AD 81-04-10

final rule

Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters

AD Number
81-04-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Kawasaki Heavy Industries, Limited KV107-II Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters
aircraft Kawasaki Heavy Industries, Limited KV107-IIA Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters

Unsafe Condition

Possible restriction of cyclic stick travel, which could result in an unsafe flight condition.

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

Required Actions

Loosen the velcro tape and camloc fasteners securing the pilot and copilot cyclic stick boots (P/N 107S2226-9), remove the boots, remove the two rivets attaching the forward spring (P/N 107S2226-12), discard the forward spring, install washers and new rivets to plug the holes, and reinstall the stick boots.

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

Compliance Time

Within the next 25 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

Kawasaki Heavy Industries, Limited Models KV107-II and KV107-IIA helicopters with pilot or copilot cyclic stick boots, P/N 107S2226-9, installed.

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

Federal Register Abstract

Cyclic Stick Boots

Applicability Source Text

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AD Number:
81-04-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters
Subject:
Cyclic Stick Boots
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/26/1981
Make:
Kawasaki Heavy Industries, Limited
Model:
KV107-II | KV107-IIA
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Superseded AD: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Superseded By: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: 81-04-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4045

AD NUMBER:   81-04-10

SUBJECT HEADING:   Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective February 26, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-04-10 KAWASAKI HEAVY INDUSTRIES, LTD.: Amendment 39-4045. Applies to Models KV107-II and KV107-IIA helicopters, certificated in all categories, with pilot or copilot cyclic stick boots, P/N 107S2226-9, installed.

Compliance required as indicated, unless already accomplished.

To prevent possible restriction of cyclic stick travel, which could result in an unsafe flight condition, accomplish the following:

(a) Within the next 25 hours time in service after the effective date of this AD, loosen the velcro tape and camloc fasteners securing the pilot and copilot cyclic stick boots, P/N 107S2226-9, and remove the boots.

(b) Remove the two rivets which attach the forward spring, P/N 107S2226-12, to the forward end of the boot base and discard the forward spring.

(c) Install washers and new rivets to plug the resulting two empty holes in the boot base.

(d) Reinstall the pilot and copilot stick boots.

(e) In accordance with FAR Sections 21.197 and 21.199, the helicopter may be flown to a base where the modification can be accomplished.

This amendment becomes effective February 26, 1981.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_81-04-10.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
81-04-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters
Subject:
Cyclic Stick Boots
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/26/1981
Make:
Kawasaki Heavy Industries, Limited
Model:
KV107-II | KV107-IIA
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: 81-04-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4045

AD NUMBER:   81-04-10

SUBJECT HEADING:   Airworthiness Directives; KAWASAKI HEAVY INDUSTRIES, LTD. Models KV107-II and KV107-IIA Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective February 26, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-04-10 KAWASAKI HEAVY INDUSTRIES, LTD.: Amendment 39-4045. Applies to Models KV107-II and KV107-IIA helicopters, certificated in all categories, with pilot or copilot cyclic stick boots, P/N 107S2226-9, installed.

Compliance required as indicated, unless already accomplished.

To prevent possible restriction of cyclic stick travel, which could result in an unsafe flight condition, accomplish the following:

(a) Within the next 25 hours time in service after the effective date of this AD, loosen the velcro tape and camloc fasteners securing the pilot and copilot cyclic stick boots, P/N 107S2226-9, and remove the boots.

(b) Remove the two rivets which attach the forward spring, P/N 107S2226-12, to the forward end of the boot base and discard the forward spring.

(c) Install washers and new rivets to plug the resulting two empty holes in the boot base.

(d) Reinstall the pilot and copilot stick boots.

(e) In accordance with FAR Sections 21.197 and 21.199, the helicopter may be flown to a base where the modification can be accomplished.

This amendment becomes effective February 26, 1981.

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.