AD 82-11-03 R1

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AD Number:
82-11-03 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model HS-125 Series 700
Subject:
Elevator Pitch Trim Switch
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/12/1982
Make:
Textron Aviation Inc.
Model:
HS.125 Series 700A | HS.125 Series 700B
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Superseded AD: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Superseded By: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: 82-11-03 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4470

AD NUMBER:   82-11-03 R1

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model HS-125 Series 700

ACTION:  

SUMMARY:  

DATES:   Effective October 12, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-11-03 R1 BRITISH AEROSPACE: Amendment 39-4383 as amended by Amendment 39- 4470. Applies to Model HS-125 Series 700 and all variants serial numbers 25/7001, 7007, 7010, 7013, 7020, 7022, 7025, 7028, 7031, and 7034, 7037, 7040, 7046; NA 0201 - NA 0240 inclusive certificated in all categories.

Compliance required within the next 100 hours time in service after the effective date of this AD. To prevent improper operation of the elevator pitch trim switch located in the control column handwheel, accomplish the following unless already accomplished.

1. Remount the elevator pitch trim switch in accordance with the accomplishment instructions of British Aerospace Service Bulletin HS-125 27-124 (2705) dated January 1, 1979.

2. 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.

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

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

Amendment 39-4383 became effective May 31, 1982.

This amendment 39-4470 becomes effective October 12, 1982.

FOOTER: