Airworthiness Directive - AD/CESSNA 210/67 - Aircraft Flight ... - CASA
CESSNA 210 · Other Documents
Overview
This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority of Australia concerning the Cessna 210 series aircraft. It specifically addresses the need for revisions to the Aircraft Flight Manual (AFM) regarding flight into icing conditions. The directive outlines the necessary actions to mitigate risks associated with severe icing, which can significantly impair aircraft performance and controllability. It applies to various models within the Cessna 210 series, including the P210N, P210R, T210N, and T210R, and mandates compliance within 30 days of its effective date. The document serves as a critical reference for pilots and operators to ensure safe operation in potentially hazardous weather conditions.
- Severe icing can occur outside certified conditions, particularly in freezing rain or drizzle.
- Visual cues for severe icing include extensive ice accumulation on the airframe and windscreen.
- Pilots must request priority handling from ATC if severe icing conditions are observed.
- Avoid using autopilot in icing conditions to maintain control of the aircraft.
- Do not extend flaps while in icing conditions to prevent ice accumulation on the wings.
Document
Open original PDFMore CESSNA 210manuals & documents
See all 28 →- Service Bulletin SB-14 - McFarlane AviationService Bulletins
- Fuel starvation involving Cessna T210M, VH-MYWOther Documents
- In-flight break-up involving Cessna 210N, VH-TFTOther Documents
- Engine failure and collision with terrain involving Cessna P210N ...Other Documents
- AIRWORTHINESS BULLETIN Cessna Single Engine Electro-Hydraulic Undercarriage Retraction SystemsOther Documents
- Request for Legal Interpretation of 14 C.F.R. §§ 91.403(c) and 43.16 Concerning Whether Requirements in an Airworthiness Limitations Section (ALS) Developed By a Design Approval Holder (DAH) and Approved by the Federal Aviation Administration (FAA) as a Change to Type DesignOther Documents
- Backdoor Rulemaking? | Savvy AviationMaintenance Manual
- ATSB Transport Safety ReportOther Documents
- SERVICE LETTER SEL-29-01 Revision 1: Hydraulic Power Pack InspectionWiring Diagram
- cessna-skycatcher-checklist.pdf - Empyrean AeroChecklist
- Airplane Upset Recovery Training Aid Revision 2Other Documents
- Airworthiness Directive AD/CESSNA 210/69 Amdt 2Airworthiness Directives
Keep exploring
Free — save the 210 to your watchlist and track it in one place.
If you fly the CESSNA 210, you may also be researching these.
In this document
Limitations Section Revision
The AD requires a revision to the Limitations Section of the AFM to include warnings about severe icing conditions. It emphasizes that severe icing may occur outside the aircraft's certification limits, particularly in freezing rain or drizzle. Pilots are instructed to recognize visual cues indicating severe icing and to request priority handling from Air Traffic Control to exit such conditions.
Normal Procedures Section Revision
The AD also mandates changes to the Normal Procedures Section of the AFM. It outlines weather conditions that may lead to severe in-flight icing, such as visible rain at temperatures below 0°C. Procedures for exiting severe icing environments are detailed, including monitoring ambient temperatures and avoiding abrupt maneuvers.
Compliance Requirements
Operators must comply with the directive within 30 days of its effective date, which is March 23, 2000. The directive must be included in the appropriate sections of the aircraft's AFM, and certification for compliance can be performed by a private pilot.
Safety notes
- Severe icing may exceed the capability of the ice protection system.
- Use of autopilot is prohibited in severe icing conditions due to potential handling issues.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Cessna 210 Series Aeroplanes AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (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 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/CESSNA 210/67 Aircraft Flight Manual, Flight into Icing Conditions 3/2000 Applicability: Models P210N S/n P21000386 to P21000834, P210R all s/n, T210N S/n 21063641 to 21064897, and T210R all S/n. 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 • may result in 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 lower surface of the wing aft of the protected area. COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES 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 AFM by incorporating the following: THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING: • Visible rain at temperatures below 0 degrees Celsius ambient air temperature; • Droplets that splash or splatter on impact at temperatures below 0 degrees Celsius ambient air temperature. PROCEDURES FOR EXITING A SEVERE ICING ENVIRONMENT: (These procedures are applicable to all flight phases from take-off to landing.) Monitor the ambient air temperature. While severe icing may form at temperatures as cold as -18 degrees Celsius, increased vigilance is warranted at temperatures around freezing when visible moisture is present. COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES If the visual cues which are specified in the Limitations Section of the AFM for identifying severe icing conditions are observed, accomplish the following: • Immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the severe icing conditions in order to avoid extended exposure to flight conditions more severe than those for which the aircraft has been certificated. • Avoid abrupt and excessive manoeuvring that may exacerbate control difficulties. • Do not engage the autopilot. • If the autopilot had previously been engaged, hold the control wheel firmly and disengage the autopilot. • If an unusual roll response or un-commanded roll control movement is observed, reduce the angle-of-attack. • Do not extend flaps when holding in icing conditions. Operation with flaps extended can result in a reduced wing angle-of-attack, with the possibility of ice forming on the upper surface further aft on the wing than normal, possibly aft of the protected area. • If the flaps are extended, do not retract them until the airframe is clear of ice. • Report these weather conditions to Air Traffic Control. Note 1: Certificate of Registration holders should initiate action to ensure notification of this change is conveyed to any person who may operate their aircraft as pilot in command. Note 2: FAA ADs 98-05-14 R1 and 98-20-33 refer. Certification for accomplishment of this Directive may be carried out: a. after a copy of this Directive is included in the appropriate sections of the aircraft's AFM; and b. may be carried out at a minimum, by the holder of a private pilot's licence. COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Compliance: Within 30 days after the effective date of this Directive. This Airworthiness Directive becomes effective on 23 March 2000. Background: This Directive is issued to minimise the potential hazards associated with operating the aircraft in severe icing conditions by providing more clearly defined procedures and limitations associated with such conditions. Eugene Paul Holzapfel Delegate of the Civil Aviation Safety Authority 15 February 2000 The above AD is notified in the Commonwealth of Australia Gazette on 23 February 2000.
CESSNA 210 for sale now
5,103 CESSNA 210 parts for sale
See all →





Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.










