEECH: Amendment 39-2510. Applies to Models 35-B33, 35-C33, E-33, F-33 and G-33 (Serial Numbers CD-388 thru CD-981 and CD-983 thru CD-1304); and Model P-35 (Serial Numbers D-6842 thru D-7139 and D-7141 thru D-7309) airplanes.

Compliance: Required as indicated unless already accomplished.

To preclude contact of the tachometer cable housing with the battery relay, within the next 50 hours' time in service after the effective date of this AD, install a tachometer cable housing stand-off bracket on the battery box and secure the tachometer cable housing to this bracket in accordance with Beechcraft Service Instruction No. 0784-241 or later FAA-approved revisions or by any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective February 17, 1976.

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.