AD 71-23-01

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AD Number:
71-23-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Pilatus Model PC-6 Airplanes
Subject:
Safety of Aileron Cable Turnbuckles
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Pilatus Aircraft Limited
Model:
PC-6 | PC-6-H1 | PC-6-H2 | PC-6/350 | PC-6/350-H1 | PC-6/350-H2 | PC-6/A | PC-6/A-H1 | PC-6/A-H2 | P...Show more
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Superseded AD: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Superseded By: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: 71-23-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1326

AD NUMBER:   71-23-01

SUBJECT HEADING:   Airworthiness Directives; Pilatus Model PC-6 Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-23-01 PILATUS AIRCRAFT: Amdt. 39-1326. Applies to Pilatus Model PC-6 (Heli-Porter) airplanes manufactured by Fairchild Hiller.

Compliance is required as indicated.

(a) Before further flight, unless already accomplished, inspect the aileron control cable turnbuckles for safety wires that meet the size and corrosion resistance specifications and the method of safetying specifications of Military Standard 20995C47 and Military Standard 33591, respectively, or FAA-approved equivalents.

(b) Within the next 50 hours' time in service after the effective date of this AD or before November 15, 1971, whichever occurs sooner, inspect the rudder, elevator, and flap control cables turnbuckles for safety wires that meet the size and corrosion resistance specifications of Military Standard 20995C47 and Military Standard 33591, respectively, or FAA-approved equivalent.

(c) If turnbuckle safety wires are found that do not meet the size or corrosion resistance specifications or the method of safetying specifications of Military Standard 20995C47 and Military Standard 33591, respectively, or FAA-approved equivalents, during an inspection required by paragraph (a) or (b), before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the repairs can be performed, replace affected turnbuckle safety wires with safety wires that meet those specifications or FAA-approved equivalents.

(d) Within the next 50 hours' time in service after the effective date of this AD or before November 15, 1971, whichever occurs sooner, inspect the rudder and elevator trim cable turnbuckles for safety wires that meet the size and corrosion resistance specifications and the method of safetying specifications of Military Standard 20995C32 and Military Standard 33591, respectively, or FAA-approved equivalents.

(e) If turnbuckle safety wires are found that do not meet the size or corrosion resistance specifications or the method of safetying specifications of Military Standard 20995C32 and Military Standard 33591, respectively, or FAA-approved equivalents, during an inspection required by paragraph (d), before further flight, except that the airplane may be flown in accordance with FAR 21.197 to a base where the repairs can be performed, replace affected turnbuckle safety wires with safety wires that meet those specifications or FAA-approved equivalents.

(Fairchild Hiller Service Letter PC-6-27-2, dated July 20, 1971, refers to this subject).

This amendment is effective upon publication in the Federal Register as to all persons except those persons to whom it was made effective immediately upon receipt of the airmail letter dated October 9, 1971, which contained this amendment.

FOOTER: