AD 47-35-02

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AD Number:
47-35-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Sikorsky Model R-4B AAF Helicopter
Subject:
Tail Rotor Gearbox Brace
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Holmes, Douglas W.
Model:
R-4B (Army)
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Superseded AD: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Superseded By: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: 47-35-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-35-02

SUBJECT HEADING:   Airworthiness Directives; Sikorsky Model R-4B AAF Helicopter

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   47-35-02 SIKORSKY: (Was Mandatory Note 2 of AD-7L-1.) Applies to Model R-4B AAF Helicopter Serial Numbers 43-46500 and 43-46504 to 43-46567 Inclusive.

Compliance required prior to November 15, 1947.

To compensate for an increased overhang of the tail rotor gearbox, a diagonal brace that changes the aft boom load distribution shall be installed in accordance with the following instructions:

(a) Fit the two tube brace assemblies, Sikorsky P/N S38566 and S38567, in telescopic position, to lower right longeron and upper left longeron. (See Figures 2 and 3.)

AD 47-35-02

(1) Insert bolts, P/N AN 4-13, into halves of clamp of each section of brace; attach washers, P/N AN 960-416, and nuts, P/N AN 310-4.

(2) Locate brace so that its center and that of vertical tube, P/N S38505-23, forward of it, are a maximum of 1 1/8 inches apart. (See Figure 2.)

(3) Tighten securely four bolts, P/N AN 4-13, which hold subject brace in position.

(4) Secure nuts, P/N AN 310-4, with cotter pins.

(b) Mark with a pencil the overlap of tube brace assembly, P/N S38566, on assembly P/N S38567. (See Figure 3.)


AD 47-35-02

(c) Fashion a wedge, using a piece of wood 1 x 3 x 14 inches, and "V" notch both ends. (See Figure 4.)

(d) Insert wedge approximately parallel to telescopic brace.

(1) Tap alternately the ends of wedge forcing the subject assembly to extend 1/16 inch beyond the pencil line requested in paragraph (b). (Extra extension of 1/16 inch permits brace to assume the desired stress load.)

(2) Wrap longerons with friction tape at point of wedge contact, or insert cardboard or any suitable material at ends of wood wedge to prevent paint abrasion.

(e) With wedge securely in position, using drill No. 40 (0.098-inch), drill two holes through brace at 90 degrees to each other. (See Figure 3.)

(1) Enlarge holes, using drill No. C (0.242 inch) and ream to 0.250 inch.

(f) Bolt two sections of brace together with bolts, P/N AN 24-17, nuts, P/N AN 320- 4, and secure with cotter pins.

(g) Remove the wood wedge.

(h) If paint on longerons of tail fuselage has been damaged, touch up with paint.

(Sikorsky Service Bulletin R-4B No. 8 and Army Technical Order 01-230HA-11 also cover this same alteration.)

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