Document ID: chunk:federal_register_of_legislation:F2006B04280:body:0:p1
Version: federal_register_of_legislation:F2006B04280
Segment Type: other
Provision Reference: 
Character Range: 4–3249

Beechcraft 90 and 65-90 (King Air) Series Aeroplanes

AIRWORTHINESS DIRECTIVE

    For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BEECH 90/97 and issues the following AD under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

    AD/BEECH 90/97
    Amdt 1

       Aircraft Flight Manual, Flight into Icing Conditions

    7/2000

    Applicability: Models 65-B90, 90 and F90 all Serial Numbers. Requirement:  Revise:
                  1. the Limitations Section of the aircraft's Aircraft Flight Manual (AFM) by incorporating the following:

                                   "WARNING"

                 Severe icing may result from environmental conditions outside of those for which the aircraft is certificated.

                 Flight in freezing rain, freezing drizzle, or mixed icing conditions (super cooled liquid water and ice crystals) may result in:

                    * ice build-up on protected surfaces and exceed the capability of the ice protection system, or

                    * ice forming aft of the protected surfaces.

                 This ice may not be shed using the ice protection systems, and may seriously degrade the performance and controllability of the aircraft.

                 During flight, severe icing conditions that exceed those for which the aircraft is certificated shall be determined by the visual cues described below. If one or more of these visual cues exists, immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the icing conditions. The cues are:

                      * unusually extensive ice accumulation on the airframe and windscreen in areas not normally observed to collect ice, and/or

                      * accumulation of ice on the upper surface of the wing aft of the protected area, and/or

                      * accumulation of ice on the engine nacelles and propeller spinners farther aft than normally observed.

             Since the auto-pilot, when installed and operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the auto-pilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or auto-pilot trim warnings are encountered while the aircraft is in icing conditions.

             All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. This direction supersedes any relief provided  by any Minimum Equipment List.

             2.     the Normal Procedures Section of the approved AFM by incorporating the following:

THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING: