AD 76-22-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 200 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | 58 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | 58A | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | 65-B80 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | 95-B55 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | 95-B55A | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | A100 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | A36 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | B100 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
| aircraft | Textron Aviation Inc. | B99 | Beech Models F33A, F33C, V35B, A36, 95-B55, 95-B55A, E55, E55A,58, 58A, 65-B80, C90, E90, B99, A100, B100, and 200 Airplanes |
Unsafe Condition
Slippage during normal use of the lap belt assembly installed with the inverted 'Y' type shoulder harness.
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Required Actions
Within 100 hours' time in service after the effective date, inspect the 'male' half of the lap belt assembly on pilot and co-pilot seats to determine if P/N 500535 roller adjuster is installed and replace with P/N 500535-401. For Model 200 specific serial numbers, inspect and replace roller adjusters on toilet seat and cabin seats aft of the cabin door as specified. Compliance may be adjusted up to 110 hours' time in service for scheduled maintenance.
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Compliance Time
within 100 hours' time in service after the effective date of this AD
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Affected Aircraft
Beech Models F33A (CE-490-CE-633), F33C (CJ-49-CJ-120), V35B (D-9582-D-9861), A36 (E-515-E-824), 95-B55 & 95-B55A (TC-1653-TC-1946), E55 and E55A (TE-966-TE-1077), 58 and 58A (TH-425-TH-732), 65-B80 (LD-477-LD-505), C90 (LJ-626-LJ-682, LJ-684), E90 (LW-93-LW-171, LW-173, LW-174, LW-178), B99 (U-157-U-164), A100 (B-199-B-226), B100 (BE-1-BE-7), and 200 (BB-7, BB-8, BB-12, BB-18-BB-87, BB-89-BB-128, BB-130-BB-136) with inverted 'Y' type shoulder harnesses, excluding those already compliant with AD 76-22-02.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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