AD 77-21-07

final rule

Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters

AD Number
77-21-07
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 Airbus Helicopters Deutschland GmbH BO-105A Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters
aircraft Airbus Helicopters Deutschland GmbH BO-105C Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters

Unsafe Condition

The unsafe condition involves improper socket connections (1 VED and 1 VEE) and plugs (110 VVa and 210 VVa) in the main relay box, which could lead to electrical system failure or fire due to arcing or short circuits.

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

Required Actions

Remove socket connections 1 VED and 1 VEE from the main relay box, remove plugs 110 VVa and 210 VVa along with their associated receptacles and wiring bundles, and install the generator wiring assembly per MBB Service Bulletin No. 90-11 dated April 17, 1975, or an FAA-approved equivalent.

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

Compliance Time

within the next 600 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

Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C helicopters, Serial Number V4 through V10, and S1 through S160

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

Federal Register Abstract

Wiring

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-21-07.html
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AD Number:
77-21-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters
Subject:
Wiring
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1977
Make:
Airbus Helicopters Deutschland GmbH
Model:
BO-105A | BO-105C
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 77-21-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3061

AD NUMBER:   77-21-07

SUBJECT HEADING:   Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   77-21-07 MESSERSCHMITT-BOLKOW-BLOHM (MBB): Amendment 39-3061. Applies to Model BO-105A and BO-105C helicopters, Serial Number V4 through V10, and S1 through S160, certificated in all categories.
Compliance required within the next 600 hours time in service after the effective date of this AD, unless already accomplished.
Remove socket connections 1 VED and 1 VEE from main relay box, remove plugs 110 VVa and 210 VVa together with associated receptacles and wiring bundles, and install generator wiring assembly, in accordance with subparagraph 2B of MBB Service Bulletin No. 90-11 dated April 17, 1975, or an FAA-approved equivalent.
This amendment becomes effective November 14, 1977.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-21-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-21-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters
Subject:
Wiring
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1977
Make:
Airbus Helicopters Deutschland GmbH
Model:
BO-105A | BO-105C
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 77-21-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3061

AD NUMBER:   77-21-07

SUBJECT HEADING:   Airworthiness Directives; Messerschmitt-Bolkow-Blohm (MBB) Model BO-105A and BO-105C Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   77-21-07 MESSERSCHMITT-BOLKOW-BLOHM (MBB): Amendment 39-3061. Applies to Model BO-105A and BO-105C helicopters, Serial Number V4 through V10, and S1 through S160, certificated in all categories.
Compliance required within the next 600 hours time in service after the effective date of this AD, unless already accomplished.
Remove socket connections 1 VED and 1 VEE from main relay box, remove plugs 110 VVa and 210 VVa together with associated receptacles and wiring bundles, and install generator wiring assembly, in accordance with subparagraph 2B of MBB Service Bulletin No. 90-11 dated April 17, 1975, or an FAA-approved equivalent.
This amendment becomes effective November 14, 1977.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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