AD 96-15-01

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Corporation Model 1900D Airplanes

AD Number
96-15-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
96-CE-41-AD
FR Citation
Federal Register: August 20, 1996 (Volume 61, Number 162)

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 1900D Airworthiness Directives; Raytheon Aircraft Corporation Model 1900D Airplanes

Unsafe Condition

High resistance short circuit condition in the heated windshield wiring, caused by the braid wire attached to the low heat power terminal block, leading to arcing and substantial heat, resulting in smoke and fire in the cockpit.

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

Required Actions

Pull and band specified windshield heat control circuit breakers on both pilot and co-pilot sides; insert AD copy into AFM Limitations section; fabricate and install placard prohibiting flight in known icing conditions.

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

Compliance Time

Required prior to further flight after the effective date of this AD, unless already accomplished, except to those operators receiving this action by priority letter issued July 10, 1996, which made these actions effective immediately upon receipt.

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

Affected Aircraft

Raytheon Aircraft Corporation Model 1900D airplanes (serial numbers UE-1 through UE-239) with windshield part number 114-384020-1 or 114-384020-2 installed.

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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