AD 87-03-06 R1

final rule
Data completeness: 70%

Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes

AD Number
87-03-06 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 100 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. 99 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. 99A Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. A100 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. A99A Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. B100 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. B99 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes
aircraft Textron Aviation Inc. C99 Airworthiness Directives; Beech Model 99, 99A, A99A, B99, C99, 100, A100 and B100 Airplanes

Unsafe Condition

Looseness of the elevator outboard hinge attachment to the stabilizer and potential loss of integrity of the hinge attachment.

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

Required Actions

Visually inspect each elevator outboard hinge attachment by holding the elevator steady at the trailing edge and pushing up and down on the leading edge. If movement is detected, replace hinge attach rivets with bolts per Service Bulletin No. 2132. For airplanes with over 1000 hours TIS, install bolts in place of rivets within 600 hours TIS after the initial inspection. Discontinue inspections after bolts are installed.

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

Compliance Time

Required as indicated after the effective date of this AD, unless already accomplished.

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

Affected Aircraft

Beech Model 99, 99A, A99A, B99, C99 (Serial Numbers U-1 thru U-240); 100 and A100 (Serial Numbers B-1 thru B-247); and B100 (Serial Numbers BE-1 thru BE-137)

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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