AD 76-10-10

final rule
Data completeness: 70%

Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes

AD Number
76-10-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 100 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. 200 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. 65-88 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. 65-90 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. 65-A90 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. A100 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. B90 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. C90 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes
aircraft Textron Aviation Inc. E90 Beech Models 65-88, 65-90, 65-A90, B90, C90, E90, 100, A100 and 200 Airplanes

Unsafe Condition

Failure of the cabin door to remain closed in flight due to improper operation or rigging of the latching mechanism and warning system.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within 50 hours' time in service after the effective date, check the cabin door for proper operation and rigging. Within 50 hours' time in service after September 15, 1976, modify the cabin door installation per specified service instructions, install specific decals, check and rerig the latching mechanism and warning system, and add FAA-approved AFM supplements with designated part numbers.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 50 hours' time in service after the effective date of this AD, and within each 50 hours' time in service thereafter for Paragraph I. Paragraph II must be accomplished within 50 hours' time in service after September 15, 1976.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Beech Models 65-88 (Serial Numbers LP-1 thru LP-47 except LP-27 and LP-29), 65-90, 65-A90, B90 (Serial Numbers LJ-1 thru LJ-351), C90 (Serial Numbers LJ-1 thru LJ-676), E90 (Serial Numbers LW-1 thru LW-163), 100 and A100 (Serial Numbers B-1 thru B-225), and 200 (Serial Numbers BB-2 thru BB-111).

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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