AD 84-06-04

final rule

Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes

AD Number
84-06-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Hamburger Flugzeugbau G.m.b.H. HFB 320 Hansa Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes

Unsafe Condition

Failure of the stabilizer/elevator outboard bearing housing fittings due to cracks greater than 0.79 inches.

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

Required Actions

Perform a one-time inspection of the stabilizer/elevator outboard bearing housing fittings within 25 hours time in service or 45 days after the effective date, whichever occurs first. Replace fittings with cracks greater than 0.79 inches prior to further flight. Stop drill fittings with cracks 0.79 inches or less and replace them within six months.

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

Compliance Time

within 25 hours time in service or 45 days after the effective date of this AD, whichever occurs first

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

Affected Aircraft

MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 airplanes listed in HFB-320 Service Bulletin 55-8 dated September 14, 1983

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

Federal Register Abstract

Stabilizer/Elevator Fittings

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
84-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes
Subject:
Stabilizer/Elevator Fittings
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/09/1984
Make:
Hamburger Flugzeugbau G.m.b.H.
Model:
HFB 320 Hansa
Product Type:
Aircraft
Product Subtype:
Large 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Superseded AD: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Superseded By: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: 84-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4834

AD NUMBER:   84-06-04

SUBJECT HEADING:   Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 9, 1984.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   84-06-04 MESSERSCHMITT-BOLKOW-BLOHM GmbH: Amendment 39-4834. Applies to HFB-320 airplanes as listed in HFB-320 Service Bulletin 55-8 dated September 14, 1983, certificated in all categories. Compliance is required as indicated unless previously accomplished. To prevent failure of the stabilizer/elevator outboard bearing housing fittings accomplish the following:

A. Within the next 25 hours time in service or 45 days after the effective date of this AD, whichever occurs first, perform a one-time inspection of the stabilizer/elevator outboard bearing housing fittings in accordance with HFB-320 Service Bulletin 55-8 dated September 14, 1983. Fittings with cracks greater than 0.79 inches must be replaced prior to further flight. Fittings cracked 0.79 inches or less must be stop drilled per the service bulletin, but also must be replaced within six months.

B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This amendment becomes effective April 9, 1984.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_84-06-04.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
84-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes
Subject:
Stabilizer/Elevator Fittings
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/09/1984
Make:
Hamburger Flugzeugbau G.m.b.H.
Model:
HFB 320 Hansa
Product Type:
Aircraft
Product Subtype:
Large 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: 84-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4834

AD NUMBER:   84-06-04

SUBJECT HEADING:   Airworthiness Directives; MESSERSCHMITT-BOLKOW-BLOHM GmbH Model HFB-320 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 9, 1984.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   84-06-04 MESSERSCHMITT-BOLKOW-BLOHM GmbH: Amendment 39-4834. Applies to HFB-320 airplanes as listed in HFB-320 Service Bulletin 55-8 dated September 14, 1983, certificated in all categories. Compliance is required as indicated unless previously accomplished. To prevent failure of the stabilizer/elevator outboard bearing housing fittings accomplish the following:

A. Within the next 25 hours time in service or 45 days after the effective date of this AD, whichever occurs first, perform a one-time inspection of the stabilizer/elevator outboard bearing housing fittings in accordance with HFB-320 Service Bulletin 55-8 dated September 14, 1983. Fittings with cracks greater than 0.79 inches must be replaced prior to further flight. Fittings cracked 0.79 inches or less must be stop drilled per the service bulletin, but also must be replaced within six months.

B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This amendment becomes effective April 9, 1984.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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