| AD Number | 76-22-02 | Status | Active |
| Effective Date | June 02, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2909 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small/Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 200 58 58A 65-B80 95-B55 95-B55A A100 A36 B100 B99 C90 E55 E55A E90 F33A F33C V35B |
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.