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Install a placard with black letters on a white background. Within 3 days after 11 May Engine torque required to maintain airspeed increases by ft.
Airspeed of KIAS cannot be maintained in level flight. Make an entry in the aircraft records showing compliance. This Amendment becomes effective on 3 August Limitations and Section 4: Exception for flaps up: One or more of the following defines moderate icing conditions for this aeroplane: The aeroplane can dispatch into forecast areas of icing but must exit moderate or greater icing conditions if encountered.
Optional Systems Description and Operating Procedures: Either buffet or aural stall warning should be treated as an imminent stall.
You may insert a copy of this AD into the appropriate sections of the POH to comply with this action. The placards shall be located on the instrument panel c08b one of the following areas: These are minimum speeds for operations in icing conditions.
You are prohibited from continued flight after encountering moderate or greater icing conditions.
Cessna 208 C208 675HP 1998 POH Cessna-Caravan-updated-to-2004
This amendment makes correction to the applicability section of the AD to include Cessna Model B aeroplanes with no other changes to the requirements or compliance sections of the AD. Indicated airspeed in level cruise flight at constant power decreases by 20 knots.
Cessna Models and B aeroplanes. Incorporate the following revisions into the aeroplane flight manual.
The issuing of this AD is to assure that the pilot has enough information to prevent loss of control of the aeroplane while in-flight during icing conditions. Indicated airspeed in level flight at constant power decreases by 20 knots. Pho Series Aeroplanes. The placard shall be located on the instrument panel in one of the following areas: Install 3 placards with black letters on a white background.
Remains unchaged as detailed in the original issue of this AD as: Under the radio stack, immediately above the pilot’s flight instruments, or below the pilot’s vertical speed indicator.
Exempt from sunsetting by the Legislative Instruments Act s 54 2 item 9. FL Table of contents.
The AD requires that the action set out in the pon 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: WARNING The aural stall warning system does not function properly in all icing conditions and should not be relied upon to provide adequate stall warning when in icing conditions.
The aural stall warning system does not function properly in all icing conditions and should not be relied upon to provide adequate stall warning when in icing conditions. Airspeed in level flight at constant power decreases by 20 KIAS. The original issue of this AD became effective eon 11 May Minimum airspeed in icing conditions, for all flight phases including approach, except takeoff and landing: Skip to primary navigation Skip to primary c208bb. Flight into Icing Conditions.
These revisions are necessary for safe operation.