AD 76-22-02

AD Final Rules - DRS_76-22-02.html
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AD Number:
76-22-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100,...Show more
Subject:
'Y' Type Shoulder Harness
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/02/1977
Make:
Textron Aviation Inc.
Model:
200 | 58 | 58A | 65-B80 | 95-B55 | 95-B55A | A100 | A36 | B100 | B99 | C90 | E55 | E55A | E90 | F33A...Show more
Product Type:
Aircraft
Product Subtype:
Small/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Superseded AD: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Superseded By: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: 76-22-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2909

AD NUMBER:   76-22-02

SUBJECT HEADING:   Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 2, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
76-22-02 BEECH: Amendment 39-2755 as amended by Amendment 39-2909. Applies to the airplane models and serial numbers listed below having inverted "Y" type shoulder harnesses installed, except those airplanes that have previously complied with AD 76-22-02 (Amendment 39-2755):

MODELS	SERIAL NUMBERS
F33A	CE-490 thru CE-633
F33C	CJ-49 thru CJ-120
V35B	D-9582 thru D-9861
A36	E-515 thru E-824
95-B55 & 95-B55A	TC-1653 thru TC-1946
E55 and E55A	TE-966 thru TE-1077
58 and 58A	TH-425 thru TH-732
65-B80	LD-477 thru LD-505
C90	LJ-626 thru LJ-682 and LJ-684
E90	LW-93 thru LW-171, LW-173, LW-174, and LW-178
B99	U-157 thru U-164
A100	B-199 thru B-226
B100	BE-1 thru BE-7
200	BB-7, BB-8, BB-12, BB-18 thru BB-87, BB-89 thru BB-128, BB-130 thru BB-136

Compliance: Required as indicated, unless already accomplished in accordance with AD 76-22-02 (Amendment 39-2755).

To prevent slippage during normal use of the lap belt assembly installed with the inverted "Y" type shoulder harness, within 100 hours' time in service after the effective date of this AD, accomplish the following in accordance with Beechcraft Service Instructions No. 0850-313, Rev. I, or later approved revisions:

NOTE: Belt roller adjuster part numbers are stamped on the tang of the "male" half of lap belt assembly.

A) On all aircraft visually inspect the "male" half of the lap belt assembly on the pilot and co-pilot seats to determine if a P/N 500535 roller adjuster is installed and if so replace it with a P/N 500535-401 roller adjuster.

B) On Model 200 (Serial Numbers BB-7, BB-8 and BB-34) airplanes visually inspect the "male" half of the lap belt assembly on the toilet seat to determine if a P/N 500535 roller adjuster is installed and if so replace it with a P/N 500535-401 roller adjuster.

C) On Model 200 (Serial Numbers BB-12, BB-20, BB-25, BB-33, BB-35, BB-37, BB-41, BB-46, BB-49, BB-55, BB-56, BB-72, BB-77, BB-82, BB-92, BB-97, BB-107, BB-111, BB-113, BB-116, BB-130, BB-133, BB-135 and BB-136) airplanes visually inspect the "male" half of the Beech P/Ns 101-530314-9 and -13 lap belt assembly on all seats located aft of the cabin door to determine if a P/N 500535 roller adjuster is installed and if so replace it with a P/N 500535-401 roller adjuster.

D) The 100 hour compliance time required by this AD may be adjusted up to 110 hours' time in service to allow inspection and modification at regularly scheduled maintenance periods.

E) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

Amendment 39-2755 became effective November 4, 1976.

This amendment 39-2909 becomes effective June 2, 1977.

FOOTER: